FIELD: aeronautical engineering. SUBSTANCE: tail rotor 7 is arranged inside channel 6 of vane-type straightening apparatus 8 connecting wall of channel with central body 14 embracing the mechanism revolving the propeller. This mechanism is enclosed in casing 17 provided with radial supports 19 with detachable member for connecting the inner flange of central body 14, thus providing for rigid attachment of straightening apparatus 8 in casing 17 and attachment of both of them in channel 6. EFFECT: enhanced efficiency. 25 cl, 16 dwg
Authors
Dates
1997-12-20—Published
1995-05-03—Filed