DE69216679T2 - Elastisches Verbindungsglied für Aufhängungssystem mit aktiver Regelung - Google Patents

Elastisches Verbindungsglied für Aufhängungssystem mit aktiver Regelung

Info

Publication number
DE69216679T2
DE69216679T2 DE69216679T DE69216679T DE69216679T2 DE 69216679 T2 DE69216679 T2 DE 69216679T2 DE 69216679 T DE69216679 T DE 69216679T DE 69216679 T DE69216679 T DE 69216679T DE 69216679 T2 DE69216679 T2 DE 69216679T2
Authority
DE
Germany
Prior art keywords
connecting rod
phase shifter
section
elastic
sections
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.)
Expired - Lifetime
Application number
DE69216679T
Other languages
German (de)
English (en)
Other versions
DE69216679D1 (de
Inventor
Andre Gennesseaux
Jean-Michel Simon
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.)
Hutchinson SA
Original Assignee
Hutchinson SA
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 Hutchinson SA filed Critical Hutchinson SA
Application granted granted Critical
Publication of DE69216679D1 publication Critical patent/DE69216679D1/de
Publication of DE69216679T2 publication Critical patent/DE69216679T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/001—Vibration damping devices
    • 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
    • F16F13/00—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs
    • F16F13/04—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper
    • F16F13/26—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper characterised by adjusting or regulating devices responsive to exterior conditions
    • F16F13/264—Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs comprising both a plastics spring and a damper, e.g. a friction damper characterised by adjusting or regulating devices responsive to exterior conditions comprising means for acting dynamically on the walls bounding a working chamber
    • 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
    • F16F7/1005—Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass
    • F16F7/1011—Vibration-dampers; Shock-absorbers using inertia effect characterised by active control of the mass by electromagnetic means
    • 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
    • B64C2027/004—Vibration damping devices using actuators, e.g. active systems

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Vibration Prevention Devices (AREA)
  • Fluid-Damping Devices (AREA)
DE69216679T 1991-04-22 1992-04-17 Elastisches Verbindungsglied für Aufhängungssystem mit aktiver Regelung Expired - Lifetime DE69216679T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9104933A FR2675558A1 (fr) 1991-04-22 1991-04-22 Barre elastique de liaison a systeme de controle actif des vibrations.

Publications (2)

Publication Number Publication Date
DE69216679D1 DE69216679D1 (de) 1997-02-27
DE69216679T2 true DE69216679T2 (de) 1997-05-28

Family

ID=9412114

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69216679T Expired - Lifetime DE69216679T2 (de) 1991-04-22 1992-04-17 Elastisches Verbindungsglied für Aufhängungssystem mit aktiver Regelung

Country Status (6)

Country Link
US (1) US5251883A (OSRAM)
EP (1) EP0511055B1 (OSRAM)
JP (1) JPH05149365A (OSRAM)
CA (1) CA2066541A1 (OSRAM)
DE (1) DE69216679T2 (OSRAM)
FR (1) FR2675558A1 (OSRAM)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1994021517A1 (fr) * 1993-03-16 1994-09-29 Mitsubishi Jukogyo Kabushiki Kaisha Helicoptere
WO1995002131A1 (en) * 1993-07-08 1995-01-19 United Technologies Corporation Split tubular elastomer damper
US5558191A (en) * 1994-04-18 1996-09-24 Minnesota Mining And Manufacturing Company Tuned mass damper
CN1066808C (zh) * 1994-04-18 2001-06-06 美国3M公司 谐振质量减振器
US5501434A (en) * 1994-05-10 1996-03-26 Lord Corporation Hybrid fluid and elastomer damper
US5540549A (en) * 1994-08-05 1996-07-30 Lord Corporation Fluid damping devices
FR2731405B1 (fr) * 1995-03-10 1997-05-09 Eurocopter France Systeme pour minimiser l'excitation dynamique d'un helicoptere
US5762295A (en) * 1996-02-23 1998-06-09 Lord Corporation Dynamically optimized engine suspension system
US5884736A (en) * 1997-03-31 1999-03-23 Virginia Tech Intellectual Properties, Inc. Active dual reaction mass absorber for vibration control
US5957440A (en) * 1997-04-08 1999-09-28 Lord Corporation Active fluid mounting
US6092795A (en) * 1997-08-04 2000-07-25 Lord Corporation Fluid and elastomer damper
US8113321B2 (en) * 2006-05-06 2012-02-14 Lord Corporation Helicopter reduced vibration isolator axial support strut
FR2928344B1 (fr) * 2008-03-06 2011-01-21 Hutchinson Dispositif d'amortissement et systeme de rotor d'aerodyne l'incorporant
FR2965850B1 (fr) * 2010-10-11 2012-12-14 Airbus Operations Sas Dispositif de liaison de securite et aeronef equipe d'un tel dispositif de liaison de securite
US8622375B2 (en) * 2012-03-16 2014-01-07 Textron Innovations Inc. Dual frequency damper for an aircraft
US9145946B2 (en) * 2013-03-15 2015-09-29 Bell Helicopter Textron Inc. Active vibration isolation system
EP3350075B1 (en) * 2015-09-14 2021-05-26 LORD Corporation Aircraft support structures, systems, and methods
US10788095B2 (en) * 2017-06-26 2020-09-29 Hrl Laboratories, Llc Fluid and elastomer vibration isolator
US11384964B2 (en) * 2019-07-08 2022-07-12 Cryo Tech Ltd. Cryogenic stirling refrigerator with mechanically driven expander
CN115289312B (zh) * 2022-06-23 2024-08-30 中国船舶重工集团公司第七一九研究所 一种频率可调的复合管路抑振装置
CN116857316A (zh) * 2023-08-03 2023-10-10 武汉理工大学 一种压电叠堆与拉索结合的筒体结构减振装置
CN120194110B (zh) * 2025-04-21 2025-12-30 西北工业大学 一种组合式刚度可调液弹隔振器及其刚度调节方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3319951A (en) * 1965-03-15 1967-05-16 Bendix Corp Flexural pivot device and method of making same
DE2921866A1 (de) * 1979-05-30 1980-12-04 Georg Albersinger Gummi-luftfederelement mit daempfung
DE3009747C2 (de) * 1980-03-14 1983-03-17 Audi Nsu Auto Union Ag, 7107 Neckarsulm Elastisches Lager, insbesondere zur Lagerung einer Brennkraftmaschine in einem Kraftfahrzeug
AU7190981A (en) * 1980-06-22 1982-03-04 Kazuto Seto Vibration isolation type handle device
GB8316419D0 (en) * 1983-06-16 1983-07-20 Dunlop Ltd Spring
US4546960A (en) * 1983-06-20 1985-10-15 Gould Inc. Vibration isolation assembly
GB2149473B (en) * 1983-11-08 1987-03-11 Lucas Ind Plc Actuator system
FR2592696B1 (fr) * 1986-01-09 1989-12-01 Aerospatiale Contre-fiche de rappel elastique a amortissement incorpore, de type hydro-elastique.
JP2693434B2 (ja) * 1986-12-29 1997-12-24 株式会社ブリヂストン サスペンション用減衰力発生装置およびそれの作動制御装置
GB8710998D0 (en) * 1987-05-08 1987-06-10 Btr Plc Vehicle engine suspension systems
FR2629163B1 (fr) * 1988-03-24 1991-01-04 Aerospatiale Contre-fiche de rappel elastique de type elasto-hydraulique a amortissement lineaire incorpore par laminage d'un fluide de viscosite elevee
FR2629545B1 (fr) * 1988-03-30 1993-02-19 Aerospatiale Contre-fiche elastique a resonateur hydro-mecanique integre notamment pour la suspension d'une boite de transmission sur un giravion et dispositif de suspension en comportant application

Also Published As

Publication number Publication date
EP0511055B1 (fr) 1997-01-15
CA2066541A1 (en) 1992-10-23
EP0511055A1 (fr) 1992-10-28
FR2675558B1 (OSRAM) 1995-01-13
FR2675558A1 (fr) 1992-10-23
JPH05149365A (ja) 1993-06-15
DE69216679D1 (de) 1997-02-27
US5251883A (en) 1993-10-12

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