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:
Apr. 03, 2018

Filed:

Nov. 26, 2013
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Deepak Manohar Kamath, Fairfield, OH (US);

Todd James Buchholz, Maineville, OH (US);

Mehdi Milani Baladi, Cincinnati, OH (US);

Michael Jay Epstein, Mason, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 37/30 (2006.01); F02C 7/236 (2006.01); F02C 3/22 (2006.01); F02C 6/08 (2006.01); F02C 7/224 (2006.01); F02C 9/40 (2006.01);
U.S. Cl.
CPC ...
B64D 37/30 (2013.01); F02C 3/22 (2013.01); F02C 6/08 (2013.01); F02C 7/224 (2013.01); F02C 7/236 (2013.01); F02C 9/40 (2013.01); Y02T 50/672 (2013.01);
Abstract

A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fuel at high pressure through the supply line where the pump is operably coupled to the compressor such that operation of the turbine engine drives the pump and a method for delivering fuel in a fuel system to a turbine engine.


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