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VTOL Aircraft Phillicopter
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The VTOL Aircraft Phillicopter is a 1970s Australian light utility helicopter designed and built by VTOL Aircraft of Newcastle West, New South Wales.〔
==Design==
Duan A. Phillips began work on design of a two seat helicopter in 1962, and started to build a prototype in 1967. The prototype, the Phillicopter Mark I, was completed and first flew in 1971, powered by a single Rolls-Royce Continental O-200 engine.〔Taylor 1976, pp. 8–9.〕 Phillips set up VTOL Aircraft Pty Ltd in 1971 to construct and develop the Phillicopter.〔Gunston 2005, p. 491.〕 The Phillicopter was granted its Australian type certificate in 1984,〔Taylor 1988, p. 7.〕 and the prototype was modified to represent a pre-production standard.〔Lambert 1993, p. 11.〕
The Phillicopter is a conventional two-seat helicopter with a two-blade rotor powered by a Lycoming O-360 piston engine.〔 It has an enclosed cabin with removable doors and is fitted with dual controls.〔 The open frame fuselage has a two-blade tail rotor at the rear.〔 A 91-litre fuel tank is fitted and an optional 91-litre central tank can be fitted, although this can also be used for crop spraying chemicals rather than fuel.〔 The Phillicopter has a fixed skid type landing gear.〔
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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