DE2715895C2 - Federbein, vorzugsweise für Flugzeugfahrwerke - Google Patents

Federbein, vorzugsweise für Flugzeugfahrwerke

Info

Publication number
DE2715895C2
DE2715895C2 DE19772715895 DE2715895A DE2715895C2 DE 2715895 C2 DE2715895 C2 DE 2715895C2 DE 19772715895 DE19772715895 DE 19772715895 DE 2715895 A DE2715895 A DE 2715895A DE 2715895 C2 DE2715895 C2 DE 2715895C2
Authority
DE
Germany
Prior art keywords
strut
cylinder
oil
pressure
load
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
Application number
DE19772715895
Other languages
German (de)
English (en)
Other versions
DE2715895B1 (de
Inventor
Heinz 2246 Henstedt Fischer
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 Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE19772715895 priority Critical patent/DE2715895C2/de
Priority to FR7809949A priority patent/FR2386427A1/fr
Priority to GB1337878A priority patent/GB1591689A/en
Publication of DE2715895B1 publication Critical patent/DE2715895B1/de
Application granted granted Critical
Publication of DE2715895C2 publication Critical patent/DE2715895C2/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60G—VEHICLE SUSPENSION ARRANGEMENTS
    • B60G17/00—Resilient suspensions having means for adjusting the spring or vibration-damper characteristics, for regulating the distance between a supporting surface and a sprung part of vehicle or for locking suspension during use to meet varying vehicular or surface conditions, e.g. due to speed or load
    • B60G17/015—Resilient suspensions having means for adjusting the spring or vibration-damper characteristics, for regulating the distance between a supporting surface and a sprung part of vehicle or for locking suspension during use to meet varying vehicular or surface conditions, e.g. due to speed or load the regulating means comprising electric or electronic elements
    • B60G17/0152—Resilient suspensions having means for adjusting the spring or vibration-damper characteristics, for regulating the distance between a supporting surface and a sprung part of vehicle or for locking suspension during use to meet varying vehicular or surface conditions, e.g. due to speed or load the regulating means comprising electric or electronic elements characterised by the action on a particular type of suspension unit

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Damping Devices (AREA)
  • Gear Transmission (AREA)
  • Gears, Cams (AREA)
DE19772715895 1977-04-09 1977-04-09 Federbein, vorzugsweise für Flugzeugfahrwerke Expired DE2715895C2 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE19772715895 DE2715895C2 (de) 1977-04-09 1977-04-09 Federbein, vorzugsweise für Flugzeugfahrwerke
FR7809949A FR2386427A1 (fr) 1977-04-09 1978-04-04 Jambe elastique, en particulier pour trains d'atterrissage d'avions
GB1337878A GB1591689A (en) 1977-04-09 1978-04-05 Oleo-leg primarily for an aircraft undercarriage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19772715895 DE2715895C2 (de) 1977-04-09 1977-04-09 Federbein, vorzugsweise für Flugzeugfahrwerke

Publications (2)

Publication Number Publication Date
DE2715895B1 DE2715895B1 (de) 1978-10-05
DE2715895C2 true DE2715895C2 (de) 1979-05-31

Family

ID=6005999

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19772715895 Expired DE2715895C2 (de) 1977-04-09 1977-04-09 Federbein, vorzugsweise für Flugzeugfahrwerke

Country Status (3)

Country Link
DE (1) DE2715895C2 (fr)
FR (1) FR2386427A1 (fr)
GB (1) GB1591689A (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2497896A1 (fr) * 1980-08-29 1982-07-16 Messier Hispano Sa Amortisseur
FR2503055A1 (fr) * 1981-04-02 1982-10-08 Messier Auto Ind Suspension pour vehicule
US4468739A (en) * 1981-11-17 1984-08-28 Woods Lonnie K Computer optimized adaptive suspension system having combined shock absorber/air spring unit
US4722548A (en) * 1981-11-17 1988-02-02 Hamilton James M Computer optimized adaptive suspension system having combined shock absorber/air spring unit
US4634142A (en) * 1983-08-15 1987-01-06 C & K Venture Income I-Coast Computer optimized adaptive suspension system
GB8328373D0 (en) * 1983-10-24 1983-11-23 Lotus Car Vehicle suspension device
US4637574A (en) * 1984-09-14 1987-01-20 Menasco Inc. Attenuating, extendible shock-absorbing strut
DE3434660A1 (de) * 1984-09-21 1986-04-03 Fa. Carl Freudenberg, 6940 Weinheim Luftfeder
DE3500929A1 (de) * 1985-01-12 1986-07-17 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn Flugzeugfahrwerk
DE3842338A1 (de) * 1988-12-16 1990-06-21 Porsche Ag Stellelement fuer ein aktives feder-daempfer-system
FR2647170B1 (fr) * 1989-05-18 1991-08-30 Aerospatiale Dispositif de reduction de la souplesse d'un amortisseur oleo-pneumatique d'atterrisseur, et amortisseur et atterrisseur le comportant
US5529152A (en) * 1994-07-08 1996-06-25 Aimrite Systems International, Inc. Variable constant force hydraulic components and systems
AU1913200A (en) 1998-11-11 2000-05-29 Kenmar Company Trust Suspension control unit and control valve
US9481452B2 (en) 2010-11-22 2016-11-01 The Boeing Company Hydraulic actuator for semi levered landing gear
GB2483734B (en) * 2011-01-24 2013-10-16 Messier Dowty Ltd Landing gear
US8939400B2 (en) 2011-02-21 2015-01-27 The Boeing Company Air-ground detection system for semi-levered landing gear
CN104443369A (zh) * 2014-10-29 2015-03-25 中国商用飞机有限责任公司 起落架缓冲支柱的缓冲装置
CN113023326B (zh) * 2021-03-16 2022-05-31 安徽春华智能科技有限公司 一种便于移动的螺栓冲运输机架
CN113482983B (zh) * 2021-06-30 2023-06-16 三一汽车制造有限公司 支腿油缸油压均衡的控制方法、***及作业机械

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3743222A (en) * 1972-02-17 1973-07-03 Boeing Co Vortex valve shock absorber
US4004762A (en) * 1974-06-06 1977-01-25 Automotive Products Company Limited Aircraft undercarriage with ride control means

Also Published As

Publication number Publication date
DE2715895B1 (de) 1978-10-05
FR2386427A1 (fr) 1978-11-03
GB1591689A (en) 1981-06-24
FR2386427B1 (fr) 1983-09-16

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Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee