The Lockheed CL-475 was a two-seat, single-engine light helicopter that Lockheed built to explore rigid rotor technology, and only one was made. It came from an idea Irv Culver presented to Lockheed management in 1958 for attaching the rotor blades rigidly to the hub and controlling the large gyroscopic moments with a feedback device he called the compliance factor. The CL-475 had a fabric-covered steel and aluminium structure, side-by-side seating under a glazed cockpit, a tricycle undercarriage and a 140 horsepower Lycoming piston engine. It first flew on 2 November 1959. Early vibration was cured after six months by moving to three metal blades and adding a gyroscopic control ring, and the stability that followed informed the Lockheed XH-51 and the AH-56 Cheyenne. Lockheed gave the helicopter to the National Air and Space Museum in 1975, and it went on display in 2018.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Lockheed CL-475 (Wikipedia)
Of Make
Source Lockheed CL-475 (Wikipedia)
Sources
1. Lockheed CL-475 (Wikipedia)
Lead
is a two-seat, single-engine light helicopter developed by Lockheed to explore rigid rotor technology
Specifications
Powerplant: 1 × Lycoming VO-360-A1A four-cylinder air-cooled piston engine , 140 hp (104 kW)
Design and development
Following a restoration, it was placed on display in 2018.
Design and development, year
It was first flown on 2 November 1959
Specifications, mass
Empty weight: 1,625 lb (737 kg)
Specifications, maximum mass
Gross weight: 2,000 lb (907 kg)
Specifications, top speed
Maximum speed: 90 mph (145 km/h, 78 kn)
Lead, manufacturer
developed by Lockheed to explore rigid rotor technology
Design and development, country of origin
taken to Rosamond Lake on Edwards Air Force Base in the Mojave Desert for testing
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