Integrated bypass turbojet engines for air craft and other...

Power plants – Reaction motor – Interrelated reaction motors

Reexamination Certificate

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C060S039430, C060S224000, C060S269000

Reexamination Certificate

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06966174

ABSTRACT:
Turbojet engines and aircraft configurations for advantageous use of the turbojet engines; the turbojet engines utilizing ram air turbine units that centrifugally compress air isothermally for use in various combustion configurations designed for stoichiometric combustion, wherein a stream of by-pass ram-air jets is mixed with combustion gas jets for discharge in a common discharge nozzle.

REFERENCES:
patent: 2404767 (1946-07-01), Heppner
patent: 2514874 (1950-07-01), Kollsaman
patent: 2611241 (1952-09-01), Schultz
patent: 2694291 (1954-11-01), Rosengart
patent: 3112610 (1963-12-01), Jerger
patent: 3269120 (1966-08-01), Sabatiuk
patent: 3283509 (1966-11-01), Nitsch
patent: 3603082 (1971-09-01), Sneeden et al.
patent: 3606210 (1971-09-01), Busby
patent: 3705775 (1972-12-01), Rioux
patent: 3892069 (1975-07-01), Hansford
patent: 4845941 (1989-07-01), Paul
patent: 4860537 (1989-08-01), Taylor
patent: 5003766 (1991-04-01), Paul
patent: 5177954 (1993-01-01), Paul
patent: 5341636 (1994-08-01), Paul

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