FR2340482A1 - Multi purpose damper for aircraft undercarriage - has hollow piston incorporating height adjusting piston lockable by clamps when set - Google Patents
Multi purpose damper for aircraft undercarriage - has hollow piston incorporating height adjusting piston lockable by clamps when setInfo
- Publication number
- FR2340482A1 FR2340482A1 FR7603126A FR7603126A FR2340482A1 FR 2340482 A1 FR2340482 A1 FR 2340482A1 FR 7603126 A FR7603126 A FR 7603126A FR 7603126 A FR7603126 A FR 7603126A FR 2340482 A1 FR2340482 A1 FR 2340482A1
- Authority
- FR
- France
- Prior art keywords
- damper
- piston
- damping
- clamps
- height adjusting
- 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
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
- B64C25/60—Oleo legs
-
- 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
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/06—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using both gas and liquid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
- B64C2025/008—Comprising means for modifying their length, e.g. for kneeling, for jumping, or for leveling the aircraft
Abstract
The hydraulic damper for the aircraft undercarriage incorporates gas springs for damping and a hollow control piston (7) in which a second piston moves. The second piston serves to alter the height of the suspension while retaining the damping control. The damper is locked in either setting by mechanical or hydraulic clamps. The damper provides good damping under different conditions, with the damping characteristics varied by control valves. The height of the suspension enables small aircraft, especially helicopters to be air freighted or to sit securely on moving decks etc. The damper also incorporates a crash protection to absorb large impact forces by progressively collapsing.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7603126A FR2340482A1 (en) | 1976-02-04 | 1976-02-04 | Multi purpose damper for aircraft undercarriage - has hollow piston incorporating height adjusting piston lockable by clamps when set |
FR7633261A FR2370196A2 (en) | 1976-02-04 | 1976-11-04 | IMPROVEMENTS TO SHOCK ABSORBERS-CYLINDERS |
IT19663/77A IT1079171B (en) | 1976-02-04 | 1977-01-26 | IMPROVEMENTS TO THE SHOCK ABSORBERS-JACKS |
GB3597/77A GB1563273A (en) | 1976-02-04 | 1977-01-28 | Shock absorber |
DE2703716A DE2703716C2 (en) | 1976-02-04 | 1977-01-29 | Shock absorbers |
US05/765,284 US4088286A (en) | 1976-02-04 | 1977-02-03 | Shock absorber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7603126A FR2340482A1 (en) | 1976-02-04 | 1976-02-04 | Multi purpose damper for aircraft undercarriage - has hollow piston incorporating height adjusting piston lockable by clamps when set |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2340482A1 true FR2340482A1 (en) | 1977-09-02 |
FR2340482B1 FR2340482B1 (en) | 1980-04-04 |
Family
ID=9168764
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7603126A Granted FR2340482A1 (en) | 1976-02-04 | 1976-02-04 | Multi purpose damper for aircraft undercarriage - has hollow piston incorporating height adjusting piston lockable by clamps when set |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2340482A1 (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0003458A1 (en) * | 1978-01-26 | 1979-08-08 | COMMISSARIAT A L'ENERGIE ATOMIQUE Etablissement de Caractère Scientifique Technique et Industriel | Shock absorber for a vehicle with an elastic suspension |
FR2415753A1 (en) * | 1978-01-26 | 1979-08-24 | Commissariat Energie Atomique | Shock absorber for vehicle with elastic suspension - has compensator piston rendered inoperative by valve responsive to deformation velocity |
EP0014660A1 (en) * | 1979-02-06 | 1980-08-20 | Messier-Hispano-Bugatti (S.A) | Shock absorber and shock absorber jack, especially for aircraft under-carriages |
FR2461852A1 (en) * | 1979-07-17 | 1981-02-06 | Messier Hispano Sa | IMPROVEMENTS TO SHOCK ABSORBER AND SHOCK ABSORBER, IN PARTICULAR FOR AERODYNE LANDING TRAINS |
EP0051506A1 (en) * | 1980-10-30 | 1982-05-12 | Messier-Hispano-Bugatti (S.A) | Damper-jack |
FR2530763A1 (en) * | 1982-07-22 | 1984-01-27 | Messier Hispano Sa | Retractable damper. |
FR2537680A1 (en) * | 1982-12-10 | 1984-06-15 | Fokker Bv | DOUBLE ACTION OLEO-PNEUMATIC SHOCK ABSORBER |
WO1988000299A1 (en) * | 1986-06-27 | 1988-01-14 | Jan Kral | Method and device for shock or vibration absorption |
FR2631308A1 (en) * | 1988-05-13 | 1989-11-17 | Israel Aircraft Ind Ltd | RETRACTION DEVICE FOR AIRCRAFT LANDING TRAIN |
US5094407A (en) * | 1989-05-18 | 1992-03-10 | Aerospatiale Societe Nationale Industrielle S.A. | Device for reducing the flexibility of an oleo-pneumatic shock absorber for an undercarriage, and shock absorber and undercarriage including it |
WO1998033371A1 (en) * | 1997-02-03 | 1998-08-06 | Kuhn S.A. | Automatic adjusting for lightening a machine working unit: method, device and machine |
CN101780841A (en) * | 2010-03-10 | 2010-07-21 | 南京航空航天大学 | Landing leg pressing, unfolding and locking device of lander |
EP3392523A1 (en) * | 2017-04-20 | 2018-10-24 | Safran Landing Systems UK Limited | Aircraft landing gear shock absorbing strut |
US11325437B2 (en) * | 2017-04-27 | 2022-05-10 | Oshkosh Defense, Llc | Suspension element lockout |
-
1976
- 1976-02-04 FR FR7603126A patent/FR2340482A1/en active Granted
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0003458A1 (en) * | 1978-01-26 | 1979-08-08 | COMMISSARIAT A L'ENERGIE ATOMIQUE Etablissement de Caractère Scientifique Technique et Industriel | Shock absorber for a vehicle with an elastic suspension |
FR2415753A1 (en) * | 1978-01-26 | 1979-08-24 | Commissariat Energie Atomique | Shock absorber for vehicle with elastic suspension - has compensator piston rendered inoperative by valve responsive to deformation velocity |
EP0014660A1 (en) * | 1979-02-06 | 1980-08-20 | Messier-Hispano-Bugatti (S.A) | Shock absorber and shock absorber jack, especially for aircraft under-carriages |
FR2461852A1 (en) * | 1979-07-17 | 1981-02-06 | Messier Hispano Sa | IMPROVEMENTS TO SHOCK ABSORBER AND SHOCK ABSORBER, IN PARTICULAR FOR AERODYNE LANDING TRAINS |
EP0051506A1 (en) * | 1980-10-30 | 1982-05-12 | Messier-Hispano-Bugatti (S.A) | Damper-jack |
FR2530763A1 (en) * | 1982-07-22 | 1984-01-27 | Messier Hispano Sa | Retractable damper. |
FR2537680A1 (en) * | 1982-12-10 | 1984-06-15 | Fokker Bv | DOUBLE ACTION OLEO-PNEUMATIC SHOCK ABSORBER |
US4593890A (en) * | 1982-12-10 | 1986-06-10 | Fokker Bv | Double acting oleo pneumatic shock absorber |
WO1988000299A1 (en) * | 1986-06-27 | 1988-01-14 | Jan Kral | Method and device for shock or vibration absorption |
FR2631308A1 (en) * | 1988-05-13 | 1989-11-17 | Israel Aircraft Ind Ltd | RETRACTION DEVICE FOR AIRCRAFT LANDING TRAIN |
US5094407A (en) * | 1989-05-18 | 1992-03-10 | Aerospatiale Societe Nationale Industrielle S.A. | Device for reducing the flexibility of an oleo-pneumatic shock absorber for an undercarriage, and shock absorber and undercarriage including it |
WO1998033371A1 (en) * | 1997-02-03 | 1998-08-06 | Kuhn S.A. | Automatic adjusting for lightening a machine working unit: method, device and machine |
FR2758938A1 (en) * | 1997-02-03 | 1998-08-07 | Kuhn Sa | AUTOMATIC ADJUSTMENT OF THE LIGHTENING OF A WORKING UNIT OF A MACHINE: METHOD, DEVICE AND MACHINE |
US6085501A (en) * | 1997-02-03 | 2000-07-11 | Kuhn S.A. | Automatic adjusting for lightening a machine working unit: method, device and machine |
CN101780841A (en) * | 2010-03-10 | 2010-07-21 | 南京航空航天大学 | Landing leg pressing, unfolding and locking device of lander |
CN101780841B (en) * | 2010-03-10 | 2013-07-03 | 南京航空航天大学 | Landing leg pressing, unfolding and locking device of lander |
EP3392523A1 (en) * | 2017-04-20 | 2018-10-24 | Safran Landing Systems UK Limited | Aircraft landing gear shock absorbing strut |
US10577088B2 (en) | 2017-04-20 | 2020-03-03 | Safran Landing Systems Uk Ltd | Aircraft landing gear shock absorbing strut |
US11325437B2 (en) * | 2017-04-27 | 2022-05-10 | Oshkosh Defense, Llc | Suspension element lockout |
US11932068B2 (en) | 2017-04-27 | 2024-03-19 | Oshkosh Defense, Llc | Suspension element lockout |
Also Published As
Publication number | Publication date |
---|---|
FR2340482B1 (en) | 1980-04-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |