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:
Mar. 06, 2012

Filed:

Sep. 17, 2008
Applicants:

Gary Lynwood Gisler, Granbury, TX (US);

Porter Davis, Anthem, AZ (US);

Roger Nagel, Peoria, AZ (US);

Dennis Wayne Smith, Phoenix, AZ (US);

Inventors:

Gary Lynwood Gisler, Granbury, TX (US);

Porter Davis, Anthem, AZ (US);

Roger Nagel, Peoria, AZ (US);

Dennis Wayne Smith, Phoenix, AZ (US);

Assignee:

Honeywell International Inc., Morristown, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 19/16 (2006.01); G01C 19/20 (2006.01); G01C 19/38 (2006.01); G01C 19/54 (2006.01); G01C 19/06 (2006.01); G01C 19/34 (2006.01);
U.S. Cl.
CPC ...
Abstract

A rotor assembly is provided for deployment within the inner gimbal assembly of a control moment gyroscope (CMG). In one embodiment, the rotor assembly includes a rotor shell, a rotor shaft fixedly coupled to the rotor shell, and a rotor rim. The rotor rim includes an annular body and a strain relief member. A first end portion of the strain relief member is fixedly coupled to the annular body, and a second end portion of the strain relief member is fixedly coupled to the rotor shell to form a rim-shell joinder interface. The strain relief member has a flexibility sufficient to reduce the mechanical stress experienced by the rim-shell joinder interface during operation of the CMG.


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