I-34 (NATO code - «Hermit» – "Hermit") It intended for passenger and freight traffic, and it is also used as a coherent and helicopter patrol. Mi-34 first flight in November 1986 g. A number of variants of the helicopter.
Mi-34S1 – video
Single-rotor helicopter circuit, with tail rotor and ski gear. The fuselage frame construction, made of aluminum alloys with wide use of composite materials, smoothly passes into a conical tail boom to the housing top for the tail rotor shaft. On the left side on the end of the tail boom set swept vertical tail assembly with a T-shaped arrangement of the horizontal tail rectangular planform. In the cab with a big seat arranged in front glass area for annuals with dual control, behind them the general seat for two passengers. On the sides of the cabin, there are two doors four-bladed main rotor, with elastic fastening blades. The sleeve has a horizontal and axial joints and elastic elements, ensuring the movement of the blades in the rotational plane.
MI-34VAZ - with two rotary-piston engine VAZ-430 with a capacity of 162 kW / 220 hp.
The blades are rectangular in plan, made of fiberglass, carbon fiber reinforced. The tail rotor (diameter 1,98 m) bilobed, push. a common horizontal hinge. Power plant the Mi-34 helicopter is a single radial piston engine nine-air cooling in the central portion of the fuselage has a good engine throttle response and immunity to exhaust gas from entering the air inlet, which is very important when performing aerobatics. The fuel system includes a tank capacitance easy 160 L in the central portion of the fuselage beneath the engine and is designed to operate during flight in an inverted position. helicopter mechanical control system, in the cockpit dual control. The equipment consists of a VHF radio, automatic direction finder, altimeter and artificial horizon.
I-34C - modification, equipped in accordance with the certification requirements equivalent to the AP-27 (FAR-27)
modifications
I-34 – Basic modification engine M-14V26V.
Mi-34VAZ – Experienced helicopter with two rotary-piston engine VAZ-426. It converted from previously issued Mi-34.
I-34C – Modification, equipped in accordance with the certification requirements equivalent to the AP-27 (FAR-27).
Mi-34S1 – With the engine M-9FV.
Mi-34C1 engine M-9FV
Performance characteristics of the Mi-34
– First flight: 17 November 1986 of the year
– Getting Started: 1989
– units produced: 27
Mi-34 Crew
– 1-2 man
Capacity Mi-34
– 2-3 man
Overall dimensions of the Mi-34
– Length: 8,851 m (excluding the main and tail rotor)
– The diameter of the rotor: 10,0 m
– The diameter of the tail rotor: 1,48 m
– Height: 2,75 m (through the hub of the rotor)
All Mi-34
– Curb weight: 1137 kg
– Maximum takeoff weight: 1450 kg
– Mass fuel in internal tanks: 131 kg
Motors Mi-34
– Power point: 1 × MI N-14V26V
– engine power: 1 × 325 l. from.
Speed Mi-34
– The maximum permissible speed: 200 kmh (of flight mass at a 1350 kg)
– Cruising speed: 155 kmh (of flight mass at a 1350 kg)
Range Mi-34 flight
– 349 km
Practical ceiling Mi-34
– 4000 m (at takeoff weight 1280 kg)
Static ceiling of the Mi-34
– 900 m
Photo Mi-34
