公开(公告)号：US10823112B2

公开(公告)日：2020-11-03

申请号：US15605120

申请日：2017-05-25

申请人： THE BOEING COMPANY

发明人： Naimishkumar Harpal ,  Chen Chuck ,  Zachariah VanDeMark ,  Tunde A. Olaniyan ,  Minkoo Han

IPC分类号： F02K1/54 ,  F02K1/72 ,  F02K1/80 ,  F02K1/64

摘要： A method for manufacturing a cascade for a thrust reverser for a jet engine includes forming a strip assembly. The strip assembly includes a strong back member which includes a length. The strip assembly includes a plurality of first vane members which extend from a first side of the strong back member in a first direction nonparallel relative to the length of strong back member wherein the plurality of the first vane members are spaced apart from one another along the length of the strong back member.

公开(公告)号：US20180340492A1

公开(公告)日：2018-11-29

申请号：US15605120

申请日：2017-05-25

申请人： THE BOEING COMPANY

发明人： Naimishkumar Harpal ,  Chen Chuck ,  Zachariah VanDeMark ,  Tunde A. Olaniyan ,  Minkoo Han

IPC分类号： F02K1/54

CPC分类号： F02K1/54 ,  F02K1/64 ,  F02K1/72 ,  F05D2230/51 ,  F05D2230/60 ,  F05D2240/129 ,  F05D2240/40

摘要： A method for manufacturing a cascade for a thrust reverser for a jet engine includes forming a strip assembly. The strip assembly includes a strong back member which includes a length. The strip assembly includes a plurality of first vane members which extend from a first side of the strong back member in a first direction nonparallel relative to the length of strong back member wherein the plurality of the first vane members are spaced apart from one another along the length of the strong back member.