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The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Patent No.:

US 9895840 B1

PDFFull Text
Date of Patent:
Feb. 20, 2018

Filed:

May. 15, 2014

Thermoformed cascades for jet engine thrust reversers

Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Aaron William Bartel, Moutlake Terrace, WA (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);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:

Yee & Associates, P.C.

Primary Examiner:

Atul P Khare

Int. Cl.
CPC ...
B29C 43/14 (2006.01); F02K 1/62 (2006.01); B29C 65/00 (2006.01); B29C 53/82 (2006.01); B29C 33/48 (2006.01); B29C 70/34 (2006.01); B29C 33/50 (2006.01); B29C 33/52 (2006.01); B29C 70/08 (2006.01); F02K 1/64 (2006.01); F02K 1/72 (2006.01); F01D 5/28 (2006.01); B29C 43/36 (2006.01); B29L 31/00 (2006.01); B29K 101/12 (2006.01); B29K 105/08 (2006.01); B29K 105/12 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 66/634 (2013.01); B29C 33/485 (2013.01); B29C 33/505 (2013.01); B29C 33/52 (2013.01); B29C 43/14 (2013.01); B29C 53/822 (2013.01); B29C 53/824 (2013.01); B29C 66/494 (2013.01); B29C 70/081 (2013.01); B29C 70/342 (2013.01); F01D 5/282 (2013.01); F02K 1/625 (2013.01); F02K 1/64 (2013.01); F02K 1/72 (2013.01); B29C 2043/3668 (2013.01); B29K 2101/12 (2013.01); B29K 2105/0872 (2013.01); B29K 2105/12 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/737 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01);
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.

Find Patent Forward Citations

Bartel, Aaron. (2018). Thermoformed cascades for jet engine thrust reversers (U.S. Patent No. 9895840). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9895840

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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