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:
Jun. 24, 2025

Filed:

Aug. 15, 2023
Applicants:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Airbus Helicopters, Marignane, FR;

Inventors:

Axel Fink, Donauworth, DE;

Reynaldo Oioli-Neto, Donauworth, DE;

Didier Bertin, Marseilles, FR;

Assignees:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/06 (2006.01); B64C 25/60 (2006.01);
U.S. Cl.
CPC ...
B64C 25/06 (2013.01); B64C 25/60 (2013.01);
Abstract

A non-retractable wheel-type landing gear for a rotorcraft, comprising: at least one wheel; a shock absorber with a circumferential direction, which is connected to the at least one wheel and comprises a shock absorber tube and a shock absorber rod telescopically mounted to the shock absorber tube; a mounting arm extending laterally from the shock absorber tube, the mounting arm being integrally formed with the shock absorber tube and adapted for attachment to a first fitting of a rotorcraft; and a link fixation extending laterally from the shock absorber tube, the link fixation being arranged in the circumferential direction of the shock absorber at an angle in a range from 45° to 120° with respect to the mounting arm and adapted for connection to a second fitting of the rotorcraft.


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