GB768698A - Improvements in or relating to shock absorbers for aircraft - Google Patents
Improvements in or relating to shock absorbers for aircraftInfo
- Publication number
- GB768698A GB768698A GB13160/54A GB1316054A GB768698A GB 768698 A GB768698 A GB 768698A GB 13160/54 A GB13160/54 A GB 13160/54A GB 1316054 A GB1316054 A GB 1316054A GB 768698 A GB768698 A GB 768698A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ports
- damping
- liquid
- spring
- head
- 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
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
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/50—Special means providing automatic damping adjustment, i.e. self-adjustment of damping by particular sliding movements of a valve element, other than flexions or displacement of valve discs; Special means providing self-adjustment of spring characteristics
- F16F9/512—Means responsive to load action, i.e. static load on the damper or dynamic fluid pressure changes in the damper, e.g. due to changes in velocity
-
- 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
- F16F9/32—Details
- F16F9/50—Special means providing automatic damping adjustment, i.e. self-adjustment of damping by particular sliding movements of a valve element, other than flexions or displacement of valve discs; Special means providing self-adjustment of spring characteristics
- F16F9/512—Means responsive to load action, i.e. static load on the damper or dynamic fluid pressure changes in the damper, e.g. due to changes in velocity
- F16F9/5126—Piston, or piston-like valve elements
-
- 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
- B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface specially adapted for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Damping Devices (AREA)
Abstract
768,698. Liquid springs. BRITISH MESSIER, Ltd. April 12, 1955 [May 5, 1954], No. 13160/54. Class 108(3). A shock absorber comprises a cylinder completely filled with liquid in which works a plunger 23 carrying a damping head 25, and having ports 46, 47, connecting opposed sides of the head 25, and a control member 48 for the ports 46, 47, such as to afford, " linear " damping to slow loadyielding movements of the plunger, and a greater rate of damping for more rapid load-yielding movements. The control member 48 comprises spaced pistons 40, 53 operating in a con centric bore 45 of the plunger 23 disposec between the ports 46 47. The control mem ber 48 also carries a valve head 41 which is loaded by the action of a spring 52 to seat in the mouth of the port 47. The head 41 is formed with ports 61 covered by a valve plate 43 under the action of a spring 44. In operation, on slow compression movement, the valve plate 43 is lifted against the action of the spring 44 and liquid flows through the ports 61 with, " linear " damping. The liquid then flows through ports 50 in the piston 40 of the control member 48 and out through ports 46 to the space below the damping piston 25. On more rapid compression movement, the control member 48 is moved downwardly against the pressure of the spring 52 and damping flow occurs through the ports 50 according to a " square law." On rebound, liquid flows from below the piston 25 to above, via ports 54, under the control of a non-return valve formed by a coiled strip 55. A cylinder 20 is filled with liquid at super-atmospheric pressure through a screw plug 60. The invention may be applied to a helicopter undercarriage similar to that described in Specification 745,915.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13160/54A GB768698A (en) | 1954-05-05 | 1954-05-05 | Improvements in or relating to shock absorbers for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13160/54A GB768698A (en) | 1954-05-05 | 1954-05-05 | Improvements in or relating to shock absorbers for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB768698A true GB768698A (en) | 1957-02-20 |
Family
ID=10017968
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13160/54A Expired GB768698A (en) | 1954-05-05 | 1954-05-05 | Improvements in or relating to shock absorbers for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB768698A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0122731A1 (en) * | 1983-04-08 | 1984-10-24 | WESTLAND plc | Suspension damper for helicopter undercarriage and helicopter incorporating same |
GB2191843A (en) * | 1986-06-12 | 1987-12-23 | Hollingsworth Uk Ltd | Vibration damper |
US11187299B1 (en) * | 2021-03-30 | 2021-11-30 | Ningbo Fenghua Rising New Energy Technology Co., Ltd. | Bidirectional self-locking damper |
AU2021277686B2 (en) * | 2021-03-30 | 2023-08-03 | Ningbo Fenghua Rising New Energy Technology Co., Ltd | Bidirectional self-locking damper |
-
1954
- 1954-05-05 GB GB13160/54A patent/GB768698A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0122731A1 (en) * | 1983-04-08 | 1984-10-24 | WESTLAND plc | Suspension damper for helicopter undercarriage and helicopter incorporating same |
GB2191843A (en) * | 1986-06-12 | 1987-12-23 | Hollingsworth Uk Ltd | Vibration damper |
GB2191843B (en) * | 1986-06-12 | 1989-12-20 | Hollingsworth Uk Ltd | Vibration damper |
US11187299B1 (en) * | 2021-03-30 | 2021-11-30 | Ningbo Fenghua Rising New Energy Technology Co., Ltd. | Bidirectional self-locking damper |
EP4040009A4 (en) * | 2021-03-30 | 2023-01-11 | Ningbo Fenghua Rising New Energy Technology Co., Ltd. | Bidirectional self-locking damper |
AU2021277686B2 (en) * | 2021-03-30 | 2023-08-03 | Ningbo Fenghua Rising New Energy Technology Co., Ltd | Bidirectional self-locking damper |
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