| 翻訳と辞書 |
Ikarus C42
The Ikarus C42 is a two-seat, fixed tricycle gear, general aviation microlight airplane, manufactured in Germany by Comco Ikarus. It is used primarily for flight training, touring, and personal flying.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', pages 36-37. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The Ikarus C42 is a single-engined high-wing monoplane with side-by-side seats for two in a wide cabin. The C42 is manufactured with either an Rotax 912 engine or a Rotax 912s engine. The Rotax engine has a low fuel consumption and relatively low noise. The engine drives the propeller, which has ground-adjustable pitch, through a gearbox with a 2.273:1 reduction ratio.
The aircraft is structurally supported by a 'backbone' of large diameter aluminium tube which runs the length of the aircraft. The cabin and fuselage shell is a composite material which, being non-structural, can be removed for inspection and repair.
The wings are constructed of tubular front and rear spars. The wings and flying control surfaces are covered in Kevlar/Mylar/Polyester laminate. The wings can be removed or folded (if an optional folding kit is installed) for storage and transportation. The wing tips are of composite construction which reduces drag and improves low speed handling. Access to the cabin is provided by two Gull-wing doors.
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「Ikarus C42」の詳細全文を読む
スポンサード リンク
| 翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|