发明名称 ENGINE HAVING VARIABLE PITCH OUTLET GUIDE VANES
摘要 An aeronautical propulsion device including a fan and a plurality of variable guide vanes is provided. The fan includes a plurality of fan blades for providing a flow of air and the plurality of variable guide vanes are configured for directing air to or from the fan in a desired direction. Each of the plurality of guide vanes defines an inner end along the radial direction and is attached to a housing of the portion device at the inner end in a rotatable manner. The propulsion device further includes a pitch change mechanism positioned in the housing and mechanically coupled to at least one of the plurality of guide vanes for changing a pitch of the at least one of the plurality of guide vanes.
申请公布号 US2017102006(A1) 申请公布日期 2017.04.13
申请号 US201514877210 申请日期 2015.10.07
申请人 General Electric Company 发明人 Miller Brandon Wayne;Becker, JR. Thomas Lee
分类号 F04D29/56;F04D29/54;F04D29/52;F02K3/06;F04D29/32 主分类号 F04D29/56
代理机构 代理人
主权项 1. An aeronautical propulsion device defining a radial direction, the propulsion device comprising: a fan including a plurality of fan blades for providing a flow of air in a flowpath; a plurality of variable guide vanes for directing air to or from the fan in a desired direction, the plurality of guide vanes each defining an inner end and an outer end along the radial direction, the plurality of guide vanes each attached to a housing of the propulsion device at the inner end in a rotatable manner; and a pitch change mechanism positioned within the housing of the propulsion device and mechanically coupled to at least one of the plurality of guide vanes for changing a pitch of the at least one of the plurality of guide vanes.
地址 Schenectady NY US