Английская Википедия:Guépard II XJ01

Материал из Онлайн справочника
Перейти к навигацииПерейти к поиску

Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English

The Guépard II XJ01 (Шаблон:Trans) is a Belgian autogyro that was designed by Joel Tilquin and produced by Guépard II Team of Boncelles, first flown on 28 May 2009 at the Bois-de-la-Pierre fly-in. Now out of production, when it was available the aircraft was supplied as a kit for amateur construction.[1]

Design and development

The XJ01 is a development of the Guépard AX 02 that was designed by Xavier Averso in the 1980s and first offered as plans in 1987. Tilquin decided not to publish plans and instead offer the updated version as a kit, starting in 2011. The kit provided by Guépard II Team included the fuselage frame but did not include the rotor system, propeller, engine or instruments.[1]

The company seems to have gone out of business at the end of 2015 and kit production ended.[2]

The design features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear without wheel pants and a twin-cylinder, liquid-cooled, two-stroke, dual-ignition Шаблон:Convert Rotax 582 engine in pusher configuration.[1]

The aircraft fuselage is made from bolted-together aluminum tubing. Its two-bladed rotor has a diameter of Шаблон:Convert and a chord of Шаблон:Convert. The aircraft has a typical empty weight of Шаблон:Convert and a gross weight of Шаблон:Convert, giving a useful load of Шаблон:Convert. With full fuel of Шаблон:Convert the payload for the pilot and baggage is Шаблон:Convert.[1]

Specifications (XJ01)

Шаблон:Aircraft specs

See also

References

Шаблон:Reflist

External links

  1. 1,0 1,1 1,2 1,3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 194. Flying Pages Europe SARL, 2015. Шаблон:ISSN
  2. Шаблон:Cite web