发明名称 VOLUME COMPENSATED FLUID MOUNT
摘要 VOLUME COMPENSATED FLUID MOUNT A fluid mount particularly suited for mounting an engine in an aircraft. The mount includes a frame which is fastened to the engine and a support movably mounted in the frame and adapted to receive a wing pylon stub shaft. Opposed liquid-filled chambers are provided on opposite sides of the stub shaft support and are fluidly interconnected by an elongate tube. An auxiliary chamber is provided on the frame adjacent to the upper liquid chamber and is divided internally into a gas-filled portion and a liquid-filled portion which is in communication with the upper liquid chamber via an orifice. The auxiliary chamber accommodates changes in liquid volume without adversely affecting either the static or dynamic performance of the mount. 28
申请公布号 CA1320711(C) 申请公布日期 1993.07.27
申请号 CA19880574034 申请日期 1988.08.05
申请人 LORD CORPORATION 发明人 JONES, PETER J.
分类号 F16F13/00;B64D27/18;B64D27/26;F01D25/28;F02C7/20;F16F13/04;F16F13/08;F16F13/26 主分类号 F16F13/00
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