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. 30, 2020
Filed:
Oct. 17, 2017
Applicant:
Rohr, Inc., Chula Vista, CA (US);
Inventors:
Pablo T. Sanz Martinez, San Diego, CA (US);
Jihad Ramlaoui, Chula Vista, CA (US);
Assignee:
Rohr, Inc., Chula Vista, CA (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); F02K 1/80 (2006.01); F02K 1/64 (2006.01); B64D 29/06 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); B64D 29/06 (2013.01); F02K 1/64 (2013.01); F02K 1/80 (2013.01); F05D 2220/323 (2013.01); F05D 2240/129 (2013.01); F05D 2260/50 (2013.01);
Abstract
An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure, a thrust reverser and a fan cowl. The thrust reverser includes a forward portion and a translating sleeve. The fan cowl is axially between the nacelle inlet structure and the translating sleeve. The fan cowl axially covers the forward portion of the thrust reverser. The fan cowl is axially structurally tied to the nacelle inlet structure. The fan cowl is radially and circumferentially structurally tied to the forward portion of the thrust reverser.