Breathing system for hypersonic aircraft

Aeronautics and astronautics – Aircraft power plants

Patent

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B64D 3302

Patent

active

053379756

ABSTRACT:
In an aircraft having an integrated turbo-ramjet engine system for hypersonic flight there is provided an air breathing system having an air intake arrangement which can be selectively functioned to supply air to the turbo-ramjet engine system when the aircraft transitions from a turbo-propulsion mode to a ramjet-propulsion mode and back to a turbo-propulsion mode.

REFERENCES:
patent: 3105661 (1963-10-01), Ferri
patent: 3161379 (1964-12-01), Lane
patent: 3324660 (1967-06-01), Lane et al.
patent: 3347496 (1967-10-01), Opfer, Jr.
patent: 4185457 (1980-01-01), Parker et al.
patent: 4934632 (1990-06-01), Kim

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