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:
Oct. 01, 2019

Filed:

Apr. 01, 2016
Applicant:

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

Inventor:

Johann S. Schrell, San Diego, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/64 (2006.01); F02K 1/60 (2006.01); F02K 1/76 (2006.01); B64D 29/06 (2006.01); F02K 1/72 (2006.01);
U.S. Cl.
CPC ...
F02K 1/605 (2013.01); B64D 29/06 (2013.01); F02K 1/72 (2013.01); F02K 1/766 (2013.01); F05D 2260/30 (2013.01); F05D 2260/36 (2013.01);
Abstract

A nacelle is provided for an aircraft propulsion system. This nacelle includes a stationary support, a fanlet, a thrust reverser sleeve and an interface assembly providing an interface between the stationary support, the fanlet and the thrust reverser sleeve where the fanlet and the thrust reverser sleeve are respectively in stowed positions. The stationary support extends circumferentially about an axial centerline. The fanlet includes an inlet structure and a fan cowl. The fanlet is configured to translate axially along the centerline. The thrust reverser sleeve is configured to translate axially along the centerline. The interface assembly includes a pair of interlocking components, wherein a first of the interlocking components is mounted to the fanlet at the aft end of the fanlet.


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