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:
Feb. 28, 2017

Filed:

Apr. 22, 2014
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Todd A. Garcia, Mansfield, TX (US);

Carson M. Ingels, Seymour, CT (US);

Jiwoo Lee, McKinney, TX (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64C 27/12 (2006.01); B64C 27/00 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64D 45/0005 (2013.01); B64C 27/008 (2013.01); B64C 27/12 (2013.01); B64C 27/82 (2013.01); B64C 2027/8236 (2013.01);
Abstract

An aircraft is provided and includes an airframe having main, pylon and tail sections, a rotor disposed at one of the pylon and tail sections and rotatable about a rotational axis to drive the airframe and a primary gearbox disposed within the main section of the airframe and a secondary gearbox disposed within one of the pylon and tail sections. The primary gearbox includes an outer housing rotationally fixed relative to the airframe and a driveshaft extending through the outer housing and coupled to the secondary gearbox to thereby drive rotation of the rotor relative to the airframe via the secondary gearbox. The aircraft further including a sensing system affixed to the outer housing and the driveshaft and configured to sense rotational characteristics of the driveshaft.


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