Fairey Gyrodyne Aircraft
| |
Production Details | |
Design Company: |
|
First Flight: |
7 December 1947 |
Gyrodyne: |
2 - Fairey |
Jet Gyrodyne: |
1 - Fairey (converted from Gyrodyne) |
Type Specification | |
Applies to: |
Fairey Gyrodyne |
Type: |
Light compound helicopter |
Rotor System: |
Three blade main rotor driven. No tail rotor |
Fuselage: |
All metal fuselage with short wings mounted on side to relieve load on rotor during forward flight |
Tail Unit: |
Tailplane mounted at rear of fuselage with twin fins at tip |
Landing Gear: |
Fixed tricycle undercarriage. Nose wheel under fuselage. Main wheels under wing |
Power Plant: |
One Alvis Leonides nine cylinder radial in fuselage driving main rotor and propeller on starboard wing tip |
Accommodation: |
Enclosed cabin |
Dimensions | |
Rotor Diameter: |
51 ft 9 in |
Length: |
25 ft |
Height: |
10 ft 2 in |
Weights | |
Empty: |
3,600 lb |
Loaded: |
4,800 lb |
Performance | |
Max Speed: |
140 mph |
Preserved in British Museums | |
Jet Gyrodyne: |
XJ389 - Museum of Berkshire Aviation, Woodley - Display |
Web Sites | |
http://avia.russian.ee/helicopters_eng/fairey_gyrodyne-r.html |