BURNER FOR COMBUSTION CHAMBER FIRING Russian patent published in 1994 - IPC

Abstract SU 1720355 A1

FIELD: aircraft engine building. SUBSTANCE: compressed air arrives at annular channel 18 and, upon passing through swirler and diaphragm, is bifurcated; one flow goes to outlet and other one, to inlet of chamber. EFFECT: provision for implementing and maintaining working process using self-combustion of fuel-air mixture. 5 cl, 4 dwg

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SU 1 720 355 A1

Authors

Novikov N.N.

Dates

1994-01-30—Published

1989-11-13—Filed