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
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