发明名称 |
Active hydraulic control pressure system for adverse g flight conditions |
摘要 |
<p>An hydraulic control system for an integrated drive generator (10) includes in flow series arrangement, a scavenge pump (32), a spool valve (50) and a boost pump (44). When the spool valve detects an interruption in the supply pressure to the boost pump due to an adverse "g" condition, it reconfigures the system to a closed loop system. In this mode, the oil returning from the CVT (14) is re-circulated back to the boost pump instead of back to the scavenge pump. A small accumulator (42) of oil is used to make up for leakage in the system. <IMAGE></p> |
申请公布号 |
EP1111273(A2) |
申请公布日期 |
2001.06.27 |
申请号 |
EP20000122991 |
申请日期 |
2000.10.23 |
申请人 |
HONEYWELL INTERNATIONAL, INC. |
发明人 |
LANGSTON, TODD;SALAFIA, DON |
分类号 |
F15B1/26;F16H57/04;F16H61/40;F16H61/4139;F16H61/4148;F16H61/4183;(IPC1-7):F16H61/40 |
主分类号 |
F15B1/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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