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. 25, 2016

Filed:

Sep. 14, 2012
Applicants:

Jonathan Sidney Edelson, Portland, OR (US);

Rodney T. Cox, North Plains, OR (US);

Nechama Cox, Baltimore, MD (US);

Isaiah W. Cox, Baltimore, MD (US);

Inventors:

Jonathan Sidney Edelson, Portland, OR (US);

Rodney T. Cox, North Plains, OR (US);

Nechama Cox, Baltimore, MD (US);

Isaiah W. Cox, Baltimore, MD (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/40 (2006.01); H02K 9/19 (2006.01); H02K 7/14 (2006.01); B60K 7/00 (2006.01); B60K 1/00 (2006.01); B60K 11/02 (2006.01);
U.S. Cl.
CPC ...
B64C 25/405 (2013.01); B60K 7/0007 (2013.01); H02K 7/14 (2013.01); H02K 9/19 (2013.01); B60K 11/02 (2013.01); B60K 2001/006 (2013.01); B60K 2007/0038 (2013.01); B60K 2007/0092 (2013.01); B60Y 2200/50 (2013.01); B60Y 2200/51 (2013.01); B60Y 2306/03 (2013.01); Y02T 50/823 (2013.01);
Abstract

A system is provided for dissipating heat in an onboard non-engine powered aircraft wheel drive assembly with drive means that power one or more aircraft wheels to drive the aircraft autonomously on the ground without directly using the aircraft engines. The heat dissipation system is integral with a wheel drive assembly mounted substantially completely within a nose or main landing gear wheel. A reservoir mounted outboard or inboard of the wheel drive assembly increases thermal distribution mass and fluidically communicates with wheel drive assembly components to automatically circulate heat transfer fluid between the wheel drive assembly and the reservoir when the operating temperature exceeds a predetermined maximum temperature during aircraft ground travel. The heat dissipating system can be retrofitted in an existing aircraft to improve thermal distribution and prolong wheel drive assembly and drive means operation and useful life.


Find Patent Forward Citations

Loading…