发明名称 Pop-off valve for an aircraft engine having a turbocharger control system and propeller control system by stepper motor
摘要 A pop-off valve that, in one embodiment, provides overboost protection for an aircraft engine, is described. The pop-off valve includes a housing adapted for connection to a portion of a drive device containing a pressure medium. It also includes a pressure body movably disposed in the housing such that, in operation, a first side of the pressure body is exposed to the pressure medium while a second side is exposed to a reference force. In addition, the pop-off valve incorporates a control device adapted to receive at least one signal concerning at least one operating parameter of the drive device and, in response to the operating parameter signal, to control the reference force. As a result of movement of the pressure body within the housing, at least one first opening in the housing is exposed, permitting venting of the pressure medium.
申请公布号 US7086230(B2) 申请公布日期 2006.08.08
申请号 US20040787247 申请日期 2004.02.27
申请人 BRP-ROTAX GMBH & CO. KG 发明人 BAYERL JOHANN
分类号 F02B33/44;F02B37/00;F02B37/10;F02B37/16;F02B37/18;F02B77/00;F02D23/00;F02D23/02;F03D1/00;F16K17/04 主分类号 F02B33/44
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