FR2354922A1 - Perfectionnements apportes a un dispositif d'entrainement des rotors d'un helicoptere - Google Patents

Perfectionnements apportes a un dispositif d'entrainement des rotors d'un helicoptere

Info

Publication number
FR2354922A1
FR2354922A1 FR7618086A FR7618086A FR2354922A1 FR 2354922 A1 FR2354922 A1 FR 2354922A1 FR 7618086 A FR7618086 A FR 7618086A FR 7618086 A FR7618086 A FR 7618086A FR 2354922 A1 FR2354922 A1 FR 2354922A1
Authority
FR
France
Prior art keywords
engine failure
gyration
lift
drive transmission
drive shaft
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
FR7618086A
Other languages
English (en)
Other versions
FR2354922B1 (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.)
ETUDES RECH AVANCEES
Original Assignee
ETUDES RECH AVANCEES
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 ETUDES RECH AVANCEES filed Critical ETUDES RECH AVANCEES
Priority to FR7618086A priority Critical patent/FR2354922A1/fr
Publication of FR2354922A1 publication Critical patent/FR2354922A1/fr
Application granted granted Critical
Publication of FR2354922B1 publication Critical patent/FR2354922B1/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gear Transmission (AREA)

Abstract

Dispositif d'entraînement des rotors d'un hélicoptère Il comprend une roue libre 6 entraînée par un arbre 5 lié au moteur de l'hélicoptère, un réducteur 8, un arbre d'entraînement 2 du rotor de sustentation et un arbre 3 d'entraînement du rotor de direction. Selon l'invention le réducteur 8 est à trains planétaires et comprend un ensemble de satellites 15 et une couronne extérieure fixe 17, solidaire du boîtier 14 du dispositif. Applications : gain d'encombrement et de poids pour les hélicoptères.
FR7618086A 1976-06-15 1976-06-15 Perfectionnements apportes a un dispositif d'entrainement des rotors d'un helicoptere Granted FR2354922A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7618086A FR2354922A1 (fr) 1976-06-15 1976-06-15 Perfectionnements apportes a un dispositif d'entrainement des rotors d'un helicoptere

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7618086A FR2354922A1 (fr) 1976-06-15 1976-06-15 Perfectionnements apportes a un dispositif d'entrainement des rotors d'un helicoptere

Publications (2)

Publication Number Publication Date
FR2354922A1 true FR2354922A1 (fr) 1978-01-13
FR2354922B1 FR2354922B1 (fr) 1979-04-06

Family

ID=9174378

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7618086A Granted FR2354922A1 (fr) 1976-06-15 1976-06-15 Perfectionnements apportes a un dispositif d'entrainement des rotors d'un helicoptere

Country Status (1)

Country Link
FR (1) FR2354922A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4659286A (en) * 1984-05-14 1987-04-21 Costruzioni Aeronautiche Giovanni Agusta S.P.A. Main helicopter drive
US4983153A (en) * 1985-12-18 1991-01-08 Daf Special Products Gear unit, particularly for use in a helicopter
WO1994000347A2 (fr) * 1992-06-22 1994-01-06 United Technologies Corporation Vehicule aerien sans equipage possedant des rotors coaxiaux, a canalisations d'air et a rotation antagoniste

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111483591B (zh) * 2020-04-24 2022-04-05 中国航发湖南动力机械研究所 尾减机匣及重载尾减速器

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4659286A (en) * 1984-05-14 1987-04-21 Costruzioni Aeronautiche Giovanni Agusta S.P.A. Main helicopter drive
US4983153A (en) * 1985-12-18 1991-01-08 Daf Special Products Gear unit, particularly for use in a helicopter
WO1994000347A2 (fr) * 1992-06-22 1994-01-06 United Technologies Corporation Vehicule aerien sans equipage possedant des rotors coaxiaux, a canalisations d'air et a rotation antagoniste
WO1994000347A3 (fr) * 1992-06-22 1994-07-07 United Technologies Corp Vehicule aerien sans equipage possedant des rotors coaxiaux, a canalisations d'air et a rotation antagoniste
EP0861775A1 (fr) * 1992-06-22 1998-09-02 United Technologies Corporation Un sous-ensemble de moyeux de transmission/centrage coaxiales pour ensemble rotor

Also Published As

Publication number Publication date
FR2354922B1 (fr) 1979-04-06

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Legal Events

Date Code Title Description
ST Notification of lapse