发明名称 SYSTEM AND APPARATUS FOR A SPLIT CASCADE
摘要 A split cascade comprises a fixed portion and a translating portion. The translating portion may be coupled to, mounted on, or otherwise attached to a translating sleeve of an aircraft nacelle. The fixed portion and the translating portion form a cascade assembly, in response to the translating sleeve being in the active position (e.g., when the thrust reverser is active). Moreover, the split cascade provides a smaller overall package when stowed (e.g., when the translating sleeve is in a forward position and seals or joins the nacelle), providing more room in the nacelle for access and equipment.
申请公布号 US2014325957(A1) 申请公布日期 2014.11.06
申请号 US201313888218 申请日期 2013.05.06
申请人 ROHR, INC. 发明人 Aten Michael
分类号 F02K1/70 主分类号 F02K1/70
代理机构 代理人
主权项 1. A cascade assembly for installation in an aircraft nacelle, comprising: a first cascade portion fixed to a non-movable portion of the nacelle, wherein the first cascade portion comprises a bracket; and a second cascade portion fixed to a translating sleeve portion of the nacelle, wherein the second cascade portion comprises a catch, wherein the bracket is configured to receive the catch, in response to the translating sleeve being in a deployed position.
地址 Chula Vista CA US