FR2983171B1 - Dispositif anti-couple a poussee longitudinale pour un giravion - Google Patents
Dispositif anti-couple a poussee longitudinale pour un giravionInfo
- Publication number
- FR2983171B1 FR2983171B1 FR1103643A FR1103643A FR2983171B1 FR 2983171 B1 FR2983171 B1 FR 2983171B1 FR 1103643 A FR1103643 A FR 1103643A FR 1103643 A FR1103643 A FR 1103643A FR 2983171 B1 FR2983171 B1 FR 2983171B1
- Authority
- FR
- France
- Prior art keywords
- giravion
- torque device
- longitudinal push
- push
- longitudinal
- 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.)
- Active
Links
Classifications
-
- 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
- B64C2027/8218—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 wherein the rotor or the jet axis is inclined with respect to the longitudinal horizontal or vertical plane of the helicopter
-
- 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
- B64C2027/8227—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 more than one rotor
-
- 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
- B64C2027/8236—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 including pusher propellers
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1103643A FR2983171B1 (fr) | 2011-11-30 | 2011-11-30 | Dispositif anti-couple a poussee longitudinale pour un giravion |
US13/678,648 US8979015B2 (en) | 2011-11-30 | 2012-11-16 | Anti-torque device with longitudinal thrust for a rotorcraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1103643A FR2983171B1 (fr) | 2011-11-30 | 2011-11-30 | Dispositif anti-couple a poussee longitudinale pour un giravion |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2983171A1 FR2983171A1 (fr) | 2013-05-31 |
FR2983171B1 true FR2983171B1 (fr) | 2014-03-21 |
Family
ID=45809046
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1103643A Active FR2983171B1 (fr) | 2011-11-30 | 2011-11-30 | Dispositif anti-couple a poussee longitudinale pour un giravion |
Country Status (2)
Country | Link |
---|---|
US (1) | US8979015B2 (fr) |
FR (1) | FR2983171B1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015173484A1 (fr) | 2014-05-14 | 2015-11-19 | Peugeot Citroen Automobiles Sa | Fixation a rupture programmee du berceau moteur au plancher d'un vehicule |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20160207623A1 (en) * | 2015-01-20 | 2016-07-21 | Franklin D. Carson | Rotary-wing aircraft with ducted anti-torque device |
US9944388B2 (en) * | 2015-08-27 | 2018-04-17 | Sikorsky Aircraft Corporation | Rotorcraft state control |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
AU2016338382B2 (en) | 2015-09-02 | 2021-04-01 | Jetoptera, Inc. | Ejector and airfoil configurations |
US10377479B2 (en) | 2016-06-03 | 2019-08-13 | Bell Helicopter Textron Inc. | Variable directional thrust for helicopter tail anti-torque system |
US10703471B2 (en) | 2016-06-03 | 2020-07-07 | Bell Helicopter Textron Inc. | Anti-torque control using matrix of fixed blade pitch motor modules |
US11332240B2 (en) * | 2016-06-03 | 2022-05-17 | Textron Innovations Inc. | Anti-torque systems for rotorcraft |
US10526085B2 (en) * | 2016-06-03 | 2020-01-07 | Bell Textron Inc. | Electric distributed propulsion anti-torque redundant power and control system |
CN106292680A (zh) * | 2016-09-18 | 2017-01-04 | 上海交通大学 | 多旋翼无人机及其系统以及飞行控制方法 |
US10059432B1 (en) | 2017-02-22 | 2018-08-28 | Pratt & Whitney Canada Corp. | Single lever control in twin turbopropeller aircraft |
US11186185B2 (en) | 2017-05-31 | 2021-11-30 | Textron Innovations Inc. | Rotor brake effect by using electric distributed anti-torque generators and opposing electric motor thrust to slow a main rotor |
WO2019005937A1 (fr) | 2017-06-27 | 2019-01-03 | Jetoptera, Inc. | Configuration pour système de décollage et d'atterrissage vertical pour véhicules aériens |
FR3071223B1 (fr) * | 2017-09-19 | 2022-04-15 | Airbus Helicopters | Helicoptere hybride comportant des helices de propulsion inclinees |
US11433997B2 (en) | 2017-10-30 | 2022-09-06 | Textron Innovations Inc. | Rotorcraft anti-torque systems and methods therefor |
US10940945B2 (en) | 2017-10-30 | 2021-03-09 | Bell Helicopter Textron Inc. | Rotorcraft anti-torque system |
FR3074142A1 (fr) * | 2017-11-30 | 2019-05-31 | Airbus Helicopters | Giravion de type hybride comportant un empennage horizontal et deux derives agencees sur l'empennage horizontal |
FR3080605B1 (fr) * | 2018-04-26 | 2020-05-29 | Airbus Helicopters | Giravion muni d'une voilure tournante et d'au moins deux helices et procede applique par ce giravion |
US11174016B2 (en) * | 2018-05-03 | 2021-11-16 | Jaunt Air Mobility, Llc | Compound rotorcraft with propeller |
US10933990B2 (en) * | 2019-01-15 | 2021-03-02 | Bell Textron Inc. | Modal tailboom flight control systems for compound helicopters |
US11613353B2 (en) * | 2019-02-04 | 2023-03-28 | The Boeing Company | Expedited design and qualification of unmanned aerial vehicles |
US11117655B2 (en) * | 2019-06-10 | 2021-09-14 | Bell Textron Inc. | Counter-rotating tail rotor |
US11572155B2 (en) * | 2019-10-28 | 2023-02-07 | Textron Innovations Inc. | Rotorcraft having propeller generated power during autorotations |
US11230373B2 (en) * | 2019-12-02 | 2022-01-25 | Textron Innovations Inc. | Assembly and method for helicopter anti-torque |
FR3108311B1 (fr) * | 2020-03-17 | 2022-02-18 | Airbus Helicopters | procédé de protection d’une marge de contrôle de l’attitude en lacet d’un hélicoptère hybride et un hélicoptère hybride. |
CN111498103A (zh) * | 2020-04-20 | 2020-08-07 | 飞的科技有限公司 | 飞行器 |
US11554860B1 (en) | 2020-06-23 | 2023-01-17 | Piasecki Aircraft Corporation | Apparatus, system and method for a convertible thruster for a compound aircraft |
US11772785B2 (en) * | 2020-12-01 | 2023-10-03 | Textron Innovations Inc. | Tail rotor configurations for rotorcraft yaw control systems |
US11720123B2 (en) | 2020-12-01 | 2023-08-08 | Textron Innovations Inc. | Airframe protection systems for use on rotorcraft |
US11866162B2 (en) | 2020-12-01 | 2024-01-09 | Textron Innovations Inc. | Power management systems for electrically distributed yaw control systems |
US11760472B2 (en) | 2020-12-01 | 2023-09-19 | Textron Innovations Inc. | Rudders for rotorcraft yaw control systems |
US11479349B2 (en) | 2020-12-01 | 2022-10-25 | Textron Innovations Inc. | Tail rotor balancing systems for use on rotorcraft |
US11685524B2 (en) | 2020-12-01 | 2023-06-27 | Textron Innovations Inc. | Rotorcraft quiet modes |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2415622A (en) * | 1944-01-18 | 1947-02-11 | Bossi Enea | Helicopter antitorque propeller system |
US2420784A (en) * | 1945-05-16 | 1947-05-20 | Glenn L Martin Co | Helicopter with antitorque propellers |
US2698147A (en) * | 1950-09-01 | 1954-12-28 | Paul E Hovgard | Aircraft with fixed wings and lifting rotor |
US3155341A (en) | 1963-04-05 | 1964-11-03 | Ryan Aeronautical Co | Convertiplane |
US3448946A (en) * | 1966-09-16 | 1969-06-10 | Kawasaki Kokuki Kogyo Kk | Compound helicopter |
US3432119A (en) * | 1966-10-24 | 1969-03-11 | Edward W Miller | Helicopter |
FR1511006A (fr) * | 1966-12-13 | 1968-01-26 | Sud Aviation | Dispositif directionnel et propulsif pour hélicoptère |
US3426982A (en) * | 1967-02-03 | 1969-02-11 | Ronald L Markwood | Vertiplane vtol aircraft |
US3540680A (en) * | 1968-05-24 | 1970-11-17 | Lockheed Aircraft Corp | Dual rotor system for helicopters |
US4899957A (en) * | 1971-03-08 | 1990-02-13 | Karl Eickmann | Air borne craft, for example helicopter, and related devices |
US3977812A (en) * | 1975-11-17 | 1976-08-31 | The United States Of America As Represented By The Secretary Of The Army | Compound helicopter drive means |
FR2451859B1 (fr) * | 1979-03-23 | 1985-07-19 | Westland Aircraft Ltd | Perfectionnement apporte aux helicopteres |
US4488851A (en) * | 1982-04-01 | 1984-12-18 | The United States Of America As Represented By The Secretary Of The Army | Power management system |
US5123613A (en) * | 1988-06-21 | 1992-06-23 | Piasecki Aircraft Corporation | Rotary wing aircraft shrouded propeller tail assembly and controls |
US5174523A (en) * | 1989-01-09 | 1992-12-29 | Westland Helicopters Limited | Compound helicopter with engine shaft power output control |
US5131603A (en) * | 1991-05-02 | 1992-07-21 | Piasecki Aircraft Corporation | Rotary wing aircraft split segmented duct shrouded propeller tail assembly |
US5269654A (en) * | 1992-07-24 | 1993-12-14 | Don Chapman | Tail rotor assembly for helicopters |
FR2916418B1 (fr) | 2007-05-22 | 2009-08-28 | Eurocopter France | Helicoptere hybride rapide a grande distance franchissable. |
US20100019079A1 (en) * | 2007-06-20 | 2010-01-28 | General Electric Company | Thrust generator for a rotary wing aircraft |
US20090216392A1 (en) * | 2007-07-11 | 2009-08-27 | Piasecki Aircraft Corporation | Vectored thruster augmented aircraft |
US7823827B2 (en) * | 2007-07-11 | 2010-11-02 | Piasecki Frederick W | Vectored thruster augmented aircraft |
JP2009051465A (ja) * | 2007-08-29 | 2009-03-12 | Mitsubishi Heavy Ind Ltd | テールロータ装置およびヘリコプタ |
US8167233B2 (en) * | 2007-12-21 | 2012-05-01 | Avx Aircraft Company | Coaxial rotor aircraft |
US8196855B2 (en) * | 2009-11-23 | 2012-06-12 | Balkus Jr Carl E | Helicopter auxiliary anti-torque system |
US9067677B2 (en) * | 2009-12-02 | 2015-06-30 | Saab Ab | Dismountable helicopter |
FR2962713A1 (fr) * | 2010-07-13 | 2012-01-20 | Eurocopter France | Procede et aeronef muni d'un rotor arriere basculant |
-
2011
- 2011-11-30 FR FR1103643A patent/FR2983171B1/fr active Active
-
2012
- 2012-11-16 US US13/678,648 patent/US8979015B2/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015173484A1 (fr) | 2014-05-14 | 2015-11-19 | Peugeot Citroen Automobiles Sa | Fixation a rupture programmee du berceau moteur au plancher d'un vehicule |
Also Published As
Publication number | Publication date |
---|---|
US20130134256A1 (en) | 2013-05-30 |
US8979015B2 (en) | 2015-03-17 |
FR2983171A1 (fr) | 2013-05-31 |
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Legal Events
Date | Code | Title | Description |
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CD | Change of name or company name |
Owner name: AIRBUS HELICOPTERS, FR Effective date: 20140602 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |