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:
Aug. 30, 2022

Filed:

Jun. 07, 2021
Applicant:

Marvin Engineering Company, Inc., Inglewood, CA (US);

Inventors:

Lee Allen Tobias, Laguna Niguel, CA (US);

Sohrab John Talebian, Beverly Hills, CA (US);

Robert Ronald Evans, Middlesex, GB;

Assignee:

Marvin Engineering Co., Inc., Inglewood, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 1/12 (2006.01); F15B 11/12 (2006.01); F15B 13/02 (2006.01); B64D 1/02 (2006.01); F15B 1/26 (2006.01); F15B 15/16 (2006.01); F16K 27/06 (2006.01); F16K 5/04 (2006.01);
U.S. Cl.
CPC ...
B64D 1/12 (2013.01); B64D 1/02 (2013.01); F15B 11/12 (2013.01); F15B 13/021 (2013.01); F15B 1/26 (2013.01); F15B 15/16 (2013.01); F16K 5/0471 (2013.01); F16K 27/065 (2013.01);
Abstract

An aircraft store ejector systems and subsystems thereof. Embodiments can include a two-reservoir re-pressurization system wherein a remote reservoir is used to maintain desired pressure in a local ejector reservoir. The system can include a release valve having a vent valve and valve piston. The release valve can control release of pressurized gas to a pitch control valve. The pitch control valve can be configured to distribute the pressurized gas between two or more ejector piston assemblies. One or more of the ejector piston assemblies can include multiple concentric piston stages and piston chambers, the piston chambers configured to contain a volume of gas. The ejector piston assemblies can be configured to compress the volume of gas within the piston chambers as the piston stages are extended out from the aircraft. Such compression can provide a return force to the piston stages.


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