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Sikorsky VS-300 : ウィキペディア英語版
Vought-Sikorsky VS-300

The Vought-Sikorsky VS-300 (or S-46) was a single-engine helicopter designed by Igor Sikorsky. It had a single three-blade rotor originally powered by a 75 horsepower (56 kW) engine. The first "free" flight of the VS-300 was on 13 May 1940.〔Munson 1968, p. 111.〕 The VS-300 was the first successful single lifting rotor helicopter in the United States and the first successful helicopter to use a single vertical tail rotor configuration for antitorque. With floats attached, it became the first practical amphibious helicopter.
==Design and development==
Igor Sikorsky's quest for a practical helicopter began in 1938, when as the Engineering Manager of the Vought-Sikorsky Division of United Aircraft Corporation, he was able to convince the directors of United Aircraft that his years of study and research into rotary-wing flight problems would lead to a breakthrough. His first experimental machine, the VS-300, was test flown by Sikorsky on 14 September 1939 tethered by cables. In developing the concept of rotary-wing flight, Sikorsky was the first to introduce a single engine to power both the main and tail rotor systems. The only previous successful attempt at a single-lift rotor helicopter, the Yuriev-Cheremukhin TsAGI-1EA in 1931 in the Soviet Union, used a pair of uprated, Russian-built Gnome Monosoupape rotary engines of 120 hp each for its power.〔(video ).〕〔Savine, Alexandre. ("TsAGI 1-EA." ) ''ctrl-c.liu.se,'' 24 March 1997. Retrieved 12 December 2010.〕 For later flights of his VS-300, Sikorsky also added a vertical aerofoil surface to the end of the tail to assist anti-torque but this was later removed when it proved to be ineffective.〔
The cyclic control was found to be difficult to perfect, and led to Sikorsky locking the cyclic and adding two smaller vertical-axis lifting rotors to either side aft of the tail boom.〔Dorr 2005, p. 32.〕 By varying pitch of these rotors simultaneously, fore and aft control was provided. Roll control was provided by differential pitching of the blades. In this configuration, it was found that the VS-300 could not fly forward easily and Sikorsky joked about turning the pilot's seat around.〔("A National Historic Engineering Landmark: VS-300 Helicopter (1939)." ) Crystal City, Virginia: ''The American Society of Mechanical Engineers, American Helicopter Society,'' 17 May 1984.〕

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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