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Phoenix Skyblazer
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Phoenix Skyblazer : ウィキペディア英語版
Phoenix Skyblazer

The Phoenix Skyblazer is an American helicopter that was designed by the Nolan brothers and produced by Phoenix Rotorcraft of Fallston, Maryland and more recently Louisburg, North Carolina. When it was available the aircraft was supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 193. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
While advertised for sale in 2011, by February 2013 the aircraft was no longer listed as being available on the manufacturer's website.〔 By January 2015 the company was offering a new gyroplane using the same name, spelled ''SkyBlazer'', as the previous helicopter design.
==Design and development==
The Skyblazer features two coaxial, contra-rotating main rotors, a single-seat open cockpit without a windshield, skid-type landing gear and two twin-cylinder, air-cooled, two-stroke, dual-ignition Rotax 503 engines for redundancy. The two engines were provided due to the aircraft lacking collective pitch control, thus precluding an autorotation in the event of a power loss. The aircraft can reportedly hover on one engine.〔
The aircraft fuselage is made from welded steel tubing. Its dual two-bladed rotors have diameters of and incorporate dual flapping hinges. Directional control is achieved by tilting the rotor mast. The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload is .〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Phoenix Skyblazer」の詳細全文を読む



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