DE69110660T2 - Gegendrehmomentvorrichtung eines Hubschraubers. - Google Patents
Gegendrehmomentvorrichtung eines Hubschraubers.Info
- Publication number
- DE69110660T2 DE69110660T2 DE69110660T DE69110660T DE69110660T2 DE 69110660 T2 DE69110660 T2 DE 69110660T2 DE 69110660 T DE69110660 T DE 69110660T DE 69110660 T DE69110660 T DE 69110660T DE 69110660 T2 DE69110660 T2 DE 69110660T2
- Authority
- DE
- Germany
- Prior art keywords
- helicopter
- counter torque
- torque device
- counter
- torque
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8254—Shrouded tail rotors, e.g. "Fenestron" fans
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
- B64C2027/8281—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/683,904 US5131604A (en) | 1991-04-11 | 1991-04-11 | Helicopter antitorque device |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69110660D1 DE69110660D1 (de) | 1995-07-27 |
DE69110660T2 true DE69110660T2 (de) | 1995-12-14 |
Family
ID=24745940
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69110660T Expired - Fee Related DE69110660T2 (de) | 1991-04-11 | 1991-12-20 | Gegendrehmomentvorrichtung eines Hubschraubers. |
Country Status (9)
Country | Link |
---|---|
US (1) | US5131604A (de) |
EP (1) | EP0508027B1 (de) |
JP (1) | JP3121417B2 (de) |
KR (1) | KR100246262B1 (de) |
AU (1) | AU637032B2 (de) |
CA (1) | CA2058011A1 (de) |
DE (1) | DE69110660T2 (de) |
ES (1) | ES2073720T3 (de) |
IL (1) | IL100493A (de) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5102067A (en) * | 1991-04-11 | 1992-04-07 | United Technologies Corporation | Integrated helicopter empennage structure |
US5108044A (en) * | 1991-04-11 | 1992-04-28 | United Technologies Corporation | Shroud-fin integration shelf for a helicopter empennage structure |
FR2689854B1 (fr) * | 1992-04-14 | 1994-07-01 | Eurocopter France | Helicoptere monorotor a systeme anticouple mixte et procede pour contrecarrer le couple induit par ce monorotor. |
FR2719550B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor et stator redresseur carénés, et modulation de phase des pales du rotor, pour hélicoptère. |
FR2719549B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor caréné et modulation de phase des pales, pour hélicoptère. |
FR2719551B1 (fr) * | 1994-05-04 | 1996-07-12 | Eurocopter France | Dispositif anti-couple à rotor et stator redresseur carénés, et à aubes redresseuses inclinées. |
FR2719552B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Aube de redresseur pour dispositif anti-couple à rotor et stator redresseur carénés d'hélicoptère. |
FR2719553B1 (fr) * | 1994-05-04 | 1996-07-26 | Eurocopter France | Dispositif anti-couple à rotor arrière et stator redresseur carénés pour hélicoptère. |
FR2721000B1 (fr) * | 1994-06-10 | 1996-08-23 | Eurocopter France | Aube de redresseur en composite, redresseur la comportant, pour dispositif anti-couple à rotor et stator redresseur carénés, et leur procédé de fabrication. |
US5607122A (en) * | 1994-12-22 | 1997-03-04 | Bell Helicopter Textron Inc. | Tail rotor authority control for a helicopter |
US5810285A (en) | 1996-12-20 | 1998-09-22 | Sikorsky Aircraft Corporation | Drive shaft casing for a ducted fan anti-torque device |
JP3051357B2 (ja) * | 1997-03-26 | 2000-06-12 | 株式会社コミュータヘリコプタ先進技術研究所 | 主ロータトルク補正装置 |
US6371408B1 (en) * | 2000-08-03 | 2002-04-16 | Dennis Halwes | Helicopter tail rotor authority altitude compensator |
US6416015B1 (en) | 2001-05-01 | 2002-07-09 | Franklin D. Carson | Anti-torque and yaw-control system for a rotary-wing aircraft |
US6755374B1 (en) | 2003-01-27 | 2004-06-29 | Franklin D. Carson | Anti-Torque and yaw-control system for a rotary-wing aircraft |
US20040169485A1 (en) * | 2003-02-28 | 2004-09-02 | Clancy Andy J. | Vehicle direction control with a crosswise fan |
US7121506B2 (en) * | 2004-12-10 | 2006-10-17 | Clancy Andy J | Remotely controlled model airplane having deflectable centrally biased control surface |
US7644893B2 (en) * | 2006-02-15 | 2010-01-12 | Sikorsky Aircraft Corporation | Full authority fly-by-wire pedal system |
FR2923456B1 (fr) * | 2007-11-08 | 2009-12-18 | Eurocopter France | Aeronef muni d'un rotor carene silencieux |
FR2926786B1 (fr) * | 2008-01-30 | 2010-02-19 | Eurocopter France | Procede d'optimisation d'un rotor anti-couple carene a gene acoustique minimale pour un giravion, notamment un helicoptere, et rotor anti-couple carene ainsi obtenu |
US20090283628A1 (en) * | 2008-05-19 | 2009-11-19 | Frederickson Kirk C | Directional control arrangement to provide stabilizing feedback to a structural bending mode |
US8240597B2 (en) | 2008-08-06 | 2012-08-14 | Honeywell International Inc. | UAV ducted fan lip shaping |
EP2154065B1 (de) * | 2008-08-14 | 2011-07-13 | Agusta S.p.A. | Hubschrauberrotor |
FR2968272B1 (fr) * | 2010-12-06 | 2013-07-12 | Eurocopter France | Element de structure ameliore d'un giravion pour diminuer la trainee aerodynamique. |
EP2671798B1 (de) * | 2012-06-08 | 2015-08-05 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Helikopter mit einem Querkanal |
CN102689687B (zh) * | 2012-06-08 | 2014-12-10 | 中国航空工业集团公司西安飞机设计研究所 | 一种平衡螺旋桨后气动旋转力矩的方法 |
EP2799334B1 (de) | 2013-04-29 | 2016-09-07 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Rotierende Blattanordnung mit aerodynamischem äußeren Toroidspoiler für eine ummantelte rotierende Antriebsanordnung |
CN103438024A (zh) * | 2013-07-03 | 2013-12-11 | 浙江理工大学 | 一种叶片非均匀分布的小型轴流风扇 |
RU2557683C2 (ru) * | 2013-10-18 | 2015-07-27 | Эйрбас Хеликоптерс Дойчланд Гмбх | Вертолет с поперечным каналом |
EP2883791B1 (de) * | 2013-12-10 | 2016-04-06 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Hubschrauber mit Heckschutz |
EP2913270B1 (de) | 2014-02-28 | 2016-02-24 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Drehflügler mit mindestens einem hauptrotor und mindestens einem rotor zum drehmomentausgleich |
EP2913269B1 (de) | 2014-02-28 | 2019-01-16 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Drehflügler mit mindestens einem Hauptrotor und mindestens einem Rotor zum Drehmomentausgleich |
EP2913271A1 (de) | 2014-02-28 | 2015-09-02 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Drehflügler mit mindestens einem Hauptrotor und mindestens einem rotor zum Drehmomentausgleich |
US20160207623A1 (en) * | 2015-01-20 | 2016-07-21 | Franklin D. Carson | Rotary-wing aircraft with ducted anti-torque device |
US10570926B2 (en) | 2015-12-03 | 2020-02-25 | The Boeing Company | Variable-geometry ducted fan |
CN109625261B (zh) * | 2017-10-06 | 2023-09-22 | 松下电器(美国)知识产权公司 | 无人飞行器 |
US10814971B2 (en) * | 2018-04-10 | 2020-10-27 | Textron Innovations Inc. | Tail rotor housing |
US10415581B1 (en) | 2018-04-25 | 2019-09-17 | Brien Aven Seeley | Ultra-quiet propeller system |
US10889366B2 (en) | 2018-09-21 | 2021-01-12 | Textron Innovations Inc. | Ducted thrusters |
US11220329B2 (en) * | 2019-02-03 | 2022-01-11 | Textron Innovations Inc. | Ducted rotor stators |
US11034440B2 (en) | 2019-03-01 | 2021-06-15 | Textron Innovations Inc. | Tail rotor gearbox support assemblies for helicopters |
CN111645875B (zh) * | 2020-04-22 | 2022-06-21 | 中国直升机设计研究所 | 一种直升机应急着水水线及其位置设计方法 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2609053A (en) * | 1946-10-31 | 1952-09-02 | United Aircraft Corp | Shrouded tail rotor |
US3241791A (en) * | 1964-04-03 | 1966-03-22 | Frank N Piasecki | Compound helicopter with shrouded tail propeller |
FR1531536A (fr) * | 1967-05-22 | 1968-07-05 | Sud Aviation | Hélice ou rotor à pas variable |
FR2600036B1 (fr) * | 1986-06-16 | 1988-09-16 | Aerospatiale | Dispositif directionnel et stabilisateur a rotor anti-couple carene et incline et a empennage en " v " dissymetrique, et helicoptere equipe d'un tel dispositif. |
FR2628062B1 (fr) * | 1988-03-07 | 1990-08-10 | Aerospatiale | Pale pour helice carenee a hautes performances, helice carenee multipale pourvue de telles pales et agencement de rotor de queue a helice carenee pour aeronef a voilure tournante |
US5108044A (en) * | 1991-04-11 | 1992-04-28 | United Technologies Corporation | Shroud-fin integration shelf for a helicopter empennage structure |
-
1991
- 1991-04-11 US US07/683,904 patent/US5131604A/en not_active Expired - Lifetime
- 1991-12-18 CA CA002058011A patent/CA2058011A1/en not_active Abandoned
- 1991-12-20 ES ES91630119T patent/ES2073720T3/es not_active Expired - Lifetime
- 1991-12-20 EP EP91630119A patent/EP0508027B1/de not_active Expired - Lifetime
- 1991-12-20 DE DE69110660T patent/DE69110660T2/de not_active Expired - Fee Related
- 1991-12-23 AU AU90040/91A patent/AU637032B2/en not_active Ceased
- 1991-12-23 KR KR1019910024313A patent/KR100246262B1/ko not_active IP Right Cessation
- 1991-12-24 JP JP03361263A patent/JP3121417B2/ja not_active Expired - Fee Related
- 1991-12-25 IL IL10049391A patent/IL100493A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
ES2073720T3 (es) | 1995-08-16 |
EP0508027A1 (de) | 1992-10-14 |
DE69110660D1 (de) | 1995-07-27 |
JPH05185992A (ja) | 1993-07-27 |
IL100493A (en) | 1995-06-29 |
IL100493A0 (en) | 1992-09-06 |
EP0508027B1 (de) | 1995-06-21 |
KR920019616A (ko) | 1992-11-19 |
US5131604A (en) | 1992-07-21 |
AU9004091A (en) | 1992-10-15 |
KR100246262B1 (ko) | 2000-04-01 |
JP3121417B2 (ja) | 2000-12-25 |
AU637032B2 (en) | 1993-05-13 |
CA2058011A1 (en) | 1992-10-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |