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.

Date of Patent:
Dec. 06, 2022

Filed:

Sep. 29, 2020
Applicant:

Rohr, Inc., Chula Vista, CA (US);

Inventor:

Erik Linde, Coronado, CA (US);

Assignee:

Rohr, Inc., Chula Vista, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 29/00 (2006.01); B64D 29/06 (2006.01); F01D 25/24 (2006.01); F02K 1/82 (2006.01); B64D 27/10 (2006.01); B64D 29/08 (2006.01); F02C 7/20 (2006.01);
U.S. Cl.
CPC ...
B64D 29/00 (2013.01); B64D 29/06 (2013.01); F01D 25/24 (2013.01); F02K 1/822 (2013.01); B64D 27/10 (2013.01); B64D 29/08 (2013.01); F02C 7/20 (2013.01); F05D 2260/30 (2013.01);
Abstract

An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inner structure and a deflection limiter. The nacelle inner structure includes an internal compartment and a cowl. The internal compartment is configured to house a core of a gas turbine engine. The cowl is configured to form an outer radial periphery of the internal compartment. The cowl is also configured to form an outer radial periphery of a compartment exhaust to the internal compartment at an aft end of the cowl. The deflection limiter is attached to the cowl. The deflection limiter is configured to limit radial outward movement of the cowl.


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