发明名称 |
DECELERATION CONTROL CIRCUIT |
摘要 |
<p>DECELERATION CONTROL CIRCUIT A deceleration control circuit for limiting the deceleration rate and applied brake pressure at vehicle speeds below a predetermined level. The invention substantially eliminates strut vibrations in aircraft resulting from "grabby" brakes during a braking operation. The invention includes a deceleration detector, operative at vehicle speeds below a particular level, to produce an output signal to the brake valve driver to reduce brake pressure when the deceleration rate exceeds a specific level. The circuitry is adapted to operate in conjunction with an antiskid system and also includes built-in test circuitry for testing the operability of both the antiskid circuitry and the deceleration control circuitry.</p> |
申请公布号 |
CA1135377(A) |
申请公布日期 |
1982.11.09 |
申请号 |
CA19800348695 |
申请日期 |
1980.03.28 |
申请人 |
GOODYEAR AEROSPACE CORPORATION |
发明人 |
FRETZ, GEORGE C., III |
分类号 |
B60T8/72;B60T8/70;B64C25/42;B64C25/46;(IPC1-7):B60T8/04 |
主分类号 |
B60T8/72 |
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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