词条 | Brantly B-1 | |||||||||||||||||
释义 |
The Brantly B-1 was a 2-seat, coaxial-rotor helicopter designed by Newby O. Brantly and constructed by the Pennsylvania Elastic Company, Brantly's employer. Design and developmentIn 1946, Brantly started flight testing the B-1 prototype (NX69125), which used a 150 hp Franklin O-335 engine in the fabric fuselage and two three-bladed rotors that rotated at 320 rpm and were fitted coaxially. The collective, cyclic, and differential controls were enclosed in the rotor hubs and ran in an oil-bath. Each rotor blade weighed 5.5 kilos. It also had a fixed wheel undercarriage with a tailwheel under the tailfin.[1] Unfortunately, the design was too heavy and complex and was abandoned. Specifications{{Aircraft specs|ref=[2] |prime units?=imp
References1. ^{{cite book|last1=Simpson|first1=R.W.|title=Airlife's Helicopters and Rotorcraft|date=26 May 1998|publisher=The Crowood Press Ltd|isbn=978-1853109683}} 2. ^{{cite book|last1=Lambermont|first1=Paul Marcel|first2=Anthony|last2=Pirie|title=Helicopters and autogyros of the world|date=1970|publisher=Barnes|edition=Illustrated, revised}} External links{{commons category|Brantly International}}
5 : United States civil utility aircraft 1940–1949|United States helicopters 1940–1949|Coaxial rotor helicopters|Brantly aircraft|Aircraft first flown in 1946 |
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