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・ Tupolev ANT-2
・ Tupolev ANT-20
・ Tupolev ANT-21
・ Tupolev ANT-22
・ Tupolev ANT-25
・ Tupolev ANT-29
・ Tupolev ANT-3
・ Tupolev ANT-35
・ Tupolev ANT-37
・ Tupolev ANT-41
・ Tupolev ANT-7
・ Tupolev ANT-8
・ Tupolev ANT-9
・ Tupolev DB-1
・ Tupolev I-12
Tupolev I-14
・ Tupolev I-4
・ Tupolev I-8
・ Tupolev MTB-1
・ Tupolev MTB-2
・ Tupolev SB
・ Tupolev TB-1
・ Tupolev TB-3
・ Tupolev TB-6
・ Tupolev Tu-1
・ Tupolev Tu-102
・ Tupolev Tu-104
・ Tupolev Tu-107
・ Tupolev Tu-110
・ Tupolev Tu-114


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Tupolev I-14 : ウィキペディア英語版
Tupolev I-14

The Tupolev I-14 (also designated ANT-31) was a Soviet fighter aircraft of the 1930s. It was a single-engined, single-seater monoplane with a retractable undercarriage and designed to carry a heavy armament, and as such was one of the most advanced fighters of its time. It was ordered into production, but this was cancelled after only a small number had been built, the competing Polikarpov I-16 being preferred.
==Development and design==
In 1932, the Soviet Air Force developed a requirement for a high-speed monoplane fighter to serve alongside agile but slower biplane fighters.〔Gunston 1995, p.301.〕 In order to meet this requirement, the Tupolev design bureau assigned a team led by Pavel Sukhoi. Sukhoi's team came up with the ANT-31, a low-winged monoplane with an unbraced cantilever wing, retractable undercarriage, an enclosed cockpit and a heavy cannon armament. As such, it was one of the most advanced fighters in the world.〔Gunston 1995, p.401.〕
The aircraft had a metal monocoque fuselage, while the wings were of corrugated metal construction. The mainwheels of the conventional landing gear retracted backwards into the wing, being operated by cables driven by a handwheel turned by the pilot. The first prototype was powered by an imported 433 kW (580 hp) Bristol Mercury radial engine enclosed by a NACA cowling and driving a two-bladed wooden propeller. It was armed with a single PV-1 machine gun, with provision for two Kurchevsky APK-37 recoilless autocannon under the wing.〔Gunston 1995, pp. 401–402.〕〔Duffy and Kandalov 1996, p.75.〕
The ANT-31, given the air-force designation I-14 (''Istrebitel'' – fighter), made its maiden flight on 27 May 1933. It proved agile but difficult to handle, and with the supercharged Mercury was underpowered, particularly at low altitude.〔〔 It was therefore decided to build a second prototype, the I-14bis (also known as the ANT-31bis and the I-142 with a more powerful (531 kW (712 kp) Wright Cyclone engine, also imported, an uncorrugated wing and a new undercarriage. The I-14bis demonstrated excellent performance, although handling was still tricky, and an order was placed for production of 55 aircraft, to be powered by the Shvetsov M-25, a licensed version of the Cyclone, and an armament of two 45 mm (1.8 in) Kurchevsky APK-11 recoilless cannons and two ShKAS machine guns.〔〔

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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