发明名称 Reverse scissor thrust reverser for a turbine engine
摘要 A turbine engine system includes a nacelle and a thrust reverser. The nacelle includes a first portion and a second portion that are arranged along an axis. The second portion of the nacelle moves axially relative to the first portion of the nacelle. The thrust reverser includes a blocker door and a linkage that links the blocker door to the first portion of the nacelle. The blocker door is located within and pivotally connected to the second portion of the nacelle.
申请公布号 US9518534(B2) 申请公布日期 2016.12.13
申请号 US201313921877 申请日期 2013.06.19
申请人 Rohr, Inc. 发明人 Kusel Curtis M.
分类号 F02K1/72 主分类号 F02K1/72
代理机构 O'Shea Getz P.C. 代理人 O'Shea Getz P.C.
主权项 1. A turbine engine system, comprising: a nacelle including a first portion and a second portion that are arranged along an axis, wherein the second portion of the nacelle moves axially relative to the first portion of the nacelle; and a thrust reverser including a blocker door and a linkage that links the blocker door to the first portion of the nacelle, wherein the blocker door is located within and pivotally connected to the second portion of the nacelle; wherein the linkage comprises a strut, a first end of the strut is directly pivotally connected to the first portion of the nacelle, and a second end of the strut is directly pivotally connected to the blocker door; and wherein a straight-line distance between the first end and the second end is constant as the linkage moves the blocker door.
地址 Chula Vista CA US
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