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. 09, 2016

Filed:

Apr. 15, 2013
Applicant:

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

Inventors:

Hunter J. Davis, Arlington, TX (US);

Paul B. Sherrill, Grapevine, TX (US);

Robert A. Self, Euless, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/50 (2006.01); B64C 27/00 (2006.01); F01D 5/14 (2006.01); B64C 27/473 (2006.01); B64C 27/48 (2006.01);
U.S. Cl.
CPC ...
F01D 5/147 (2013.01); B64C 27/473 (2013.01); B64C 27/48 (2013.01);
Abstract

The electrical harness system is configured for routing a harness between a rotor yoke and a rotor blade. A recess in an inboard cap member is configured to house a connector and an associated harness. As the recess extends along a radial path in the chordwise direction of the rotor blade, the harness is configured to lie within the recess. Operationally induced centrifugal forces promote positioning the slack of harness within the recess, while the slack in the harness remains available for relative dynamic movements between the rotor blade and the rotor yoke. Such a routing of the harness reduces aerodynamic drag and minimizes damage that could otherwise occur to the harness.


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