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 (Aviation) Ltd / Vickers-Armstrong

Vickers was formed in Sheffield as a steel foundry by the miller Edward Vickers and his father-in-law George Naylor in 1828. Naylor was a partner in the foundry Naylor & Sanderson and Vickers’ brother William owned a steel rolling operation. Edward’s investments in the railway industry allowed him to gain control of the company, based at Millsands and known as Naylor Vickers and Company. It began life making steel castings and quickly became famous for casting church bells. In 1854 Vickers’ sons Thomas (a militia officer known familiarly as ‘Colonel Tom’) and Albert joined the business and their talents – Tom Vickers as a metallurgist and Albert as a team-builder and salesman – were key to its subsequent rapid development. “Its great architects,” the historian Clive Trebilcock writes, “Colonel T.E. (1833-1915) and Albert (1838-1919) Vickers… provided both inspired technical leadership… and equally astute commercial direction. Both men were autocrats by temperament, but neither shunned advice or avoided delegation; each, but particularly Albert, had a marked gift for the selection of talented subordinates.”

Vickers (Aviation) Ltd / Vickers-Armstrong Article

In 1863 the company moved to a new site in Sheffield on the River Don in Brightside.

The company went public in 1867 as Vickers, Sons & Company and gradually acquired more businesses, branching out into various sectors. In 1868 Vickers began to manufacture marine shafts, in 1872 they began casting marine propellers and in 1882 they set up a forging press. Vickers produced their first armour plate in 1888 and their first artillery piece in 1890.

Vickers bought out the Barrow-in-Furness shipbuilder The Barrow Shipbuilding Company in 1897, acquiring its subsidiary the Maxim Nordenfelt Guns and Ammunition Company. at the same time, to become Vickers, Sons & Maxim.

Ordnance and ammunition made during this period, including World War I, was stamped V.S.M.

The yard at Barrow became the “Naval Construction Yard”. With these acquisitions, Vickers could now produce a complete selection of products, from ships and marine fittings to armour plate and a whole suite of ordnance. In 1901 the Royal Navy’s first submarine, Holland 1, was launched at the Naval Construction Yard. In 1902 Vickers took a half share in the famous Clyde shipyard John Brown and Company.

Further diversification occurred in 1901 with the acquisition of a proposed business which was incorporated as The Wolseley Tool and Motor Car Company and in 1905 the goodwill and patent rights of the Siddeley car. In 1911 a controlling interest was acquired in Whitehead and Company, the torpedo manufacturers.

Vickers Airships Article

In 1911 the company name was changed to Vickers Ltd and expanded its operations into aircraft manufacture by the formation of Vickers Ltd (Aviation Department) on March 28, 1911, under Capt. H. F. Wood, and a Vickers School of Flying was opened at Brooklands, Surrey on 20 January 1912. Production rights for Esnault-Pelterie REP tractor monoplane obtained in 1911; several variants built before First World War.

In 1912 Vickers produced Type 18 Destroyer for Admiralty; pusher-engined gun-carrying fighter from which evolved, via successive E.F.B. (Experimental Fighting Biplane) prototypes, the F.B.5 and F.B.9 “Gunbus” fighters of First World War. Later front-gunned tractor-engined F.19 was less successful. During war also built RAF B.E.2 series, B.E.8, F.E.8, and S.E.5a and Sopwith 1 1/2-Strutters under license. Vickers Vimy of 1917 remained standard RAF bomber throughout 1920s: one used by Alcock and Brown for first non-stop Atlantic crossing by airplane on June 14/15 1919. Vimy Commercial was 11 -passenger airliner with enlarged fuselage; Vernon troop transport developed from this.

In 1919, the British Westinghouse electrical company was taken over as the Metropolitan Vickers Electrical Company; Metrovick. At the same time they came into Metropolitan’s railway interests.

Vimy and Vernon succeeded respectively by Virginia and Victoria in mid-1920s, followed by Pegasus engined development, the Valentia.

By the end of 1924 Armstrong’s was virtually bankrupt. The bank of England discreetly moved in, and eventually brought pressure to force a merger with Vickers, using the Sun Insurance Company as their front to guarantee the new company, now called Vickers Armstrong. It was a condition of the rescue that the new company would restrict themselves to ship building, heavy engineering, and predominantly armaments.

A reorganisation during 1926 led to the retention of the rolling stock group: Metropolitan Carriage wagon and Finance Company and The Metropolitan -Vickers Company and the disposal of: Vickers-Petters Limited, British Lighting and Ignition Company, the Plywood department at Crayford Creek, Canadian Vickers, William Beardmore and Co, and Wolseley Motors.

In 1927, Vickers merged with the Tyneside based engineering company Armstrong Whitworth, founded by W. G. Armstrong, to become Vickers-Armstrongs, Ltd. Armstrong Whitworth had developed along similar lines to Vickers, expanding into various military sectors and was notable for their artillery manufacture at Elswick and shipbuilding at a yard at High Walker on the River Tyne. Armstrongs shipbuilding interests became the “Naval Yard”, those of Vickers on the west coast the “Naval Construction Yard”. Armstrong Whitworth Aircraft was not absorbed by the new company.

In 1928 the Aviation Department became Vickers (Aviation) Ltd and four months later acquired Supermarine, which became the “Supermarine Aviation Works (Vickers) Ltd”. In 1938, both companies were re-organised as Vickers-Armstrongs (Aircraft) Ltd, although the former Supermarine and Vickers works continued to brand their products under their former names. Supermarine became Vicker-Supermarine in 1929. 1929 saw the merger of the acquired railway business with those of Cammell Laird to form Metropolitan Cammell Carriage and Wagon (MCCW); Metro Cammell.

Vickers’ own products continued in early 1930s with Vildebeest torpedo- bomber and Vincent general-purpose biplane. June 1935 saw first flight of Pegasus engined long-range Wellesley bomber, first RAF aircraft to use system of geodetic construction devised by Dr. B. N. (later Sir Barnes) Wallis, who remained head of research until early 1970s. Subcontract production included Armstrong Whitworth Siskin IIIAs (1929-1930), Hawker Harts (1932-1934) and Hart Trainers (1936). In March 1936 the prototype was flown of R. J. Mitchell’s supreme design, the Supermarine Spitfire; and in June 1936 prototype of Vickers Wellington twin-engined bomber.

Vickers’ main concern up to and during Second World War was production of Wellington bomber and Avro Lancaster; Wellington replaced at end of war and early postwar by its non-geodetic successor, the Warwick. In August 1946 came first flight of VC1 Viking, first postwar British transport to enter airline service. Subsequent products included four-jet Valiant (first British V-bomber); world’s first turboprop airliner to enter production/service, the Viscount; and in 1959 the four-turboprop Vanguard airliner.

In 1960 the aircraft interests were merged with those of the Bristol, English Electric Company and Hunting Aircraft to form the British Aircraft Corporation. This was owned by Vickers, English Electric and Bristol (holding 40%, 40% and 20% respectively). BAC in turn owned 70% of Hunting. The Supermarine operation was closed in 1963 and the Vickers name for aircraft was dropped in 1965. Under the terms of the Aircraft and Shipbuilding Industries Act BAC was officially nationalised in 1977 to become part of the British Aerospace group, which exists today in the guise of BAE Systems.

The Aircraft and Shipbuilding Industries Act also led to the nationalisation of Vickers’ shipbuilding division as part of British Shipbuilders. These had been renamed Vickers Armstrong Shipbuilders in 1955, changing again to Vickers Limited Shipbuilding Group in 1968. This division was privatised as Vickers Shipbuilding and Engineering Ltd (VSEL) in 1986, later part of GEC’s Marconi Marine. It remains in operation to this day as BAE Systems Submarine Solutions.

With their steelworking operations also nationalised into British Steel the remnants of Vickers became Vickers plc. In 1986, Vickers acquired the armaments manufacturer Royal Ordnance Factory, Leeds, which became Vickers Defence Systems. Other acquisitions included automotive engineers Cosworth in 1990, waterjet manufacturer Kamewa in 1986 and Norwegian marine propulsion and engineering company Ulstein in 1998. 1998 also saw the sale of Rolls-Royce Motors and Cosworth to Volkswagen Group for £430 million, beating out BMW’s offer of £340 million.

Vickers remained independent until 1999 when the then Vickers plc was acquired by Rolls-Royce plc who sold the defence arm to Alvis plc, which became Alvis Vickers. Vickers plc and the subsidiaries retained by Rolls-Royce were renamed Vinters in March 2003. This Vickers name lived on in Alvis Vickers, until the latter was acquired by BAE Systems in 2004 to form BAE Systems Land Systems.

BAE Systems announced on 31 May 2012 that the ex Vickers Defence Systems factory on Scotswood Road, Newcastle would close at the end of 2013.

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

Viberti

Italy
Formed shortly after Second World War by Dr. Angelo Viberti to build light aircraft. First product, Musca 1 two-seat tourer/trainer low-wing monoplane, first flown 1948; slightly modified Musca 1Ws appeared in 1949. There were designs for Musca 2 three-seat cabin monoplane and Musca 4 high-wing version of 1, and floatplane variant, but doubtful if they were built. Probably dissolved about 1950-1951.

Verzilov Staliniets 5

Encouraged by the excellent results obtained by his gliders in the competitions of 1934 and 1937, for the XII National Competitions, Verzilov presented a last model called “Staliniets-5” (Russian: Верзилов “Сталинец-5”), designed as a record-breaking single-seater for long-range flights and also built in the facilities. from the Yeisk Naval Pilot School.

The “Staliniets-5” was designed as a single-seater monoplane with a cantilever wing of medium implantation, characterized by its gull-like shape. The shape in the plane was trapezoidal with a marked decrease in the chord and an R-III profile. The trailing edge featured long louvered ailerons covering the entire span to the point of angle change.

The glider was characterized by the presence of a closed celluloid-coated cockpit, equipped with instrumentation to be able to carry out night and blind flights and with radio equipment to maintain contact with the ground.

The landing gear consisted of a wooden ski with an extension located at the bottom of the keel.

Like the previous models, the “Staliniets-5” stood out for its good construction finish.

The atmospheric conditions during the 1937 XII National Sailing Competitions (of the 18 days only 4 allowed to fly) did not offer the possibility of obtaining appreciable results.

From 1937 the development of gliders in Yeisk died. For various reasons its developers were assigned to other units. Yeremeyev left Yeisk in 1936, Sujomlin and Lisitsyn in the summer of 1937. Verzilov would also drop out of school shortly thereafter.

Staliniets-5
Wingspan: 18.00 m
Wing area: 14.60 m²
Aspect ratio: 22.2
Length: 6.84 m
Height: 1.62 m
Empty weight: 280 kg
Wing loading: 24.7 kg / m²
Glide ratio: 24
Minimum descent speed: 0.73 m / s
Surface of the horizontal planes: 1.00 m²
Vertical plane surface: 1.3 m²
Ailerons surface: 2.00 m²
Accommodation: 1

Verzilov Staliniets 4

For the XI National Flying Competition held in Koktebel, Vladimir Verzilov developed two new gliders: the two-seater trailed “Staliniets-2bis”, built as a development of the “Staliniets-2” and the single-seater “Staliniets-4” (Russian: Верзилов “Сталинец-4”). Both were valued by the technical commission, receiving approval for the flights without objections.

The “Staliniets-4” glider was designed as a single-seater training and competition monoplane.

Structurally, it was a high-wing glider with variable chord cantilever wings and a trapezoidal shape in the plane. The wing, with a single spar, was constructed of wood with plywood covering and featured a P3-2 profile. The trailing edge featured long louvered ailerons covering 2/3 of the wingspan.

The tail was of the conventional type, with the horizontal planes located near the base of the empennage.

The landing gear consisted of a non-depreciated wooden ski with an extension located at the bottom of the keel.

The pilot was located in an open cockpit located in the bow. A notable feature was the use of a radio in the glider, which allowed communication with the ground.

Built at the VVS RKKA Naval Pilot School, this glider successfully participated in the XI National Competitions Gliding in Koktebel between 6 September and 6 October 1935. In the opinion of the pilot Iván M. Sujomlin, the glider was very obedient to the controls and stable in flight. The only defect noted was its one-piece wing construction, which caused problems during transport and maintenance actions.

With the pilot IM Sujomlin at the controls, this glider managed, between October 2 and 3, to stay in the air for 38 hours and 10 minutes, which meant a new record. The Stalinits-4 received a special award in the competition’s training glider category.

These were the last gliding competitions in which the duration of the flight was competed. In the new competitions, they moved the mountainous Crimea, to new sites such as Rostov and the Moscow airfields.

In 1937 the “Staliniets-4” glider was produced by various organizations in the country. Many competitors built developments of this model for participation in competitions. The XII national competitions, which took place between 10 and 28 of July 1937 at the airfield of the sports society “Spartak” near the village Tioply Stan (now a suburb of Moscow) participated with three copies under the name ” Staliniets-4bis “.

Staliniets-4
Wingspan: 14.00 m
Wing area: 11.30 m²
Aspect ratio: 17.3
Length: 6.15 m
Height: 1.30 m
Empty weight: 173 kg
Wing loading: 22.4 kg / m²
Glide ratio: 19.8
Surface of the horizontal planes: 1.57 m²
Rudder surface: 0.80 m²
Aileron surface: 1.35 m²
Accommodation: 1

Verzilov Staliniets-2bis

A development of the “Staliniets-2” built in 1935, the “Staliniets-2bis” (Russian: Верзилов “Сталинец-2бис”) glider was designed as a towed two-seater.

Structurally it was designed as a monoplane with a high wing in parasol, braced by uprights. The wing featured an R-II profile with a single spar structure and was built in two independent sections, which were fixed to the upper fuselage structure, featuring an upright on each side to ensure the necessary structural rigidity. The entire wing was covered by 1.5 – 2 mm thick plywood sheets and had a total weight of 158 kg.

The fuselage featured oval section and plywood overlay. Eighteen frames and four main spars were included in its structure.

The vibration problems presented by the previous “Staliniets-2” made it necessary to locate the tail planes somewhat lower in the empennage. The stabilizer was attached to the keel structure at two points and a bracing post.

The landing gear consisted of a rigid, trunk-shaped ski, to which a trolley was attached, which could be released after take-off from the second seat.

The two crew members sat in tandem seats. The second position was located just above the center of gravity of the glider, so the absence of its occupant did not bring problems of variation of the centering.

As a result of the modifications made, the new glider was 25 kg heavier than its predecessor.

For the XI National Competition gliding in Koktebel between 6 September and 6 October of 1935 both “Staliniets- 2” and the “Staliniets-4” were valued by the technical commission, receiving approval for the flights without objections.

During the XI National Sailing Competitions on the “Staliniets-2bis”, test pilot Valentin V. Licitsyn with passenger B. Dolya set a new world record for flight duration for a two-seater glider by staying in the air between 2 and October 3 for 38 hours and 40 minutes. Again the record was recognized only as a national one, because the USSR in those years was not a member of the FAI.

Staliniets-2bis
Wingspan: 20.10 m
Wing area: 25.00 m²
Aspect ratio: 16.2
Length: 8.22 m
Height: 1.60 m
Empty weight: 320 kg
Wing loading: 19.2 kg / m²
Ailerons area: 4.20 m²
Glide ratio: 21
Accommodation: 2

Verzilov Staliniets-2

From a visit to the IX National Competition gliding, which took place in the town of Koktebel in Crimea between 12 August and 20 September of 1933, a group of students and instructors Pilot School Navales of the RKKA VVS named Stalin decided to develop self-built gliders to participate in these competitions. The gliders carried the name Staliniets (Сталинец), which can be translated as Staliniano, in relation to the name of the school.

With more desire than experience and using the facilities of the local carpentry they began to work.

The “Staliniets-2” was designed as a two-seater competition glider.

Structurally it was designed as a monoplane with a high wing in parasol, braced by uprights. The wing featured an R-II profile with a single spar structure and was built in two independent sections, which were fixed to the upper fuselage structure, featuring an upright on each side to ensure the necessary structural rigidity. The central section of the wing was rectangular in shape, which became trapezoidal towards the ends. The entire wing was covered by 1.5 – 2 mm thick plywood sheets and had a total weight of 158 kg.

The fuselage featured oval section and plywood overlay. Eighteen frames and four main spars were included in its structure.

The tail planes were located high on the empennage. The stabilizer was attached to the keel structure at two points and a bracing post.

The landing gear consisted of a rigid, trunk-shaped ski, to which a trolley was attached, which could be released after take-off from the second seat.

The two crew members sat in tandem seats. The second position was located just above the center of gravity of the glider, so the absence of its occupant did not bring problems of variation of the centering.

The “Staliniets-2” (Russian: Верзилов “Сталинец-2”) was manufactured between June and September 1934 and this glider stood out for its good finish.

In the next competition, held also in Koktebel from 1 September to the 6 October of 1934 two gliders were presented: the “Staliniets-1” developed by the instructor flying school Pavel Yeyemeyev and two – seater “Staliniets -2 ”developed by Vladimir Verzilov.

The “Staliniets-2” glider successfully participated in the X National Sailing Competition, held in Koktebel.

Unlike the unsuccessful “Staliniets-1” of Yeremeyev, the “Staliniets-2” flown by instructor pilot Ivan M. Sujomlin established a new record in the competition extension flight to stay airborne 24 hours and 10 minutes between on October 18 and 19. Despite surpassing international results, this record was recognized only as national because the USSR was not a member of the FAI.

As a positive feature of the glider, it is worth highlighting its excellent longitudinal and transverse stability, as well as the excellent balance achieved by its builders.

Its disadvantages include the operation of the large unbalanced ailerons, which required a great effort o and some vibration in the tail, due to an ineffective location of the stabilizer.

Staliniets-2
Wingspan: 20.20 m
Wing area: 25.00 m²
Aspect ratio: 16.3
Length: 8.05 m
Height: 1.95 m
Empty weight: 295 kg
Wing loading: 18.2 kg / m²
Surface of the horizontal planes: 3.16 m²
Vertical plane surface: 1.72 m²
Ailerons surface: 3.68 m²
Accommodation: 2