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 |