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:
Mar. 05, 2019

Filed:

Jan. 19, 2017
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Bruce Bennett Bacon, Fort Worth, TX (US);

Michael Edwin Rinehart, Fort Worth, TX (US);

Thomas Boudreau, Fort Worth, TX (US);

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64C 29/00 (2006.01); F02C 7/20 (2006.01); F16F 15/06 (2006.01); B64C 27/00 (2006.01); B64D 27/00 (2006.01); B64D 29/02 (2006.01); F16B 2/06 (2006.01); B64D 27/10 (2006.01); F16F 1/16 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64C 27/00 (2013.01); B64C 29/0033 (2013.01); B64D 27/00 (2013.01); B64D 27/10 (2013.01); B64D 29/02 (2013.01); F02C 7/20 (2013.01); F16B 2/06 (2013.01); F16F 1/16 (2013.01); F16F 15/063 (2013.01); B64D 2027/262 (2013.01); F05D 2260/36 (2013.01); Y02T 50/672 (2013.01);
Abstract

A rotorcraft, such as a tiltrotor aircraft having helicopter and airplane modes, includes an airframe, an engine and an engine mount assembly for coupling the engine to the airframe. The engine includes an engine lug forming an aperture. The engine mount assembly includes a mount having an aperture substantially aligned with the engine lug aperture. A sleeved bolt assembly extends through the apertures to secure the engine lug to the mount. The sleeved bolt assembly includes a bolt undersized relative to the apertures forming a circumferential gap within the apertures, a sleeve disposed around at least a portion of the bolt substantially filling the circumferential gap and a nut adapted to thread onto a threaded portion of the bolt. The use of the undersized bolt within the sleeve permits increased clearance between the sleeved bolt assembly and the engine while maintaining strength requirements in high load environments.


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