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:
Sep. 16, 2025

Filed:

Dec. 21, 2022
Applicant:

Wing Aviation Llc, Mountain View, CA (US);

Inventors:

Ray Leung, Fremont, CA (US);

Elizabeth Marshman, San Francisco, CA (US);

Adem Rudin, Mountain View, CA (US);

Assignee:

Wing Aviation LLC, Palo Alto, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64U 60/50 (2023.01); B64C 25/34 (2006.01); B64C 25/62 (2006.01); B64U 10/25 (2023.01);
U.S. Cl.
CPC ...
B64U 60/50 (2023.01); B64C 25/34 (2013.01); B64C 25/62 (2013.01); B64U 10/25 (2023.01);
Abstract

A landing gear assembly for an unmanned aerial vehicle (UAV) includes a shock tower, a pair of leg members, and suspension assemblies. The shock tower is adapted to mount to a frame of a fuselage of the UAV and includes upper and lower end mounts. The leg members are adapted to extend out from opposing sides of the lower end mounts. The leg members are flexible and each include an upper leg section pivotally mounted to the lower end mount and a lower leg section adapted to connect to a ground gear. The suspension assemblies are each mounted to and extend between the upper end mount and a corresponding one of the leg members. The suspension assemblies each include a damper and a spring.


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