| 翻訳と辞書 |
| Robertson B1-RD ： ウィキペディア英語版 |
Robertson B1-RD
The Robertson B1-RD is an American ultralight aircraft that was designed by Glen Bashforth and Bruce Bashforth and produced by the Robertson Aircraft Corporation. The aircraft was supplied as a kit for amateur construction with production starting in June 1982.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page E-4. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕
==Design and development==
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The B1-RD has a standard empty weight of . It has a cable-braced high-wing, single-seat, open cockpit, single engine in tractor engine configuration, and is equipped with conventional landing gear.〔
The aircraft is made from bolted together aluminum tubing with the wings and tail surfaces covered in Dacron sailcloth. Its span wing is cable-braced to a top surface inverted "V" kingpost. The wing is a single-surface airfoil with a double-surface wing covering optional. The controls are conventional three-axis, including Junkers-style flaperons. The main fuselage structure is an aluminum keel tube that runs from the tail, mounts the wings and then the engine at the front. The original standard engines were the Cuyuna 430R and the Cuyuna 215. The landing gear has bungee-suspension on all three wheels and the tailwheel is steerable.〔
Production of the B1-RD was curtailed circa 1984 due to liability concerns.〔
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「Robertson B1-RD」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.
|
|