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:
Jul. 06, 2021

Filed:

Jan. 19, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Mark R. Meyer, Edmonds, WA (US);

Tyler S. Gregson, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16D 3/06 (2006.01); B64C 13/28 (2006.01); F16D 1/108 (2006.01); F16D 3/38 (2006.01); B64C 9/22 (2006.01); B64C 9/16 (2006.01); B64C 13/34 (2006.01); F16D 3/84 (2006.01); F16D 3/41 (2006.01); F16C 3/03 (2006.01); F16D 1/08 (2006.01); B64C 9/00 (2006.01); F16D 1/10 (2006.01);
U.S. Cl.
CPC ...
F16D 3/06 (2013.01); B64C 13/28 (2013.01); F16D 1/108 (2013.01); F16D 3/387 (2013.01); B64C 9/00 (2013.01); B64C 9/16 (2013.01); B64C 9/22 (2013.01); B64C 13/34 (2013.01); F16C 3/03 (2013.01); F16C 2326/43 (2013.01); F16D 1/0847 (2013.01); F16D 3/41 (2013.01); F16D 3/848 (2013.01); F16D 2001/103 (2013.01); F16D 2300/06 (2013.01); Y10T 403/7033 (2015.01);
Abstract

Example torque tube assemblies may be used with aircraft high lift devices. An example torque tube assembly includes a torque tube having a first end and a second end opposite the first end. A first fitting is coupled to the first end and a second fitting is coupled to the second end. The first fitting is to be coupled to a first high lift device of an aircraft. The second fitting has a spline section. The torque tube assembly also includes a sliding spline shaft having a channel and a first yoke. The second fitting is slidably received within the channel. The torque tube assembly further includes a spline coupling having a second yoke, which is coupled to the first yoke of the sliding spline shaft to form a U-joint. The spline coupling is to be coupled to a second high lift device of the aircraft.


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