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JP7365942B2 - Stator blade ring of axial flow rotating machine and axial flow rotating machine - Google Patents
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JP7365942B2 - Stator blade ring of axial flow rotating machine and axial flow rotating machine - Google Patents

Stator blade ring of axial flow rotating machine and axial flow rotating machine Download PDF

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JP7365942B2
JP7365942B2 JP2020041124A JP2020041124A JP7365942B2 JP 7365942 B2 JP7365942 B2 JP 7365942B2 JP 2020041124 A JP2020041124 A JP 2020041124A JP 2020041124 A JP2020041124 A JP 2020041124A JP 7365942 B2 JP7365942 B2 JP 7365942B2
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axial flow
stator
piezoelectric element
voltage
rotating machine
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正幸 富井
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Mitsubishi Heavy Industries Aero Engines Ltd
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Description

本開示は、軸流回転機械の静翼環の固有振動数を変化させる静翼環及び軸流回転機械に関するものである。 The present disclosure relates to a stator vane ring that changes the natural frequency of the stator vane ring of the axial-flow rotary machine, and to an axial-flow rotary machine.

軸流回転機械の圧縮機の静翼環は、上流側及び下流側の動翼の翼枚数と回転数で決まる周期的な流体力の作用を受ける。周期的な流体力は、圧縮機の静翼環に対する励振力として作用し、静翼環が振動する。これまでは、圧縮機について述べたが、タービンについても同様である。 A stator vane ring of a compressor of an axial flow rotary machine is subjected to a periodic fluid force determined by the number of blades and the rotation speed of the rotor blades on the upstream side and the downstream side. The periodic fluid force acts as an excitation force on the stator vane ring of the compressor, causing the stator vane ring to vibrate. So far, the compressor has been described, but the same applies to the turbine.

軸流回転機械の設計においては、固有振動数と励振周波数が一致することにより発生する共振を回避するように設計が行われている。静翼環の固有振動数は構成要素の材質、形状、支持方法等の要因によって変化する。従って、軸流回転機械の構成要素の固有振動数と、軸流回転機械の通常使用状態における励振周波数が一致しないように設計することで、共振を回避することが一般的に行われている。 Axial flow rotating machines are designed to avoid resonance that occurs when the natural frequency and excitation frequency match. The natural frequency of the stator blade ring varies depending on factors such as the material, shape, and support method of the components. Therefore, resonance is generally avoided by designing the axial-flow rotating machine so that the natural frequencies of the components thereof do not match the excitation frequencies under normal use of the axial-flow rotating machine.

ところで、軸流回転機械の内、航空機用エンジンに用いられるガスタービンエンジンは、使用中に急加速が必要になる場合がある。また、高度・機速で表現したフライトエンベロープが広範囲の場合は、高度・機速の変化に伴って、エンジン入口の空気の圧力・温度が変化することから、回転数が変化する。従って、発電用ガスタービンエンジンとは異なり、広範囲の回転数で運転される。飛行安全を考慮すると、広範囲の回転数において、共振の発生を防ぐ必要がある。 By the way, among axial flow rotary machines, gas turbine engines used in aircraft engines may require rapid acceleration during use. Furthermore, if the flight envelope expressed in terms of altitude and aircraft speed is wide, the rotation speed will change because the pressure and temperature of the air at the engine inlet will change as the altitude and aircraft speed change. Therefore, unlike a gas turbine engine for power generation, it can be operated at a wide range of rotation speeds. Considering flight safety, it is necessary to prevent resonance from occurring over a wide range of rotational speeds.

一方、固有振動数と励振周波数とが、一致することにより発生する共振によって生じる動的応力に静翼が耐えることが出来るように、静翼の構造強度を上げる手法によって対処することが出来る。翼の構造強度を上げる方法としては、静翼の翼厚さの厚肉化が挙げられる。しかし、静翼の翼厚さの厚肉化を採用した場合の弊害として、静翼部の圧力損失の増加が挙げられる。何故ならば、静翼の翼厚さの厚肉化により、流体の流路を塞ぐブロッケージが大きくなり、静翼部の圧力損失が増加するからである。静翼部での圧力損失が増加すると、圧縮機の静翼の場合は、動翼で圧縮した空気の圧力が、静翼を通過する際に減少する。また、タービンの静翼の場合は、静翼を通過する際に圧力が減少し、動翼で回収する圧力を下げてしまう。その結果、全体としての軸流回転機械の性能が低下する。従って、静翼の翼厚さを薄く保った状態で、固有振動数と励振周波数の一致による共振を避ける必要がある。 On the other hand, it is possible to deal with this problem by increasing the structural strength of the stator blade so that the stator blade can withstand the dynamic stress caused by the resonance that occurs when the natural frequency and the excitation frequency match. One way to increase the structural strength of a blade is to increase the thickness of the stator blade. However, one of the disadvantages of increasing the thickness of the stator blades is an increase in pressure loss in the stator blade portion. This is because, as the thickness of the stator blade increases, the blockage that blocks the fluid flow path becomes larger, and the pressure loss in the stator blade portion increases. When the pressure loss at the stator blade increases, in the case of the stator blade of a compressor, the pressure of the air compressed by the rotor blade decreases when it passes through the stator blade. In addition, in the case of turbine stator blades, the pressure decreases when the air passes through the stator blades, reducing the pressure recovered by the rotor blades. As a result, the performance of the axial flow rotating machine as a whole deteriorates. Therefore, it is necessary to avoid resonance due to coincidence of the natural frequency and the excitation frequency while keeping the thickness of the stationary blade thin.

従来技術として、特許文献1に記載のように、動翼シュラウドの隣接する動翼シュラウドとの接触部に圧電素子を設け、動翼シュラウドの間に働く接触反力を調整可能とすることで、動翼に適切な減衰力を作用させ、振動を減衰させる発明が開示されている。 As a conventional technique, as described in Patent Document 1, a piezoelectric element is provided at the contact portion of a rotor blade shroud with an adjacent rotor blade shroud, and the contact reaction force acting between the rotor blade shrouds can be adjusted. An invention is disclosed in which vibrations are damped by applying an appropriate damping force to a rotor blade.

特開2003-138904号公報Japanese Patent Application Publication No. 2003-138904

しかし、上述の開示は、動翼に作用する励振力に対して、減衰力を作用させて対処するものであるから、固有振動数と励振周波数の一致を回避することは出来ないという問題があった。 However, since the above-mentioned disclosure deals with the excitation force acting on the rotor blade by applying a damping force, there is a problem in that it is impossible to avoid coincidence between the natural frequency and the excitation frequency. Ta.

本開示は上記問題点に鑑みてなされたものであって、静翼環の支持剛性を変えることによって、静翼環の固有振動数を変化させ、静翼環の固有振動数と励振周波数の一致による共振を回避することを可能とする軸流回転機械の静翼環及び軸流回転機械を提供することを目的とするものである。 The present disclosure has been made in view of the above problems, and by changing the support rigidity of the stator blade ring, the natural frequency of the stator blade ring is changed, and the natural frequency of the stator blade ring and the excitation frequency are matched. An object of the present invention is to provide a stator vane ring for an axial flow rotating machine and an axial flow rotating machine that make it possible to avoid resonance caused by the axial flow rotating machine.

上述した課題を解決し、目的を達成する為に、本開示に係る軸流回転機械の静翼環は、複数の静翼と、複数の静翼の先端部に設けられる外周側シュラウドと、複数の静翼の根元部に設けられる内周側シュラウドと、外周側シュラウド、及び、内周側シュラウドの内の一方に設けられる一以上の支持部材と、支持部材に対向して設けられる固定部材と、固定部材に対する支持部材の拘束状態を変更可能に拘束する一以上の拘束部と、拘束部の拘束状態を変更可能に制御する制御部と、を備える。 In order to solve the above-mentioned problems and achieve the purpose, a stator vane ring for an axial flow rotating machine according to the present disclosure includes a plurality of stator blades, an outer circumferential shroud provided at the tips of the plurality of stator blades, and a plurality of stator blades. an inner shroud provided at the root of the stator blade, an outer shroud, and one or more support members provided on one of the inner shrouds; and a fixing member provided opposite the support member. , one or more restraint parts that changeably restrain the restraint state of the support member relative to the fixing member, and a control part that controls the restraint state of the restraint part in a changeable manner.

本開示に係る軸流回転機械は、上記の軸流回転機械の静翼環を備える。 An axial flow rotary machine according to the present disclosure includes the stator vane ring of the axial flow rotary machine described above.

本開示によれば、静翼環の支持剛性を変えることによって、運転範囲内での回転数では静翼環の固有振動数と励振周波数が一致しないように、静翼環の固有振動数を変えることが出来ることから、静翼環の固有振動数と励振周波数の一致による共振を回避することが可能となる。 According to the present disclosure, by changing the support rigidity of the stator blade ring, the natural frequency of the stator blade ring is changed so that the natural frequency of the stator blade ring and the excitation frequency do not match at the rotation speed within the operating range. This makes it possible to avoid resonance due to coincidence of the natural frequency of the stator blade ring and the excitation frequency.

図1は、本開示が適用される軸流回転機械の全体構成を示す概略図である。FIG. 1 is a schematic diagram showing the overall configuration of an axial flow rotating machine to which the present disclosure is applied. 図2は、本開示の課題に係る運転範囲内での共振を説明する説明図である。FIG. 2 is an explanatory diagram illustrating resonance within the operating range related to the problem of the present disclosure. 図3は、本開示の軸流回転機械の静翼環を示す概略図である。FIG. 3 is a schematic diagram showing a stator blade ring of the axial flow rotary machine of the present disclosure. 図4は、本開示の静翼環の拘束部の第一実施例を示す概略図である。FIG. 4 is a schematic diagram showing a first embodiment of a restraining portion of a stator vane ring according to the present disclosure. 図5は、本開示の静翼環の拘束部の第二実施例を示す概略図である。FIG. 5 is a schematic diagram showing a second embodiment of the constraint portion of the stator vane ring of the present disclosure. 図6は、本開示の静翼環の拘束部の第三実施例を示す概略図である。FIG. 6 is a schematic diagram showing a third embodiment of the constraint portion of the stator vane ring of the present disclosure. 図7は、本開示の静翼環の制御部を用いた静翼環の固有振動数の変化の第一実施例を示す説明図である。FIG. 7 is an explanatory diagram showing a first example of a change in the natural frequency of a stator blade ring using the stator blade ring control unit of the present disclosure. 図8は、本開示の静翼環の制御部を用いた静翼環の固有振動数の変化の第二実施例を示す説明図である。FIG. 8 is an explanatory diagram showing a second example of a change in the natural frequency of a stator blade ring using the stator blade ring control unit of the present disclosure. 図9は、本開示の静翼環の制御部を用いた静翼環の固有振動数の変化の第三実施例を示す説明図である。FIG. 9 is an explanatory diagram showing a third example of changing the natural frequency of a stator blade ring using the stator blade ring control unit of the present disclosure.

以下に、本開示に係る軸流回転機械の静翼環の実施例を図面に基づいて詳細に説明する。なお、この実施例により、この開示が限定されるものではない。 DESCRIPTION OF THE PREFERRED EMBODIMENTS Examples of stator vane rings for axial flow rotary machines according to the present disclosure will be described in detail below based on the drawings. Note that this disclosure is not limited to this example.

図1は、本開示が適用される軸流回転機械の全体構成を示す概略図である。本開示に係る軸流回転機械としては、例えば、航空機用のターボファンエンジン、ターボジェットエンジン、ターボプロップエンジン、ターボシャフトエンジン、ギアードターボファンエンジン、ターボラムジェットエンジン、発電用のガスタービンエンジン、船舶用のガスタービンエンジン等が挙げられるがこれに限定するものではない。以下の説明では航空機用のターボファンエンジンを例に挙げて説明する。 FIG. 1 is a schematic diagram showing the overall configuration of an axial flow rotating machine to which the present disclosure is applied. Examples of the axial rotating machine according to the present disclosure include aircraft turbofan engines, turbojet engines, turboprop engines, turboshaft engines, geared turbofan engines, turbo ramjet engines, gas turbine engines for power generation, and marine vessels. Examples include, but are not limited to, gas turbine engines. In the following explanation, an aircraft turbofan engine will be used as an example.

図1に示すように、ターボファンエンジン1は、ファン2と、圧縮機3と、燃焼室4と、タービン5とを備える。ターボファンエンジン1の基本的な動作は、ファン2が回転軸6に沿って、回転することによって、吸入した流体(本実施例では空気)を、圧縮機3によりさらに高温・高圧に圧縮する。燃焼室4は圧縮機3によって、高温・高圧に圧縮された流体に燃料を混合し、着火させることで、熱エネルギーを流体に付与する。タービン5は、膨張する燃焼ガスの熱エネルギーを、運動エネルギーに変換して、タービン5と同一の軸に取り付けられたファン2、及び、圧縮機3を駆動する。そして、タービン5を通過した燃焼ガスは、排気ダクトから排出される。なお、圧縮機3は、複数の圧縮機で構成され、それぞれが別々の軸に組み付けられる多軸式のものを採用しても良い。これは、タービン5についても同様である。 As shown in FIG. 1, the turbofan engine 1 includes a fan 2, a compressor 3, a combustion chamber 4, and a turbine 5. The basic operation of the turbofan engine 1 is that the fan 2 rotates along the rotating shaft 6, and the compressor 3 compresses the sucked fluid (air in this embodiment) to a higher temperature and pressure. The combustion chamber 4 mixes fuel with a fluid compressed to high temperature and high pressure by the compressor 3, and ignites the mixture, thereby imparting thermal energy to the fluid. The turbine 5 converts the thermal energy of the expanding combustion gas into kinetic energy, and drives the fan 2 and the compressor 3, which are attached to the same shaft as the turbine 5. The combustion gas that has passed through the turbine 5 is then exhausted from the exhaust duct. Note that the compressor 3 may be a multi-shaft type compressor that is composed of a plurality of compressors, each of which is assembled to a separate shaft. This also applies to the turbine 5.

圧縮機3は、動翼と、静翼と、動翼が組み付けられるディスクと、静翼の両端に形成される外周側シュラウド、及び、内周側シュラウドと、静翼の内周側シュラウドの内周側に組み付けられるシール保持板と、シール保持板が取り付けられたシールと、を備える。 The compressor 3 includes a rotor blade, a stator blade, a disk to which the rotor blade is assembled, an outer shroud formed at both ends of the stator blade, an inner shroud, and an inner shroud of the inner shroud of the stator blade. It includes a seal holding plate assembled on the circumferential side and a seal to which the seal holding plate is attached.

タービン5は、動翼と、静翼と、動翼が組み付けられるディスクと、静翼の両端に形成される外周側シュラウド、及び、内周側シュラウドと、静翼の内周側シュラウドの内周側に組み付けられるシール保持板と、シール保持板が取り付けられたシールと、を備える。 The turbine 5 includes a rotor blade, a stator blade, a disk to which the rotor blade is assembled, an outer shroud formed at both ends of the stator blade, an inner shroud, and an inner periphery of the inner shroud of the stator blade. It includes a seal retaining plate that is assembled to the side, and a seal to which the seal retaining plate is attached.

図2は、本開示の課題に係る共振を説明する説明図である。図2に示すように、軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数と一致した場合、共振が発生する。所定の次数の励振周波数が、所定の次数の固有振動数に一致しない場合であっても、励振周波数が、固有振動数に近付くと、共振による振幅が大きくなる。 FIG. 2 is an explanatory diagram illustrating resonance related to the subject of the present disclosure. As shown in FIG. 2, when the excitation frequency of a predetermined order of the axial flow rotating machine matches the natural frequency of a predetermined order of the stator vane ring, resonance occurs. Even if the excitation frequency of a predetermined order does not match the natural frequency of the predetermined order, as the excitation frequency approaches the natural frequency, the amplitude due to resonance increases.

(静翼環の構成)
図3は、本開示に係る軸流回転機械の静翼環の概略図である。本開示に係る軸流回転機械の静翼環は、例えば、上記の圧縮機3の静翼部を構成するものとなっている。静翼環は、周方向に並べて設けられることで、円環形状となる静翼段を構成する。本開示に係る軸流回転機械の静翼環は、複数の静翼75と、複数の静翼75の先端部に設けられる外周側シュラウド76と、複数の静翼75の根元部に設けられる内周側シュラウド74と、外周側シュラウド76、及び、内周側シュラウド74の内の一方に設けられる一以上の支持部材73(73A、73B、73C)と、支持部材73に対向して設けられる固定部材72と、固定部材72に対する支持部材73の拘束状態を変更可能に拘束する一以上の拘束部と、拘束部の拘束状態を変更可能に制御する制御部8と、を備える。
(Configuration of stationary blade ring)
FIG. 3 is a schematic diagram of a stator blade ring of an axial flow rotary machine according to the present disclosure. The stator vane ring of the axial flow rotary machine according to the present disclosure constitutes, for example, the stator vane portion of the compressor 3 described above. The stator vane rings are arranged in the circumferential direction to form a stator vane stage having an annular shape. The stator vane ring of the axial flow rotary machine according to the present disclosure includes a plurality of stator blades 75, an outer circumferential shroud 76 provided at the tips of the plurality of stator blades 75, and an inner shroud 76 provided at the root portion of the plurality of stator blades 75. One or more support members 73 (73A, 73B, 73C) provided on one of the circumferential shroud 74, the outer shroud 76, and the inner shroud 74, and a fixing member provided opposite the support member 73. It includes a member 72, one or more restraint parts that changeably restrain the restraint state of the support member 73 with respect to the fixed member 72, and a control part 8 that controls the restraint state of the restraint part so that the restraint state can be changed.

外周側シュラウド76は、翼の先端部分の圧縮空気のシール作用を得る目的などの為、複数の翼に対して翼の先端部分を、共通の一体構造とすることで、ケーシング部への圧縮空気の流入を防ぐ構造に形成される。 The outer shroud 76 has the purpose of sealing the compressed air at the tips of the blades by making the tips of the blades have a common integral structure for multiple blades, thereby preventing the compressed air from reaching the casing. The structure is formed to prevent the inflow of water.

内周側シュラウド74は、翼の付け根部分の圧縮空気のシール作用を得る目的などの為、複数の翼に対して翼の付け根部分を、共通の一体構造とすることで、内部側への圧縮空気の流入を防ぐ構造に形成される。 The inner shroud 74 has a common integral structure at the root of the blade for the purpose of sealing the compressed air at the root of the blade. It is formed in a structure that prevents air from entering.

支持部材73は、静翼環を支持する機能を備える部材である。支持部材73は、静翼環を支持可能な強度を備える部材によって形成されることが好ましい。支持部材73は、静翼環を支持する機能を備える形状に形成されることが好ましい。支持部材73は、内周側シュラウド74の内周面に設けられる。支持部材73は、内周側の端部が、固定部材72を挟み込む形状、例えば、凹形状となっている。 The support member 73 is a member that has a function of supporting the stator blade ring. It is preferable that the support member 73 is formed of a member having enough strength to support the stator vane ring. It is preferable that the support member 73 is formed in a shape that has a function of supporting the stator vane ring. The support member 73 is provided on the inner peripheral surface of the inner shroud 74 . The support member 73 has an inner peripheral end shaped to sandwich the fixing member 72, for example, a concave shape.

固定部材72は、支持部材73を介して、静翼環を固定する対象となる部材である。固定部材72は、支持部材73を介して、静翼環を固定可能な強度を備える部材によって形成される。固定部材72は、支持部材73を介して、静翼環を支持する機能を備える形状に形成される。固定部材72は、例えば、シール保持板である。シール保持板は、シール71を保持する機能を有する部材である。シール保持板は、内周側シュラウド74の内周側に設けられ、支持部材73に対向して設けられる。具体的に、シール保持板は、凹形状となる支持部材73に挟み込まれるように配置される。シール保持板はシール71を備える。シール保持板に備えられるシールとしては、一例としてラビリンスシールが挙げられる。ラビリンスシールは、ハニカム形状のシール受け面と、鋸歯形状のシール歯面によって構成される。 The fixing member 72 is a member to which the stator blade ring is fixed via the support member 73. The fixing member 72 is formed of a member having enough strength to fix the stationary blade ring via the support member 73. The fixing member 72 is formed into a shape that has the function of supporting the stationary blade ring via the support member 73. The fixing member 72 is, for example, a seal holding plate. The seal holding plate is a member that has the function of holding the seal 71. The seal retaining plate is provided on the inner circumferential side of the inner circumferential shroud 74 and is provided facing the support member 73. Specifically, the seal holding plate is arranged so as to be sandwiched between support members 73 having a concave shape. The seal holding plate includes a seal 71. An example of the seal provided on the seal holding plate is a labyrinth seal. The labyrinth seal is composed of a honeycomb-shaped seal receiving surface and sawtooth-shaped seal tooth surfaces.

拘束部は、固定部材72に対する支持部材73の拘束状態を変更可能に拘束する機能を備える。拘束部において、上述したように、支持部材73は、内周側シュラウド74に設けられ、固定部材72は、シール保持板が適用される。 The restraint section has a function of restraining the support member 73 with respect to the fixing member 72 so that the restraint state of the support member 73 can be changed. In the restraining portion, as described above, the support member 73 is provided on the inner circumferential shroud 74, and the fixing member 72 is a seal retaining plate.

制御部8は、拘束部の拘束状態を変更可能に制御する機能を備える。静翼環に備えられた制御部8は、軸流回転機械の制御部の一部を構成するものであって良いし、軸流回転機械の外部に備えられた制御部と、無線又は電気通信回線を介して接続される制御部であっても良い。制御部8は、一例として、CPU(Central Processing Unit)等の集積回路を含んでいる。 The control unit 8 has a function of controlling the restraint state of the restraint unit in a changeable manner. The control unit 8 provided in the stator vane ring may constitute a part of the control unit of the axial flow rotating machine, or may communicate with the control unit provided outside the axial flow rotating machine by radio or electrical communication. It may also be a control unit connected via a line. The control unit 8 includes, for example, an integrated circuit such as a CPU (Central Processing Unit).

本開示に係る軸流回転機械の静翼環は、上述の構成を備えることによって、静翼環に備えられた支持部材73の拘束状態を、制御部8の制御によって変化させ、静翼環の支持剛性を変化させることが出来る。従って、静翼環の支持剛性を変化させることで、静翼環の固有振動数を変化させることが出来る。 The stator vane ring of the axial flow rotary machine according to the present disclosure has the above-described configuration, so that the restraint state of the support member 73 provided in the stator vane ring is changed by the control of the control unit 8, and the stator vane ring is Support rigidity can be changed. Therefore, by changing the support rigidity of the stator blade ring, the natural frequency of the stator blade ring can be changed.

(静翼環の拘束部の構成)
本開示の一態様に係る拘束部は、支持部材と固定部材との間に設けられ、支持部材に対して固定部材を押圧することで固定する付勢部材と、付勢部材に作用する荷重を付加する荷重負荷部材と、を備えることが好ましい。
(Configuration of restraint part of stator vane ring)
A restraining portion according to one aspect of the present disclosure includes a biasing member that is provided between a support member and a fixing member, and that fixes the fixing member by pressing the fixing member against the support member, and a biasing member that suppresses a load acting on the biasing member. It is preferable to include a load bearing member to be applied.

付勢部材は、エネルギーを蓄えることによって、付勢力を発生させる機能を有する部材である。付勢部材としては、板バネ、コイルばね等のバネを用いることが出来るが、これに限定されるものではない。 The biasing member is a member that has a function of generating biasing force by storing energy. As the biasing member, a spring such as a plate spring or a coil spring can be used, but the present invention is not limited thereto.

荷重負荷部材は、荷重を負荷する機能を有する部材である。荷重負荷部材としては、圧電素子、油圧アクチュエータ、電動アクチュエータ等を用いることが出来るが、これに限定されるものではない。 The load bearing member is a member having a function of applying a load. As the load bearing member, a piezoelectric element, a hydraulic actuator, an electric actuator, etc. can be used, but the present invention is not limited thereto.

本開示の一態様に係る拘束部を備える軸流回転機械の静翼環は、上述の構成を備えることによって、荷重負荷部材の荷重を発生させることで、付勢部材の付勢力に対抗する荷重が生じ、付勢部材による固定部材の支持状態が変化する。その結果、静翼環の支持剛性が変化し、静翼環の固有振動数を変化させることが出来る。 A stator vane ring of an axial flow rotary machine including a restraining portion according to an aspect of the present disclosure has the above-described configuration, thereby generating a load of the load-bearing member, thereby generating a load that opposes the biasing force of the biasing member. occurs, and the state in which the fixing member is supported by the biasing member changes. As a result, the support rigidity of the stator blade ring changes, and the natural frequency of the stator blade ring can be changed.

(静翼環の拘束部の第一実施例)
図4は、本開示の静翼環の拘束部の第一実施例を示す概略図である。本開示の第一実施例の静翼環の拘束部は、屈曲部の外側が固定部材72に当接した板バネ77を付勢部材として備え、固定部材72の板バネ77が当接する箇所の反対側に圧電素子78を荷重負荷部材として備える。
(First embodiment of restraint part of stator vane ring)
FIG. 4 is a schematic diagram showing a first embodiment of a restraining portion of a stator vane ring according to the present disclosure. The restraining portion of the stator vane ring according to the first embodiment of the present disclosure includes a leaf spring 77 as a biasing member, the outer side of the bent portion being in contact with the fixing member 72, and the portion of the securing member 72 where the leaf spring 77 comes into contact is A piezoelectric element 78 is provided on the opposite side as a load bearing member.

板バネ77は、平板形状の部材を、板金加工することによって形成される。板バネの形状は、平板の中央部が屈曲した形状に形成されることが好ましい。板バネの材質は特に限定しないが、ステンレスを用いても良い。 The leaf spring 77 is formed by sheet metal processing a flat member. The shape of the leaf spring is preferably a flat plate with a bent central portion. The material of the leaf spring is not particularly limited, but stainless steel may be used.

圧電素子78は、電圧を印加すると形状が変化する性質を有する圧電材料と、電源装置からの電圧が印加される電極と、絶縁物と、を含んで構成される。圧電素子は、電圧に対する高速応答性、形状の微細な制御が可能である等の特性を有している。圧電効果、逆圧電効果を持つ圧電材料には、ジルコン酸チタン酸鉛(PZT)セラミックス、圧電単結晶、圧電高分子ポリマ、圧電コンポジット、圧電積層体などがある。 The piezoelectric element 78 includes a piezoelectric material whose shape changes when a voltage is applied, an electrode to which a voltage from a power supply is applied, and an insulator. Piezoelectric elements have characteristics such as high-speed response to voltage and fine control of shape. Piezoelectric materials having a piezoelectric effect or an inverse piezoelectric effect include lead zirconate titanate (PZT) ceramics, piezoelectric single crystals, piezoelectric polymers, piezoelectric composites, and piezoelectric laminates.

本開示の静翼環の第一実施例に係る拘束部を備える軸流回転機械の静翼環は、上述の構成を備えることによって、図4に示すように、圧電素子78への電圧の印加前(非印加時)において、圧電素子78が収縮状態となるため、固定部材72は、板バネ77により付勢されることで、支持部材73に面接触する。一方で、圧電素子78に電圧を印加することで、圧電素子78が膨張し、板バネ77の付勢力に対抗する荷重が発生する。その結果、板バネ77と圧電素子78との間に把持された固定部材72の支持状態が、図4に示すように面接触から点接触に変化し、静翼環の支持剛性が変化することで、静翼環の固有振動数を変化させることが出来る。 The stator vane ring of an axial flow rotary machine including the restraint part according to the first embodiment of the stator vane ring of the present disclosure has the above-described configuration, so that the voltage can be applied to the piezoelectric element 78 as shown in FIG. Before (when no voltage is applied), the piezoelectric element 78 is in a contracted state, so the fixing member 72 is biased by the plate spring 77 and comes into surface contact with the support member 73 . On the other hand, by applying a voltage to the piezoelectric element 78, the piezoelectric element 78 expands, and a load that opposes the biasing force of the leaf spring 77 is generated. As a result, the support state of the fixed member 72 held between the leaf spring 77 and the piezoelectric element 78 changes from surface contact to point contact as shown in FIG. 4, and the support rigidity of the stator vane ring changes. This allows the natural frequency of the stator blade ring to be changed.

(第一実施例の制御部の作用)
本開示の第一実施例の拘束部を備える静翼環の制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の前記所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、圧電素子に対して、所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された圧電素子の寸法を変化させ、板バネの付勢力に対抗する荷重が変化し、拘束部の支持剛性が変化するように圧電素子を制御する。
(Operation of the control section of the first embodiment)
The control unit for a stator vane ring including a restraint unit according to the first embodiment of the present disclosure is such that the excitation frequency of a predetermined order of the axial flow rotating machine is set to a predetermined value with respect to the natural frequency of the predetermined order of the stator vane ring. A voltage of a predetermined value, which is set such that the excitation frequency of the predetermined order does not match the natural frequency of the predetermined order, for the piezoelectric element connected to the power supply when the value in the range is reached. By applying , the dimensions of the piezoelectric element to which the voltage is applied are changed, the load opposing the biasing force of the leaf spring is changed, and the piezoelectric element is controlled so that the support rigidity of the restraint part is changed.

所定の次数の励振周波数とは、軸流回転機械の基本周波数の整数倍の値を意味する。その為、所定の次数の励振周波数は基本周波数、すなわち基本周波数の1倍を含む。所定の次数の励振周波数が、それと次数が一致する所定の次数の固有振動数と一致した場合に、共振が発生し、静翼に動的応力が作用する。 The excitation frequency of a predetermined order means a value that is an integral multiple of the fundamental frequency of the axial flow rotating machine. Therefore, the excitation frequency of a predetermined order includes the fundamental frequency, ie, one time the fundamental frequency. When the excitation frequency of a predetermined order matches the natural frequency of a predetermined order that matches the excitation frequency, resonance occurs and dynamic stress acts on the stationary blade.

静翼環の所定の次数の固有振動数に対して、それと次数が一致する所定の次数の励振周波数が、所定の範囲の値に達した場合であっても、共振によって静翼の振幅が増加し、静翼に動的応力が作用する。従って、「軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の範囲の値に達した場合」とは、所定の次数の励振周波数が、所定の次数の固有振動数に近付くと発生する共振によって、引き起こされる静翼に作用する動的応力が、静翼の材料の耐力に対して、十分な安全マージンを確保した範囲の境界の値に達した場合を意味する。 Even if the excitation frequency of a given order that matches the natural frequency of a given order of the stator vane ring reaches a value within a given range, the amplitude of the stator vane increases due to resonance. However, dynamic stress acts on the stator blade. Therefore, "when the excitation frequency of a predetermined order of the axial flow rotating machine reaches a value within a predetermined range with respect to the natural frequency of a predetermined order of the stator blade ring" means that the excitation frequency of a predetermined order is , the dynamic stress acting on the stator vane caused by the resonance that occurs as it approaches the natural frequency of a given order is the boundary value of the range that ensures a sufficient safety margin with respect to the yield strength of the stator vane material. This means that the value is reached.

圧電素子は印加された電圧に比例して、圧電材料部分の寸法が膨張する。圧電材料の寸法の変化と電圧の関係に従って、静翼環の支持剛性が変化する程度の電圧値を決定することが出来る。すなわち、静翼環の支持剛性と静翼環の固有振動数との関係を、数値シミュレーション、もしくは、実験によって、調査することによって、共振回避が可能な電圧値を決定することが出来る。従って、「所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧」とは、所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して、所定の範囲の値に達した場合に、静翼環の固有振動数を、所定の次数の励振周波数に対して、静翼の材料の耐力を考慮して十分な安全マージンを確保した離れた値に、変更可能な電圧値を意味する。 The piezoelectric element expands in size in proportion to the applied voltage. According to the relationship between the change in the dimensions of the piezoelectric material and the voltage, it is possible to determine the voltage value at which the support rigidity of the stator vane ring changes. That is, by investigating the relationship between the support rigidity of the stator blade ring and the natural frequency of the stator blade ring through numerical simulation or experiment, it is possible to determine a voltage value that allows resonance to be avoided. Therefore, "a voltage of a predetermined value that is set so that the excitation frequency of a predetermined order does not match the natural frequency of a predetermined order" means that the excitation frequency of a predetermined order does not match the natural frequency of a predetermined order of the stator blade ring. When the natural frequency of the stator vane ring reaches a value within a predetermined range, the natural frequency of the stator vane ring is determined to be sufficient for the excitation frequency of the predetermined order, taking into account the yield strength of the material of the stator vane. It means a voltage value that can be changed to a distant value with a safety margin.

図7は、上述の制御部によって静翼環の固有振動数を変更した結果の一例を示す説明図である。軸流回転機械の所定の次数の励振周波数が、それと一致する所定の次数の固有振動数に対して、所定の範囲の値に達した場合に、圧電素子に固有振動数に一致しないよう設定された所定の電圧を印加し、固有振動数が減少する方向に圧電素子の寸法を変化させ、静翼環の支持剛性を変化させることで、固有振動数を減少させる方向に変化させる。本例では、固有振動数が励振周波数を跨いで、励振周波数以下の値であり、かつ、励振周波数に対して十分に離れた値となるように、固有振動数を変化させ、共振の発生を回避する。 FIG. 7 is an explanatory diagram showing an example of the result of changing the natural frequency of the stator blade ring by the above-mentioned control unit. When the excitation frequency of a predetermined order of the axial flow rotating machine reaches a value within a predetermined range with respect to the natural frequency of a predetermined order that matches it, the piezoelectric element is set so that it does not match the natural frequency. By applying a predetermined voltage, the dimensions of the piezoelectric element are changed in a direction that reduces the natural frequency, and the supporting rigidity of the stator vane ring is changed, thereby changing the natural frequency in a direction that reduces the natural frequency. In this example, the natural frequency is changed so that it straddles the excitation frequency, is below the excitation frequency, and is sufficiently far away from the excitation frequency to prevent the occurrence of resonance. To avoid.

図8は、上述の制御部によって静翼環の固有振動数を変更した結果の他の例を示す説明図である。本例では、静翼環の固有振動数を増加させる方向に、静翼環の支持剛性を変化させる。その後、励振周波数の増加に伴い、再度、励振周波数が固有振動数に対して所定の範囲に達した場合には、再び同様の制御を行うことで、固有振動数を増加させ、共振を回避する。この際に固有振動数は、低次励振周波数を超えた値であり、かつ、高次励振周波数未満の値となるように、低次励振周波数が固有振動数に近付く度に段階的に制御される。なお、上述の制御部による固有振動数の具体的な制御結果は、図7、及び、図8に示す態様に限定されるものではない。 FIG. 8 is an explanatory diagram showing another example of the result of changing the natural frequency of the stator blade ring by the above-mentioned control unit. In this example, the support rigidity of the stator blade ring is changed in a direction that increases the natural frequency of the stator blade ring. After that, as the excitation frequency increases, if the excitation frequency reaches a predetermined range with respect to the natural frequency again, the same control is performed again to increase the natural frequency and avoid resonance. . At this time, the natural frequency is controlled in stages as the low-order excitation frequency approaches the natural frequency so that the value exceeds the low-order excitation frequency and is less than the high-order excitation frequency. Ru. Note that the specific control results of the natural frequency by the above-mentioned control section are not limited to the modes shown in FIGS. 7 and 8.

上述の構成を備えることによって、本開示の第一実施例の拘束部を備える静翼環の制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の範囲の値に達した場合に、圧電素子に対して、所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された圧電素子の寸法が変化し、板バネの付勢力に対抗する荷重が変化し、静翼環の支持剛性が変化し、静翼環の固有振動数が変化することで、共振を回避することが可能となる。共振回避が可能となることから、共振発生時に静翼に作用する動的応力に耐えられるように、静翼の翼厚さを厚肉化する必要がなくなり、軸流回転機械の性能向上に寄与することが出来る。 By having the above-mentioned configuration, the control unit for the stator vane ring including the restraint unit according to the first embodiment of the present disclosure can control the excitation frequency of the predetermined order of the axial flow rotating machine to the characteristic of the predetermined order of the stator vane ring. A voltage of a predetermined value that is set so that the excitation frequency of a predetermined order does not match the natural frequency of a predetermined order for the piezoelectric element when a value in a predetermined range for the vibration frequency is reached. By applying , the dimensions of the piezoelectric element to which voltage is applied change, the load that opposes the urging force of the leaf spring changes, the supporting rigidity of the stator blade ring changes, and the natural frequency of the stator blade ring changes. This change makes it possible to avoid resonance. Since it is possible to avoid resonance, there is no need to increase the thickness of the stator blades in order to withstand the dynamic stress that is applied to the stator blades when resonance occurs, contributing to improved performance of axial flow rotating machines. You can.

(静翼環の拘束部の第二実施例)
図5は、本開示の静翼環の拘束部の第二実施例を示す概略図である。本開示の第二実施例の静翼環の拘束部は、屈曲部の外側が固定部材72に当接した板バネ77を付勢部材として備え、板バネ77の屈曲部の内側に圧電素子78を備える。
(Second embodiment of restraint part of stator vane ring)
FIG. 5 is a schematic diagram showing a second embodiment of the constraint portion of the stator vane ring of the present disclosure. The restraining portion of the stator vane ring according to the second embodiment of the present disclosure includes a plate spring 77 as a biasing member, the outer side of the bent portion being in contact with the fixed member 72, and a piezoelectric element 78 inside the bent portion of the plate spring 77. Equipped with.

板バネ77は、静翼環の拘束部の第一実施例に係るものと、同様のものを用いて良い。 The leaf spring 77 may be the same as that used in the first embodiment of the restraining portion of the stationary vane ring.

圧電素子78は、折り曲げ可能な圧電素子を用いる。圧電セラミック粉と、圧電ゾルゲル溶液を混合し、攪拌、塗布、焼結して作製される圧電膜を用いることで、折り曲げ可能な圧電素子を得ることが出来る。圧電素子78は、板バネ77の屈曲部の内側に施工される。 The piezoelectric element 78 uses a bendable piezoelectric element. A bendable piezoelectric element can be obtained by using a piezoelectric film produced by mixing piezoelectric ceramic powder and a piezoelectric sol-gel solution, stirring, coating, and sintering. The piezoelectric element 78 is installed inside the bent portion of the leaf spring 77.

本開示の第二実施例に係る拘束部を備える軸流回転機械の静翼環は、上述の構成を備えることによって、圧電素子78に電圧を印加することで、圧電素子78が膨張し、板バネ77の屈曲部を内側から広げる作用が生じる。その結果、板バネ77に把持された固定部材72の支持状態が、図5に示すように面接触から接触無し状態に変化し、静翼環の支持剛性が変化することで、静翼環の固有振動数を変化させることが出来る。 The stator vane ring of an axial flow rotary machine including a restraining portion according to the second embodiment of the present disclosure has the above-described configuration, so that when a voltage is applied to the piezoelectric element 78, the piezoelectric element 78 expands and the plate This creates an effect of widening the bent portion of the spring 77 from the inside. As a result, the supporting state of the fixed member 72 gripped by the leaf spring 77 changes from surface contact to non-contact state as shown in FIG. The natural frequency can be changed.

(第二実施例の制御部の作用)
本開示の第二実施例の拘束部を備える静翼環の制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、圧電素子に対して、所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された圧電素子の寸法が変化し、板バネの付勢力が変化し、拘束部の支持剛性が変化するように、圧電素子を制御する。
(Operation of the control unit of the second embodiment)
The control unit for a stator vane ring including a restraint unit according to the second embodiment of the present disclosure is arranged such that the excitation frequency of a predetermined order of the axial flow rotating machine is within a predetermined range with respect to the natural frequency of a predetermined order of the stator vane ring. When the value of is reached, a voltage of a predetermined value is applied to the piezoelectric element connected to the power supply, which is set so that the excitation frequency of the predetermined order does not match the natural frequency of the predetermined order. By applying the voltage, the piezoelectric element is controlled so that the dimensions of the piezoelectric element to which the voltage is applied change, the biasing force of the leaf spring changes, and the support rigidity of the restraint part changes.

「軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の値に達した場合」の意味は、本開示の第一実施例の拘束部を備える静翼環の制御部において用いた用語の意味と同一である。 The meaning of "when the excitation frequency of a predetermined order of the axial flow rotating machine reaches a predetermined value with respect to the natural frequency of a predetermined order of the stator blade ring" is defined by the constraint section of the first embodiment of the present disclosure. The meaning of the term is the same as that used in the control section of the stator vane ring.

同様に、「所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧」の意味は、本開示の第一実施例の拘束部を備える静翼環の制御部において用いた用語の意味と同一である。 Similarly, "a voltage of a predetermined value that is set such that the excitation frequency of a predetermined order does not match the natural frequency of a predetermined order" means that the static The meanings of the terms used in the control section of the blade ring are the same.

図9は、上述の制御部によって静翼環の固有振動数を変更した結果の一例を示す説明図である。軸流回転機械の所定の次数の励振周波数が、それと次数が一致する固有振動数に対して、所定の範囲の値に達した場合に、固有振動数に一致しないよう設定された所定の電圧を圧電素子に印加し、圧電素子の寸法を変化させ、静翼環の支持剛性を変化させることで、固有振動数を変化させ、共振の発生を回避する。図9に示す例では、静翼環の固有振動数を増加させる方向に、静翼環の支持剛性を変化させる。具体的には、励振周波数の増加に伴って、固有振動数が、低次励振周波数を超えた値であり、かつ、高次励振周波数未満の値となるように、連続的に固有振動数を変化させ、共振を回避する。なお、上述の制御部による固有振動数の具体的な制御結果は、図9に示す態様に限定されるものではない。 FIG. 9 is an explanatory diagram showing an example of the result of changing the natural frequency of the stator blade ring by the above-mentioned control unit. When the excitation frequency of a predetermined order of the axial flow rotating machine reaches a value within a predetermined range with respect to the natural frequency of the same order, a predetermined voltage set so as not to match the natural frequency is applied. By applying an electric current to the piezoelectric element, changing the dimensions of the piezoelectric element, and changing the support rigidity of the stator vane ring, the natural frequency is changed and resonance is avoided. In the example shown in FIG. 9, the support rigidity of the stator blade ring is changed in a direction that increases the natural frequency of the stator blade ring. Specifically, as the excitation frequency increases, the natural frequency is continuously increased so that the natural frequency exceeds the low-order excitation frequency and is less than the high-order excitation frequency. change and avoid resonance. Note that the specific control result of the natural frequency by the above-mentioned control unit is not limited to the mode shown in FIG. 9 .

上述の構成を備えることによって、本開示の第二実施例の拘束部を備える静翼環の制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、圧電素子に対して、所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された圧電素子の寸法が変化し、板バネの付勢力が変化し、静翼環の支持剛性が変化し、静翼環の固有振動数が変化することで、共振を回避することが可能となる。共振回避が可能となることから、共振発生時に静翼に作用する動的応力に耐えられるように、静翼の翼厚さを厚肉化する必要がなくなり、軸流回転機械の性能向上に寄与することが出来る。 By having the above-described configuration, the control unit for the stator vane ring including the restraint unit according to the second embodiment of the present disclosure can control the excitation frequency of the predetermined order of the axial flow rotating machine to the characteristic of the predetermined order of the stator vane ring. When the vibration frequency reaches a value within a predetermined range, the excitation frequency of the predetermined order of the piezoelectric element connected to the power supply is set so that it does not match the natural frequency of the predetermined order. In addition, by applying a voltage of a predetermined value, the dimensions of the piezoelectric element to which the voltage is applied change, the biasing force of the leaf spring changes, the supporting rigidity of the stator vane ring changes, and the characteristic of the stator vane ring changes. By changing the frequency, resonance can be avoided. Since it is possible to avoid resonance, there is no need to increase the thickness of the stator blades in order to withstand the dynamic stress that is applied to the stator blades when resonance occurs, contributing to improved performance of axial flow rotating machines. You can.

(静翼環の拘束部の第三実施例)
図6は、本開示の静翼環の拘束部の第三実施例を示す概略図である。本開示の第三実施例の静翼環の拘束部は、一以上の孔が形成された固定部材72と、一以上の孔の数と同一の数の圧電素子78と、を備え、圧電素子78は、固定部材72に形成された一以上の孔に挿入された上で、その両端部が支持部材73に対して固定される。
(Third embodiment of restraint part of stator vane ring)
FIG. 6 is a schematic diagram showing a third embodiment of the constraint portion of the stator vane ring of the present disclosure. The restraining portion of the stator vane ring according to the third embodiment of the present disclosure includes a fixing member 72 in which one or more holes are formed, and piezoelectric elements 78 of the same number as the one or more holes, and the piezoelectric elements 78 is inserted into one or more holes formed in the fixing member 72, and both ends thereof are fixed to the support member 73.

固定部材72に形成される孔は、圧電素子を挿入可能な直径の円形の形状に形成される。 The hole formed in the fixing member 72 is formed in a circular shape with a diameter that allows insertion of the piezoelectric element.

本開示の第三実施例に係る拘束部を備える軸流回転機械の静翼環は、上述の構成を備えることによって、圧電素子78に電圧を印加することで、圧電素子78が膨張し、図6に示すように、固定部材に形成された孔と圧電素子の接触範囲が狭い支持状態から、接触範囲が広い支持状態に変化する。その結果、固定部材72の支持状態が変化し、静翼環の支持剛性が変化することで、静翼環の固有振動数を変化させることが出来る。 The stator vane ring of an axial flow rotary machine including a restraining part according to the third embodiment of the present disclosure has the above-described configuration, so that when a voltage is applied to the piezoelectric element 78, the piezoelectric element 78 expands, and as shown in FIG. As shown in 6, the supported state in which the contact range between the hole formed in the fixing member and the piezoelectric element is narrow changes to the supported state in which the contact range is wide. As a result, the supporting state of the fixed member 72 changes, and the support rigidity of the stator blade ring changes, so that the natural frequency of the stator blade ring can be changed.

(第三実施例の制御部の作用)
本開示の第三実施例の拘束部を備える静翼環の制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、圧電素子に対して、所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、所定の値の電圧が印加された圧電素子の寸法が変化し、拘束部の支持剛性が変化するように、圧電素子を制御する。
(Operation of the control section of the third embodiment)
The control unit for a stator vane ring including a restraint unit according to the third embodiment of the present disclosure is arranged such that the excitation frequency of a predetermined order of the axial flow rotating machine is within a predetermined range with respect to the natural frequency of a predetermined order of the stator vane ring. When the value of is reached, a voltage of a predetermined value is applied to the piezoelectric element connected to the power supply, which is set so that the excitation frequency of the predetermined order does not match the natural frequency of the predetermined order. By applying the voltage, the dimensions of the piezoelectric element to which the voltage of a predetermined value is applied change, and the piezoelectric element is controlled so that the support rigidity of the restraint part changes.

「軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の値に達した場合」の意味は、本開示の第一実施例の拘束部を備える静翼環の制御部において用いた用語の意味と同一である。 The meaning of "when the excitation frequency of a predetermined order of the axial flow rotating machine reaches a predetermined value with respect to the natural frequency of a predetermined order of the stator blade ring" is defined by the constraint section of the first embodiment of the present disclosure. The meaning of the term is the same as that used in the control section of the stator vane ring.

同様に、「所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧」の意味は、本開示の第一実施例の拘束部を備える静翼環の制御部において用いた用語の意味と同一である。 Similarly, "a voltage of a predetermined value that is set such that the excitation frequency of a predetermined order does not match the natural frequency of a predetermined order" means that the static The meanings of the terms used in the control section of the blade ring are the same.

上述の構成を備えることによって、本開示の第三実施例の拘束部を備える静翼環の制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、圧電素子に対して、所定の次数の励振周波数が所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された圧電素子の寸法が変化し、拘束部の支持剛性が変化し、静翼環の固有振動数が変化することで、共振を回避することが可能となる。共振回避が可能となることから、共振発生時に静翼に作用する動的応力に耐えられるように、静翼の翼厚さを厚肉化する必要がなくなり、軸流回転機械の性能向上に寄与することが出来る。 By having the above-described configuration, the control unit for a stator vane ring equipped with a restraint unit according to the third embodiment of the present disclosure can control the excitation frequency of a predetermined order of the axial flow rotating machine to the characteristic of a predetermined order of the stator vane ring. When the vibration frequency reaches a value within a predetermined range, the excitation frequency of the predetermined order of the piezoelectric element connected to the power supply is set so that it does not match the natural frequency of the predetermined order. In addition, by applying a voltage of a predetermined value, the dimensions of the piezoelectric element to which the voltage is applied change, the support rigidity of the restraint part changes, and the natural frequency of the stator vane ring changes, causing resonance. It is possible to avoid this. Since it is possible to avoid resonance, there is no need to increase the thickness of the stator blades in order to withstand the dynamic stress that is applied to the stator blades when resonance occurs, contributing to improved performance of axial flow rotating machines. You can.

なお、上述の本開示に係る軸流回転機械の静翼環では、支持部材73を内周側シュラウド74に設け、固定部材72をシール保持板としたが、この構成に限定されない。支持部材73を、外周側シュラウド76に設け、固定部材72を、外周側シュラウドの外周側に設けられるケーシングに適用しても良い。 Note that in the stator vane ring of the axial flow rotary machine according to the present disclosure described above, the support member 73 is provided on the inner peripheral side shroud 74 and the fixing member 72 is a seal holding plate, but the structure is not limited to this. The support member 73 may be provided on the outer shroud 76, and the fixing member 72 may be applied to a casing provided on the outer circumferential side of the outer shroud.

また、上述の本開示に係る軸流回転機械の静翼環を、ターボファンエンジン1に適用したが、他の軸流回転機械に適用しても良い。 Moreover, although the stationary blade ring of the axial flow rotary machine according to the present disclosure described above is applied to the turbofan engine 1, it may be applied to other axial flow rotary machines.

本開示の軸流回転機械の静翼環は、複数の静翼75と、前記複数の静翼75の先端部に設けられる外周側シュラウド76と、前記複数の静翼75の根元部に設けられる内周側シュラウド74と、前記外周側シュラウド76、及び、前記内周側シュラウド74の内の一方に設けられる一以上の支持部材73と、前記支持部材73に対向して設けられる固定部材72と、前記固定部材72に対する前記支持部材73の拘束状態を変更可能に拘束する一以上の拘束部と、前記拘束部の拘束状態を変更可能に制御する制御部8と、を備える。 The stator vane ring of the axial flow rotary machine according to the present disclosure includes a plurality of stator blades 75, an outer peripheral side shroud 76 provided at the tips of the plurality of stator blades 75, and a stator blade ring provided at the root of the plurality of stator blades 75. An inner shroud 74, an outer shroud 76, one or more support members 73 provided on one of the inner shrouds 74, and a fixing member 72 provided opposite the support member 73. , one or more restraint parts that changeably restrain the restraint state of the support member 73 with respect to the fixing member 72, and a control part 8 that controls the restraint state of the restraint part in a changeable manner.

この構成によれば、静翼環の支持剛性を変えることによって、静翼環の固有振動数と励振周波数が一致しないように、静翼環の固有振動数を変えることが出来ることから、静翼環の固有振動数と励振周波数の一致による共振を回避することが可能となる。 According to this configuration, by changing the support rigidity of the stator blade ring, the natural frequency of the stator blade ring can be changed so that the natural frequency of the stator blade ring and the excitation frequency do not match. It becomes possible to avoid resonance due to coincidence of the natural frequency of the ring and the excitation frequency.

前記拘束部は、前記支持部材73と前記固定部材72との間に設けられ、前記支持部材73に対して前記固定部材72を押圧することで固定する付勢部材と、前記付勢部材に作用する荷重を付加する荷重負荷部材と、を備える。 The restraint part is provided between the support member 73 and the fixing member 72, and includes a biasing member that fixes the fixing member 72 by pressing it against the support member 73, and a biasing member that acts on the biasing member. and a load bearing member that applies a load.

この構成によれば、付勢部材と荷重負荷部材とを用いた簡易な構成により、支持部材73と固定部材72との拘束状態を変更することができる。 According to this configuration, the restraint state between the support member 73 and the fixing member 72 can be changed with a simple configuration using the urging member and the load application member.

前記付勢部材は、屈曲部の外側が前記固定部材72に当接した板バネ77を備え、かつ、前記荷重負荷部材は、前記固定部材72の前記板バネ77が当接する箇所の反対側に圧電素子78を備える。 The biasing member includes a leaf spring 77 whose bent portion is in contact with the fixing member 72 on the outside, and the load-bearing member is provided on the opposite side of the fixing member 72 from where the leaf spring 77 comes into contact. A piezoelectric element 78 is provided.

この構成によれば、板バネ77及び圧電素子78を用いて、固定部材72の接触状態を、面接触と点接触との間で変更することができるため、支持部材73と固定部材72との拘束状態を適切に変更することができる。 According to this configuration, the contact state of the fixing member 72 can be changed between surface contact and point contact using the leaf spring 77 and the piezoelectric element 78. The restraint state can be changed appropriately.

前記制御部8は、軸流回転機械の所定の次数の励振周波数が、静翼環の前記所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、前記圧電素子78に対して、前記所定の次数の励振周波数が前記所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された前記圧電素子78の寸法が変化し、前記板バネ77の付勢力に対抗する荷重が変化し、前記拘束部の支持剛性が変化するように制御する。 The control unit 8 is connected to the power supply device when the excitation frequency of a predetermined order of the axial flow rotating machine reaches a value within a predetermined range with respect to the natural frequency of the predetermined order of the stator blade ring. Further, a voltage is applied to the piezoelectric element 78 by applying a voltage of a predetermined value, which is set so that the excitation frequency of the predetermined order does not match the natural frequency of the predetermined order. The dimensions of the piezoelectric element 78 are changed, the load opposing the biasing force of the leaf spring 77 is changed, and the support rigidity of the restraining portion is controlled to change.

この構成によれば、圧電素子78への電圧の印加を制御することで、固有振動数と励振周波数とが一致しないように、拘束部の支持剛性を変化させることができる。 According to this configuration, by controlling the application of voltage to the piezoelectric element 78, it is possible to change the support rigidity of the restraining portion so that the natural frequency and the excitation frequency do not match.

前記付勢部材は、屈曲部の外側が前記固定部材に当接した板バネ77を備え、かつ、前記荷重負荷部材は、前記板バネ77の屈曲部の内側に圧電素子78を備える。 The biasing member includes a plate spring 77 with the outside of the bent portion in contact with the fixing member, and the load applying member includes a piezoelectric element 78 inside the bent portion of the plate spring 77.

この構成によれば、板バネ77及び圧電素子78を用いて、固定部材72の接触圧を連続的に変更することができるため、支持部材73と固定部材72との拘束状態をより詳細に変更することができる。 According to this configuration, since the contact pressure of the fixing member 72 can be continuously changed using the leaf spring 77 and the piezoelectric element 78, the restraint state between the support member 73 and the fixing member 72 can be changed in more detail. can do.

前記制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の前記所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、前記圧電素子78に対して、前記所定の次数の励振周波数が前記所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された前記圧電素子78の寸法が変化し、前記板バネ77の付勢力が変化し、前記拘束部の支持剛性が変化するように制御する。 The control unit is connected to a power supply device when the excitation frequency of a predetermined order of the axial flow rotating machine reaches a value in a predetermined range with respect to the natural frequency of the predetermined order of the stator blade ring. , a voltage is applied to the piezoelectric element 78 by applying a voltage of a predetermined value, which is set such that the excitation frequency of the predetermined order does not match the natural frequency of the predetermined order. Control is performed so that the dimensions of the piezoelectric element 78 change, the biasing force of the plate spring 77 changes, and the support rigidity of the restraint part changes.

この構成によれば、圧電素子78への電圧の印加を制御することで、固有振動数と励振周波数とが一致しないように、拘束部の支持剛性を変化させることができる。 According to this configuration, by controlling the application of voltage to the piezoelectric element 78, it is possible to change the support rigidity of the restraining portion so that the natural frequency and the excitation frequency do not match.

前記拘束部は、一以上の孔が形成された前記固定部材と、前記一以上の孔に対応する数の圧電素子と、を備え、前記圧電素子は、前記固定部材に形成された一以上の孔に挿入された上で、両端部が前記支持部材に対して固定される。 The restraint section includes the fixing member in which one or more holes are formed, and a number of piezoelectric elements corresponding to the one or more holes, and the piezoelectric elements are arranged in one or more holes formed in the fixing member. After being inserted into the hole, both ends are fixed to the support member.

この構成によれば、付勢部材を省いた構成とすることができるため、拘束部をより簡素化した構成とすることができる。 According to this configuration, since the biasing member can be omitted, the restraining portion can be configured more simply.

前記制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の前記所定の次数の固有振動数に対して所定の範囲の値に達した場合に、電源装置に接続された、前記圧電素子に対して、前記所定の次数の励振周波数が前記所定の次数の固有振動数に一致しないように設定された、所定の値の電圧を印加することで、電圧が印加された前記圧電素子の寸法が変化し、前記拘束部の支持剛性が変化するように制御する。 The control unit is connected to a power supply device when the excitation frequency of a predetermined order of the axial flow rotating machine reaches a value in a predetermined range with respect to the natural frequency of the predetermined order of the stator blade ring. , by applying a voltage of a predetermined value to the piezoelectric element such that the excitation frequency of the predetermined order does not match the natural frequency of the predetermined order, the voltage is applied to the piezoelectric element. Control is performed so that the dimensions of the piezoelectric element change and the support rigidity of the restraint part changes.

この構成によれば、圧電素子78への電圧の印加を制御することで、固有振動数と励振周波数とが一致しないように、拘束部の支持剛性を変化させることができる。 According to this configuration, by controlling the application of voltage to the piezoelectric element 78, it is possible to change the support rigidity of the restraining portion so that the natural frequency and the excitation frequency do not match.

前記支持部材は、前記内周側シュラウドに設けられ、前記固定部材は、シール保持板を備える。 The support member is provided on the inner shroud, and the fixing member includes a seal retaining plate.

この構成によれば、拘束部を内周側シュラウドに設けることができるため、圧電素子78を用いた支持剛性の変更を行うことができる。 According to this configuration, since the restraining portion can be provided on the inner peripheral side shroud, the support rigidity can be changed using the piezoelectric element 78.

前記支持部材は、前記外周側シュラウドに設けられ、前記固定部材は、ケーシングを備えてもよい。 The support member may be provided on the outer shroud, and the fixing member may include a casing.

軸流回転機械は、上述の軸流回転機械の静翼環を備える。 The axial flow rotary machine includes the stator vane ring of the axial flow rotary machine described above.

この構成によれば、静翼環の共振を抑制した軸流回転機械を提供することができる。 According to this configuration, it is possible to provide an axial flow rotary machine in which resonance of the stator blade ring is suppressed.

1 ターボファンエンジン
2 ファン
3 圧縮機
4 燃焼室
5 タービン
6 回転軸
1 Turbofan engine 2 Fan 3 Compressor 4 Combustion chamber 5 Turbine 6 Rotating shaft

Claims (11)

複数の静翼と、
前記複数の静翼の先端部に設けられる外周側シュラウドと、
前記複数の静翼の根元部に設けられる内周側シュラウドと、
前記外周側シュラウド、及び、前記内周側シュラウドの内の一方に設けられる一以上の支持部材と、
前記支持部材に対向して設けられる固定部材と、
前記固定部材に対する前記支持部材の拘束状態を変更可能に拘束する一以上の拘束部と、
前記拘束部の拘束状態を変更可能に制御する制御部と、
を備え
前記拘束部は、一以上の圧電素子を備え、
前記制御部は、軸流回転機械の所定の次数の励振周波数が、静翼環の前記所定の次数の固有振動数に対して所定の範囲の値に達した場合に、
電源装置に接続された、前記圧電素子に対して、前記所定の次数の励振周波数が前記所定の次数の固有振動数に一致しないように設定された、
所定の値の電圧を印加することで、
電圧が印加された前記圧電素子の寸法が変化し、前記拘束部の支持剛性が変化することで前記拘束状態を変更する、
軸流回転機械の静翼環。
a plurality of stationary blades;
an outer peripheral shroud provided at the tips of the plurality of stator blades;
an inner circumferential shroud provided at the root portion of the plurality of stator blades;
one or more support members provided on one of the outer shroud and the inner shroud;
a fixing member provided opposite to the support member;
one or more restraint portions that restrain the support member in a manner that can change the restraint state of the support member relative to the fixing member;
a control unit configured to changeably control the restraint state of the restraint unit;
Equipped with
The restraint section includes one or more piezoelectric elements,
The control unit is configured to:
The piezoelectric element connected to the power supply device is set such that the excitation frequency of the predetermined order does not match the natural frequency of the predetermined order.
By applying a voltage of a predetermined value,
changing the restraint state by changing the dimensions of the piezoelectric element to which a voltage is applied and changing the support rigidity of the restraint part;
Stator blade ring of axial flow rotating machine.
前記拘束部は、前記支持部材と前記固定部材との間に設けられ、
前記支持部材に対して前記固定部材を押圧することで固定する付勢部材と、
前記付勢部材に作用する荷重を付加する荷重負荷部材と、
を備える請求項1に記載の軸流回転機械の静翼環。
The restraining part is provided between the supporting member and the fixing member,
an urging member that fixes the fixing member by pressing it against the support member;
a load-bearing member that applies a load acting on the biasing member;
The stationary blade ring for an axial flow rotating machine according to claim 1, comprising:
前記付勢部材は、屈曲部の外側が前記固定部材に当接した板バネを備え、かつ、
前記荷重負荷部材は、前記固定部材の前記板バネが当接する箇所の反対側に圧電素子を備える
請求項2に記載の軸流回転機械の静翼環。
The biasing member includes a leaf spring whose outer side of a bent portion is in contact with the fixing member, and
The stator vane ring for an axial flow rotary machine according to claim 2, wherein the load bearing member includes a piezoelectric element on the opposite side of the portion of the fixed member that is in contact with the leaf spring.
前記制御部が印加する所定の値の電圧により、電圧が印加された前記圧電素子の寸法が変化し、前記板バネの付勢力に対抗する荷重が変化し、前記拘束部の支持剛性が変化する
請求項3に記載の軸流回転機械の静翼環。
A voltage of a predetermined value applied by the control section changes the dimensions of the piezoelectric element to which the voltage is applied, changes the load opposing the biasing force of the leaf spring, and changes the support rigidity of the restraint section. A stator blade ring for an axial flow rotating machine according to claim 3.
前記付勢部材は、屈曲部の外側が前記固定部材に当接した板バネを備え、かつ、
前記荷重負荷部材は、前記板バネの屈曲部の内側に圧電素子を備える
請求項2に記載の軸流回転機械の静翼環。
The biasing member includes a leaf spring whose outer side of a bent portion is in contact with the fixing member, and
The stator vane ring for an axial flow rotary machine according to claim 2, wherein the load bearing member includes a piezoelectric element inside a bent portion of the leaf spring.
前記制御部が印加する所定の値の電圧により、電圧が印加された前記圧電素子の寸法が変化し、前記板バネの付勢力が変化し、前記拘束部の支持剛性が変化する
請求項5に記載の軸流回転機械の静翼環。
According to claim 5, the voltage of a predetermined value applied by the control unit changes the dimensions of the piezoelectric element to which the voltage is applied, changes the biasing force of the leaf spring, and changes the support rigidity of the restraint part. Stator blade ring of the described axial flow rotating machine.
前記拘束部は、一以上の孔が形成された前記固定部材と、
前記一以上の孔に対応する数の圧電素子と、を備え、
前記圧電素子は、前記固定部材に形成された一以上の孔に挿入された上で、両端部が前記支持部材に対して固定された
請求項1に記載の軸流回転機械の静翼環。
The restraining portion includes the fixing member in which one or more holes are formed;
comprising a number of piezoelectric elements corresponding to the one or more holes,
The stator vane ring for an axial flow rotary machine according to claim 1, wherein the piezoelectric element is inserted into one or more holes formed in the fixing member, and both ends thereof are fixed to the support member.
前記制御部が印加する所定の値の電圧により、電圧が印加された前記圧電素子の寸法が変化し、前記拘束部の支持剛性が変化する
請求項7に記載の軸流回転機械の静翼環。
The stator vane ring for an axial flow rotating machine according to claim 7 , wherein the voltage of a predetermined value applied by the control unit changes the dimensions of the piezoelectric element to which the voltage is applied, and the support rigidity of the restraint part changes. .
前記支持部材は、前記内周側シュラウドに設けられ、
前記固定部材は、シール保持板を備える、
請求項2から請求項8のいずれか一項に記載の軸流回転機械の静翼環。
The support member is provided on the inner shroud,
The fixing member includes a seal retaining plate.
A stator vane ring for an axial flow rotating machine according to any one of claims 2 to 8.
前記支持部材は、前記外周側シュラウドに設けられ、
前記固定部材は、ケーシングを備える、
請求項1から請求項8のいずれか一項に記載の軸流回転機械の静翼環。
The support member is provided on the outer shroud,
The fixing member includes a casing.
A stator vane ring for an axial flow rotating machine according to any one of claims 1 to 8.
請求項1から請求項10のいずれか一項に記載の軸流回転機械の静翼環を備える、軸流回転機械。 An axial-flow rotary machine, comprising the stator vane ring of the axial-flow rotary machine according to any one of claims 1 to 10.
JP2020041124A 2020-03-10 2020-03-10 Stator blade ring of axial flow rotating machine and axial flow rotating machine Active JP7365942B2 (en)

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JP2003214399A (en) 2002-01-18 2003-07-30 Ishikawajima Harima Heavy Ind Co Ltd Characteristic frequency variable mechanism for stationary blade of compressor
JP2010151045A (en) 2008-12-25 2010-07-08 Mitsubishi Heavy Ind Ltd Turbine blade and gas turbine
JP2012112383A (en) 2010-11-24 2012-06-14 Alstom Technology Ltd Method for affecting mechanical vibration occurring during operation in turbo machine blade, turbo machine blade for executing the method, and piezoelectric damping member to be assembled to the turbo machine blade
JP2013072688A (en) 2011-09-27 2013-04-22 Mitsubishi Heavy Ind Ltd Natural frequency measuring device and natural frequency measuring method
US20190360354A1 (en) 2018-05-24 2019-11-28 MTU Aero Engines AG Turbomachine assembly with a detuning device for different detuning of natural frequencies of the blades

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003214399A (en) 2002-01-18 2003-07-30 Ishikawajima Harima Heavy Ind Co Ltd Characteristic frequency variable mechanism for stationary blade of compressor
JP2010151045A (en) 2008-12-25 2010-07-08 Mitsubishi Heavy Ind Ltd Turbine blade and gas turbine
JP2012112383A (en) 2010-11-24 2012-06-14 Alstom Technology Ltd Method for affecting mechanical vibration occurring during operation in turbo machine blade, turbo machine blade for executing the method, and piezoelectric damping member to be assembled to the turbo machine blade
JP2013072688A (en) 2011-09-27 2013-04-22 Mitsubishi Heavy Ind Ltd Natural frequency measuring device and natural frequency measuring method
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