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FR2328609A1 - Helicoptere a helices horizontales de neutralisation du couple de torsion - Google Patents

Helicoptere a helices horizontales de neutralisation du couple de torsion

Info

Publication number
FR2328609A1
FR2328609A1 FR7533284A FR7533284A FR2328609A1 FR 2328609 A1 FR2328609 A1 FR 2328609A1 FR 7533284 A FR7533284 A FR 7533284A FR 7533284 A FR7533284 A FR 7533284A FR 2328609 A1 FR2328609 A1 FR 2328609A1
Authority
FR
France
Prior art keywords
rotor
airscrew
helicopter rotor
contrarotating
fixed pitch
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.)
Granted
Application number
FR7533284A
Other languages
English (en)
Other versions
FR2328609B1 (fr
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR7533284A priority Critical patent/FR2328609A1/fr
Publication of FR2328609A1 publication Critical patent/FR2328609A1/fr
Application granted granted Critical
Publication of FR2328609B1 publication Critical patent/FR2328609B1/fr
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • 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
    • B64C2027/8263Rotorcraft; 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
    • B64C2027/8272Rotorcraft; 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 fins, or movable rudders

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7533284A 1975-10-23 1975-10-23 Helicoptere a helices horizontales de neutralisation du couple de torsion Granted FR2328609A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7533284A FR2328609A1 (fr) 1975-10-23 1975-10-23 Helicoptere a helices horizontales de neutralisation du couple de torsion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7533284A FR2328609A1 (fr) 1975-10-23 1975-10-23 Helicoptere a helices horizontales de neutralisation du couple de torsion

Publications (2)

Publication Number Publication Date
FR2328609A1 true FR2328609A1 (fr) 1977-05-20
FR2328609B1 FR2328609B1 (fr) 1981-01-09

Family

ID=9161847

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7533284A Granted FR2328609A1 (fr) 1975-10-23 1975-10-23 Helicoptere a helices horizontales de neutralisation du couple de torsion

Country Status (1)

Country Link
FR (1) FR2328609A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569387A1 (fr) * 1984-08-23 1986-02-28 United Technologies Corp Organe flexible pour le centrage du plateau oscillant pour la commande du pas des pales d'un rotor d'helicoptere
US5240204A (en) * 1991-07-19 1993-08-31 Kunz Bernard P Lift generating method and apparatus for aircraft
US9145205B2 (en) 2009-08-07 2015-09-29 Guy Jonathan James Rackham Rotor assembly for a rotorcraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569387A1 (fr) * 1984-08-23 1986-02-28 United Technologies Corp Organe flexible pour le centrage du plateau oscillant pour la commande du pas des pales d'un rotor d'helicoptere
US5240204A (en) * 1991-07-19 1993-08-31 Kunz Bernard P Lift generating method and apparatus for aircraft
US9145205B2 (en) 2009-08-07 2015-09-29 Guy Jonathan James Rackham Rotor assembly for a rotorcraft

Also Published As

Publication number Publication date
FR2328609B1 (fr) 1981-01-09

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Legal Events

Date Code Title Description
ST Notification of lapse