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.

Patent No.:

US 9815549 B1

PDF
Full Text
Expired
Date of Patent:
Nov. 14, 2017

Filed:

May. 03, 2017
Applicant:

Ali A. A. J. Shammoh, Safat, KW;

Inventor:
Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/30 (2006.01); B64C 25/34 (2006.01); B64C 25/22 (2006.01); B64C 25/12 (2006.01); B64C 25/60 (2006.01); F15B 15/10 (2006.01);
U.S. Cl.
CPC ...
B64C 25/30 (2013.01); B64C 25/12 (2013.01); B64C 25/22 (2013.01); B64C 25/34 (2013.01); B64C 25/60 (2013.01); F15B 15/10 (2013.01); B64D 2201/00 (2013.01);
Abstract

The emergency landing gear actuator for aircraft utilizes a pair of airbags for rapid emergency deployment of landing gear when the conventional hydraulic actuator fails. In the retracted position, the at least one wheel of the landing gear is stored in a first cavity formed in the lower portion of the wing. The shock strut and the side strut are stored in an adjacent second cavity formed in the lower portion of the wing. First and second airbags are respectively mounted in the first and second cavities. The first airbag and the second airbag are each selectively inflatable for emergency deployment of the at least one wheel, the shock strut and the side strut. When the hydraulic actuator fails to deploy the landing gear, the first and second airbags are inflated, forcing the shock strut to rotate and position the at least one wheel in its deployed position.


Find Patent Forward Citations

Shammoh, Ali A. A. J.. (2017). Emergency landing gear actuator for aircraft (U.S. Patent No. 9815549). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9815549

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