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JPH0220831B2 - - Google Patents
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JPH0220831B2 - - Google Patents

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Publication number
JPH0220831B2
JPH0220831B2 JP57047281A JP4728182A JPH0220831B2 JP H0220831 B2 JPH0220831 B2 JP H0220831B2 JP 57047281 A JP57047281 A JP 57047281A JP 4728182 A JP4728182 A JP 4728182A JP H0220831 B2 JPH0220831 B2 JP H0220831B2
Authority
JP
Japan
Prior art keywords
valve
air
circuit
wave
waves
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.)
Expired - Lifetime
Application number
JP57047281A
Other languages
Japanese (ja)
Other versions
JPS58165579A (en
Inventor
Yoshio Masuda
Takeaki Myazaki
Hironori Yokomizo
Yukihisa Washio
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.)
KAIYO KAGAKU GIJUTSU CENTER
Original Assignee
KAIYO KAGAKU GIJUTSU CENTER
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 KAIYO KAGAKU GIJUTSU CENTER filed Critical KAIYO KAGAKU GIJUTSU CENTER
Priority to JP57047281A priority Critical patent/JPS58165579A/en
Publication of JPS58165579A publication Critical patent/JPS58165579A/en
Publication of JPH0220831B2 publication Critical patent/JPH0220831B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B13/00Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
    • F03B13/12Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy
    • F03B13/14Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy using wave energy
    • F03B13/141Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy using wave energy with a static energy collector
    • F03B13/142Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates characterised by using wave or tide energy using wave energy with a static energy collector which creates an oscillating water column
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/30Energy from the sea, e.g. using wave energy or salinity gradient

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Description

【発明の詳細な説明】 本発明は波力発電機空気室の空気出力増加を計
るために空気流を蝶番式弁およびその制御回路に
よつて3状態に制御する装置に関するものであ
る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a device for controlling air flow in three states by means of a hinged valve and its control circuit for increasing the air output of a wave power generator air chamber.

空気タービン方式波力発電機は航路標識ブイ用
の実用実績をもとにし大型浮体式波力発電機(海
明等)による大出力を目標とした研究および海岸
固定式などの諸研究が行なわれている。
Based on the practical experience of using air turbine type wave power generators for navigational beacon buoys, research has been carried out with the aim of achieving high output using large floating wave power generators (Kaimei, etc.), as well as studies on shore-fixed types. ing.

当発明者等は大型浮体式波力発電機(海明)実
海域実験およびこれらの改良研究を通じて空気タ
ービン方式波力発電機の実用化に努力を続けてい
るが、これを実用化するために解決すべき問題と
しての次の様な点がある。
The present inventors have been making efforts to commercialize air turbine type wave power generators through actual sea experiments with large floating wave power generators (Kaimei) and research on their improvement. There are the following issues that need to be resolved.

(A) 実海域実験を行つた日本海の波でも波周期は
4秒〜12秒位まで変化する。このうち4〜6秒
の波は波高も低いが年間を通じ非常に多く存在
している。このような小波で良好な発電を行な
うことは発電出力の平均レベルを高めるのに特
に必要である。エネルギーが高いのは長周期の
波で周期8〜10秒、波長100m〜160m程度であ
り、この様な長周期の波では空気タービンのノ
ズル絞り比一定のものでは利用効率が低下して
くる。
(A) Even in the waves of the Sea of Japan where the actual ocean experiment was conducted, the wave period varies from 4 seconds to 12 seconds. Among these waves, waves with a duration of 4 to 6 seconds have a low wave height, but they occur in large numbers throughout the year. Good power generation with such small waves is especially necessary to increase the average level of power generation output. Long-period waves with a period of 8 to 10 seconds and a wavelength of about 100 m to 160 m have high energy, and with such long-period waves, the utilization efficiency of an air turbine with a constant nozzle aperture ratio decreases.

(B) 大型化の時には、発電を停止し装置および系
統の安全を計る必要がある。この事は電気事業
法の規定からも要望される機能の1つである。
(B) When increasing the size, it is necessary to stop power generation and ensure the safety of the equipment and system. This is one of the functions required by the provisions of the Electricity Business Law.

本発明は以上の2つの技術的改善を目的とする
もので下記の点の組合せを特徴とする。
The present invention aims at the above two technical improvements and is characterized by the combination of the following points.

(1) 海波の持つエネルギーを空気力に変換し空気
タービンを回転させ発電する波力発電機におい
て、変化する海波条件に常に最適な運転を確保
するため、空気の出口または他の適当な通路に
蝶番式弁を設け、弁自体の閉止特性と開位置保
持能力をサーボ機構と組合せることにより、比
較的波長の長い波に対しては波高または水圧等
の信号により得られた一波一波毎に弁を開閉さ
せて空気流の位相と空気圧力の位相を合致せる
様に制御し、波長の長い波における空気出力を
大きく改善する。一方、波長の短い波において
は常時弁を開位置に保持する様に制御し、空気
流は通常に往復させて短周期における最適運転
を確保する。次に大時化または他の特別な場合
には、弁を常時閉になる様に制御して発電装置
や負荷の安全を計る。
(1) In a wave power generator that converts the energy of sea waves into aerodynamic force and rotates an air turbine to generate electricity, an air outlet or other suitable By installing a hinge-type valve in the passage and combining the valve's closing characteristics and ability to maintain the open position with a servo mechanism, it is possible to handle waves with relatively long wavelengths by controlling the speed of each wave obtained from signals such as wave height or water pressure. The valve is opened and closed for each wave to control the phase of the air flow and the phase of the air pressure to match, greatly improving the air output for waves with long wavelengths. On the other hand, for waves with short wavelengths, the valve is controlled to be kept in the open position at all times, and the airflow is normally reciprocated to ensure optimal operation in short periods. Next, in the event of a severe storm or other special circumstances, the valve is controlled to remain closed at all times to ensure the safety of the generator and load.

以上の様な機能を持つた蝶番式弁およびその
3状態空気流制御方法を特徴とした制御装置を
有する空気タービン方式波力発電機。
An air turbine type wave power generator having a hinge type valve having the above-mentioned functions and a control device characterized by its three-state air flow control method.

(2) 空気流の状態を変化させるための開閉される
弁装置として、バタフライ弁を用い、その受圧
面積差により大きな空気圧力差がどの方向より
加わつても弁の閉止を保持できる能力と、一度
開かれた後は空気流の作用により空気流による
圧力差がなくなるまで弁の開位置を保持する能
力とを組合せ、小さなサーボ力と最小の動力消
費で空気流3状態制御を可能にするバタフライ
弁方式空気流開閉装置を附設したこと。
(2) A butterfly valve is used as a valve device that opens and closes to change the state of air flow, and the ability to keep the valve closed even when a large air pressure difference is applied from any direction due to the difference in pressure receiving area, and the ability to keep the valve closed once Combined with the ability of the valve to remain open until the pressure difference due to the air flow disappears after it has been opened, the butterfly valve enables three-state control of air flow with small servo forces and minimal power consumption. Equipped with an airflow opening/closing device.

(3) 空気タービンとして無弁式ウエールズタービ
ンを用いることによりバタフライ弁を閉じた空
気流がない状態でタービンが回転するアイドル
回転時に発生する空気渦等によるエネルギー損
失を最小にするようにしたこと。本発明を実施
することにより、長周期の波からの改善された
効率による発電、大時化または非常時の発電の
停止、および短周期の波における通常の運転の
維持と3つの異つた制御を可能にするものであ
る。
(3) By using a valveless Wales turbine as the air turbine, energy loss due to air vortexes, etc. that occur during idle rotation, when the butterfly valve is closed and the turbine rotates without airflow, is minimized. By implementing the present invention, three different types of control can be achieved: power generation with improved efficiency from long-period waves, stopping power generation in times of storm or emergency, and maintaining normal operation in short-period waves. It is what makes it possible.

前記第1項の空気流の位相制御に関しては、例
えばノルウエーのブダ教授による一点係留ブイの
上下運動をラツチング機構によつて位相制御する
ことにより3〜4倍の出力増加を計ることができ
るとの報告があるが、本発明者等の研究によれば
位相制御を行なうことが常に有効な出力向上の手
段とならない波が多くあることが判明した。
Regarding the phase control of the air flow mentioned in item 1 above, for example, Professor Buda of Norway states that by controlling the phase of the vertical movement of a buoy moored at one point using a latching mechanism, it is possible to increase the output by 3 to 4 times. Although there have been reports, research by the present inventors has revealed that there are many waves for which phase control is not always an effective means of improving output.

日本海由良で観測したところでは周期6秒以下
の波が1年の全体の波の60%を占めており、この
ような波で位相制御を行うことは出力および効率
に大きな減少をもたらすおそれがある。また位相
制御を行うと空気出力は増大するが、一方におい
て空気室内の最大空気圧力が位相制御を行わない
場合に比べて約4倍となり、弁を閉じて空気出口
を無くした場合に比べても約2倍となるので、空
気室の安全性の点から見て大波の場合には空気流
の位相制御は行わない方がよいのであつて、本発
明の3状態空気流制御はかかる事実から出発した
ものである。
According to observations at Japan Sea Yura, waves with a period of 6 seconds or less account for 60% of the total waves in a year, and performing phase control on such waves may result in a significant decrease in output and efficiency. be. Furthermore, when phase control is performed, the air output increases, but on the other hand, the maximum air pressure in the air chamber is approximately four times that of the case without phase control, and even compared to the case where the valve is closed and the air outlet is eliminated. Therefore, from the point of view of the safety of the air chamber, it is better not to perform airflow phase control in the case of large waves, and the three-state airflow control of the present invention is based on this fact. This is what I did.

以下図面について本発明実施の1例を説明する
と、第1図は全体配置図で、空気室1は下面を波
に対して開放した部屋で浮体構造物の中に組込ま
れるかまたは海岸の岩場などに固定して設置され
る。
An example of the implementation of the present invention will be explained below with reference to the drawings. Fig. 1 is an overall layout diagram, in which the air chamber 1 is a room whose lower surface is open to the waves, and may be incorporated into a floating structure or placed in a rocky area on the coast. It is fixedly installed.

この空気室1の底附近に水圧計2が取付けられ
て波の上下を水圧として検知し、この水圧計2よ
りの信号が制御の基本信号となる。空気室1の上
に取り付けられた発電箱3の中には空気タービン
方式発電機4が入る。
A water pressure gauge 2 is attached near the bottom of the air chamber 1 to detect the top and bottom of waves as water pressure, and the signal from this water pressure gauge 2 becomes the basic signal for control. An air turbine type generator 4 is placed in a power generation box 3 mounted above the air chamber 1.

本実施例では2枚のウエールズタービン5,6
を発電機軸7でタンデム型に連結した特許第
1060243号の方式の空気タービン方式波力発電機
を例として示し、空気室1よりの空気流はダクト
8,9を通り空気タービン5,6を回転させて空
気出口10に通じている。
In this embodiment, two Welsh turbines 5 and 6 are used.
The patent No.
1060243 is shown as an example, the air flow from the air chamber 1 passes through ducts 8 and 9, rotates the air turbines 5 and 6, and leads to the air outlet 10.

この空気出口10には弁座11、パツキン12
が設けてあり、これに適合した蝶番式弁13が弁
軸14により保持され、空気出口10の外側へ極
力気密になる様貫通した弁軸14を回転させるタ
ーボモータ15を設け、実線にて示した弁閉の位
置から点線にて示した弁開の位置へ制御される。
弁ストツパー金物16は蝶番式弁13の開位置の
限界を与える。
This air outlet 10 has a valve seat 11 and a gasket 12.
A hinge-type valve 13 adapted to this is held by a valve shaft 14, and a turbo motor 15 is provided to rotate the valve shaft 14 that passes through the air outlet 10 so as to be as airtight as possible, as shown by a solid line. The valve is controlled from the closed position shown by the dotted line to the open position shown by the dotted line.
Valve stop hardware 16 limits the open position of hinged valve 13.

次に蝶番式弁13の作動機能の1つである自動
閉位置保持能力について第2図を用いて説明す
る。蝶番式弁13の片側に復帰用小重量17が取
り付けてあり、普通の状態では蝶番式弁13はパ
ツキン12に密着した畳態になつている。
Next, the automatic closed position holding ability, which is one of the operating functions of the hinged valve 13, will be explained using FIG. 2. A small weight 17 for return is attached to one side of the hinge type valve 13, and in a normal state, the hinge type valve 13 is in a folded state in close contact with the gasket 12.

この様にパツキン12に蝶番式弁13が密着し
た状態において、弁13の上方の空気圧力18を
P1、下方の空気圧力19をP2とし、弁の片方の
面積をS1、これよりパツキン接触面積を引いた面
積をS2,S1にかかる合成空気力の作用点の軸心か
らの距離をL1、同じくS2にかかる合成空気力の
作用点の軸心からの距離をL2とすれば、P1によ
り弁を閉止するモーメントは P1S1L1−P1S2L2 =P1(S1L1−S2L2) P2により弁を閉止するモーメントは P2S1L1−P2S2L2 =P2(S1L1−S2L2) したがつて、P1,P2により弁を閉止するモー
メントは (P1+P2)(S1L1−S2L2) であり、S1L1−S2L2>0であるから、P1,P2
変化にかかわらず常に蝶番式弁13は弁軸14の
まわりに弁を閉止し、かつその閉止を維持する左
回りのモーメントを有することになる。
With the hinged valve 13 in close contact with the gasket 12 in this way, the air pressure 18 above the valve 13 is
P 1 , the lower air pressure 19 is P 2 , the area of one side of the valve is S 1 , the area obtained by subtracting the packing contact area from this is S 2 , the area from the axis of the point of application of the synthetic air force applied to S 1 is If the distance is L 1 and the distance from the axis of the point of action of the synthetic aerodynamic force on S 2 is L 2 , then the moment to close the valve due to P 1 is P 1 S 1 L 1 −P 1 S 2 L 2 = P 1 (S 1 L 1 − S 2 L 2 ) The moment to close the valve due to P 2 is P 2 S 1 L 1 − P 2 S 2 L 2 = P 2 (S 1 L 1 − S 2 L 2 ) Therefore, the moment for closing the valve due to P 1 and P 2 is (P 1 + P 2 ) (S 1 L 1S 2 L 2 ), and S 1 L 1 − S 2 L 2 >0. Therefore, regardless of changes in P 1 and P 2 , the hinged valve 13 always has a counterclockwise moment around the valve stem 14 that closes the valve and maintains its closure.

この弁を開くにはサーボモータ15の外力によ
り閉止保持モーメントより大きい右回りのモーメ
ントを与える必要がある。
In order to open this valve, it is necessary to apply a clockwise moment larger than the moment for holding the valve closed by an external force of the servo motor 15.

この蝶番式弁13がその閉止を維持する能力を
持つているのは空気流の閉動作を確実にする上で
非常に有効である。即ち、もしサーボモータ15
が動作しない時には波により空気圧力P1,P2
どの様に大きくなつても弁は破損するまで開か
ず、設計上は弁の強度さえ充分なら良い事にな
る。これは、弁制御に要求される機能の1つであ
り、大時化又は非常の指令によるタービンおよび
発電機の回転停止を可能にする基本的な弁の特性
として重要である。
The ability of the hinged valve 13 to maintain its closure is very effective in ensuring the closing action of the air flow. That is, if the servo motor 15
When the valve does not operate, no matter how large the air pressures P 1 and P 2 become due to waves, the valve will not open until it is damaged, and from a design point of view, it is a good thing as long as the valve is strong enough. This is one of the functions required for valve control, and is important as a basic valve characteristic that makes it possible to stop the rotation of the turbine and generator in response to an emergency command.

次にサーボモータ15にて開かれた蝶番式弁1
3は第3図に示す様に弁ストツパー金物16によ
り運動を制限される位置まで行くが、この位置で
空気圧力差P1−P2=△Pによつて発生する空気
流20,21がなくなるまで開の位置を保持する
ために、各種の設計上の工夫が必要である。
Next, the hinged valve 1 was opened by the servo motor 15.
3 reaches a position where its movement is restricted by the valve stopper fitting 16 as shown in Fig. 3, but at this position the air flows 20 and 21 generated by the air pressure difference P 1 -P 2 =△P disappear. In order to maintain the open position until the opening, various design measures are required.

第3図に示したものは、蝶番式弁13の両端に
空気抵抗小板22,23を各々図に示す様に逆方
向に付け、空気流が20の時も21の時も常に空
気流が存在するかぎりその空気力により弁は開の
位置を保つ。
The one shown in Figure 3 has air resistance plates 22 and 23 attached to both ends of the hinged valve 13 in opposite directions as shown in the figure, so that the air flow is always maintained both when the air flow is 20 and when the air flow is 21. As long as it is present, the aerodynamic force will keep the valve in the open position.

第4図に示すのは別の工夫であり、蝶番式弁1
3自体の曲面形状により開の位置保持を可能にす
る 第5図に示す蝶番式弁13は平板型であるが、
空気流を弁の片方にあてる様にふた板24,25
を空気流の通路に設けた例である。
Fig. 4 shows another device, hinge type valve 1.
The hinge type valve 13 shown in FIG. 5 is a flat plate type, which allows the valve 3 to maintain its open position due to its curved shape.
Cover plates 24 and 25 so that the air flow hits one side of the valve.
This is an example in which the airflow is provided in the airflow passage.

次に波高について述べれば、波高の変化により
水圧が変化することは既知の事である。
Next, regarding wave height, it is known that water pressure changes as the wave height changes.

第6図は制御のため水圧計2によつて検出した
水圧の変化記録であり、波高変化に比例するデー
タである。実海域の波は不規則波であり、波高と
周期を比較した時、周期の方が不規則性が少な
く、各波間の周期については比較的変動が少ない
事が波高測定の経験より言える。
FIG. 6 is a record of changes in water pressure detected by the water pressure gauge 2 for control purposes, and is data proportional to changes in wave height. Waves in actual sea areas are irregular waves, and when comparing wave height and period, it can be said from experience in wave height measurement that the period is less irregular, and the period between waves has relatively little variation.

第6図より波高H26と周期T27が求められ
る。この波高データより制御信号を発生する制御
回路の1例を第7図制御回路ブロツクダイヤグラ
ムにより説明する。
From FIG. 6, the wave height H26 and the period T27 are determined. An example of a control circuit that generates a control signal from this wave height data will be explained with reference to the control circuit block diagram in FIG.

波高計28のデータは或る基準の波高以上にな
つた場合、蝶番式弁サーボ停止回路30側に指令
を出し、トリガー指令回路34を停止させる。ま
た一方では波の山と谷の時間を正確に示す基本ト
リガー指令回路31により波の山と谷との時刻を
得る。また、周期計29のデータより平均周期計
算回路32が働き、平均周期Tmeanが計算され、
これより蝶番式弁13が波が山または谷に来て空
気圧力の位相がピーク値に達する時に蝶番式弁が
全開の位置にあり、かつ空気室1の中の内部波面
の上昇または下降速度がピーク値に達し、空気圧
力と空気速度の両ピーク値が同位相になる様に、
空気室1の持つ自然振動周期T0のT0/4前に蝶
番式弁13が全開する様に、サーボモータを含ん
だ蝶番式弁13の応答の遅れ時間Tdを考慮にい
れ、トリガー時間計算回路により、 Tmean/2−T0/4−Td=Ta すなわち、トリガー遅れ時間Taが計算され、先
に基本トリガー指令回路31よりのトリガー命令
をTaだけ遅らせるトリガー指令回路34より蝶
番式弁13開閉用サーボモータ15への開信号が
送られる。但し大時化または非常時の指令等によ
り蝶番式弁サーボ停止回路より信号がある時は動
作しない。
When the data on the wave height meter 28 exceeds a certain standard wave height, a command is issued to the hinge type valve servo stop circuit 30 to stop the trigger command circuit 34. On the other hand, the times of the crests and troughs of the waves are obtained by the basic trigger command circuit 31 which accurately indicates the times of the crests and troughs of the waves. In addition, the average period calculation circuit 32 operates based on the data of the period meter 29, and calculates the average period Tmean.
From this, the hinged valve 13 is in the fully open position when the wave reaches a peak or trough and the phase of the air pressure reaches its peak value, and the internal wave front in the air chamber 1 has a rising or falling speed. so that the peak value is reached and both the peak values of air pressure and air velocity are in the same phase.
The trigger time is calculated by taking into account the response delay time Td of the hinged valve 13 including the servo motor so that the hinged valve 13 fully opens before T 0 / 4 of the natural vibration period T 0 of the air chamber 1. The circuit calculates Tmean/2-T 0 /4-Td=Ta, that is, the trigger delay time Ta, and first delays the trigger command from the basic trigger command circuit 31 by Ta.The trigger command circuit 34 then opens and closes the hinged valve 13. An open signal is sent to the servo motor 15. However, it will not operate if there is a signal from the hinge type valve servo stop circuit due to a command in the event of a heavy traffic or emergency.

第7図にて得た各時間の関係を第6図において
説明すると、波の谷35を基本トリガー指令回路
31により求め、次の波の山36のT0/4前に
相当する37の時間とTdに相当する38だけを
平均周期の半分Tmean/2から引いたトリガー
遅れ時間Ta39を計算し、蝶番式弁13開信号
をトリガー点40において出す。一方平均周期計
算回路32よりのTmeanの値が短い時には、蝶
番式弁13の開信号を出す。無論正確には次の山
の点を予察してこれよりトリガー点40を求めて
もよいが、不規則波の次の波のピークを正確に予
察するには高度の計算が必要であるので本実施例
は簡便法につき説明を行つた。この外の実施例と
しては波の山と谷の時間を測るのでなく、波のゼ
ロクロスの時間を測ることもある。この場合理論
値および水槽実験値より得た蝶番式弁13開閉サ
ーボモータ15への開信号はサーボの遅れを無視
した場合、1サイクル360゜として外部波面のゼロ
クロス時より約20〜30゜の遅れでよい。よつて、
別に計算された平均周期計算回路32よりの
Tmeanをもとに Tmean×25゜/360゜=0.07Tmean=Tb を計算して、外部波面がゼロクロスした時刻に加
え、開信号を送り蝶番式弁13を開く。この設計
は他の如何なる制御回路よりも簡単かつ実用的で
ある。
To explain the relationship between the respective times obtained in FIG. 7 in FIG. 6, the trough 35 of the wave is determined by the basic trigger command circuit 31, and the time 37 corresponding to T 0 /4 before the crest 36 of the next wave is determined. Trigger delay time Ta39 is calculated by subtracting 38 corresponding to Td from half of the average period Tmean/2, and the hinged valve 13 opening signal is issued at the trigger point 40. On the other hand, when the value of Tmean from the average cycle calculating circuit 32 is short, an opening signal for the hinged valve 13 is output. Of course, it is possible to accurately predict the point of the next peak and find the trigger point 40 from this, but accurate calculation of the altitude is required to accurately predict the peak of the next wave of irregular waves, so this is not recommended in this book. In the example, a simple method was explained. In another embodiment, instead of measuring the time of the peak and trough of the wave, the time of the zero crossing of the wave may be measured. In this case, the opening signal to the hinged valve 13 opening/closing servo motor 15 obtained from theoretical values and water tank experimental values is approximately 20 to 30 degrees behind the zero cross of the external wavefront, assuming one cycle of 360 degrees, if the servo delay is ignored. That's fine. Then,
from the average period calculation circuit 32 calculated separately.
Based on Tmean, Tmean×25°/360°=0.07Tmean=Tb is calculated, and in addition to the time when the external wave front crosses zero, an open signal is sent to open the hinged valve 13. This design is simpler and more practical than any other control circuit.

第8図はサーボ機構の1例を示すもので、蝶番
式弁13の軸14には腕41が付き、これに連結
部42が付きピストン軸43に連結されている。
空気ピストンシリンダー44は空気ピストン筒4
5に入つている。高圧空気室46からの高圧空気
はトリガー指令回路34からの信号によりマグネ
ツト47を引き空気バルブ48を開き、高圧空気
を空気ピストン筒45にいれて空気ピストンシリ
ンダー44を動かし、ピストン軸43、連結部4
2、腕41を通じて蝶番式弁13を軸14のまわ
りに回転させ、蝶番式弁13を開にする。但し、
トリガー指令回路34より信号のない時、すなわ
ち大時化時や蝶番式弁サーボ停止回路30より停
止信号が出た場合は作動しない。
FIG. 8 shows an example of a servo mechanism, in which an arm 41 is attached to the shaft 14 of the hinge type valve 13, and a connecting portion 42 is attached to this arm 41, which is connected to a piston shaft 43.
The air piston cylinder 44 is the air piston cylinder 4
It's in 5. The high pressure air from the high pressure air chamber 46 pulls the magnet 47 in response to a signal from the trigger command circuit 34, opens the air valve 48, puts the high pressure air into the air piston cylinder 45, moves the air piston cylinder 44, and moves the piston shaft 43 and the connecting part. 4
2. Rotate the hinged valve 13 around the shaft 14 through the arm 41 to open the hinged valve 13. however,
It does not operate when there is no signal from the trigger command circuit 34, that is, when there is a heavy rush or when a stop signal is issued from the hinge type valve servo stop circuit 30.

一方、空気ピストンシリンダー44が動き外部
への空気の逃げ口49を通過した時、空気は外へ
逃げようとする。波の発達初期における周期の短
い波あるいは装置の安全上危険と思われる波高の
高い波以外の波では平均周期計算回路32からの
特別な信号がなくマグネツト50は動作せず空気
は排出されるので、空気圧力差△Pがなくなつた
時に空気ピストンシリンダー44は復帰する。こ
の場合蝶番式弁13にうけた復帰用錘17により
復帰し閉の状態となる。
On the other hand, when the air piston cylinder 44 moves and passes through the air escape port 49 to the outside, the air tries to escape to the outside. In waves other than waves with short periods at the beginning of wave development or waves with high wave heights that are considered dangerous for the safety of the equipment, there is no special signal from the average period calculation circuit 32, so the magnet 50 does not operate and the air is discharged. , the air piston cylinder 44 returns when the air pressure difference ΔP disappears. In this case, the return weight 17 attached to the hinge type valve 13 returns to the closed state.

次に、平均周期Tmeanが極めて短くなつた時
には(例えば5秒以下)、平均周期計算回路32
からの信号によりマグネツト50は引かれ、空気
バルブ51を閉じ、空気は排気されず空気ピスト
ンシリンダー44は開のまま保持され蝶番式弁1
3は常常に開となる。
Next, when the average period Tmean becomes extremely short (for example, 5 seconds or less), the average period calculation circuit 32
The magnet 50 is pulled by the signal from the hinged valve 1, which closes the air valve 51, air is not exhausted, and the air piston cylinder 44 remains open.
3 is always open.

以上のように動作する機能を持つた固定空気室
による1次変換効率、すなわち空気幅と等しい波
エネルギーを入力とした時の波から空気エネルギ
ーへの変換効率を第9図に示す。
FIG. 9 shows the primary conversion efficiency of a fixed air chamber having the function of operating as described above, that is, the conversion efficiency from waves to air energy when wave energy equal to the width of the air is input.

図中実線52で示したものは蝶番式弁13を開
とした時の波エネルギー変換効率、点線53に示
したのは蝶番式弁13を作動させ制御を行なつた
時の波エネルギー変換効率である。
In the figure, the solid line 52 indicates the wave energy conversion efficiency when the hinged valve 13 is open, and the dotted line 53 indicates the wave energy conversion efficiency when the hinged valve 13 is operated and controlled. be.

以上より短周期の波では実線52になる様蝶番
式弁13を開放状態に保ち長周期の波では点線5
3になる様に蝶番式弁13の制御を行う。また大
時化時基準以上の波高になれば蝶番式弁13を閉
の状態に保持し空気タービンおよび発電機の回転
を止めると共に波がかかり損傷するのを防止す
る。
From the above, for short-period waves, the solid line 52 appears, while the hinged valve 13 is kept open, and for long-period waves, the dotted line 5
The hinge type valve 13 is controlled so that the angle becomes 3. Furthermore, if the wave height exceeds the standard for severe storms, the hinged valve 13 is held closed to stop the rotation of the air turbine and generator, and to prevent damage caused by waves.

これにより常に空気タービン方式発電機の最適
運転を確保し、安全かつ経済的な実用化を可能に
するものである。
This ensures optimal operation of the air turbine generator at all times and enables safe and economical practical use.

なお、空気流3状態制御を実施すると、空気は
短時間にラツシユ状態で非常に早い速度で空気タ
ービンを通過する。従つて、この高速の空気流に
適合した空気タービンは当然高速で回転しようと
する。しかし弁を閉じて空気流を止めた別の条件
では高速にて回転する空気タービンの動翼はアイ
ドル回転となり、空気の中に渦流を発生し大きな
動力損失を起こしてタービンの高速回転は大きく
減殺される。このために空気タービンの動翼とし
ては回転方向への翼の断面が最小で、またその空
気中での回転方向への抵抗力が小さいことが必要
となつてくる。
Note that when air flow three-state control is implemented, air passes through the air turbine at a very high speed in a lash state in a short period of time. Therefore, an air turbine adapted to this high-speed air flow naturally tends to rotate at high speed. However, under other conditions where the valve is closed and the airflow is stopped, the rotor blades of the air turbine rotating at high speed become idle, generating vortices in the air and causing a large power loss, which greatly reduces the high speed rotation of the turbine. be done. For this reason, it is necessary for the moving blades of the air turbine to have a minimum cross section in the direction of rotation, and to have a small resistance force in the direction of rotation in the air.

以上の条件に最適なタービンは、ピツチ角のな
い対称翼断面を持つた第10図56に示したウエ
ールズタービンであり、54の衝動型タービン動
翼や55のプロペラ型動翼などに比較するとアイ
ドル回転中の空気抵抗力が極めて小さな値であ
る。従つて空気タービンとしてウエールズタービ
ンを用いることは性能を向上させる上で非常に有
効かつ必要なことである。
The optimal turbine for the above conditions is the Wales turbine shown in Figure 10, which has a symmetrical blade cross section with no pitch angle. The air resistance force during rotation is extremely small. Therefore, using a Wales turbine as an air turbine is very effective and necessary for improving performance.

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

第1図は本発明の実施の1例を示す全体配置
図、第2図〜第5図は本発明実施例第1例〜第4
例の要部断面図、第6図は水圧の変化計録図、第
7図は制御回路図、第8図はサーボ機構の1例を
示す断面図、第9図は本発明による波から空気エ
ネルギーへの変換効率曲線図、第10図は各種タ
ービンの翼断面図を示すものである。 図中の符号はそれぞれ下記部材を示す。1:空
気室、2:水圧計、3:発電箱、4:発電機、
5:ウエールズタービン、6:ウエールズタービ
ン、7:発電機軸、8:ダクト、9:ダクト、1
0:空気出口、11:弁座、12:パツキン、1
3:蝶番式弁、14:弁軸、15:サーボモー
タ、16:弁ストツパー金物、17:復帰用小重
量、24:ふた板、25:ふた板、28:波高
計、29:周期計、30:蝶番式弁サーボ停止回
路、31:基体トリガー指令回路、32:平均周
期計算回路、33:トリガー時間計算回路、3
4:トリガー指令回路、41:腕、42:連結
部、43:ピストン軸、44:空気ピストンシリ
ンダー、45:空気ピストン筒、、46:高圧空
気室、47:マグネツト、48:空気バルブ、4
9:空気の逃げ口、50:マグネツト、51:空
気バルブ、54:衝動型タービン動翼、55:プ
ロペラ型動翼、56:ウエールズタービン動翼。
FIG. 1 is an overall layout diagram showing one example of the implementation of the present invention, and FIGS. 2 to 5 are the first to fourth embodiments of the present invention.
FIG. 6 is a water pressure change record diagram, FIG. 7 is a control circuit diagram, FIG. 8 is a sectional view of an example of a servo mechanism, and FIG. The energy conversion efficiency curve diagram, FIG. 10, shows cross-sectional views of blades of various turbines. The symbols in the drawings indicate the following members, respectively. 1: Air chamber, 2: Water pressure gauge, 3: Power generation box, 4: Generator,
5: Wales turbine, 6: Wales turbine, 7: Generator shaft, 8: Duct, 9: Duct, 1
0: Air outlet, 11: Valve seat, 12: Packing, 1
3: Hinge type valve, 14: Valve stem, 15: Servo motor, 16: Valve stopper hardware, 17: Small weight for return, 24: Lid plate, 25: Lid plate, 28: Wave height meter, 29: Period meter, 30 : Hinge type valve servo stop circuit, 31: Base trigger command circuit, 32: Average period calculation circuit, 33: Trigger time calculation circuit, 3
4: Trigger command circuit, 41: Arm, 42: Connecting section, 43: Piston shaft, 44: Air piston cylinder, 45: Air piston cylinder, 46: High pressure air chamber, 47: Magnet, 48: Air valve, 4
9: Air escape port, 50: Magnet, 51: Air valve, 54: Impulse type turbine rotor blade, 55: Propeller type rotor blade, 56: Wales turbine rotor blade.

Claims (1)

【特許請求の範囲】 1 波力発電機空気室において変化する波力エネ
ルギーより最適化された空気出力を得るために、
空気の出口または他の適当な通路に蝶番式弁を設
けると共に該蝶番式弁を開閉するサーボ機構と水
圧計の指令により該サーボ機構を作動させる制御
回路とを設け、比較的波長の長い波に対しては一
波一波毎に弁を開閉させて空気流の位相と空気圧
力の位相を合致させるように制御し、波長の短い
波に対しては常時弁を開位置に保持するように制
御し、また大時化その他必要時には弁を常時閉に
制御するように3状態の制御を行うことを特徴と
する波力発電機空気室の3状態空気流制御装置。 2 前記蝶番式弁としてバタフライ弁を用い、そ
の受圧面積により大きな空気圧力差がどの方向に
加わつても弁の閉止が保持でき、また一度開いた
後は空気流による圧力差がなくなるまで弁の開位
置を保持するようにしたことを特徴とする特許請
求の範囲第1項に記載の波力発電機空気室の3状
態空気流制御装置。 3 前記制御回路として水圧計に接続される波高
計と周期計とを設け、測定される海波は不規則波
であるが周期は比較的一定である傾向を利用し、
該周期計を順次平均周期計算回路、トリガー時間
計算回路を経て前記トリガー指令回路に、また該
波高計を蝶番式弁サーボ停止回路を経てトリガー
指令回路に接続し、計算された平均周期が短い場
合には蝶番式弁を開放の状態に保持する信号を発
生し、また平均周期が長い場合には蝶番式弁を開
くトリガー信号を、波の山又は谷の検知時刻より
平均周期Tmeanと空気室の自然振動周期Toと蝶
番式弁の遅れ時間Tdより Tmean/2−To/4−Td=Ta により計算されるTaだけ遅れた時刻に、発生す
ることにより蝶番式弁の開動作を行なわせ、また
波高が基準波高以上になると蝶番式弁サーボ停止
回路を通じてトリガー指令回路を停止して蝶番式
弁を閉の状態に保持することを可能ならしめる簡
素化された制御回路をもつたことを特徴とする特
許請求の範囲第1項に記載の波力発電機空気室の
3状態空気流制御装置。 4 前記制御回路により制御されるサーボ機構と
して蝶番式弁を腕とピストン軸を介して開閉する
空気ピストンシリンダーを設け、該空気ピストン
シリンダーにトリガー指令回路の指令によりマグ
ネツトに抗して高圧空気室から空気を供給する空
気バルブを供給側に接続するとともに平均周期計
算回路の指令によりマグネツトに抗して開く空気
バルブを排気側に接続したことを特徴とする特許
請求の範囲第1項または第3項に記載の波力発電
機空気室の3状態空気流制御装置。 5 空気タービンとして無弁式ウエールズタービ
ンを用いることを特徴とする特許請求の範囲第1
項に記載の波力発電機空気室の3状態空気流制御
装置。 6 前記制御回路として平均周期が長い場合に蝶
番式弁を開くトリガー信号を、簡略のため波面の
ゼロクロス時刻より約0.07×Tmean=Tbだけ遅
れた時刻に、発生するようにしたことを特徴とす
る特許請求の範囲第1項に記載の波力発電機空気
室の3状態空気流制御装置。
[Claims] 1. In order to obtain optimized air output from changing wave energy in the wave power generator air chamber,
A hinge type valve is provided at the air outlet or other suitable passage, and a servo mechanism for opening and closing the hinge type valve and a control circuit for operating the servo mechanism based on commands from a water pressure gauge are provided, and a control circuit for operating the servo mechanism based on commands from a water pressure gauge is provided. For waves with short wavelengths, the valve is controlled to open and close for each wave to match the phase of the air flow and the phase of the air pressure, and for waves with short wavelengths, the valve is controlled to be kept in the open position at all times. A three-state air flow control device for an air chamber of a wave power generator, characterized in that it performs three-state control so that the valve is always closed in times of emergency or other necessity. 2 A butterfly valve is used as the hinge type valve, and its pressure receiving area allows the valve to remain closed even when a large air pressure difference is applied in any direction. A three-state air flow control device for a wave power generator air chamber according to claim 1, characterized in that the device maintains its position. 3. A wave height meter and a period meter connected to the water pressure gauge are provided as the control circuit, and the sea waves to be measured are irregular waves, but the period tends to be relatively constant,
If the period meter is sequentially connected to the trigger command circuit via an average cycle calculation circuit and a trigger time calculation circuit, and the wave height meter is connected to the trigger command circuit via a hinged valve servo stop circuit, and the calculated average cycle is short. A signal is generated to keep the hinged valve open, and a trigger signal to open the hinged valve is generated when the average period is long. The occurrence causes the hinged valve to open at a time delayed by Ta calculated by Tmean/2-To/4-Td=Ta from the natural vibration period To and the delay time Td of the hinged valve, and It is characterized by having a simplified control circuit that makes it possible to stop the trigger command circuit through the hinged valve servo stop circuit to maintain the hinged valve in a closed state when the wave height exceeds the reference wave height. A three-state air flow control device for a wave power generator air chamber according to claim 1. 4. An air piston cylinder is provided as a servo mechanism controlled by the control circuit to open and close a hinged valve via an arm and a piston shaft, and the air piston cylinder is moved from a high pressure air chamber against a magnet by a command from a trigger command circuit. Claims 1 or 3, characterized in that an air valve for supplying air is connected to the supply side, and an air valve that opens against the magnet according to a command from the average period calculation circuit is connected to the exhaust side. A three-state airflow control device for a wave power generator air chamber as described in . 5. Claim 1, characterized in that a valveless Welsh turbine is used as the air turbine.
A three-state airflow control device for a wave power generator air chamber as described in paragraphs. 6. The control circuit is characterized in that the trigger signal for opening the hinged valve when the average period is long is generated at a time delayed by approximately 0.07×Tmean=Tb from the zero-crossing time of the wavefront for the sake of simplicity. A three-state air flow control device for a wave power generator air chamber according to claim 1.
JP57047281A 1982-03-26 1982-03-26 Air stream controlling apparatus for air turbine system wave power generator Granted JPS58165579A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57047281A JPS58165579A (en) 1982-03-26 1982-03-26 Air stream controlling apparatus for air turbine system wave power generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57047281A JPS58165579A (en) 1982-03-26 1982-03-26 Air stream controlling apparatus for air turbine system wave power generator

Publications (2)

Publication Number Publication Date
JPS58165579A JPS58165579A (en) 1983-09-30
JPH0220831B2 true JPH0220831B2 (en) 1990-05-10

Family

ID=12770903

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57047281A Granted JPS58165579A (en) 1982-03-26 1982-03-26 Air stream controlling apparatus for air turbine system wave power generator

Country Status (1)

Country Link
JP (1) JPS58165579A (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114382636B (en) * 2022-01-14 2024-04-09 中国科学院电工研究所 Gas-liquid energy storage and power generation system based on air bags and caisson and control method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58588B2 (en) * 1977-10-11 1983-01-07 海洋科学技術センタ− Wave power generator overspeed prevention device

Also Published As

Publication number Publication date
JPS58165579A (en) 1983-09-30

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