FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to flight vehicle. Proposed flight vehicle comprises fuselage accommodating gas turbine turbo shaft engine. Air feed inlet nozzle is communicated with gas turbine turbo shaft engine air intake while propulsive jet discharge device is communicated via bearing assembly with rotor hollow shaft that may be revolved with swash plate and rotor. Two arms arranged in opposition and provided with rotary branches with jet nozzles are arranged above rotor in hollow shaft and tightly jointed therewith.
EFFECT: improved flight performances.
1 dwg
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Authors
Dates
2011-06-20—Published
2009-11-26—Filed