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JPH0960599A - Blade angle adjustment mechanism of axial blower - Google Patents
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JPH0960599A - Blade angle adjustment mechanism of axial blower - Google Patents

Blade angle adjustment mechanism of axial blower

Info

Publication number
JPH0960599A
JPH0960599A JP7214306A JP21430695A JPH0960599A JP H0960599 A JPH0960599 A JP H0960599A JP 7214306 A JP7214306 A JP 7214306A JP 21430695 A JP21430695 A JP 21430695A JP H0960599 A JPH0960599 A JP H0960599A
Authority
JP
Japan
Prior art keywords
blade
blade angle
angle adjusting
rotor hub
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP7214306A
Other languages
Japanese (ja)
Other versions
JP3617133B2 (en
Inventor
Masaaki Fujisaki
正晃 藤崎
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fuji Electric Co Ltd
Original Assignee
Fuji Electric Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fuji Electric Co Ltd filed Critical Fuji Electric Co Ltd
Priority to JP21430695A priority Critical patent/JP3617133B2/en
Publication of JPH0960599A publication Critical patent/JPH0960599A/en
Application granted granted Critical
Publication of JP3617133B2 publication Critical patent/JP3617133B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

(57)【要約】 【課題】軸流送風機の動翼に関する翼角の初期設定,お
よび現地据付け後に行う翼角微調整の作業性を改善し、
ロータハブを分解することなく外部からのねじ操作のみ
で翼角微調整が簡単行えるようにする。 【解決手段】駆動モータ軸に連結した中空状のロータハ
ブ6に対し、その周面上に取付けた動翼7を、各動翼ご
とにそのブレード根元側の支軸7bをロータハブに軸支
固定し、かつロータハブの端面をハブカバー6aで閉塞
した軸流送風機において、ロータハブの内部側で動翼の
支軸にキー12を介して翼角調整レバー11を結合し、
さらに該翼角調整レバーに形成した二股状の操作脚部1
1a,11bにねじ先端を突き当てるようにロータハブ
の前面壁に翼角調整ねじ15を螺設し、動翼をロータハ
ブに組立てた状態で前記の翼角調整ねじを外部からねじ
操作することにより、翼角調整レバーを揺動させて動翼
の翼角を微調整する。
(57) [Abstract] [PROBLEMS] Improving the workability of the initial setting of the blade angle of the moving blade of the axial flow fan and the fine adjustment of the blade angle after the on-site installation.
Fine adjustment of blade angle can be easily performed by only external screw operation without disassembling the rotor hub. SOLUTION: For a hollow rotor hub 6 connected to a drive motor shaft, rotor blades 7 mounted on the peripheral surface of the rotor hub, and a support shaft 7b on the blade root side of each rotor blade are pivotally fixed to the rotor hub. In the axial blower in which the end surface of the rotor hub is closed by the hub cover 6a, the blade angle adjusting lever 11 is coupled to the spindle of the rotor blade via the key 12 on the inner side of the rotor hub,
Further, a bifurcated operation leg portion 1 formed on the blade angle adjusting lever
A blade angle adjusting screw 15 is screwed on the front wall of the rotor hub so that the screw tips abut against 1a and 11b, and by operating the blade angle adjusting screw from the outside with the moving blade assembled to the rotor hub, Finely adjust the blade angle of the moving blade by swinging the blade angle adjustment lever.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、自動車道路のトン
ネル換気設備などに適用する軸流送風機の翼角調整機構
に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a blade angle adjusting mechanism for an axial blower applied to tunnel ventilation equipment for automobile roads.

【0002】[0002]

【従来の技術】まず、頭記した軸流送風機の全体構造を
図3に示す。図において、1は送風機の風胴を構成する
ケーシングの外筒、2は外筒1の筒内中央に静翼3,ス
テーベーン4を介して固定した内筒、5は内筒2に組み
込んだ駆動モータ、6は駆動モータ5の軸に連結したロ
ータハブ、7はロータハブ6の周面上に配列して取付け
た動翼、8はロータハブ6の前方に設けたコーン状の風
向カバーである。
2. Description of the Related Art First, FIG. 3 shows the entire structure of the axial blower described above. In the figure, 1 is an outer cylinder of a casing forming a wind tunnel of a blower, 2 is an inner cylinder fixed to the center of the outer cylinder 1 through a vane 3, stay vanes 4, and 5 is a drive incorporated in the inner cylinder 2. A motor, 6 is a rotor hub connected to the shaft of the drive motor 5, 7 is a rotor blade arranged and mounted on the peripheral surface of the rotor hub 6, and 8 is a cone-shaped wind direction cover provided in front of the rotor hub 6.

【0003】次に、前記送風機における動翼の詳細な取
付け構造を図4に示す。ロータハブ6は中空体に作られ
ており、そのセンターのボス部6aが駆動モータ5の軸
5aに嵌め合い連結され、塵埃などの侵入を防ぐために
軸方の開放端面はハブカバー6bで閉塞されている。こ
のロータハブ6対して、動翼7はブレード7aに連なる
根元側の支軸7bをロータハブ6の周面に穿孔した取付
穴へ差し込み、ブレード7aの翼角を所定の角度に初期
設定した上で、この位置から動翼が動かないいないよう
に支軸7bを二重の固定ナット9でロータハブ6へ強固
に締結固定するようにしている。
Next, FIG. 4 shows a detailed structure for mounting the moving blades in the blower. The rotor hub 6 is formed as a hollow body, the boss portion 6a of the center thereof is fitted and connected to the shaft 5a of the drive motor 5, and the open end surface of the axial direction is closed by a hub cover 6b to prevent intrusion of dust and the like. . With respect to the rotor hub 6, the rotor blade 7 is such that the root side support shaft 7b connected to the blade 7a is inserted into a mounting hole formed in the peripheral surface of the rotor hub 6, and the blade angle of the blade 7a is initially set to a predetermined angle. The support shaft 7b is firmly fastened and fixed to the rotor hub 6 with the double fixing nut 9 so that the moving blade does not move from this position.

【0004】この場合に、前記した動翼7は工場での送
風機組立時に標準の翼角設定しておき、送風機の製品を
自動車道路トンネルなどの現地に据付けた後に、現地で
行う送風試験で風圧,風量などを確認しながら改めて最
適な翼角に微調整するようにしている。そして、据付現
地で行う翼角微調整の作業手順としては、送風機を据付
けたままその風向カバー8(図3参照)を外し、さらに
ロータハブ6からハブカバー6aを取り外した上で固定
ナット9を緩めて動翼7の翼角を微調整し、調整後には
再び二重ナット9を締付けて動翼7を強固に固定した上
で、ハブカバー6a,風向カバー8を組立てる。なお、
実際には前記の翼角微調整と送風試験を繰り返し行って
最適な翼角を決定するようにしている。
In this case, the above-mentioned moving blade 7 is set with a standard blade angle at the time of assembling the blower at the factory, and after the blower product is installed at a site such as an automobile road tunnel, a wind pressure test is carried out at the site. The fine wing angle is fine-tuned again while checking the air volume. As a work procedure for fine adjustment of the blade angle performed at the installation site, the wind direction cover 8 (see FIG. 3) is removed with the blower installed, the hub cover 6a is further removed from the rotor hub 6, and the fixing nut 9 is loosened. The blade angle of the moving blade 7 is finely adjusted, and after the adjustment, the double nut 9 is tightened again to firmly fix the moving blade 7, and then the hub cover 6a and the wind direction cover 8 are assembled. In addition,
Actually, the blade angle fine adjustment and the air blowing test are repeated to determine the optimum blade angle.

【0005】[0005]

【発明が解決しようとする課題】上記の作業手順から判
るように、送風機の据付現地で動翼7の翼角を微調整す
る場合に、図4に示した従来の動翼取付け構造では、そ
の都度ロータハブ6のハブカバー6aを外した上で動翼
7を固定しているナット9を緩めたり,締付けたりする
煩雑な分解作業を必要とする。また、動翼7を新たな翼
角に微調整セットした後に固定ナット9を工具で締付け
ていくと、摩擦力により動翼7の支軸7bに回転トルク
が働いて動翼7のブレード7aが調整セットした位置か
らずれるおそれがある。
As can be seen from the above work procedure, when the blade angle of the moving blade 7 is finely adjusted at the installation site of the blower, the conventional moving blade mounting structure shown in FIG. It is necessary to remove the hub cover 6a of the rotor hub 6 each time and then loosen or tighten the nut 9 fixing the rotor blade 7 to perform a troublesome disassembling operation. Further, when the fixing nut 9 is tightened with a tool after the rotor blade 7 is finely adjusted and set to a new blade angle, a rotational torque acts on the support shaft 7b of the rotor blade 7 due to a frictional force, so that the blade 7a of the rotor blade 7 is moved. There is a risk that it will be displaced from the adjusted and set position.

【0006】本発明は上記の点にかんがみなされたもの
であり、その目的は前記課題を解決して動翼に対する翼
角の初期設定,および送風機の現地据付け後に行う翼角
微調整の作業性を改善し、その都度ロータハブを分解す
ることなく外部からのねじ操作のみで動翼の翼角微調整
が簡単行えるようにした軸流送風機の翼角調整機構を提
供することにある。
The present invention has been made in view of the above points, and an object thereof is to solve the above problems and to improve the workability of the initial setting of the blade angle with respect to the moving blade and the fine adjustment of the blade angle after the on-site installation of the blower. An object of the present invention is to provide a blade angle adjusting mechanism for an axial blower, which is improved and allows fine adjustment of the blade angle of a moving blade simply by screw operation from the outside without disassembling the rotor hub each time.

【0007】[0007]

【課題を解決するための手段】上記目的を達成するため
に、本発明によれば、駆動モータの軸端に連結した中空
状のロータハブに対し、その周面上には各動翼ごとにそ
のブレード根元側の支軸をロータハブに軸支固定して複
数枚の動翼を取付け、かつロータハブの軸方開口端面を
ハブカバーで閉塞した軸流送風機において、ロータハブ
の内部側で動翼の支軸に翼角調整レバーを結合するとと
もに、該翼角調整レバーの操作端にねじ先端を突き当て
て前記ロータハブの前面に翼角調整ねじを螺設し、動翼
をロータハブに組立てた状態で前記の翼角調整ねじを外
部からねじ操作することにより、翼角調整レバーを介し
て動翼の翼角調整を行うように構成するものとする。
In order to achieve the above object, according to the present invention, a hollow rotor hub connected to the shaft end of a drive motor is provided on its peripheral surface for each rotor blade. In the axial blower in which the support shaft of the blade root side is pivotally fixed to the rotor hub and multiple rotor blades are attached, and the axial opening end surface of the rotor hub is closed by the hub cover, the rotor hub inner side is used as the rotor shaft support shaft. A blade angle adjusting lever is connected, and a blade tip is pressed against the operating end of the blade angle adjusting lever to screw a blade angle adjusting screw on the front surface of the rotor hub, and the blade is assembled in the rotor hub. The angle adjustment screw is externally operated to adjust the blade angle of the moving blade via the blade angle adjustment lever.

【0008】ここで、前記構成における翼角調整レバー
は、その周上2箇所に振り分けて操作脚部を形成したリ
ング体としてなり、かつ前記操作脚部の端面をロータハ
ブに螺合した一対の操作用ねじに向い合わせて動翼の支
軸に嵌め込み結合するものとする。そして、前記動翼の
支軸と翼角調整レバーのリング体との間の結合手段とし
ては、キーを用いて結合する方式、あるいは動翼の支軸
と翼角調整レバーとの間の溝内に楔状の押圧リングを介
装するとともに、翼角調整レバーの端面に前記押圧リン
グを押し込む固定フランジ,および固定フランジの締結
ボルトを取付け、該締結ボルトの締付け操作により固定
フランジを介して前記押圧リングを溝内へ押し込んで動
翼の支軸と翼角調整レバーとの間を結合する方式が採用
できる。
Here, the blade angle adjusting lever in the above-mentioned configuration is a ring body in which the operating legs are formed by being divided into two portions on the circumference thereof, and a pair of operating members in which the end faces of the operating legs are screwed into the rotor hub. It shall be fitted and connected to the spindle of the moving blade by facing the screw for use. The means for connecting the support shaft of the moving blade and the ring body of the blade angle adjusting lever may be a method of connecting with a key, or a groove between the support shaft of the moving blade and the blade angle adjusting lever. A wedge-shaped pressing ring is installed on the blade, and a fixing flange for pressing the pressing ring onto the end surface of the blade angle adjusting lever and a fastening bolt for the fixing flange are attached, and the pressing ring is tightened through the fixing flange by the tightening operation of the fastening bolt. It is possible to adopt a method in which the shaft of the moving blade and the blade angle adjusting lever are connected by pushing the blade into the groove.

【0009】さらに、動翼の翼角調整後には、前記の翼
角調整ねじを弛み防止用のロックねじで固定するのがよ
い。上記の構成によれば、送風機の組立状態で動翼の翼
角微調整を行う場合には、その都度ロータハブのハブカ
バーを取り外すことなく、外部から翼角調整ねじをねじ
操作するだけの簡単な作業で翼角の微調整が行える。つ
まり、ロータハブに立てた一対の翼角調整ねじのうち、
一方の調整ねじを緩めつつ他方の調整ねじを締め込む
と、調整ねじの拘束を受けて翼角調整レバーが回動し、
これに連れて動翼のブレードはその支軸の回りに回転し
て翼角が変化する。なお、翼角の調整後はロックねじを
用いて調整ボルトを固定しておくことにより、動翼を調
整位置に安定よく固定保持できる。
Further, after adjusting the blade angle of the moving blade, it is preferable to fix the blade angle adjusting screw with a lock screw for preventing loosening. According to the above configuration, when fine-adjusting the blade angle of the moving blade in the assembled state of the blower, the simple operation of screwing the blade angle adjusting screw from the outside without removing the hub cover of the rotor hub each time is required. Fine adjustment of the blade angle can be done with. In other words, of the pair of blade angle adjustment screws set up on the rotor hub,
When loosening one adjustment screw and tightening the other adjustment screw, the blade angle adjustment lever rotates due to the constraint of the adjustment screw,
Along with this, the blade of the moving blade rotates around its supporting shaft and the blade angle changes. In addition, after adjusting the blade angle, the moving bolt can be stably fixed and held at the adjusting position by fixing the adjusting bolt with the lock screw.

【0010】また、動翼の支軸と翼角調整レバーとの結
合に関しては、一般的な結合手段であるキーが採用でき
るほか、特に楔状の押圧リングを使用した結合構造で
は、動翼の支軸に対して調整レバーの相対的な取付け角
度を任意に設定できる。なお、キー結合方式では、動翼
の支軸に対する調整レバーの相対的な取付け位置はキー
により拘束されて一義的に決まる。
Further, with respect to the connection between the support shaft of the moving blade and the blade angle adjusting lever, a key which is a general connecting means can be adopted, and particularly in the connecting structure using a wedge-shaped pressing ring, the support of the moving blade is supported. The mounting angle of the adjustment lever relative to the shaft can be set arbitrarily. In the key coupling method, the relative mounting position of the adjusting lever with respect to the spindle of the moving blade is uniquely determined by being constrained by the key.

【0011】[0011]

【発明の実施の形態】以下、本発明の具体的な実施例を
図面に基づいて説明する。なお、各実施例の図中で図4
に対応する同一部材には同じ符号が付してある。〔実施
例1〕図1(a),(b)において、動翼7はブレード7
aの根元側に連なる支持7bがロータハブ6の周面に嵌
合軸支され、ストッパナット10により回転可能に抜け
止め支持されている。また、ロータハブ6を貫通してそ
の内方に突出した支軸7bの軸端にはリング状の翼角調
整レバー11がキー12を介して結合されており、さら
に固定フランジ13,および締結ボルト14を介して結
合位置に締結固定されている。
Embodiments of the present invention will be described below with reference to the drawings. Note that FIG.
The same reference numerals are attached to the same members corresponding to. [Embodiment 1] In FIGS. 1A and 1B, the moving blade 7 is a blade 7.
A support 7b connected to the root side of "a" is supported by a fitting shaft on the peripheral surface of the rotor hub 6, and is rotatably supported by a stopper nut 10 so as not to come off. A ring-shaped blade angle adjusting lever 11 is connected via a key 12 to the shaft end of a support shaft 7b that penetrates the rotor hub 6 and projects inwardly thereof, and further, a fixing flange 13 and a fastening bolt 14 are provided. It is fastened and fixed to the coupling position via.

【0012】ここで、翼角調整レバー11は図1(b)
で示すように周上2箇所に振り分けて二股状に形成した
操作脚部11a,11bを有しており、ロータハブ6に
対して動翼7のブレード7aを標準の翼角にセットした
状態で、調整レバー11に形成した二股状の操作脚部の
端面がロータハブ6の前面と平行に向き合うようにキー
12を介して支軸7bに結合されている。また、翼角調
整レバー11の操作脚部11a,11bに対向してその
端面へねじ先端を突き当てるようにロータハブ6の前面
壁には一対の翼角調整ねじ15が螺設されている。
The blade angle adjusting lever 11 is shown in FIG. 1 (b).
As shown in FIG. 3, the operating leg portions 11a and 11b are formed in two forks on the circumference, and the blade 7a of the rotor blade 7 is set to the standard blade angle with respect to the rotor hub 6, An end surface of a bifurcated operation leg portion formed on the adjusting lever 11 is connected to the support shaft 7b via a key 12 so that the end surface of the operation leg portion faces the front surface of the rotor hub 6 in parallel. Further, a pair of blade angle adjusting screws 15 are screwed on the front wall of the rotor hub 6 so as to face the operation leg portions 11a and 11b of the blade angle adjusting lever 11 and abut the screw tips on the end faces thereof.

【0013】かかる構成で、動翼7の翼角を標準角度か
ら微調整する場合には、ロータハブ6の前面に螺合した
一対の翼角調整ねじ15について、外側からのねじ操作
により一方の調整ねじを緩めつつ、他方の調整ねじを締
め込む。これにより、翼角調整レバー11は2本の調整
ねじ15の拘束を受けて図1(b)の実線位置から鎖線
位置に回動し、これに連れて調整レバー11に結合した
動翼7がその支軸7bの回りに回動してその翼角が微調
整される。すなわち、調整レバー11における操作脚部
11a,11bのうち、操作脚部11aに対向する調整
ねじ15を緩め、操作脚部11bに対向する調整ねじ1
5を締め込むと、動翼7は反時計方向に回動し、前記と
は逆方向にねじ操作を行えば動翼7は時計方向に回動し
て翼角が微調整されることになる。しかも、動翼7の支
軸7bと翼角調整レバー11との間はキー12で結合さ
れているので、翼角が調整位置からずれ動くおそれはな
く、また、翼角調整後には調整ねじ15を弛み防止用の
ロックねじ16で押え込むことで調整ねじ15のガタ付
きを抑えて動翼7を安定よく固定保持できる。なお、必
要に応じてねじ穴に接着剤を注入してロックねじ16を
封止してもよい。
With this configuration, when finely adjusting the blade angle of the moving blade 7 from the standard angle, one of the pair of blade angle adjusting screws 15 screwed to the front surface of the rotor hub 6 is adjusted by operating the screw from the outside. While loosening the screw, tighten the other adjusting screw. As a result, the blade angle adjusting lever 11 is constrained by the two adjusting screws 15 to rotate from the solid line position in FIG. 1 (b) to the chain line position, and the moving blade 7 coupled to the adjusting lever 11 accordingly. The blade angle is finely adjusted by rotating around the support shaft 7b. That is, of the operating legs 11a and 11b of the adjusting lever 11, the adjusting screw 15 facing the operating leg 11a is loosened, and the adjusting screw 1 facing the operating leg 11b is loosened.
When 5 is tightened, the moving blade 7 rotates counterclockwise, and when the screw operation is performed in the opposite direction to the above, the moving blade 7 rotates clockwise and the blade angle is finely adjusted. . Moreover, since the support shaft 7b of the moving blade 7 and the blade angle adjusting lever 11 are connected by the key 12, there is no risk of the blade angle shifting from the adjustment position, and the adjusting screw 15 is used after adjusting the blade angle. By pressing the lock screw 16 for preventing loosening, the backlash of the adjusting screw 15 can be suppressed and the moving blade 7 can be stably fixed and held. Note that the lock screw 16 may be sealed by injecting an adhesive into the screw hole, if necessary.

【0014】〔実施例2〕図2(a)〜(c)は実施例
1の応用実施例を示すものであり、この実施例において
は、動翼7の支軸7bと翼角調整レバー11との間の結
合手段として、支軸7bとその外周に嵌合した調整レバ
ー11との間の周溝内には、図2(c)で示すように、
断面形状が直角三角形になる2枚の楔状押圧リング17
を図示のように互い違いの向きに重ね合わせて介装し、
この押圧リング17を軸方向から溝内に押し込むように
調整レバー7の端面に固定フランジ(フランジの内周側
には周溝内のぞ押圧リング17に向けて突出した突起部
13aを備えている)13,締結ボルト14が取付けて
あり、その他の構造は実施例1と同様に構成されてお
り、動翼7の翼角微調整方法も同様に行われる。
[Second Embodiment] FIGS. 2A to 2C show an application example of the first embodiment. In this embodiment, the support shaft 7b of the moving blade 7 and the blade angle adjusting lever 11 are shown. As a coupling means between the support shaft 7b and the adjustment lever 11 fitted to the outer periphery of the support shaft 7b, as shown in FIG.
Two wedge-shaped pressing rings 17 whose cross-sectional shape is a right triangle
And insert them in alternate directions as shown in the figure,
A fixing flange is provided on the end surface of the adjusting lever 7 so as to push the pressing ring 17 into the groove from the axial direction (a protrusion 13a protruding toward the pressing ring 17 in the circumferential groove is provided on the inner peripheral side of the flange). ) 13 and fastening bolts 14 are attached, and other structures are the same as those in the first embodiment, and the blade angle fine adjustment method of the moving blade 7 is also performed in the same manner.

【0015】かかる構成で、ロータハブ6に対して動翼
7を標準翼角に初期設定した上で、支軸7bに嵌合した
翼角調整レバー11をその操作脚部11a,11bが平
行してロータハブ6の前面壁と向かい合うように位置決
めし、この状態で締結ボルト14を締付けると、固定フ
ランジ13の突起13aを介して周溝内に押し込まれた
楔状の押圧リング17がその重なり合いを深めて支軸7
b,および調整レバー11を半径方向に押し、その摩擦
力で支軸7bと調整レバー11との間が結合される。し
たがって、この実施例によれば先記実施例1のキー結合
方式のように支軸7bと調整レバー11との相対的な結
合位置(周方向の結合位置)がキー12によって一義的
に規制されることなく任意に変更することができる。
With such a construction, the rotor blade 6 is initially set to the standard blade angle, and the blade angle adjusting lever 11 fitted to the support shaft 7b is arranged such that the operating legs 11a and 11b thereof are parallel to each other. When positioning is performed so as to face the front wall of the rotor hub 6, and the fastening bolt 14 is tightened in this state, the wedge-shaped pressing ring 17 pushed into the circumferential groove via the protrusion 13a of the fixed flange 13 deepens the overlapping and supports it. Axis 7
b and the adjusting lever 11 are pushed in the radial direction, and the frictional force connects the support shaft 7b and the adjusting lever 11 to each other. Therefore, according to this embodiment, the key 12 uniquely regulates the relative connecting position (circumferential connecting position) between the support shaft 7b and the adjusting lever 11 as in the key connecting system of the first embodiment. It can be changed arbitrarily without the need.

【0016】[0016]

【発明の効果】以上述べたように、本発明の構成によれ
ば次記の効果を奏する。 1)動翼に対する翼角調整ねじがロータハブの前面に螺
合されており、動翼をロータハブに取付けた送風機の組
立状態で翼角を微調整する場合には、ロータハブを分解
(ハブカバーを取り外す)ことなく、外部から調整ねじ
を操作するだけで簡単に動翼の翼角を微調整することが
できる。したがって、送風機を納入先の現地に据付けた
状態で行う翼角微調整の作業性を大幅に改善できる。
As described above, according to the structure of the present invention, the following effects can be obtained. 1) The blade angle adjusting screw for the rotor blade is screwed on the front surface of the rotor hub, and when finely adjusting the blade angle in the assembled state of the fan with the rotor blade attached to the rotor hub, disassemble the rotor hub (remove the hub cover). It is possible to easily fine-tune the blade angle of the moving blade by simply operating the adjusting screw from outside. Therefore, it is possible to greatly improve the workability of fine adjustment of the blade angle when the blower is installed at the delivery site.

【0017】2)しかも、従来のようにロータハブに対
して動翼の支軸をナットを用いて直接締付け固定する構
造とは異なり、あらかじめ動翼の支軸に結合しておいた
翼角調整レバーを2本の調整ねじで調整位置に拘束する
ようにしたので、動翼が翼角調整位置から不当にずれ動
くおそれはない。 3)また、翼角調整後に調整ねじをロックねじで固定す
ることにより、調整ねじの不要な弛みを阻止して動翼を
調整位置に安定よく固定保持でき、これにより信頼性が
向上する。
2) Further, unlike the conventional structure in which the rotor shaft is fixed to the rotor hub by directly tightening and fixing it with a nut, the blade angle adjusting lever is previously coupled to the rotor shaft. Since the adjustment blade is constrained to the adjusting position by the two adjusting screws, there is no possibility that the moving blade is unduly displaced from the blade angle adjusting position. 3) Further, by fixing the adjusting screw with the lock screw after adjusting the blade angle, unnecessary loosening of the adjusting screw can be prevented and the moving blade can be stably fixed and held at the adjusting position, thereby improving reliability.

【0018】4)動翼の支軸と翼角調整レバーとの間の
結合手段として、楔状の押圧リングを採用することによ
り、動翼に対する調整レバーの相対的な結合位置を任意
に設定,変更すること可能であり、これにより翼角の初
期設定に際しての動翼の取付け角度を送風機の様々な運
転条件に合わせて変更することができる。
4) By adopting a wedge-shaped pressing ring as a connecting means between the support shaft of the moving blade and the blade angle adjusting lever, the relative connecting position of the adjusting lever with respect to the moving blade is arbitrarily set and changed. It is possible to change the mounting angle of the moving blade at the time of initial setting of the blade angle according to various operating conditions of the blower.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の実施例1に対応する翼角調整機構の構
成を表す図であり、(a)は断面側視図、(b)は
(a)図の矢視R方向から見た端面図
1A and 1B are diagrams showing a configuration of a blade angle adjusting mechanism corresponding to a first embodiment of the present invention, in which FIG. 1A is a sectional side view, and FIG. 1B is a view seen from an arrow R direction in FIG. End view

【図2】本発明の実施例2に対応する翼角調整機構の構
成を表す図であり、(a)は断面側視図、(b)は
(a)図の矢視R方向から見た端面図
2A and 2B are diagrams showing a configuration of a blade angle adjusting mechanism corresponding to a second embodiment of the present invention, in which FIG. 2A is a sectional side view and FIG. 2B is a view from a direction R in FIG. End view

【図3】軸流送風機の全体構成の側面図FIG. 3 is a side view of the overall configuration of an axial blower.

【図4】従来における動翼の取付け構造を表す断面図FIG. 4 is a sectional view showing a conventional blade mounting structure.

【符号の説明】[Explanation of symbols]

6 ロータハブ 6a ハブカバー 7 動翼 7a ブレード 7b 支軸 11 翼角調整レバー 11a,11b 操作脚部 12 キー 13 固定フランジ 14 締結ボルト 15 翼角調整ねじ 16 ロックねじ 6 rotor hub 6a hub cover 7 moving blade 7a blade 7b spindle 11 blade angle adjusting levers 11a, 11b operation leg 12 key 13 fixing flange 14 fastening bolt 15 blade angle adjusting screw 16 lock screw

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】駆動モータの軸端に連結した中空状のロー
タハブに対し、その周面上には各動翼ごとにそのブレー
ド根元側の支軸をロータハブに軸支固定して複数枚の動
翼を取付け、かつロータハブの軸方開口端面をハブカバ
ーで閉塞した軸流送風機において、ロータハブの内部側
で動翼の支軸に翼角調整レバーを結合するとともに、該
翼角調整レバーの操作端にねじ先端を突き当てて前記ロ
ータハブの前面に翼角調整ねじを螺設し、動翼をロータ
ハブに組立てた状態で前記の翼角調整ねじを外部からね
じ操作することにより、翼角調整レバーを介して動翼の
翼角調整を行うようにしたことを特徴とする軸流送風機
の翼角調整機構。
1. A hollow rotor hub connected to a shaft end of a drive motor, and on its peripheral surface, a support shaft on the blade root side of each rotor blade is fixed to the rotor hub so as to support a plurality of rotor blades. In an axial blower in which blades are attached and the axially open end surface of the rotor hub is closed by a hub cover, the blade angle adjusting lever is connected to the support shaft of the rotor blade on the inner side of the rotor hub, and at the operating end of the blade angle adjusting lever. A blade angle adjusting screw is screwed on the front surface of the rotor hub by abutting the screw tip, and the blade angle adjusting screw is externally operated while the moving blade is assembled to the rotor hub. A blade angle adjusting mechanism for an axial blower, which is characterized in that the blade angle of a moving blade is adjusted.
【請求項2】請求項1記載の翼角調整機構において、翼
角調整レバーが周上2箇所に振り分けて操作脚部を形成
したリング体としてなり、かつ前記操作脚部の端面をロ
ータハブに螺合した一対の操作用ねじに向い合わせて動
翼の支軸に嵌め込み結合したことを特徴とする軸流送風
機の翼角調整機構。
2. The blade angle adjusting mechanism according to claim 1, wherein the blade angle adjusting lever is a ring body which is divided into two portions on the circumference to form an operating leg portion, and the end face of the operating leg portion is screwed into a rotor hub. A blade angle adjusting mechanism for an axial-flow fan, comprising a pair of operation screws facing each other, fitted and connected to a spindle of a moving blade.
【請求項3】請求項2記載の翼角調整機構において、動
翼の支軸と翼角調整レバーのリング体との間をキーを用
いて結合したことを特徴とする軸流送風機の翼角調整機
構。
3. The blade angle adjusting mechanism according to claim 2, wherein the spindle of the moving blade and the ring body of the blade angle adjusting lever are connected by using a key. Adjustment mechanism.
【請求項4】請求項2記載の翼角調整機構において、動
翼の支軸と翼角調整レバーとの間の溝内に楔状の押圧リ
ングを介装するとともに、翼角調整レバーの端面に前記
押圧リングを押し込む固定フランジ,および固定フラン
ジの締結ボルトを取付け、該締結ボルトの締付け操作に
より固定フランジを介して前記押圧リングを溝内へ押し
込んで動翼の支軸と翼角調整レバーとの間を結合したこ
とを特徴とする軸流送風機の翼角調整機構。
4. A blade angle adjusting mechanism according to claim 2, wherein a wedge-shaped pressing ring is provided in the groove between the spindle of the moving blade and the blade angle adjusting lever, and the end face of the blade angle adjusting lever is provided. A fixing flange for pushing in the pressing ring and a fastening bolt for the fixing flange are attached, and the pressing ring is pushed into the groove through the fixing flange by a fastening operation of the fastening bolt so that the spindle of the moving blade and the blade angle adjusting lever A blade angle adjusting mechanism for an axial-flow blower, which is characterized by connecting the two.
【請求項5】請求項1記載の翼角調整機構において、翼
角調整後に翼角調整ねじを弛み防止用のロックねじを用
いて固定したことを特徴とする軸流送風機の翼角調整機
構。
5. The blade angle adjusting mechanism according to claim 1, wherein after adjusting the blade angle, the blade angle adjusting screw is fixed with a lock screw for preventing loosening.
JP21430695A 1995-08-23 1995-08-23 Axle-flow fan blade angle adjustment mechanism Expired - Fee Related JP3617133B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21430695A JP3617133B2 (en) 1995-08-23 1995-08-23 Axle-flow fan blade angle adjustment mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21430695A JP3617133B2 (en) 1995-08-23 1995-08-23 Axle-flow fan blade angle adjustment mechanism

Publications (2)

Publication Number Publication Date
JPH0960599A true JPH0960599A (en) 1997-03-04
JP3617133B2 JP3617133B2 (en) 2005-02-02

Family

ID=16653561

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21430695A Expired - Fee Related JP3617133B2 (en) 1995-08-23 1995-08-23 Axle-flow fan blade angle adjustment mechanism

Country Status (1)

Country Link
JP (1) JP3617133B2 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006002649A (en) * 2004-06-17 2006-01-05 Anest Iwata Corp Vibration prevention device for scroll fluid machine
JP2011002399A (en) * 2009-06-22 2011-01-06 Honda Kogyo Kk Environmental test device of solar panel
KR101007472B1 (en) * 2010-10-05 2011-01-12 주식회사 우승산업 Pump with adjustable impeller
CN108895030A (en) * 2018-08-06 2018-11-27 无锡市海星船舶动力有限公司 The compressor impeller of blade detachable type
CN116576152A (en) * 2023-07-12 2023-08-11 中国空气动力研究与发展中心低速空气动力研究所 Wind tunnel fan blade fixing device and wind tunnel fan with adjustable blade mounting angle
CN116816719A (en) * 2023-05-17 2023-09-29 华能聊城热电有限公司 Single-pole centrifugal pump capable of preventing impeller from loosening
KR102641661B1 (en) * 2022-12-09 2024-02-28 (주)삼원이앤비 Variable pitch axial flow blower
CN121139490A (en) * 2025-11-19 2025-12-16 中国空气动力研究与发展中心高速空气动力研究所 A composite material blade with anti-torsion structure and its installation method

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006002649A (en) * 2004-06-17 2006-01-05 Anest Iwata Corp Vibration prevention device for scroll fluid machine
JP2011002399A (en) * 2009-06-22 2011-01-06 Honda Kogyo Kk Environmental test device of solar panel
KR101007472B1 (en) * 2010-10-05 2011-01-12 주식회사 우승산업 Pump with adjustable impeller
CN108895030A (en) * 2018-08-06 2018-11-27 无锡市海星船舶动力有限公司 The compressor impeller of blade detachable type
KR102641661B1 (en) * 2022-12-09 2024-02-28 (주)삼원이앤비 Variable pitch axial flow blower
WO2024123128A1 (en) * 2022-12-09 2024-06-13 (주)삼원이앤비 Variable-pitch axial flow fan
CN116816719A (en) * 2023-05-17 2023-09-29 华能聊城热电有限公司 Single-pole centrifugal pump capable of preventing impeller from loosening
CN116576152A (en) * 2023-07-12 2023-08-11 中国空气动力研究与发展中心低速空气动力研究所 Wind tunnel fan blade fixing device and wind tunnel fan with adjustable blade mounting angle
CN116576152B (en) * 2023-07-12 2023-09-22 中国空气动力研究与发展中心低速空气动力研究所 Wind tunnel fan blade fixing device and wind tunnel fan with adjustable blade mounting angle
CN121139490A (en) * 2025-11-19 2025-12-16 中国空气动力研究与发展中心高速空气动力研究所 A composite material blade with anti-torsion structure and its installation method

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