词条 | Lioré et Olivier LeO 40 | |||||||||||||||
释义 |
The Lioré et Olivier LeO 40 was a French experimental biplane built by Lioré et Olivier. The two-seat LeO 40 had full span slats fitted to both wings, it was powered by a {{convert|95|hp|kW|0|abbr=on}} Argus engine in Pusher configuration. Only one was built and the design was abandoned. Specifications{{Aircraft specs|ref= |prime units?= |crew= |capacity=2 |length m= |length ft= |length in= |span m= |span ft= |span in= |width m= |width ft= |width in= |height m= |height ft= |height in= |wing area sqm= |wing area sqft= |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |eng1 number=1 |eng1 name=Argus Motoren-built engine |eng1 type= |eng1 kw= |eng1 hp=95 |perfhide=Y |max speed kmh= |max speed mph= |cruise speed kmh= |cruise speed mph= |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |climb rate ms= |climb rate ftmin= }}{{aircontent |see also= |related= |sequence= |similar aircraft= |lists= }} ReferencesNotesBibliography
4 : French experimental aircraft 1930–1939|Lioré et Olivier aircraft|Biplanes|Single-engined pusher aircraft |
|||||||||||||||
随便看 |
|
开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。