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Weir W-5
Cierva W.5

 

weir_w5


Weir's chief designer, C.G.Pullin, first thought of converting the W.4 autogyro into a helicopter by using two co-axial rotors, but he finally adopted the system of rotors carried by outriggers on either side of the fuselage, like the 1937 Focke 61.
The W.5 was a single-seater powered by a 50 hp 4-cylinder air-cooled Weir engine; each of the two two-bladed rotors had cyclic and collective pitch control and they turned at 430 r.p.m.
This helicopter made its first flight at Dalrymple, Ayrshire, on 7th June 1938, when it was piloted by R.A.Pullin, son of the chief designer. By the outbreak of World War II it had logged eighty hours' flying time.


Weir W.5
Seats: 1
Engine: 1 x Weir, 50hp
Rotor diameter: 4.57m
Gross weight: 381kg
Max. speed: 112km/h
Rate of climb: 122m/min

weir_w5

 

 

 


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