FR2167249A1 - - Google Patents

Info

Publication number
FR2167249A1
FR2167249A1 FR7200751A FR7200751A FR2167249A1 FR 2167249 A1 FR2167249 A1 FR 2167249A1 FR 7200751 A FR7200751 A FR 7200751A FR 7200751 A FR7200751 A FR 7200751A FR 2167249 A1 FR2167249 A1 FR 2167249A1
Authority
FR
France
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
Application number
FR7200751A
Other languages
French (fr)
Other versions
FR2167249B1 (en
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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7200751A priority Critical patent/FR2167249B1/fr
Publication of FR2167249A1 publication Critical patent/FR2167249A1/fr
Application granted granted Critical
Publication of FR2167249B1 publication Critical patent/FR2167249B1/fr
Expired legal-status Critical Current

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
    • B64C2027/8254—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
    • B64C2027/829—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 a V-tail units
FR7200751A 1972-01-11 1972-01-11 Expired FR2167249B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7200751A FR2167249B1 (en) 1972-01-11 1972-01-11

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7200751A FR2167249B1 (en) 1972-01-11 1972-01-11

Publications (2)

Publication Number Publication Date
FR2167249A1 true FR2167249A1 (en) 1973-08-24
FR2167249B1 FR2167249B1 (en) 1974-06-21

Family

ID=9091703

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7200751A Expired FR2167249B1 (en) 1972-01-11 1972-01-11

Country Status (1)

Country Link
FR (1) FR2167249B1 (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2534222A1 (en) * 1982-10-06 1984-04-13 Aerospatiale IMPROVED TAIL ROTOR ARRANGEMENT FOR AN AIRCRAFT WITH A TURNING SAIL AND DEVICE FOR INCREASING THE THRUST OF SUCH AN ARRANGEMENT
FR2600036A1 (en) * 1986-06-16 1987-12-18 Aerospatiale DIRECTIONAL DEVICE AND STABILIZER WITH CARENE AND INCLINE ANTI - TORQUE ROTOR AND DISSYMETRIC V - RING, AND HELICOPTER EQUIPPED WITH SUCH A DEVICE.
FR2689854A1 (en) * 1992-04-14 1993-10-15 Eurocopter France Monorotor helicopter with mixed anti-torque system and method for counteracting the torque induced by this monorotor.
EP0871583A1 (en) * 1996-01-17 1998-10-21 Mcdonnell Douglas Corporation Slotted cam control system
FR2769284A1 (en) * 1997-10-07 1999-04-09 Eurocopter France Control device of helicopter tail rotor aerodynamic steering surface
FR2769285A1 (en) * 1997-10-07 1999-04-09 Eurocopter France Control device for helicopter tail rotor
WO1999067130A1 (en) * 1998-06-25 1999-12-29 Sikorsky Aircraft Corporation Horizontal stabilizer for rotorcraft
DE102008046486A1 (en) * 2008-09-08 2010-03-18 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for landing rotary-wing aircraft, particularly helicopter, involves reducing drive moment on main rotor, such that no blade-rotator interaction effect arises
EP2708466A1 (en) 2012-09-17 2014-03-19 Airbus Helicopters Pitch stabilisation means and rotorcraft comprising such means
EP3061689A1 (en) * 2015-02-27 2016-08-31 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3116036A (en) * 1961-04-17 1963-12-31 Eltra Corp Long range convertible helicopter
FR1511006A (en) * 1966-12-13 1968-01-26 Sud Aviation Directional and propulsion device for helicopter
FR1576475A (en) * 1968-04-26 1969-08-01

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3116036A (en) * 1961-04-17 1963-12-31 Eltra Corp Long range convertible helicopter
FR1511006A (en) * 1966-12-13 1968-01-26 Sud Aviation Directional and propulsion device for helicopter
FR1576475A (en) * 1968-04-26 1969-08-01

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2534222A1 (en) * 1982-10-06 1984-04-13 Aerospatiale IMPROVED TAIL ROTOR ARRANGEMENT FOR AN AIRCRAFT WITH A TURNING SAIL AND DEVICE FOR INCREASING THE THRUST OF SUCH AN ARRANGEMENT
EP0107543A1 (en) * 1982-10-06 1984-05-02 AEROSPATIALE Société Nationale Industrielle Increased thrust tail rotor arrangement for a rotor craft
FR2600036A1 (en) * 1986-06-16 1987-12-18 Aerospatiale DIRECTIONAL DEVICE AND STABILIZER WITH CARENE AND INCLINE ANTI - TORQUE ROTOR AND DISSYMETRIC V - RING, AND HELICOPTER EQUIPPED WITH SUCH A DEVICE.
EP0254605A1 (en) * 1986-06-16 1988-01-27 AEROSPATIALE Société Nationale Industrielle Directional and stabilizing device with a tilted shrouded tail rotor and "V" shaped asymmetric tail unit, and helicopter so equipped
US4809931A (en) * 1986-06-16 1989-03-07 Aerospatiale, Societe Nationale Industrielle Directional and stabilizing device having a faired and slanted antitorque rotor and a disymmetric "V" empennage, and a helicopter equipped with such a device
FR2689854A1 (en) * 1992-04-14 1993-10-15 Eurocopter France Monorotor helicopter with mixed anti-torque system and method for counteracting the torque induced by this monorotor.
EP0566452A1 (en) * 1992-04-14 1993-10-20 EUROCOPTER FRANCE, Société Anonyme dite: Single-rotor helicopter with mixed counter-torque system and method to counter the torque induced by this single rotor
US5388785A (en) * 1992-04-14 1995-02-14 Societe Anonyme Dite: Eurocopter France Single-rotor helicopter having a compound anti-torque system, and a method of countering the torque induced by said single rotor
EP0871583A1 (en) * 1996-01-17 1998-10-21 Mcdonnell Douglas Corporation Slotted cam control system
EP0871583A4 (en) * 1996-01-17 2000-07-12 Mc Donnell Douglas Corp Slotted cam control system
FR2769285A1 (en) * 1997-10-07 1999-04-09 Eurocopter France Control device for helicopter tail rotor
FR2769284A1 (en) * 1997-10-07 1999-04-09 Eurocopter France Control device of helicopter tail rotor aerodynamic steering surface
US6142413A (en) * 1997-10-07 2000-11-07 Eurocopter Device for control of an aerodynamic steering surface of a helicopter
US6290171B1 (en) 1997-10-07 2001-09-18 Eurocopter Device for controlling a helicopter hybrid countertorque system
WO1999067130A1 (en) * 1998-06-25 1999-12-29 Sikorsky Aircraft Corporation Horizontal stabilizer for rotorcraft
DE102008046486A1 (en) * 2008-09-08 2010-03-18 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for landing rotary-wing aircraft, particularly helicopter, involves reducing drive moment on main rotor, such that no blade-rotator interaction effect arises
EP2708466A1 (en) 2012-09-17 2014-03-19 Airbus Helicopters Pitch stabilisation means and rotorcraft comprising such means
US9205911B2 (en) 2012-09-17 2015-12-08 Airbus Helicopters Pitch stabilizer and rotary-wing aircraft equipped with such stabilizer
EP3061689A1 (en) * 2015-02-27 2016-08-31 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly
CN105923157A (en) * 2015-02-27 2016-09-07 空客直升机德国有限公司 Tail Assembly For Rotorcraft, Rotorcraft And Method Of Manufacture Of Strengthened Tail Assembly
US9963226B2 (en) 2015-02-27 2018-05-08 Airbus Helicopters Deutschland GmbH Tail assembly for a rotorcraft, rotorcraft and method of manufacture of a strengthened tail assembly
CN105923157B (en) * 2015-02-27 2018-07-17 空客直升机德国有限公司 For the rail unit of rotor craft, the method for rotor craft and manufacture reinforcement rail unit

Also Published As

Publication number Publication date
FR2167249B1 (en) 1974-06-21

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Legal Events

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