FIELD: gas-turbine engine. SUBSTANCE: method for preventing ingress of foreign bodies into engine air intake during take-off and landing of flying vehicle involves blow-out of high-pressure air upstream of air intake and organizing its continuous flow in the form of conical jet along engine axis away from air intake. In this way, reduced amount of high-pressure air is taken off high-pressure condenser for air intake protection. EFFECT: improved efficiency. 1 dwg
Authors
Dates
2000-09-20—Published
1998-12-31—Filed