Design and development
Fred Landgraf formed the Landgraf Helicopter Company in September 1943 to develop and manufacture the H-2. It had an enclosed structure for one pilot and an 85 hp (63 kW) radial engine driving two rotors, each rotor fitted to a short boom on each side of the fuselage. It had a fixed tricycle landing gear. The H-2 first flew on 2 November 1944 and the company was awarded a development contract by the United States Army. It was not developed or bought and the company ceased operations by the end of the 1940s. Unlike conventional helicopters, the H-2 used a tension-rod drive system to drive the side-by-side rotors. Control of blade pitch was also unconventional, with the blade shells rotating freely about the spars, controlled by ailerons near the tips.Specifications
See also
References
Bibliography
* *External links
* {{citation, title=Of Fleets, Luscombes, and a Plywood Helicopter, url=http://pacificcoastairmuseum.org/files/newsletters/newsletters2013/2013-June-Straight-Scoop.pdf, author=PCAM, date=June 2013, publisher= Pacific Coast Air Museum, volume=XVIII, number=6, pages=2–3 1940s United States military utility aircraft 1940s United States helicopters H-2 Transverse rotor helicopters Single-engined piston helicopters Aircraft first flown in 1944