FR2441902A2 - Dispositif de suspension multidirectionnelle pour giravion - Google Patents

Dispositif de suspension multidirectionnelle pour giravion

Info

Publication number
FR2441902A2
FR2441902A2 FR7832281A FR7832281A FR2441902A2 FR 2441902 A2 FR2441902 A2 FR 2441902A2 FR 7832281 A FR7832281 A FR 7832281A FR 7832281 A FR7832281 A FR 7832281A FR 2441902 A2 FR2441902 A2 FR 2441902A2
Authority
FR
France
Prior art keywords
giravion
suspension device
suspension
longitinally
flange
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
FR7832281A
Other languages
English (en)
Other versions
FR2441902B2 (fr
Inventor
Rene Louis Mouille
Edwin Ortega
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 FR7832281A priority Critical patent/FR2441902A2/fr
Priority to GB7909622A priority patent/GB2018942B/en
Priority to DE2910729A priority patent/DE2910729C2/de
Priority to US06/021,778 priority patent/US4274510A/en
Priority to IT21152/79A priority patent/IT1163655B/it
Priority to JP3181979A priority patent/JPS54129698A/ja
Publication of FR2441902A2 publication Critical patent/FR2441902A2/fr
Application granted granted Critical
Publication of FR2441902B2 publication Critical patent/FR2441902B2/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B64C2027/002—Vibration damping devices mounted between the rotor drive and the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Vehicle Body Suspensions (AREA)

Abstract

L'ADDITION CONCERNE LES DISPOSITIFS DE SUSPENSION POUR ORGANES MECANIQUES. ELLE A POUR OBJET UN DISPOSITIF DE SUSPENSION COMPRENANT UN FLASQUE 17 SOLIDAIRE DE L'ORGANE A SUSPENDRE. CE FLASQUE EST RELIE A DES FERRURES FIXES 220A,B, 221A, B PAR DES PLOTS LAMIFIES 184A, B INCOMPRESSIBLES, MAIS ELASTIQUES EN CISAILLEMENT, PAR UNE TRAVERSE FLOTTANTE 130 ET PAR DES BRAS 225A, B ARTICULES A LEURS EXTREMITES ET LONGITUDINALEMENT INCOMPRESSIBLES, MAIS FLEXIBLES LATERALEMENT, L'ENSEMBLE PROCURANT UNE LIAISON RIGIDE EN ROTATION QUI ASSURE LA REPRISE D'UN COUPLE DONT LEDIT ORGANE EST LE SIEGE, TOUT EN PERMETTANT A CELUI-CI DES DEBATTEMENTS EN TRANSLATION. APPLICATION A LA SUSPENSION, AVEC FILTRAGE DES VIBRATIONS, DE LA BOITE DE TRANSMISSION PRINCIPALE D'UN GIRAVION SUR SON FUSELAGE.
FR7832281A 1978-03-20 1978-11-15 Dispositif de suspension multidirectionnelle pour giravion Granted FR2441902A2 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR7832281A FR2441902A2 (fr) 1978-11-15 1978-11-15 Dispositif de suspension multidirectionnelle pour giravion
GB7909622A GB2018942B (en) 1978-03-20 1979-03-19 Multi-directional suspension means
DE2910729A DE2910729C2 (de) 1978-03-20 1979-03-19 Multidirektionale Aufhängung für Hubschrauber-Antriebe
US06/021,778 US4274510A (en) 1978-03-20 1979-03-19 Multi-directional suspension means for rotor aircraft
IT21152/79A IT1163655B (it) 1978-03-20 1979-03-20 Dispositivo di sospensione multidirezionale per giroplano
JP3181979A JPS54129698A (en) 1978-03-20 1979-03-20 Suspension system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7832281A FR2441902A2 (fr) 1978-11-15 1978-11-15 Dispositif de suspension multidirectionnelle pour giravion

Publications (2)

Publication Number Publication Date
FR2441902A2 true FR2441902A2 (fr) 1980-06-13
FR2441902B2 FR2441902B2 (fr) 1982-07-02

Family

ID=9214928

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7832281A Granted FR2441902A2 (fr) 1978-03-20 1978-11-15 Dispositif de suspension multidirectionnelle pour giravion

Country Status (1)

Country Link
FR (1) FR2441902A2 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2179922A1 (fr) * 2008-10-21 2010-04-28 Agusta S.p.A. Hélicoptère
FR3006022A1 (fr) * 2013-05-21 2014-11-28 Eurocopter France Architecture de montage d'une boite de transmission de puissance d'un giravion, comprenant un dispositif amortisseur de vibrations mettant en oeuvre des amortisseurs lamifies
US10384770B2 (en) * 2014-07-04 2019-08-20 Leonardo S.P.A. Helicopter with noise and vibration damping transmission mounting

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR676215A (fr) * 1928-07-19 1930-02-20 Perfectionnements au montage des moteurs ou d'autres machines rotatives
FR2228662A1 (fr) * 1973-05-08 1974-12-06 Aerospatiale
FR2233227A1 (fr) * 1973-06-13 1975-01-10 United Aircraft Corp

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR676215A (fr) * 1928-07-19 1930-02-20 Perfectionnements au montage des moteurs ou d'autres machines rotatives
FR2228662A1 (fr) * 1973-05-08 1974-12-06 Aerospatiale
FR2233227A1 (fr) * 1973-06-13 1975-01-10 United Aircraft Corp

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2179922A1 (fr) * 2008-10-21 2010-04-28 Agusta S.p.A. Hélicoptère
US8141813B2 (en) 2008-10-21 2012-03-27 Agusta S.P.A. Helicopter
FR3006022A1 (fr) * 2013-05-21 2014-11-28 Eurocopter France Architecture de montage d'une boite de transmission de puissance d'un giravion, comprenant un dispositif amortisseur de vibrations mettant en oeuvre des amortisseurs lamifies
US10384770B2 (en) * 2014-07-04 2019-08-20 Leonardo S.P.A. Helicopter with noise and vibration damping transmission mounting

Also Published As

Publication number Publication date
FR2441902B2 (fr) 1982-07-02

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