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FR2951137B1 - Dispositif anticouple d'un giravion - Google Patents

Dispositif anticouple d'un giravion

Info

Publication number
FR2951137B1
FR2951137B1 FR0904898A FR0904898A FR2951137B1 FR 2951137 B1 FR2951137 B1 FR 2951137B1 FR 0904898 A FR0904898 A FR 0904898A FR 0904898 A FR0904898 A FR 0904898A FR 2951137 B1 FR2951137 B1 FR 2951137B1
Authority
FR
France
Prior art keywords
anticouple
giravion
anticouple device
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
Application number
FR0904898A
Other languages
English (en)
Other versions
FR2951137A1 (fr
Inventor
Gilles Herpin
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.)
Airbus Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0904898A priority Critical patent/FR2951137B1/fr
Priority to CA2714815A priority patent/CA2714815C/fr
Publication of FR2951137A1 publication Critical patent/FR2951137A1/fr
Application granted granted Critical
Publication of FR2951137B1 publication Critical patent/FR2951137B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; 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
    • B64C2027/8236Rotorcraft; 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Tires In General (AREA)
FR0904898A 2009-10-13 2009-10-13 Dispositif anticouple d'un giravion Active FR2951137B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0904898A FR2951137B1 (fr) 2009-10-13 2009-10-13 Dispositif anticouple d'un giravion
CA2714815A CA2714815C (fr) 2009-10-13 2010-09-15 Dispositif anticouple d'un giravion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0904898A FR2951137B1 (fr) 2009-10-13 2009-10-13 Dispositif anticouple d'un giravion

Publications (2)

Publication Number Publication Date
FR2951137A1 FR2951137A1 (fr) 2011-04-15
FR2951137B1 true FR2951137B1 (fr) 2012-03-09

Family

ID=42115443

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0904898A Active FR2951137B1 (fr) 2009-10-13 2009-10-13 Dispositif anticouple d'un giravion

Country Status (2)

Country Link
CA (1) CA2714815C (fr)
FR (1) FR2951137B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10703471B2 (en) 2016-06-03 2020-07-07 Bell Helicopter Textron Inc. Anti-torque control using matrix of fixed blade pitch motor modules
US10526085B2 (en) 2016-06-03 2020-01-07 Bell Textron Inc. Electric distributed propulsion anti-torque redundant power and control system
US10377479B2 (en) 2016-06-03 2019-08-13 Bell Helicopter Textron Inc. Variable directional thrust for helicopter tail anti-torque system
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

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB572417A (en) * 1943-05-24 1945-10-08 G & J Weir Ltd Improvements in helicopters
DE1581060B1 (de) * 1966-04-02 1969-09-18 Messerschmitt Boelkow Blohm Hubschrauber mit schwenkbarem Heckrotor
EP0018114A1 (fr) * 1979-04-03 1980-10-29 The Secretary of State for Defence in Her Britannic Majesty's Government of the United Kingdom of Great Britain and Dispositifs de propulsion
GB8507875D0 (en) * 1985-03-26 1985-05-01 Univ Open Aerodynamic/hydrodynamic control device

Also Published As

Publication number Publication date
CA2714815C (fr) 2012-12-04
FR2951137A1 (fr) 2011-04-15
CA2714815A1 (fr) 2011-04-13

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