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. 26, 2024

Filed:

Jul. 25, 2022
Applicant:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Inventors:

Joyel M. Schaefer, Earlville, NY (US);

Michael King, Sauquoit, NY (US);

Brayton Reed, New York Mills, NY (US);

Mark R. Gurvich, Middletown, CT (US);

Assignee:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 3/02 (2006.01); F16D 1/027 (2006.01); F16D 3/72 (2006.01); F16D 1/068 (2006.01);
U.S. Cl.
CPC ...
F16C 3/026 (2013.01); F16C 3/023 (2013.01); F16D 1/027 (2013.01); F16D 3/725 (2013.01); F16C 2208/02 (2013.01); F16C 2226/36 (2013.01); F16C 2326/06 (2013.01); F16C 2326/43 (2013.01); F16D 1/068 (2013.01); F16D 2200/006 (2013.01); F16D 2250/0076 (2013.01); Y10S 138/02 (2013.01); Y10S 285/919 (2013.01);
Abstract

A mechanical system for an aerospace application includes a drive input connected to a first axial end of a first diaphragm member, and a drive output connected to a second axial end of a second diaphragm member. The drive output is an aerospace component. The first and second diaphragm members are formed with two axial ends and at least one undulation extending radially of the axial ends. The at least one undulation is intermediate the ends. A tubular portion connects the first and second diaphragm members. The first and second diaphragm members and the tubular member are formed of fiber reinforced polymer matrix composites. The first and second diaphragm members are connected to axial ends of the tubular member by welding of the axial ends of the tubular portion to one of the inner ends of each of said first and second diaphragm members. The aerospace component is a propeller.


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