FIELD: aircraft engineering. SUBSTANCE: helicopter has fuselage 1, autonomous rotary crew cabin 2 with ejection seats 8 and control system 11 with cable 16, cargo compartment 6, rotor 3, front and aft undercarriages 4 and 5 respectively, canopy 10 and guides 9. The cabin rotates around the longitudinal axis of the helicopter. EFFECT: improved functional efficiency. 2 cl, 5 dwg
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|---|---|---|---|
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|
RU2005656C1 |
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RU2207968C2 |
