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.:
Date of Patent:
Jun. 04, 2019
Filed:
Mar. 31, 2016
Applicant:
The Boeing Company, Chicago, IL (US);
Inventors:
Fedor Kleshchev, Seattle, WA (US);
Kyle Thomas, Bellevue, WA (US);
Billy P. Tung, Seattle, WA (US);
Michael Maffeo, Seattle, WA (US);
Robert Shaun Farrell, Seattle, WA (US);
Assignee:
The Boeing Company, Chicago, IL (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16B 5/01 (2006.01); F01D 25/24 (2006.01); F02K 1/54 (2006.01); F16B 5/02 (2006.01); F02C 7/20 (2006.01); B64D 27/12 (2006.01); B64D 29/06 (2006.01); F02K 1/60 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F16B 5/01 (2013.01); B64D 27/12 (2013.01); B64D 29/06 (2013.01); F01D 25/243 (2013.01); F02C 7/20 (2013.01); F02K 1/54 (2013.01); F02K 1/605 (2013.01); F02K 1/766 (2013.01); F16B 5/02 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2250/283 (2013.01); F05D 2260/30 (2013.01); F05D 2260/31 (2013.01); Y02T 50/672 (2013.01);
Abstract
Provided is an aircraft propulsor thrust reverser with a fastening system. The fastening system may include a male spool and a female spool configured to be threaded into the male spool. The male spool and the female spool may be coupled to a honeycomb structure and may evenly distribute force to the honeycomb structure to prevent plastic deformation of a honeycomb core of the honeycomb structure.