| 词条 | Bensen B-10 | ||||||||||||||||
| 释义 |
The Bensen B-10 Propcopter was an unconventional VTOL aircraft developed by Igor Bensen in the United States in the late 1950s. The pilot sat astride a beam that had an engine mounted at either end of it, each driving a rotor to provide lift. Each of these rotors was surrounded by a system of four pivotable vanes to direct its downwash, and linked to a control stick for the pilot, this provided control of the craft. Only a single prototype (registered N56U) was built. Specifications{{aerospecs|ref= |met or eng?=eng |crew=1 pilot |capacity= |length m= |length ft= |length in= |span m= |span ft= |span in= |swept m= |swept ft= |swept in= |rot number=2 |rot dia m=1.20 |rot dia ft=4 |rot dia in=0 |dia m= |dia ft= |dia in= |width m= |width ft= |width in= |height m= |height ft= |height in= |wing area sqm= |wing area sqft= |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |lift kg= |lift lb= |eng1 number=2 |eng1 type=McCulloch piston engines |eng1 kw=54 |eng1 hp=72 |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= |perfhide=Y |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= }} See also{{aircontent|related= |similar aircraft=
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}} References{{commons category|Bensen aircraft}}
3 : United States experimental aircraft 1950–1959|VTOL aircraft|Bensen aircraft |
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