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Aviation of World War II |
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Soviet Gyroplanes in WW II![]() Gyroplane A-7
Double autogyro had an aircraft-type fuselage, a small wing, a power plant with a pulling propeller. The autorotating rotor - braced type, four-bladed - was located above the front cockpit. The blades were attached to the hub using vertical and horizontal hinges. The design of each included a steel tubular spar, a set of wooden ribs, plywood and canvas sheathing. In the future, a similar design was used on all domestic autogyros and the first helicopters, including the Mi-1, Mi-4. The main rotor axis was fixed. Longitudinal and transverse control of the apparatus was carried out using aircraft controls: ailerons, elevators and rudders. The takeoff weight of the device is 930 kg. Subsequently, a more powerful engine of 230 hp was installed on the KASKR-2 autogyro, which made it possible to obtain a maximum speed of 110 km / h. The minimum had an amazing value - 35 km / h! These two types of gyroplanes performed 79 test flights. The A-7 gyroplane became even more advanced Kamov's apparatus. The design of the machine began in 1931 in the section of special designs of TsAGI. The design team was headed by N.I. Kamov. This creative team also included M.L. Mil. A-7 was created according to the terms of reference of the Air Force and was intended for adjusting artillery fire, communications and close reconnaissance. It was also envisaged to use the machine from the ships of the Navy. It was a winged autogyro with a mechanical spin-up of the main rotor before takeoff, which was carried out from the engine with the help of a transmission. The fuselage of the truss structure had two cockpits: the pilot's and the observer's. The low-lying wing folded up at the junction with the center section, which, in combination with the folding blades, ensured the convenience of transporting and storing the apparatus in hangars and on ships. The A-7 had a tricycle landing gear with a nose wheel and an auxiliary tail support. The landing gear was equipped with hydraulic damping. The three-bladed main rotor was located above the fuselage in front of it. The blades were distinguished by the care taken in manufacturing and balancing. Steel spar of elliptical section had three joints. The tail stringer of the blade was cut in three places to ensure that the blade deformation in the plane of rotation was acceptable in flight. The aircraft-type propeller power plant included a fixed-pitch wooden propeller and an M-22 air-cooled engine. The designer paid special attention to the streamlined aerodynamic contours of the airframe. The landing gear and main rotor mounts, as well as the wheels, were covered with fairings. Small arms included a front fixed mount with a PV-1 machine gun for synchronous firing through the propeller rotation plane (500 rounds of ammunition) and a rear turret with a Degtyarev machine gun (12 magazines). Bomb armament provided the suspension of two 250 kg bombs or four 100 kg each. The autogyro had a transceiver station 13 SK-3, later replaced by RSI-3. For planned photography, a PO1TE 1B camera was installed. Tests of the A-7 began in 1934. During them, the following flight data were confirmed: takeoff weight - 2300 kg, crew - 2 people; engine power - 480 hp; full load - 800 kg, maximum speed - 221 km / h; flight duration - 4 hours; take-off run - 28 m, run - 18 m. ![]() For comparison, the data of the Sierva Avra C-40 gyroplane, built in 1938 under the guidance of the first inventor of this apparatus, the Spanish engineer Juan de la Cierva: takeoff weight - 885 kg; crew - 2 people; engine power - 175 hp; full load - 272 kg; maximum speed - 193 km / h. In early 1941, Narkomles and Aeroflot organized an expedition to the foothills of the Tien Shan to prove the possibility of using gyroplanes in forestry and agriculture. The mountain slopes were covered with thousands of hectares of orchards, which suffered from an insect pest - apple moth. The autogyro coped with such tasks as well, if not better than the aircraft. Firstly, the rotorcraft did not need large areas for takeoff and landing; secondly, the air flow from the rotor directed the flow of pesticides straight down, and the efficiency of their application increased. The expedition spent a month in the foothills of the Tien Shan, and even the central press noted the results of its excellent work. The Pravda newspaper wrote about the experiment with a pollinating autogyro: “Participants of the aviation chemical expedition of the timber industry trust of the USSR People's Commissariat of Forests have recently returned to Moscow. The expedition conducted an experience of using a Soviet autogyro designed by engineer Nikolai Kamov to control pests of fruit trees in South Kyrgyzstan. Piloted by pilot Vladimir Karpov, the A-7 went up steeply and, tacking along steep mountain slopes, quickly reached areas inaccessible to aircraft. The device easily maneuvered in narrow valleys, descended into bowl-shaped mountain tracts, turned around at the bottom and rose again. 32 flights were performed by an autogyro ... " Back in the spring of 1940, on the initiative of N. I. Kamov, the first plant of rotary-wing aircraft in the USSR was created at the Ukhtomskaya station. Subsequently, it was from this small enterprise that the Ukhtomsk Helicopter Plant grew, which today bears the name of its creator. Kamov was appointed director of the plant and chief designer, and M. L. Mil became his deputy. In the middle of 1940, the plant began building five A-7-Za military gyroplanes. Pilot Kositz began their tests.
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