Power plants – Reaction motor – Intermittent combustion
Reexamination Certificate
2006-01-03
2006-01-03
Kim, Ted (Department: 3746)
Power plants
Reaction motor
Intermittent combustion
C060S039380, C060S039390, C060S771000, C060S039780
Reexamination Certificate
active
06981365
ABSTRACT:
The disclosed device is directed toward a periodic combustion propulsion system. The periodic combustion propulsion system comprises at least one periodic combustion chamber configured to contain periodic combustion and at least one supersonic exhaust nozzle coupled to the at least one periodic combustion chamber. The supersonic exhaust nozzle is configured with a variable exhaust expansion ratio.
REFERENCES:
patent: 2412173 (1946-12-01), Pope
patent: 2611317 (1952-09-01), Africano
patent: 2942412 (1960-06-01), Bollay
patent: 3146589 (1964-09-01), Twyford
patent: 3678692 (1972-07-01), Heise
patent: 4741154 (1988-05-01), Eidelman
patent: 4994660 (1991-02-01), Hauer
patent: 5345758 (1994-09-01), Bussing
patent: 5353588 (1994-10-01), Richard
patent: 5511376 (1996-04-01), Barcza
patent: 5513489 (1996-05-01), Bussing
patent: 5694768 (1997-12-01), Johnson et al.
patent: 5775105 (1998-07-01), Zinsmeyer
patent: 5873240 (1999-02-01), Bussing et al.
patent: 5901550 (1999-05-01), Bussing et al.
patent: 6003301 (1999-12-01), Bratkovich et al.
T. R. Bussing et al., “Practical Implementation of Pulse Detonation Engines”, American Institute of Aeronautics and Astronautics, AIAA 97-2748, 1986.
Kim Ted
Sierra Engineering Incorporated
Sierra Patent Group Ltd.
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