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:
Apr. 05, 2016

Filed:

Jan. 17, 2014
Applicant:

Borealis Technical Limited, North Plains, OR (US);

Inventor:

Jonathan Sidney Edelson, North Plains, OR (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16D 41/069 (2006.01); F16D 41/07 (2006.01); B64C 25/44 (2006.01); B60B 27/00 (2006.01); B64C 25/40 (2006.01); F16D 41/14 (2006.01); F16D 27/00 (2006.01); B60B 25/12 (2006.01);
U.S. Cl.
CPC ...
B60B 27/0021 (2013.01); B64C 25/405 (2013.01); F16D 41/14 (2013.01); B60B 25/12 (2013.01); B60Y 2200/51 (2013.01); F16D 27/00 (2013.01);
Abstract

A sprag clutch assembly for an aircraft drive wheel drive system capable of moving an aircraft autonomously on the ground in both forward and reverse directions is provided. The clutch is mounted within an aircraft drive wheel to be operatively engaged to control drive means braking torque when the aircraft is driven in a forward or reverse direction. The clutch assembly includes a plurality of pivoted sprag elements activatable to transmit torque and configured so that ratcheting occurs only when the aircraft drive wheel is driven in a forward direction and a braking torque is applied when the aircraft drive wheel is driven in reverse when the relative speed of the drive system is slower than the drive wheel speed, thereby permitting the drive system drive motor to function as a brake when the clutch assembly is engaged and the aircraft is reversing.


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