发明授权
- 专利标题: Hydraulic system for aircraft
- 专利标题(中): 飞机液压系统
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申请号: US12413818申请日: 2009-03-30
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公开(公告)号: US08038094B2公开(公告)日: 2011-10-18
- 发明人: Hiroki Oyama
- 申请人: Hiroki Oyama
- 申请人地址: JP Tokyo
- 专利权人: Honda Motor Co., Ltd.
- 当前专利权人: Honda Motor Co., Ltd.
- 当前专利权人地址: JP Tokyo
- 代理机构: Rankin Hill & Clark LLP
- 主分类号: B64C13/36
- IPC分类号: B64C13/36 ; B64C25/42
摘要:
A hydraulic system for aircraft operating devices provides a secondary pressure source for direction and deceleration control in case of loss of pressure from a primary pressure source. The system includes multiple pressure accumulators that include a primary accumulator, which supplies pressurized fluid to a first actuator, and first and second secondary accumulators, which supply pressurized fluid to second and third actuators, respectively. If the primary accumulator is disabled, the first secondary accumulator will supply pressurized fluid to the first actuator. If the first secondary accumulator is disabled, the second secondary accumulator will supply pressurized fluid to the second actuator. By providing multiple, substantially independent accumulators, direction and deceleration control is maintained even in the event of loss of the primary accumulator.
公开/授权文献
- US20090242694A1 HYDRAULIC SYSTEM FOR AIRCRAFT 公开/授权日:2009-10-01
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