Gray Goose Airways Windmill Plane

Built circa 1936, the Windmill Plane was an ornithopter type, with four tandem walking beams that opened and closed ten overhead slats, all of this mounted on a four-wheeled gondola with an unknown, but large, powerplant. No record of flight was found. The Windmill Plane appears in the video, “Golden Years of Aviation,” showing its set of rotating wings on either side of a horizontal axle. It was able to taxi only after being pushed by 10 men, but was never seen flying.

Gray & Buchanan Brokker

In August 1922 the Daily Mail newspaper offered a £1,000 prize for the longest duration flight by an unpowered, heavier than air aircraft. The competition was to be organized by the Royal Aero Club, who chose the site (Itford Hill, on the Sussex South Downs near Lewes) and the date (16–21 October). This gave competitors six weeks to design, build and transport their entries. Thirteen arrived in time and one of these was the aircraft nicknamed Brokker, competition number 31.

Built by Sqn. Ldr. Alec Gray and F/O W. J. Buchanan, the Brokker was, as its name suggested, a fusion of a Bristol and a Fokker aircraft. Specifically, the upper wing of a Fokker D.VII married to the engineless fuselage of a Bristol Fighter.

The Brokker was a glider which got its name from the fact that it was constructed from the wings of a Fokker D.VII and the fuselage (less engine) of a Bristol F.2B Fighter. It was put together from two of the cheap and unwanted airframes left at the end of World War I; the wings and fuselage each cost 5/- (25 p), with 8/6 (42.5 p) chiefly for dope and plywood, a total of 18/6 or 92.5 p.

The Fokker D.VII wing had advantages over most other World War I fighters as it was one of the few to use a thick airfoil. The merits of these only emerged towards the end of the war, and then only in Germany: structurally, they could be internally braced and more importantly they produced lower drag and higher lift, particularly at high angles of attack, than the usual thin wings.

On the Brokker, the D.VII wing was simply clamped to the top of the rectangular cross section Bristol fuselage, forming a high wing cantilever monoplane. Since there was no propeller to need ground clearance, the Fighter’s tall undercarriage was replaced with a pair of wheels mounted outside the lower longerons. The now empty nose of the Bristol was enclosed with a new, single curvature fairing.

It first flew on 21 October 1922 at Itford Hill, on the South Downs near Lewes, East Sussex.

The Brokker arrived late at the Iford meeting and was not flown until the final day. Its first launch was not successful but the next resulted in a flight of over 90 mins ended only by darkness, the third longest flight of the week. The relative steadiness of the heavy Brokker in the strong winds of the last day, compared with all other competitors with their low wing loadings, was noted. Gray received the Royal Aero Club prize of £50 third longest flight.

After the competition Gray took it to Salisbury Plain where he was to conduct tests for the Air Ministry on the suitability of gliders in pilot training programmes.

The aircraft was lost in a fatal glider accident on 28 August 1923. The pilot, Neville Charles Waltho, was thrown out of the cockpit when the Brokker stalled on a hillside near Pewsey.

According to a contemporary report in Flight dated September 6 1923:

“LAST week the first fatal glider accident in England occurred when Flight-Lieut. Neville Charles Waltho was piloting a monoplane glider at Milton Hill, near Pewsey, Wilts. It appears that Waltho had been gliding for several minutes and was about to land, when the machine went into a dive.

The pilot was thrown out and killed instantly. The machine used was, we believe, the ” Brokker,” flown by Squadron Leader Gray at Itford last year.”

It was the first fatal glider accident in England since Percy Pilcher’s death in 1899.

Wingspan: 29 ft 4 in (8.93 m)
Gross weight: 500 lb (227 kg) approx
Seats: 1

Grant-Morse Virginia I

Rudolph R. Grant, who later became Chairman of the Technical Board of the Aeronautic Society of America and Charles Oliver Morse of Norfolk, VA, were busy to develop a mechanism for automatic directional and lateral stability in aeroplanes, an interesting device with air pressure spring-loaded wings and counter-wise adjusted incidence of the small lower wing. The Virginia I monoplane was their first, built in the summer of 1910. It proved to be a stable flyer, that in spring 1911 was tested as a hydroplane in the Willoughby Bay, just North of Norfolk. It might have been the first motor aeroplane built in Virginia.

Grant Aerostable

Built in the USA, R. R. Grant’s Aerostable hydroplane of 1913 featured a device whereby the angle of incidence could be changed while in flight. The operator turned a small wheel when changing or adjusting for the proper angle. The wing framework was built of white ash and steel tubing covered with Goodrich alumina cloth. The floats were of the catamaran type, each two ft wide by 21 ft long. Each pontoon was divided into five watertight compartments.

Engine: Emerson two-cycle, 100 hp
Wingspan: 42 ft
Length: 41 ft
Weight: 1600 lb

Granger Archaeopteryx

Designed in 1926 by R.F.T. and R.J.T.Granger and C.H.Latimer-Needham, the Archaeopteryx was built over the next four year at Attenborough, Notts. With a parasol configuration it retains a normal fin and rudder.

Granger Archaeopteryx G-ABXL, ailerons taking up the entire wing tips pivoting from a central point.

First flown in October 1930, it was flown regularly on short trial hops, mainly from Tollerton, Notts, before being officially registered on 3 June 1932 as G-ABXL cn 3A. The sole example built survived until stored through the war years at Chilwell, and after the war was presented to the Shuttleworth Trust.

It was restored to flying condition in 1971 and flown from Old Warden since.

Engine: Bristol Cherub I, 32 hp
Wingspan: 27 ft 6 in
Length: 15 ft
AUW: 612 lb
Max speed: 95 mph