| 翻訳と辞書 |
| Taggart GyroBee ： ウィキペディア英語版 |
Taggart GyroBee
The Taggart GyroBee is an American autogyro that was designed by Ralph E. Taggart of Michigan State University and made available as free documentation. The aircraft is also produced in kit form by Star Bee Gyros of Worcester, Massachusetts for amateur construction.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 184 and 187. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The GyroBee was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . It features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear and a twin-cylinder, air-cooled, two-stroke, dual-ignition Zanzottera MZ 201 engine in pusher configuration.〔
The aircraft fuselage is made from bolted-together 6061-T6 aluminum tubing. Its diameter Sport Copter rotor has a chord of . With its empty weight of and a gross weight of , it has a useful load of .〔
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「Taggart GyroBee」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.
|
|