Vickers EFB.3 / Type 30

In December 1913, a third Vickers Experimental Fighting Biplane, the E.F.B.3, made its debut. The slight overhang of the top wing was eliminated to result in an equi-span biplane, the fuselage nacelle underwent further redesign, the celluloid windows being eliminated, and, most important, ailerons on both upper and lower wings supplanted the wing-warping control of its predecessors. The 100hp Gnome Monosoupape rotary was retained as was also the 7.7mm Vickers gun. Displayed at the Aero Show held at Olympia in 1914, the E.F.B.3. was the subject of an order from the Admiralty for six aircraft placed in December 1913. This contract was subsequently taken over by the War Office, the six aircraft embodying a number of modifications – at least one was fitted with an eight-cylinder Vee-type 80hp Wolseley engine – and being referred to as the Vickers No (or Type) 30. These were to lead in turn to the E.F.B.5 and F.B.5 Gunbus.

Engine: 100hp Gnome Monosoupape
Max take-off weight: 762 kg / 1680 lb
Empty weight: 476 kg / 1049 lb
Wingspan: 11.38 m / 37 ft 4 in
Length: 8.38 m / 28 ft 6 in
Height: 2.97 m / 10 ft 9 in
Wing area: 35.77 sq.m / 385.02 sq ft
Max. speed: 97 km/h / 60 mph
Range: 483 km / 300 miles

Vickers E.F.B.3

Vickers EFB.2

Following the loss of the E.F.B.1, Vickers undertook major redesign of its gun carrier while retaining the basic configuration to result in the E.F.B.2, again against an Admiralty contract. The E.F.B.2 eliminated the wing stagger of the previous aircraft and increased the span of the lower wing while retaining warping for lateral control. The fuselage nacelle was redesigned and large celluloid windows were inserted in its sides; the angular horizontal tail surfaces gave place to surfaces of elliptical form and a 100hp Gnome Monosoupape nine-cylinder rotary engine was fitted. The 7.7mm machine gun on a ball-and-socket mounting in the forward cockpit was retained, and the E.F.B.2 entered flight test at Bognor in the autumn of 1913, but crashed there during the course of October.

Max take-off weight: 798 kg / 1759 lb
Empty weight: 476 kg / 1049 lb
Wingspan: 11.76 m / 39 ft 7 in
Length: 8.89 m / 29 ft 2 in
Height: 2.92 m / 10 ft 7 in
Wing area: 35.30 sq.m / 379.97 sq ft
Max. speed: 97 km/h / 60 mph
Range: 241 km / 150 miles

Vickers E.F.B.2

Vickers EFB.1

On 19 November 1912, Vickers received a contract from the Admiralty for an experimental fighting biplane armed with a machine gun. Various configurations were investigated before the desirability of placing the gunner in the extreme nose of the aircraft, in order to achieve a clear field of fire, led to choice of a fuselage nacelle carrying at its rear an engine driving a pusher propeller. This nacelle was mated with an unequal-span heavily-staggered biplane configuration, the tail surfaces being carried by paired and vertically disposed booms attaching to the upper and lower rear wing spars on each side of the engine.

Designated E.F.B. (Experimental Fighting Biplane) 1 and dubbed “Destroyer”, the Vickers aircraft was armed with a single 7.7mm Maxim machine gun on a mount affording 60 degrees elevation and traverse. The airframe of the E.F.B.1 was primarily of metal construction, the nacelle accommodating the pilot and gunner, and carrying an 80hp Wolseley eight-cylinder Vee-type engine, being of steel tube with duralumin skinning. Wing warping was employed for lateral control.

Prior to its first flight, the E.F.B.1 was displayed at the Aero Show held at Olympia, London, in February 1913.

The gun was fitted for the first flight test, made at Joyce Green, but this rendered the aircraft so nose-heavy that it briefly left the ground, then nosed down, struck the ground and turned over.

Max take-off weight: 1207 kg / 2661 lb
Empty weight: 798 kg / 1759 lb
Wingspan: 12.19 m / 40 ft 0 in
Length: 8.38 m / 28 ft 6 in
Height: 3.63 m / 12 ft 11 in
Wing area: 35.77 sq.m / 385.02 sq ft
Max. speed: 113 km/h / 70 mph

Vickers E.F.B.1

Vickers No.VIII monoplane

In the Vickers’ works at Erith.

The Vickers No.8 Monoplane was built at Erith and displayed at the Fourth International Aero Show at Olympia, in February 1913. This aircraft resembled the No.6 Monoplane and seated its two occupants side-by-side and had a twin wheel undercarriage with a single central skid.

The elevators were aerodynamically balanced and the triangular fin and rudder resembled that used on the No.7 Monoplane. The 70 hp Gnome engine, with front and rear plate mountings, drove a two-blade propeller and was cowled over the upper part of the engine.

Performance figures were also quoted with an 80 hp Gnome fitted. As with the other Vickers monoplanes, the fuselage structure was of steel tube construction. Transparent ‘Cellon’ panels were provided in the lower cockpit sides and floor to improve the crew’s view of the ground. The cockpits were also provided with small transparent windshields.

The tailplane was formed by splaying out the rear longerons. The machine was designed to fold, allowing it to be transported by road mounted on a wooden trailer.

The No 8 monoplane packed for road transport, being towed behind a Napier car.

Only one was built.

Powerplant: One 70 hp Gnome rotary
Span: 34’6″
Empty weight: 700 lb
Speed: 45-69 mph
Endurance: 3 hours 30 min
Capacity: Pilot and passenger
Price: £1300

Vickers No.VII monoplane

The Vickers No.7 Monoplane returned to the same configuration as the No.5 Monoplane. It accommodated the two occupants, seated in tandem and featured two-skids and a four-wheel undercarriage as used on the earlier machines. Power was provided by a 100 hp Rolls-Royce Gnome rotary engine driving a three-blade propeller.

The tail surfaces were again modified, with a fixed fin ahead of a re-shaped, unbalanced rudder. The Gnome engine was supported by a front mounting, with the upper part of the engine being cowled, presumably to prevent hot oil being thrown into the face of the front seat occupant.

The Vickers No.7 Monoplane was flown for the first time by Robert Barnwell at Brooklands on 1st January 1913. However, this aircraft was later reported to have been turned over by a student pilot on 4th October 1913, after which nothing more is heard of it. It is assumed that the company decided not to repair it for further use.

Engine: 100 hp Gnome
Span: 34’6″
Length: 25′
Weight all-up: 1200 lb
Speed: 70 mph
Range: 350 miles
Seats: 2

Vickers No.1

The 1911 Vickers No. 1 monoplane was designed and built by Vickers Aircraft in the UK

The Vickers No 1 was based on a REP design, but used originally designed wings. It was powered by a 5-cylinder, air cooled REP engine developing 60 h.p. The second airframe was sold to Douglas Mawson for possible use in an Antarctic expedition, but was badly damaged in a crash landing at Adelaide in October 1911. The remains (the fuselage and engine) were used by the expedition as a motorized sledge or “air tractor”, but engine problems made it more or less useless. The remains are buried in the ice at Cape Denison, where efforts have been made to retrieve it.

Span: 47’6″
Weight: 1000 lb
Speed: 56 mph

Vickers Aircraft Co Wave

The Vickers Aircraft Company Wave is a two-seat, side-by-side configuration, high wing amphibious aircraft under development by the Vickers Aircraft Company of Hamilton, New Zealand.

The fuselage and wings are constructed from a combination of aluminum and carbon fibre composite materials. An automatic folding wing mechanism and ballistic parachute are planned to be integrated. The standard engine is the 180 hp (134 kW) Continental Titan 340 four-stroke powerplant, mounted in a pusher configuration.

It was introduced at the Sport Aviation Expo in Sebring, Florida in 2014, intended for the US light-sport aircraft category.

Wave
Engine: 1 × Continental Titan 340, 180 hp (130 kW)
Propeller: 3-bladed Catto
Wingspan: 30 ft 10 in (9.40 m)
Wing area: 149.3 sq ft (13.87 sq.m)
Length: 24 ft 7 in (7.5 m)
Height: 7 ft 6 in (2.29 m)
Empty weight: 928 lb (421 kg)
Gross weight: 1,430 lb (649 kg)
Fuel capacity: 50 U.S. gallons (190 L; 42 imp gal)
Maximum speed: 120 kn (138 mph, 222 km/h)
Cruise speed: 120 kn (140 mph, 220 km/h)
Range: 720 nmi (830 mi, 1,330 km)
Wing loading: 10.2 lb/sq ft (49.7 kg/sq.m)
Crew: 1
Capacity: 1 passenger