发明名称 Gas turbine engine with transmission
摘要 A gas turbine engine with a transmission having a first rotatable member coupled to an engine spool, a second rotatable member coupled to a compressor rotor, and coupled rotatable members defining at least first and second alternate transmission paths between the first and second members. Each transmission path defines a different fixed transmission ratio of a rotational speed of the second member on a rotational speed of the first member.
申请公布号 US9316159(B2) 申请公布日期 2016.04.19
申请号 US201313754045 申请日期 2013.01.30
申请人 PRATT & WHITNEY CANADA CORP. 发明人 Dubreuil Jean;Kenny Stephen
分类号 F02K3/00;F02C7/36 主分类号 F02K3/00
代理机构 Norton Rose Fulbright Canada 代理人 Norton Rose Fulbright Canada
主权项 1. A gas turbine engine comprising: at least one turbine rotor drivingly engaged to an engine spool; a transmission having a rotatable first member coupled to the spool, a rotatable second member, and rotatable coupled members defining at least first and second alternate transmission paths between the first and second members, each transmission path being defined by the coupled members of the respective one of the transmission paths and defining a different fixed transmission ratio of a rotational speed of the second member on a rotational speed of the first member; an actuation mechanism having at least first and second positions, the actuation mechanism in each position drivingly engaging the first and second members to the coupled members of a single respective one of the transmission paths, the actuation mechanism in each position including at least one brake removably engaged with and preventing rotation of one of the coupled members of the respective one of the transmission paths; and at least one compressor rotor coupled to the second member.
地址 Longueuil, Quebec unknown