发明授权
US5004215A Resilient return strut of the elastic-hydraulic type with incorporated
linear damping by throttling a high-viscosity fluid
失效
通过节流高粘度流体,弹性液压型回弹支撑弹性回弹支撑结合线性阻尼
- 专利标题: Resilient return strut of the elastic-hydraulic type with incorporated linear damping by throttling a high-viscosity fluid
- 专利标题(中): 通过节流高粘度流体,弹性液压型回弹支撑弹性回弹支撑结合线性阻尼
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申请号: US525301申请日: 1990-05-17
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公开(公告)号: US5004215A公开(公告)日: 1991-04-02
- 发明人: Jacques A. Aubry , Jean J. Mondet
- 申请人: Jacques A. Aubry , Jean J. Mondet
- 申请人地址: FRX Paris
- 专利权人: Societe Nationale Industrielle et Aerospatiale
- 当前专利权人: Societe Nationale Industrielle et Aerospatiale
- 当前专利权人地址: FRX Paris
- 优先权: FRX8803880 19880324
- 主分类号: B64C27/51
- IPC分类号: B64C27/51 ; F16F9/52 ; F16F13/08 ; F16F13/18
摘要:
The resilient return strut is of the elastic-hydraulic type with incorporated linear damping by throttling a high-viscosity fluid, and comprises a damper (1) mounted between two return springs (2, 3) in elastomer-based sleeves (17, 18), undergoing a shearing action and sealing the chambers (34, 35) set off within the body of the damper (12) by a transverse wall (10) which marks off a permanent throttling passage around a central brace (23). Limiting valves equipped with spring-leaves (45) sealing the holes (40) bored in the wall (10) increase the throttling section. A compressed-air system (52), mounted in a spring (2), compensates for thermal expansion of the fluid. The device is used with helicopter rotors.
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