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. 10, 2026

Filed:

Jan. 09, 2025
Applicant:

Anduril Industries, Inc., Costa Mesa, CA (US);

Inventors:

Dane Chantrill, Irvine, CA (US);

Neil Gupta, Costa Mesa, CA (US);

Jeff Lipari, Long Beach, CA (US);

Assignee:

Anduril Industries, Inc., Costa Mesa, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/02 (2006.01); B64C 3/32 (2006.01); B64C 25/36 (2006.01); B64C 25/58 (2006.01); B64U 10/20 (2023.01); B64U 10/25 (2023.01); B64U 20/50 (2023.01);
U.S. Cl.
CPC ...
B64C 29/02 (2013.01); B64C 3/32 (2013.01); B64C 25/36 (2013.01); B64C 25/58 (2013.01); B64U 10/20 (2023.01); B64U 10/25 (2023.01); B64U 20/50 (2023.01);
Abstract

The present application discloses an aircraft. The aircraft comprises (i) a first wing and a second wing, (ii) a fuselage disposed between the first wing and the second wing, and (iii) a first landing gear system disposed at an aft of the aircraft. The first landing gear system comprises a first leg and a second leg that are configured to at least partially rotate around an axis defined by a length of the first wing when the first leg and the second leg are transitioned to a deployed state or a stowed state. The first landing gear system comprises a first actuation system comprising at least a first actuator and a first shock absorber.


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