FR2167249B1 - - Google Patents

Info

Publication number
FR2167249B1
FR2167249B1 FR7200751A FR7200751A FR2167249B1 FR 2167249 B1 FR2167249 B1 FR 2167249B1 FR 7200751 A FR7200751 A FR 7200751A FR 7200751 A FR7200751 A FR 7200751A FR 2167249 B1 FR2167249 B1 FR 2167249B1
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.)
Expired
Application number
FR7200751A
Other languages
French (fr)
Other versions
FR2167249A1 (de
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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR7200751A 1972-01-11 1972-01-11 Expired FR2167249B1 (de)

Priority Applications (1)

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

Applications Claiming Priority (1)

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

Publications (2)

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

Family

ID=9091703

Family Applications (1)

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

Country Status (1)

Country Link
FR (1) FR2167249B1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2534222A1 (fr) * 1982-10-06 1984-04-13 Aerospatiale Agencement de rotor de queue a poussee accrue pour aeronef a voilure tournante et dispositif pour accroitre la poussee d'un tel agencement
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.
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.
US5727757A (en) * 1996-01-17 1998-03-17 Mcdonnell Douglas Helicopter Co. Slotted cam control system
FR2769285B1 (fr) 1997-10-07 1999-12-03 Eurocopter France Dispositif de commande d'un systeme anticouple mixte d'un helicoptere
FR2769284B1 (fr) * 1997-10-07 1999-12-03 Eurocopter France Dispositif de commande d'une surface aerodynamique de direction d'un helicoptere
WO1999067130A1 (en) * 1998-06-25 1999-12-29 Sikorsky Aircraft Corporation Horizontal stabilizer for rotorcraft
DE102008046486A1 (de) * 2008-09-08 2010-03-18 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum Landen eines Drehflüglers und Drehflügler
FR2995586B1 (fr) 2012-09-17 2014-08-22 Eurocopter France Moyen de stabilisation en tangage et aeronef a voilure tournante muni d'un tel moyen
EP3061689B1 (de) * 2015-02-27 2017-09-27 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Heckanordnung für ein drehflügelflugzeug, drehflügelflugzeug und verfahren zur herstellung einer verstärkten heckanordnung

Family Cites Families (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 (fr) * 1966-12-13 1968-01-26 Sud Aviation Dispositif directionnel et propulsif pour hélicoptère
FR1576475A (de) * 1968-04-26 1969-08-01

Also Published As

Publication number Publication date
FR2167249A1 (de) 1973-08-24

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Legal Events

Date Code Title Description
ST Notification of lapse