发明名称 Linear actuator for a bleed valve
摘要 In a control system for a turbine engine having a variable geometry air compressor, a valve arrangement responsive to a first operational pressure differential created between a discharge fluid pressure produced by the air compressor and an environmental fluid pressure for controlling the communication of a first fluid pressure to an actuator assembly which responds to a second operational pressure differential created across a piston between the first fluid pressure and a second fluid pressure produced through a modification of the discharge fluid pressure. The second fluid pressure being developed by compressor discharge fluid pressure flowing from a blind bore in a shaft through a variable opening to one side if the piston while at the same time fluid pressure flows through a restriction to the surrounding environment. The resulting second pressure differential acts on the piston to provide the shaft with a force which is communicated through linkage to linearly change the shape of a variable area geometry device of the air compressor.
申请公布号 US5216877(A) 申请公布日期 1993.06.08
申请号 US19920830047 申请日期 1992.01.31
申请人 ALLIED-SIGNAL INC. 发明人 MOORE, JR., ROBERT G.
分类号 F02C9/16;F04D27/02 主分类号 F02C9/16
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