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・ Polikarpov I-17
・ Polikarpov I-180
・ Polikarpov I-185
・ Polikarpov I-3
・ Polikarpov I-5
・ Polikarpov I-6
・ Polikarpov ITP
・ Polikarpov Ivanov
・ Polikarpov NB
・ Polikarpov P-2
・ Polikarpov Po-2
・ Polikarpov R-5
・ Polikarpov R-Z
・ Polikarpov SPB (D)
・ Polikarpov TB-2
Polikarpov TIS
・ Polikarpov VIT-1
・ Polikarpov VIT-2
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Polikarpov TIS : ウィキペディア英語版
Polikarpov TIS

The Polkarpov TIS was a heavily armed Soviet heavy fighter designed during the early 1940s. Only two prototypes were built because its intended engines proved to be too unreliable to be placed into production and the engines' manufacturer lacked the resources to fix the problems. The second prototype crashed in September 1944 and the program was canceled after the death of Nikolai Nikolaevich Polikarpov, the chief designer of his eponymous OKB, earlier that year.
==Design and development==
The original request for proposals for a heavy escort fighter (''Tyazholyy Istrebitel' Soprovozhdeniya'') was received at the Polikarpov OKB in November 1938, but the press of work with the I-180 and SPB prototypes prevented any significant design work until the third quarter of 1940. Mikhail Yangel was appointed head designer, but his job was complicated by multiple changes in the role of the aircraft from escort fighter to interceptor, dive bomber, and eventually reconnaissance.〔Gordon 2008, p. 279〕
The prototype, internally designated as aircraft or TIS "A", was a low-wing, all-metal, cantilever monoplane with two Mikulin AM-37 engines and a twin tail. The monocoque fuselage had four ShKAS machine guns in the nose, each with 1,000 rounds. The pilot and the gunner/radio-operator were seated back-to-back, separated by an armor plate, under sliding canopies. The gunner had a dorsal ShKAS on a TSS-1 mount with 750 rounds that could be used once his canopy was slid forward. He also had a ventral ShKAS mounted below the armored floor that he could access by raising a hatch in the floor and kneeling down to fire the machine guns. The ventral gun was provided with 500 rounds of ammunition. A UBK machine gun with 400 rounds and a ShVAK cannon with 350 rounds were mounted in each wing root.〔Gordon 2008, pp. 279–280.〕 Underneath the wings were two racks each capable of carrying a single FAB-500 bomb. The wing had automatic leading edge slats and four split flaps separated by the engine nacelles. The single wheel landing gear retracted into the rear part of the nacelles, as did the tailwheel into the fuselage.〔Gunston 2008, p. 309.〕
The 'A' prototype first flew in September 1941 and reached a speed of at altitude. It suffered from a lack of directional stability and the engines were unreliable and vibrated above . Factory No. 51 attempted to fix the stability problem in late September by increasing the area of the rear fins, but was unsuccessful. Flight testing continued in October in Novosibirsk, to where the LII ((ロシア語:Лётно-исследовательский институт)—Flight Research Institute) had been evacuated. Eliminating the stability problem took until March 1942, although the engines remained as unreliable as ever.〔Gordon 2008, p. 280.〕
By the summer of 1942 it was clear that the Mikulin OKB lacked the resources to fix the problems with the AM-37 and that the TIS would need a new engine, but the OKB's resources were fully utilized on the I-185 and ITP programs and the TIS program was put on hold. Work did not resume on the TIS until the second half of 1943, after the I-185 had been canceled, and the Mikulin AM-39 engine was selected. A new prototype was built, internally called the "MA", with a completely revised armament. Two ShVAK cannon replaced the nose ShKAS machine guns and a UBT machine gun in a VUB-1 mount replaced the dorsal ShKAS, while the ventral machine gun was removed entirely. Two Shpitalny Sh-37 or 111P cannon replaced the wing root guns. The intended AM-39s were unavailable and therefore two Mikulin AM-38Fs were used as a temporary expedient. The engine radiators were moved from the nacelles into the wings.〔 They were fed by inlets in the leading edge and outlets on the undersurface of the wing.〔Gordon 2008, p. 281〕

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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