JPH10505040A - 回転装置 - Google Patents
回転装置Info
- Publication number
- JPH10505040A JPH10505040A JP8509292A JP50929296A JPH10505040A JP H10505040 A JPH10505040 A JP H10505040A JP 8509292 A JP8509292 A JP 8509292A JP 50929296 A JP50929296 A JP 50929296A JP H10505040 A JPH10505040 A JP H10505040A
- Authority
- JP
- Japan
- Prior art keywords
- rotating device
- rotor
- power
- control signal
- supplied
- 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
Links
- 238000004891 communication Methods 0.000 claims abstract description 22
- 238000004804 winding Methods 0.000 claims description 26
- 238000010438 heat treatment Methods 0.000 claims description 11
- 239000000463 material Substances 0.000 claims description 8
- 238000012544 monitoring process Methods 0.000 claims description 5
- 230000003287 optical effect Effects 0.000 claims description 4
- 230000006698 induction Effects 0.000 claims description 3
- 238000010248 power generation Methods 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims 1
- 239000004020 conductor Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000001939 inductive effect Effects 0.000 description 2
- 230000005284 excitation Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/04—Arrangements for transmitting signals characterised by the use of a wireless electrical link using magnetically coupled devices
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Control Of Resistance Heating (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Control Of Electric Motors In General (AREA)
- Reciprocating, Oscillating Or Vibrating Motors (AREA)
- Rotary Switch, Piano Key Switch, And Lever Switch (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Apparatus For Radiation Diagnosis (AREA)
- Control Of Eletrric Generators (AREA)
Abstract
Description
Claims (1)
- 【特許請求の範囲】 1.ロータ(1)上に少なくとも1個の電力被供給装置(3)を有するとともに、制御 信号に応じて少なくとも1個の電力被供給装置(3)に電力を供給する切替手段(4) をロータ(1)上に備えた回転装置において、前記制御信号は、ロータ(1)とこのロ ータが回転可能に設けられた材構との間の非接触通信リンクを介して、切替手段 (4)に供給されることを特徴とする回転装置。 2.前記ロータは、このロータ(1)の回転動作によってその中に電力が発生する 誘導巻線(7,8,9)を含む発電材を備え、前記通信リンクは、前記発電材に組み込 まれている誘導リンクを含むことを特徴とする請求項1に記載の回転装置。 3.前記発電材は、永久磁石発電材であり、前記巻線(7,8,9)は、前記ロータ(1) が固定磁石(6)に対して回転したときに誘導電圧を発生させるために、ロータ(1) 上に設けられていることを特徴とする請求項2に記載の回転装置。 4.前記巻線(7,8,9)は、通信リンクの一部から成ることを特徴とする請求項3 に記載の回転装置。 5.制御巻線(13)が、磁石(6)上に設けられ、この制御巻線(13)は、データを前 記通信リンクを介して送信するために、制御信号によって変調されることを特徴 とする請求項4に記載の回転装置。 6.少なくとも1個の電力被供給装置(3)への電力供給を制御する制御装置(12) を備え、前記制御装置(12)は、前記制御巻線(13)内の前記制御信号を変調するこ とによって制御信号を送信するための制御巻線(13)への接続を有することを特徴 とする請求項5に記載の回転装置。 7.前記制御信号は、符号化されたバイナリ信号から成り、前記切替手段(4)は 、 前記制御信号を復号するための復号手段を含むことを特徴とする請求項5に記載 の回転装置。 8.前記ロータ(1)から前記制御装置(12)に実行情報を送信するために非接触通 信リンクが使用され、前記制御装置(12)は、適切な制御信号を前記切替手段(4) に送信することによって、実行情報に応答するようにアレンジされていることを 特徴とする請求項1に記載の回転装置。 9.前記制御信号及び前記実行情報は、同じ通信リンクを介して送信されること を特徴とする請求項8に記載の回転装置。 10.前記制御信号及び前記実行情報は、それぞれの通信リンクを介して送信さ れることを特徴とする請求項8に記載の回転装置。 11.各非接触通信リンクは、無線周波数リンク、又は、光リンクから成ること を特徴とする請求項1に記載の回転装置。 12.前記回転装置は、複数のプロペラ翼(2)を支えるプロペラハブ(1)であり、 前記少なくとも1個の電力被供給装置(3)は、各プロペラ翼(2)上に設けられた加 熱要素から成ることを特徴とする請求項10に記載の回転装置。 13.前記回転装置は、複数のプロペラ翼(2)を支えるプロペラハブ(1)であり、 前記少なくとも1個の電力被供給装置は、各プロペラ翼(2)上に設けられた加熱 要素から成り、個々の加熱要素に供給される電圧及び電流の少なくとも一方が、 制御装置12に送信される被監視及び調整情報であることを特徴とする請求項8 に記載の回転装置。 14.前記切替手段は、電気制御可能なスイッチであることを特徴とする請求項 1に記載の回転装置。 15.複数の前記電力被供給装置を備え、各電力被供給装置には、周期的に電力 が供給されることを特徴とする請求項1に記載の回転装置。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9417639A GB2293522B (en) | 1994-09-02 | 1994-09-02 | Rotary apparatus |
GB9417639.3 | 1994-09-02 | ||
PCT/GB1995/002082 WO1996007588A1 (en) | 1994-09-02 | 1995-09-04 | Rotary apparatus |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH10505040A true JPH10505040A (ja) | 1998-05-19 |
JP3616103B2 JP3616103B2 (ja) | 2005-02-02 |
Family
ID=10760711
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP50929296A Expired - Fee Related JP3616103B2 (ja) | 1994-09-02 | 1995-09-04 | 回転装置 |
Country Status (8)
Country | Link |
---|---|
US (1) | US6181235B1 (ja) |
EP (1) | EP0777602B1 (ja) |
JP (1) | JP3616103B2 (ja) |
CA (1) | CA2198753C (ja) |
DE (1) | DE69516150T2 (ja) |
ES (1) | ES2146317T3 (ja) |
GB (1) | GB2293522B (ja) |
WO (1) | WO1996007588A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009508746A (ja) * | 2005-09-23 | 2009-03-05 | エアバス フランス | 航空機の表面の霜取りおよび/または曇り取りを行なうシステムと、このようなシステムを制御する方法と、このようなシステムを備える航空機 |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2093426C1 (ru) * | 1996-03-21 | 1997-10-20 | Йелстаун Корпорейшн Н.В. | Тепловая противообледенительная система вращаемого элемента |
AU2000255480A1 (en) * | 2000-06-19 | 2002-03-21 | Ultra Electronics Limited | Adaptive balancing arrangement for a rotating mass |
US7254182B2 (en) * | 2002-07-09 | 2007-08-07 | Tsui Philip Y W | Transmitter for operating multiple devices |
GB0216870D0 (en) | 2002-07-19 | 2002-08-28 | Ultra Electronics Ltd | Rotor balance arrangement for a rotating mass |
DE10301978A1 (de) | 2003-01-20 | 2004-08-05 | Eurocopter Deutschland Gmbh | Vorrichtung und Verfahren zum Übertragen und Bereitstellen der Energie kapazitiver Aktuatoren |
FR2863586B1 (fr) * | 2003-12-12 | 2007-01-19 | Eurocopter France | Dispositif de degivrage/antigivrage modulaire d'une surface aerodynamique. |
GB2440289B (en) * | 2004-01-30 | 2008-09-17 | Ultra Electronics Ltd | Modular aircraft control system and method |
US7081696B2 (en) | 2004-08-12 | 2006-07-25 | Exro Technologies Inc. | Polyphasic multi-coil generator |
US20060033392A1 (en) * | 2004-08-12 | 2006-02-16 | Ritchey Jonathan G | Polyphasic multi-coil generator |
BRPI0518456A2 (pt) * | 2005-02-24 | 2008-11-18 | Bell Helicopter Textro Inc | sistema de gerenciamento de gelo para aeronave tiltrotor |
US8550402B2 (en) | 2005-04-06 | 2013-10-08 | Sikorsky Aircraft Corporation | Dual-channel deicing system for a rotary wing aircraft |
CA2654462A1 (en) | 2006-06-08 | 2007-12-13 | Exro Technologies Inc. | Poly-phasic multi-coil generator |
FR2917066B1 (fr) * | 2007-06-07 | 2010-05-21 | Messier Bugatti | Procede pour collecter une information relative a une surface aerodynamique mobile d'aeronef |
GB0814391D0 (en) * | 2008-08-07 | 2008-09-10 | Rolls Royce Plc | Electrical power provision to a rotatable assembly |
EP2218643B1 (en) * | 2009-02-04 | 2011-08-31 | Alenia Aeronautica S.p.A. | Antiicing system for aircraft propellers |
US20100222937A1 (en) * | 2009-02-27 | 2010-09-02 | Gm Global Technology Operations, Inc. | Heater control system |
FR2960516B1 (fr) * | 2010-05-28 | 2012-05-04 | Eurocopter France | Dispositif d'alimentation electrique et de controle d'un equipement d'un rotor, et aeronef muni d'un tel dispositif |
US8522522B2 (en) * | 2010-07-30 | 2013-09-03 | Hamilton Sundstrand Corporation | Fan embedded power generator |
FR2975842B1 (fr) | 2011-05-24 | 2013-05-17 | Eurocopter France | Dispositif d'alimentation electrique d'au moins un equipement d'un rotor tournant d'un aeronef, et aeronef |
US20130156906A1 (en) * | 2011-12-14 | 2013-06-20 | J.K. Raghavan | Salamander Element for Closed System Oven |
EP2629407B1 (en) | 2012-02-17 | 2014-12-24 | Bell Helicopter Textron Inc. | Electrical generator for rotating structure |
FR2990812B1 (fr) | 2012-05-16 | 2014-05-02 | Eurocopter France | Dispositif d'alimentation electrique d'au moins un equipement d'un rotor d'un aeronef, et aeronef |
CA2908128C (en) | 2012-05-31 | 2021-02-16 | Universite Laval | Method and apparatus for determining an icing condition status of an environment |
US9638044B2 (en) * | 2014-03-11 | 2017-05-02 | Hamilton Sundstrand Corporation | Resistive-inductive propeller blade de-icing system including contactless power supply |
US9598176B2 (en) | 2015-01-27 | 2017-03-21 | Goodrich Corporation | Health monitoring pneumatic deicer |
DE102015006313B4 (de) | 2015-05-16 | 2021-03-18 | Audi Ag | Ladevorrichtung zum induktiven Laden eines elektrischen Energiespeichers eines Kraftfahrzeugs und Verfahren zum Betreiben einer Ladevorrichtung |
MX2019012806A (es) | 2017-05-23 | 2020-01-20 | Dpm Tech Inc | Configuracion de sistema de control de bobina variable, aparato y metodo. |
EP3650349B1 (en) | 2018-11-07 | 2022-03-02 | Ratier-Figeac SAS | De-icing system and method |
WO2020113448A1 (zh) * | 2018-12-04 | 2020-06-11 | 深圳市大疆创新科技有限公司 | 旋转系统和传感器 |
US11722026B2 (en) | 2019-04-23 | 2023-08-08 | Dpm Technologies Inc. | Fault tolerant rotating electric machine |
DE102020205901A1 (de) | 2020-05-11 | 2021-11-11 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Lüftervorrichtung zum Induzieren einer Flügelverformung sowie Verfahren und Verwendung |
CA3217299A1 (en) | 2021-05-04 | 2022-11-10 | Tung Nguyen | Battery control systems and methods |
EP4324089A1 (en) | 2021-05-13 | 2024-02-21 | Exro Technologies Inc. | Method and apparatus to drive coils of a multiphase electric machine |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2247718A1 (de) * | 1972-09-28 | 1974-04-11 | Siemens Ag | Einrichtung zur induktiven uebertragung von daten zwischen einem feststehenden und einem rotierenden teil von elektrischen maschinen |
FR2281273A1 (fr) | 1974-08-05 | 1976-03-05 | Bronzavia Sa | Dispositif antigivrage d'une helice d'avion |
US4292502A (en) * | 1979-02-05 | 1981-09-29 | The B.F. Goodrich Company | Helicopter deicer control system |
DE3045544A1 (de) * | 1980-12-03 | 1982-07-01 | Robert Bosch Gmbh, 7000 Stuttgart | Vorrichtung zur aufzeichnung digitaler signale auf einem magnetband |
US4556366A (en) * | 1983-10-17 | 1985-12-03 | General Electric Company | Propeller actuation system |
US4756667A (en) * | 1987-07-06 | 1988-07-12 | United Technologies Corporation | Pitch control capacitance coupling |
DE3908982A1 (de) * | 1989-03-18 | 1990-09-27 | Scherz Michael | Uebertragungsvorrichtung |
US5144299A (en) | 1990-05-29 | 1992-09-01 | United Technologies Corporation | Telemetry power carrier pulse encoder |
FR2665215B1 (fr) * | 1990-07-27 | 1997-12-26 | Elf Aquitaine | Ensemble de mesure dynamometrique pour tige de forage muni de moyens de transmission radio. |
GB9100709D0 (en) * | 1991-01-12 | 1991-02-27 | Westland Aerostructures Ltd | Data transmission system |
DE4129373C2 (de) * | 1991-09-04 | 1995-05-18 | Roland Man Druckmasch | Vorrichtung zur Passerverstellung an einem Plattenzylinder einer Druckmaschine |
GB2264812B (en) * | 1992-03-04 | 1995-07-19 | Dowty Defence & Air Syst | Electrical power generators |
US5558495A (en) * | 1993-12-02 | 1996-09-24 | Sundstrand Corporation | Electromagnetic heating devices, particularly for ram air turbines |
-
1994
- 1994-09-02 GB GB9417639A patent/GB2293522B/en not_active Expired - Fee Related
-
1995
- 1995-09-04 US US08/793,694 patent/US6181235B1/en not_active Expired - Lifetime
- 1995-09-04 WO PCT/GB1995/002082 patent/WO1996007588A1/en active IP Right Grant
- 1995-09-04 JP JP50929296A patent/JP3616103B2/ja not_active Expired - Fee Related
- 1995-09-04 EP EP95930626A patent/EP0777602B1/en not_active Expired - Lifetime
- 1995-09-04 ES ES95930626T patent/ES2146317T3/es not_active Expired - Lifetime
- 1995-09-04 CA CA002198753A patent/CA2198753C/en not_active Expired - Fee Related
- 1995-09-04 DE DE69516150T patent/DE69516150T2/de not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009508746A (ja) * | 2005-09-23 | 2009-03-05 | エアバス フランス | 航空機の表面の霜取りおよび/または曇り取りを行なうシステムと、このようなシステムを制御する方法と、このようなシステムを備える航空機 |
US8612067B2 (en) | 2005-09-23 | 2013-12-17 | Airbus Operations S.A.S. | System for deicing and/or defogging an aircraft surface, method for controlling same, and aircraft equipped with same |
Also Published As
Publication number | Publication date |
---|---|
CA2198753C (en) | 2005-01-04 |
EP0777602B1 (en) | 2000-04-05 |
WO1996007588A1 (en) | 1996-03-14 |
JP3616103B2 (ja) | 2005-02-02 |
GB2293522B (en) | 1999-01-20 |
GB9417639D0 (en) | 1994-10-26 |
GB2293522A (en) | 1996-03-27 |
ES2146317T3 (es) | 2000-08-01 |
DE69516150T2 (de) | 2001-08-23 |
CA2198753A1 (en) | 1996-03-14 |
DE69516150D1 (de) | 2000-05-11 |
US6181235B1 (en) | 2001-01-30 |
EP0777602A1 (en) | 1997-06-11 |
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