发明名称 STATOR VANE ACTUATING MECHANISM
摘要 <p>In a vane actuation system including several actuated stages, unison rings for pairs of stages are actuated in opposite directions. The bell-cranks for actuating the unison rings are all connected to a common carrier wherein the oppositely directed loads substantially balance out so that only the difference is transmitted into the engine casing. The bell-crank actuator is also mounted on the common carrier and therefore none of its loads are transmitted into the engine casing. The common carrier is substantially isolated from the casing by support members which permit the casing to grow and deflect without inducing large stresses in the common carrier.</p>
申请公布号 CA1015277(A) 申请公布日期 1977.08.09
申请号 CA19750221073 申请日期 1975.02.27
申请人 UNITED AIRCRAFT CORPORATION 发明人 NORRIS, JAMES R.;PENDOLEY, FREDERICK M.
分类号 F04D29/56;F01D9/02;F01D17/16;F01D17/20;F02C9/22 主分类号 F04D29/56
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