翻訳と辞書
Words near each other
・ Zenaga language
・ Zenaida
・ Zenaida and Philonella
・ Zenaida dove
・ Zenaida doves
・ Zenaida Manfugás
・ Zenaida Moya
・ Zenaida Yanowsky
・ Zenaide Vieira
・ Zenair
・ Zenair CH 100
・ Zenair CH 150
・ Zenair CH 200
・ Zenair CH 300
・ Zenair CH 640
Zenair Zipper
・ Zenamorpha
・ Zenamorpha discophoralis
・ Zenana
・ Zenana missions
・ Zenani Mandela-Dlamini
・ Zenarchopteridae
・ Zenarchopterus
・ Zenarchopterus dispar
・ Zenarestat
・ Zenargomyia
・ Zenari
・ Zenas
・ Zenas Beach
・ Zenas Bliss


Dictionary Lists
翻訳と辞書 辞書検索 [ 開発暫定版 ]
スポンサード リンク

Zenair Zipper : ウィキペディア英語版
Zenair Zipper

The Zenair Zipper is a Canadian ultralight high-wing, single seat aircraft that was designed by Chris Heintz and produced by Zenair.
The Zipper is a highly innovative design that strongly emphasizes portability over speed or carrying capacity.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-46. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕
==Development==
The Zipper was designed in the early 1980s by established Canadian aircraft designer Chris Heintz and put into production by his company Zenair, of Midland, Ontario. Heintz's motivation for the Zipper was the ultralight aviation boom that was occurring in Canada at that time and the introduction of new aviation regulations by Transport Canada legally permitting the operation of ultralights.
The Zipper incorporates many unique features, all aimed at making the aircraft more portable. This focus was due the nature of operations in the early days of the ultralight popularity. Aircraft were not flown great distances to fly-ins or other sites, but were transported by trailer or on car top to be flown locally at remote locations.〔
The Zipper has a quick-folding wing, built around a D-cell leading edge and spar. There are no wing ribs and the trailing edge of the wing is established by a cable which tensions the sailcloth wing covering. The wing is folded by releasing the anti-drag cables next to the nosewheel and folding the wings back along the tailboom, still supported by their struts. The wing is designed to +6 and -3 g.〔
The Zipper features conventional three-axis controls, which was unusual in ultralights designed at this time. The all-metal, one piece, all-flying rudder and the elevator are quickly removable for transport. The tailboom is aluminum and square in cross section.〔
The standard powerplants provided with the Zipper kits were the JPX PUL 425 engine of and the Rotax 277 of . Fuel capacity is . The twin-engined Zipper II used a similar engine configuration to its competitor, the Ultraflight Lazair, placing both engines close together to minimize engine-out requirements.〔

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「Zenair Zipper」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.