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:
Nov. 17, 2015

Filed:

Nov. 12, 2012
Applicants:

Mark R. Plickys, Unionville, CT (US);

Paul A. Carvalho, Hadley, MA (US);

Inventors:

Mark R. Plickys, Unionville, CT (US);

Paul A. Carvalho, Hadley, MA (US);

Assignee:

Hamilton Sundstrand Corporation, Windsor Locks, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01P 7/06 (2006.01); F01D 25/02 (2006.01); B64D 15/12 (2006.01); B64C 11/02 (2006.01); B64D 35/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/02 (2013.01); B64C 11/02 (2013.01); B64D 15/12 (2013.01); B64D 35/00 (2013.01);
Abstract

A propeller system for an aircraft includes a propeller assembly rotatable about a central axis and a reduction gearbox operably connected to the propeller assembly via a propeller shaft. An electrical power transfer system is positioned such that the gearbox is located axially between the electrical power transfer system and the propeller assembly. The electrical power transfer system includes a slip ring assembly operably connected to an oil transfer tube extending to the propeller assembly and a brush block interactive with the slip ring assembly to transfer electrical power to a plurality of lead wires extending from the slip ring assembly to the propeller assembly. The brush block is positioned such that brush block tips of the brush block extend toward the slip ring assembly in a substantially axial direction relative to the central axis.


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