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Title:
MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM
Document Type and Number:
WIPO Patent Application WO/2017/116613
Kind Code:
A3
Abstract:
A propulsion system includes a first compressor in fluid communication with a fluid source. A first conduit is coupled to the first compressor, and a heat exchanger is in fluid communication with the first compressor via the first conduit. A second conduit is positioned proximal to the heat exchanger. A combustor is in fluid communication with the heat exchanger via the second conduit and is configured to generate a high-temperature gas stream. A third conduit is coupled to the combustor, and a first thrust augmentation device is in fluid communication with the combustor via the third conduit. The heat exchanger is positioned within the gas stream generated by the combustor.

Inventors:
EVULET ANDREI (US)
Application Number:
PCT/US2016/064827
Publication Date:
November 02, 2017
Filing Date:
December 02, 2016
Export Citation:
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Assignee:
JETOPTERA INC (US)
International Classes:
F02C3/04; F02C7/08
Foreign References:
US20100107647A12010-05-06
US2469439A1949-05-10
US20030183723A12003-10-02
US2626501A1953-01-27
US6758653B22004-07-06
US20110094236A12011-04-28
US7284363B22007-10-23
US6918244B22005-07-19
US3011311A1961-12-05
US2946192A1960-07-26
Other References:
See also references of EP 3384141A4
Attorney, Agent or Firm:
BORN, P. G. Scott (US)
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