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Breguet G.II Gyroplane / G.III Gyroplane

Breg-G2-1

 

Louis Breguet produced his third "Gyroplane" in 1949; the Model G.IIE. The GIIE had a streamlined fuselage and T-tail and cabin space for a pilot and four passengers. Constructed on behalf of the Societe Francaise du Gyroplane by Breguet, the prototype had an all-metal fuselage with a tall fin and small T-tailplane. It had a cabin for five people and a fixed tricycle undercarriage. The 240hp Potez 9E engine was buried in the fuselage behind the cabin, and three-bladed all-metal rotors were used.

First flew on 21 May 1949, at Villacoublay-Velizy to the south of Paris, the G.IIE was found to be underpowered and it was re-engined with a 450hp Pratt & Whitney Wasp Junior - in which form it became the G.III. Following testing in 1951 development was discontinued and F-WFKC was donated to the Musee de l'Air.

 

Breg-G2-2

 

G.IIE
Engine: 1 x Pratt & Whitney R-985, 335kW
Rotor diameter: 9.60m
Length with rotors turning: 9.70m
Height: 4.24m
Max take-off weight: 2100kg
Empty weight: 1473kg
Max speed: 215km/h
Hovering ceiling, IGE: 1600m
Service ceiling: 4600m
Range: 470km
Crew: 1
Passengers: 4

 

Breg-G2-ld

 

 

 

 

 

 


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