FR2363737A1 - Systeme d'isolation de vibrations - Google Patents

Systeme d'isolation de vibrations

Info

Publication number
FR2363737A1
FR2363737A1 FR7726805A FR7726805A FR2363737A1 FR 2363737 A1 FR2363737 A1 FR 2363737A1 FR 7726805 A FR7726805 A FR 7726805A FR 7726805 A FR7726805 A FR 7726805A FR 2363737 A1 FR2363737 A1 FR 2363737A1
Authority
FR
France
Prior art keywords
vibration isolation
isolation system
lever
pivot connection
vibrating mass
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
FR7726805A
Other languages
English (en)
Other versions
FR2363737B1 (fr
Inventor
Rene Augustin Desjardins
Charles Warren Ellis
Vladimir Sankewitsch
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of FR2363737A1 publication Critical patent/FR2363737A1/fr
Application granted granted Critical
Publication of FR2363737B1 publication Critical patent/FR2363737B1/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
    • F16F7/00—Vibration-dampers; Shock-absorbers
    • F16F7/10—Vibration-dampers; Shock-absorbers using inertia effect
    • F16F7/104—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted
    • F16F7/116—Vibration-dampers; Shock-absorbers using inertia effect the inertia member being resiliently mounted on metal springs
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • B64C2027/005—Vibration damping devices using suspended masses
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/21—Elements
    • Y10T74/2121—Flywheel, motion smoothing-type
    • Y10T74/213—Damping by increasing frictional force

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

Système d'isolation de vibrations. Chaque point d'accouplement comprend en plus d'un ressort d'accouplement, un bras de levier lesté d'un poids, relié de manière pivotante à la masse vibrante et au corps, la connexion à pivot entre corps et levier étant située entre le centre de gravité du bras et la connexion à pivot entre masse vibrante et levier. Isolation entre rotor et fuselage d'hélicoptère.
FR7726805A 1976-09-07 1977-09-05 Systeme d'isolation de vibrations Granted FR2363737A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/720,601 US4088042A (en) 1976-09-07 1976-09-07 Vibration isolation system

Publications (2)

Publication Number Publication Date
FR2363737A1 true FR2363737A1 (fr) 1978-03-31
FR2363737B1 FR2363737B1 (fr) 1984-05-04

Family

ID=24894613

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7726805A Granted FR2363737A1 (fr) 1976-09-07 1977-09-05 Systeme d'isolation de vibrations

Country Status (7)

Country Link
US (1) US4088042A (fr)
JP (1) JPS5336899A (fr)
CA (1) CA1067876A (fr)
DE (2) DE2760119C2 (fr)
FR (1) FR2363737A1 (fr)
GB (2) GB1586786A (fr)
IT (1) IT1084440B (fr)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2376342A1 (fr) * 1976-12-29 1978-07-28 Brewer Eng Lab Element d'absorption des vibrations
FR2402808A1 (fr) * 1977-09-13 1979-04-06 Boeing Co Systeme d'isolation des vibrations
EP0006088A2 (fr) * 1978-06-07 1979-12-12 United Technologies Corporation Absorbeur de vibrations à système masse-ressort antagoniste
FR2449593A1 (fr) * 1979-02-26 1980-09-19 Textron Inc Dispositif de suspension du fuselage a la transmission d'un helicoptere
FR2499505A1 (fr) * 1981-02-09 1982-08-13 Aerospatiale Dispositif simplifie de suspension antiresonnante pour helicoptere
FR2503663A1 (fr) * 1981-04-10 1982-10-15 Aerospatiale Dispositif de suspension antivibratoire pour helicoptere
EP0034092B1 (fr) * 1980-02-05 1983-11-02 Aerospatiale Societe Nationale Industrielle Dispositif de suspension antirésonnante pour hélicoptère
FR2749901A1 (fr) * 1996-06-12 1997-12-19 Eurocopter France Dispositif pour reduire les vibrations engendrees par un rotor de sustentation d'un aeronef a voilure tournante
FR2982583A1 (fr) * 2011-11-15 2013-05-17 Eurocopter France Moyen de suspension antivibratoire d'une barre de maintien d'une boite de transmission de puissance d'aeronef, dispositif de suspension antivibratoire, et aeronef

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4365771A (en) * 1979-02-26 1982-12-28 Textron, Inc. Inplane nodalization system
EP0015378B1 (fr) * 1979-03-01 1984-04-25 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Isolateur de vibrations
US4275992A (en) * 1979-04-09 1981-06-30 Textron, Inc. Mode controlled attachment of rotor mounted components
US4430045A (en) 1979-04-24 1984-02-07 Bell Helicopter Textron, Inc. Helicopter power train for distributing rotor blade flapping displacements through a plurality of drive train components
US4311213A (en) * 1979-09-05 1982-01-19 The Boeing Company Vibration isolation system
US4372431A (en) * 1979-11-05 1983-02-08 The Boeing Company Six axis vibration isolation system
US4403681A (en) * 1980-09-30 1983-09-13 The Boeing Company Three directional vibration isolator
US4420134A (en) * 1980-10-27 1983-12-13 Kaman Aerospace Corporation Vibration isolator with crank driven inertia bar
US4405101A (en) * 1980-10-29 1983-09-20 United Technologies Corp. Vibration isolation system
DE3428820C2 (de) * 1984-08-04 1986-11-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Schwingungsisolator
DE3706379A1 (de) * 1987-02-27 1988-09-08 Porsche Ag Aufhaengungssystem fuer ein antriebsaggregat eines hubschraubers
US5687948A (en) * 1995-09-26 1997-11-18 Lord Corporation Vibration isolation system including a passive tuned vibration absorber
US5647726A (en) * 1996-02-15 1997-07-15 Bell Helicopter Textron Inc. Rotor system vibration absorber
DE19711845C2 (de) * 1997-03-21 1999-01-14 Eurocopter Deutschland Mechanischer Schwingungstilger
FR2787762B1 (fr) * 1998-12-29 2001-03-09 Eurocopter France Dispositif de suspension antivibratoire avec ressort en torsion, pour helicoptere
FR2795386B1 (fr) 1999-06-22 2001-11-09 Eurocopter France Dispositif de suspension antivibratoire avec ressorts en torsion entre batteurs et structure, pour helicoptere
US6644590B2 (en) 2000-09-15 2003-11-11 General Dynamics Advanced Information Systems, Inc. Active system and method for vibration and noise reduction
KR100570139B1 (ko) * 2001-09-04 2006-04-12 인터내셔널 비지네스 머신즈 코포레이션 기계적 충격 민감성 저감 장치, 로컬 탐침 저장 장치 및 탐침 이미징 시스템
AU2002311128A1 (en) 2002-06-10 2003-12-22 Canadian Space Agency Vibration control apparatus
US7159317B1 (en) 2003-06-04 2007-01-09 K.D.L. Industries Llc Inner metal link bushing for a vibration isolator and method for forming
US7900873B2 (en) * 2005-11-15 2011-03-08 The Boeing Company Vibration isolation system
US20110148666A1 (en) * 2007-04-04 2011-06-23 Honeywell International, Inc. User interface passive haptic feedback system
FR2933068B1 (fr) * 2008-06-27 2011-02-25 Eurocopter France Pale pour reduire les mouvements en trainee de ladite pale et procede pour reduire un tel mouvement en trainee.
FR2951700B1 (fr) 2009-10-28 2012-04-20 Eurocopter France Mecanisme de filtration des vibrations subies par un equipement d'un appareil volant en mouvement, un giravion notamment
US8534594B2 (en) 2011-04-11 2013-09-17 Gulfstream Aerospace Corporation Vibration isolation system using electrical cables as mass
EP2607232B1 (fr) 2011-12-21 2014-10-29 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Amortisseur de vibrations de train d'atterrissage pour un hélicoptère et procédé de fonctionnement de cet amortisseur de vibrations de train d'atterrissage
CN111038694A (zh) * 2019-12-04 2020-04-21 中国直升机设计研究所 一种新型反共振主减隔振装置
CN112498708B (zh) * 2020-06-01 2022-02-08 重庆宗申航空发动机制造有限公司 一种航空无人机以及航空发动机安装支架
CN112173092B (zh) * 2020-09-25 2023-06-06 中国直升机设计研究所 一种直升机旋翼振动调节系统
US20220144416A1 (en) * 2020-11-08 2022-05-12 Bell Textron Inc. Liquid inertia vibration elimination system with compound period strut

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1855570A (en) * 1928-02-28 1932-04-26 Edison Inc Thomas A Vibration eliminating means
FR1457506A (fr) * 1965-08-25 1966-01-24 Kaman Aircraft Corp Isolateur de vibrations
US3487888A (en) * 1966-08-22 1970-01-06 Mc Donnell Douglas Corp Cabin engine sound suppressor
US3845917A (en) * 1971-10-18 1974-11-05 Textron Inc Helicopter vibration isolation

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1142684A (fr) * 1956-02-15 1957-09-20 Dispositif amortisseur pour véhicules
FR1181260A (fr) * 1957-08-16 1959-06-12 Renault Dispositif amortisseur de vibrations
US3322379A (en) * 1964-11-03 1967-05-30 Kaman Aircraft Corp Dynamic antiresonant vibration isolator
US3467350A (en) * 1967-05-09 1969-09-16 Ntt Enterprises Inc Vibration damping mount
US3514054A (en) * 1967-06-05 1970-05-26 United Aircraft Corp Vibration isolation system
US3857534A (en) * 1972-02-04 1974-12-31 Textron Inc Multi-frequency helicopter vibration isolation
US3858831A (en) * 1973-12-26 1975-01-07 Textron Inc Nodal beam inertial flexure

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1855570A (en) * 1928-02-28 1932-04-26 Edison Inc Thomas A Vibration eliminating means
FR1457506A (fr) * 1965-08-25 1966-01-24 Kaman Aircraft Corp Isolateur de vibrations
US3487888A (en) * 1966-08-22 1970-01-06 Mc Donnell Douglas Corp Cabin engine sound suppressor
US3845917A (en) * 1971-10-18 1974-11-05 Textron Inc Helicopter vibration isolation

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2376342A1 (fr) * 1976-12-29 1978-07-28 Brewer Eng Lab Element d'absorption des vibrations
FR2402808A1 (fr) * 1977-09-13 1979-04-06 Boeing Co Systeme d'isolation des vibrations
EP0006088A2 (fr) * 1978-06-07 1979-12-12 United Technologies Corporation Absorbeur de vibrations à système masse-ressort antagoniste
EP0006088A3 (en) * 1978-06-07 1980-01-09 United Technologies Corporation Tuned spring-mass vibration absorber
FR2449593A1 (fr) * 1979-02-26 1980-09-19 Textron Inc Dispositif de suspension du fuselage a la transmission d'un helicoptere
EP0034092B1 (fr) * 1980-02-05 1983-11-02 Aerospatiale Societe Nationale Industrielle Dispositif de suspension antirésonnante pour hélicoptère
EP0058117A1 (fr) * 1981-02-09 1982-08-18 AEROSPATIALE Société Nationale Industrielle Dispositif simplifié de suspension antirésonnante pour hélicoptère
FR2499505A1 (fr) * 1981-02-09 1982-08-13 Aerospatiale Dispositif simplifie de suspension antiresonnante pour helicoptere
FR2503663A1 (fr) * 1981-04-10 1982-10-15 Aerospatiale Dispositif de suspension antivibratoire pour helicoptere
EP0063078A1 (fr) * 1981-04-10 1982-10-20 AEROSPATIALE Société Nationale Industrielle Dispositif de suspension antivibratoire pour hélicoptère
FR2749901A1 (fr) * 1996-06-12 1997-12-19 Eurocopter France Dispositif pour reduire les vibrations engendrees par un rotor de sustentation d'un aeronef a voilure tournante
US6045090A (en) * 1996-06-12 2000-04-04 Eurocopter Device for reducing the vibrations generated by a lift rotor of a rotary-wing aircraft
FR2982583A1 (fr) * 2011-11-15 2013-05-17 Eurocopter France Moyen de suspension antivibratoire d'une barre de maintien d'une boite de transmission de puissance d'aeronef, dispositif de suspension antivibratoire, et aeronef
EP2594481A1 (fr) 2011-11-15 2013-05-22 Eurocopter Moyen de suspension antivibratoire d'une barre de maintien d'une boîte de transmission de puissance d'aéronef, dispositif de suspension antivibratoire, et aéronef
US8888037B2 (en) 2011-11-15 2014-11-18 Airbus Helicopters Antivibration suspension means for a tie bar of an aircraft power transmission gearbox, an antivibration suspension device, and an aircraft

Also Published As

Publication number Publication date
DE2739617A1 (de) 1978-03-30
IT1084440B (it) 1985-05-25
GB1586785A (en) 1981-03-25
CA1067876A (fr) 1979-12-11
JPH0134839B2 (fr) 1989-07-21
FR2363737B1 (fr) 1984-05-04
GB1586786A (en) 1981-03-25
US4088042A (en) 1978-05-09
DE2760119C2 (de) 1984-10-18
JPS5336899A (en) 1978-04-05
DE2739617C2 (de) 1984-10-04

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