Title: Method and apparatus for total energy fuel conversion systems
Application Number: 97181618 Application Date: 1997.12.23
Publication Number: 1245480 Publication Date: 2000.02.23
Approval Pub. Date: Granted Pub. Date:
International Classifi-cation: B01D19/00;B63H11/12;C01B31/30;C06D5/00;C07C1/02;C07C4/02;C10J1/20;C21C7/10;F02G1/00
Applicant(s) Name: EGT Developments, LLC Address:
Inventor(s) Name: B. P. Ennis;A. Cirrito
Attorney & Agent: long chuangong
Abstract:
    An independent and conserved source of fuel and/or power comprises a top stage rocket engine firing up to 5000 F at very high pressures, delivering jet flows up to transonic velocities into a near adiabatic tunnel for mixing in general and/or for transforming reactants introduced to suit specific objectives. The related compression is supplied by an independent prime mover which compresses its exhaust and other recoverable fluids. Low grade flows, thereby upgraded in temperature and pressure, are adiabatically contained, are further upgraded in the tunnel to become part of the prescribed fuel for export at the tunnel ends; or fuel to be fired in a prime mover for electric or other power; or hydrogen for chemical use. Expansion turbines for this purpose are relieved of the load used to compress the excess air in standard gas turbines thus increasing export power. A portion of the expansion turbine
Time: 7
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