Multiple flow turbojet with adjustable bypass ratio

Details Multiple flow turbojet with adjustable bypass ratio Multiple flow turbojet with adjustable bypass ratio

1980-07-16

1983-03-15

Hart, Douglas

Power plants

Reaction motor

Interrelated reaction motors

60262, F02K 306

Patent

active

043763758

ABSTRACT:
A multiple-flow turbojet with adjustable bypass ratio comprising a low pressure spool and a high pressure spool casing. Aerodynamic surfaces mechanically integral with the high pressure spool are disposed in a cold secondary flow whose characteristics vary as a function of the setting of a guide means and cause a variation in the bypass ratio.

REFERENCES:
patent: 3368352 (1968-02-01), Hewson
patent: 3486328 (1969-12-01), Boudigues
patent: 4054030 (1977-10-01), Pederson

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