| 词条 | Borel Torpille | |||||||||||||||
| 释义 |
The Borel Torpille (French: "Torpedo") was a French single-engine single-seat aircraft built in 1913. Design and developmentThe Torpille had a wire-braced monoplane wing attached to a monocoque fuselage. The streamlined fuselage was the basis for the plane's appellation. Its powerplant was a {{cvt|50|hp}} rotary engine. Operational historyPierre Daucourt used the Torpille to compete in the 1913 Coupe Pommery. He flew it in the first leg of the 1913 competition, and later used it in an attempt to reach Egypt by air. Specifications{{aerospecs|met or eng?=met |crew=one, pilot |capacity= |length m=5.80 |length ft=19 |length in=0 |span m=8.00 |span ft=26 |span in=3 |dia m= |dia ft= |dia in= |height m=2.35 |height ft=7 |height in=8 |wing area sqm= |wing area sqft= |rot area sqm= |rot area sqft= |aspect ratio= |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |eng1 number=1 |eng1 type=Gnome rotary |eng1 kw=37 |eng1 hp=50 |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh= |max speed mph= |max speed mach= |cruise speed kmh= |cruise speed mph= |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} References
See also{{aircontent|related= |similar aircraft= |sequence= |lists= |see also= }}{{Borel aircraft}}{{aero-1910s-stub}} 7 : French sport aircraft 1910–1919|Racing aircraft|Mid-engined aircraft|Single-engined pusher aircraft|Rotary-engined aircraft|Borel aircraft|Aircraft first flown in 1913 |
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