US Patent:
20180236720, Aug 23, 2018
Inventors:
- Chicago IL, US
Robert Darel Morrow - Milton WA, US
Alan James Scott - Kent WA, US
Alexandre D. Curaudeau - Kirkland WA, US
Tunde Abiodun Olaniyan - Bothell WA, US
Leonard Joseph England - Seattle WA, US
Randall Dow Wilkerson - O'Fallon MO, US
Robin L. Westberg - Ramona CA, US
International Classification:
B29C 65/00
F02K 1/62
B29C 53/82
F01D 5/28
B29C 70/08
F02K 1/72
B29C 33/52
B29C 33/50
F02K 1/64
B29C 70/34
B29C 33/48
B29C 43/14
B29C 43/36
B29K 105/08
B29K 105/12
B29L 31/30
B29K 101/12
B29L 31/00
Abstract:
A cascade for a jet engine thrust reverser is fabricated by co-consolidating pre-consolidated thermoplastic strongbacks and vanes. The strongbacks are reinforced with continuous fibers, and the vanes are reinforced with discontinuous fibers.