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. 02, 1994

Filed:

Jan. 14, 1993
Applicant:
Inventor:

Ronald E Loving, Simi Valley, CA (US);

Assignee:

Hughes Aircraft Company, Los Angeles, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C / ;
U.S. Cl.
CPC ...
60722 ; 60752 ; 431353 ;
Abstract

A liquid fuel power plant (100) including an open-ended combustion chamber (102) and a first mechanism (110) for delivering a combustible fuel to the open-ended combustion chamber (102). A second mechanism (136) is included for igniting the fuel in the open-ended combustion chamber (102). A folded tubular mechanism (140) is provided for extending the length of the combustion chamber (102) to decompose the ignited fuel and to provide an exhaust gas comprised of fundamental elements. Finally, a third mechanism (160) is provided for using the exhaust gas to perform useful work. In a preferred embodiment the liquid fuel power plant (100) includes separate fuel and air inlet lines (110, 120). The air inlet line (120) delivers compressed air, which can be preheated, in an air passageway (130) and thereafter is mixed with the combustible fuel in the open-ended combustion chamber (102). An igniter (136) causes combustion of a compressed air-fuel mixture in an ignition region (118) of the combustion chamber (102). The residue of the combusted air-fuel mixture is thereafter forced by the compressed air into a folded tubular extension (140) which forms a reaction region (152) of the combustion chamber (102). The reaction region (152) becomes sufficiently hot to ensure complete decomposition of the combustible fuel. The hot pressurized exhaust gas, which is very low polluting, is directed by an exhaust tube (150) to a load such as a turbine (160) .


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