King of the Propellers - Kalinin K7

Kalinin K7 potkurit kuningas

Kalinin K-7 (venäjä: Калинин К-7; ukraina: Калінін К-7) oli raskas koelentokone joka suunniteltiin ja testattiin Neuvostoliitossa 1930-luvun alussa.

Se oli hyvin epätavallinen kokoonpano jossa kaksi erillistä puomisto ja suuret siipien alla olevat konsolit matkustajille, kiinteät laskutelineet ja erillisiä konekivääritorneja.

Matkustajaversiossa istuimet oli sijoitettu 2,3 metriä paksujen siipien sisäpuolelelle 
Lentokoneen rungon materiaali oli KhMA, taotusta molybdeeniteräksestä hitsattu.

Alkuperäisessä suunnittelmassa oli kuusi moottoria siiven etureunassa mutta kun ennakoitu lastattu paino ylittyi, kaksi moottoria lisättiin molempien siipien taakse, yksi oikealle ja yksi vasemmalle matkustajien keskikonsolin sivuille.

Nemecek toteaa kirjassaan että koneeseen lisättiin vielä yksi moottori keskikonsolin taakse, potkuri työntävään asentoon

Koneen suunnitteli maailmansodan ja sisällissodan aikaisen lentäjän, Konstantin Kalinin ilmailun suunnittelutoimisto joka sijaitsi Kharkovassa. Koneen siipien kärkiväli oli  lähes sama kuin B-52 pommikoneen ja paljon suurempi siipi pinta-alue.
K-7 on yksi suurimmista koskaan rakennetuista lentokoneista ennen suihkumoottori koneiden aikaa. Siinä oli epätavallinen järjestely, kuusi moottoria siiven etureunassa ja yhden moottori työntämässä keskikonsolin takana.

Tuolloisessa siviilikuljetus tarkoituksessa koneen kapasiteetti olisi ollut tilaa 120 matkustajalle ja 7000 kg (15000 lb) matkatavaralle. Armeijan joukkojen kuljetuskone versiossa olisi ollut kapasiteettia 112 täysin varustettulle laskuvarjojääkärille. 
Pommikone versiossa aseistuksena olisi ollut 8 x 20 mm automaatti tykkiä, 8 x 7,62 mm konekivääriä, ja jopa 9600 kg (21200 lb) pommeja.


K-7 koneita on rakennettu Harkovassa kaksi, vuoden 1931 aikana ja sen jälkeen.
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The Kalinin K-7 (Russian: Калинин К-7; Ukrainian: Калінін К-7) was a heavy experimental aircraft designed and tested in the Soviet Union in the early 1930s. 

It was of unusual configuration with twin booms and large underwing pods housing fixed landing gear and machine gun turrets. In the passenger version, seats were arranged inside the 2.3-meter thick (7 ft 7 in) wings. The airframe was welded from KhMA chrome-molybdenum steel. 

The original design called for six engines in the wing leading edge but when the projected loaded weight was exceeded, two more engines were added to the trailing edges of each wing, one right and one left of the central passenger pod. 
Nemecek states in his book that at first only one further pusher engine was added.
                     
Designed by World War I and civil war pilot Konstantin Kalinin at the aviation design bureau he headed in Kharkov, with a wingspan close to that of a B-52 and a much greater wing area, the K-7 was one of the biggest aircraft built before the jet age. It had an unusual arrangement of six tractor engines on the wing leading edge and a single engine in pusher configuration at the rear.

General characteristics
Crew: minimum 11
Capacity: 120 passengers in civilian configuration
Length: 28 m (91 ft 10 in)
Wingspan: 53 m (173 ft 11 in)
Height: 12.4m (estimated to top of engine shell)
Wing area: 454 m² (4,886.8 ft²)
Empty weight: 24,400 kg (53,793 lb)
Loaded weight: 38,000 kg (83,776 lb)
Powerplant: 7 × Mikulin AM-34F V-12 piston engines, 560 kW (750 hp) each
Maximum speed: 225 km/h (121 knots, 140 mph)
Service ceiling: 4,000 m (13,123 ft)
Wing loading: 84 kg/m² (17 lb/ft²)
Power/mass: 103 W/kg (0.06 hp/lb)

In civil transport configuration, it would have had a capacity for 120 passengers and 7,000 kg (15,000 lb) of mail. As a troop transport it would have had capacity for 112 fully equipped paratroopers. In bomber configuration it would have been armed with 8 x 20mm autocannons, 8 x 7.62mm machine guns and up to 9,600 kg (21,200 lb) of bombs. 

The K-7 was built in two years at Kharkiv starting in 1931.

The K-7 first flew on 11 August 1933. The very brief first flight showed instability and serious vibration caused by the airframe resonating with the engine frequency. The solution to this was thought to be to shorten and strengthen the tail booms, little being known then about the natural frequencies of structures and their response to vibration. The aircraft completed seven test flights before a crash due to structural failure of one of the tail booms on 21 November 1933. 

The existence of the aircraft had only recently been announced by Pravda which declared it was "victory of the utmost political importance" since it had been built with steel produced in the USSR rather than imported. The accident killed 14 people aboard and one on the ground.[6] Flight speculated that sabotage was suspected as the investigating committee had representation by the state security organization, the Joint State Political Directorate (OGPU).

However, there appeared recently some speculation in the Russian aviation press about the role of politics and the competing design office of Andrei Tupolev, suggesting possible sabotage. Although two more prototypes were ordered in 1933, the project was cancelled in 1935 before they could be completed