with the XH-51 and AH-56, Lockheed dominate the compound helicopter segment in the 60's. The firm wanted to use the system of the cheyenne for civilian applications.
The last of this cheyenne derivatives was the "Composite aircraft" of 1967. The revolutionnary idea was to stop and then, retract the rotor in the fuselage! As there was no rotor anymore, the plane could fly as fast as ordinary airplanes...(no destructive vibrations, no increasing drag, no speed limitation at 600 km/h...)
The concept was aparently validated at Ames in 1967, but the conflict between the US Army and USAF about fixed-wing aircraft prevented any prototype to be build.
This is the ultimate convertible aircraft for me, so i wanted to know if someone has more datas about this project (which seems much better than a V-22!)
The last of this cheyenne derivatives was the "Composite aircraft" of 1967. The revolutionnary idea was to stop and then, retract the rotor in the fuselage! As there was no rotor anymore, the plane could fly as fast as ordinary airplanes...(no destructive vibrations, no increasing drag, no speed limitation at 600 km/h...)
The concept was aparently validated at Ames in 1967, but the conflict between the US Army and USAF about fixed-wing aircraft prevented any prototype to be build.
This is the ultimate convertible aircraft for me, so i wanted to know if someone has more datas about this project (which seems much better than a V-22!)