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84-472: In response to a Royal Navy request for a helicopter, Dr. James Allan Jamieson Bennett designed the gyrodyne whilst serving as the chief engineer of the Cierva Autogiro Company . The gyrodyne was envisioned as an intermediate type of rotorcraft , its rotor operating parallel to the flightpath to minimize axial flow with one or more propellers providing propulsion. Bennett's patent covered

168-471: A Bristol Siddeley Viper ASV.8 turbojet, giving a speed of 600 mph (970 km/h) and an operational ceiling in excess of 50,000 ft. The "Fairey V.T.O" was a vertical take-off delta wing aircraft was designed to explore the possibility of making an aircraft launched from short ramps with low acceleration. Shown for the first time at the Society of British Aircraft Constructors (SBAC) Show in 1952,

252-565: A Defense Advanced Research Projects Agency (DARPA) program to develop advances in rotorcraft technology with the goal of overcoming the current limitations of helicopters in both speed and payload. Where a conventional helicopter has a powered rotor which provides both lift and forward thrust, and is capable of true VTOL performance, a gyroplane or autogyro has a free-spinning rotor which relies on independent powered thrust to provide forward airspeed and keep it spinning. The gyrodyne combines aspects of each. It has an independent thrust system like

336-473: A crew of three. For training purposes the Malkara Mk I was used, with a range of some 2,000 m (6,600 ft). The operational weapon was the Malkara Mk 1 A, which had a different type of tracking flare, thinner guidance wire, and other improvements to give approximately double the range of Mk 1. The Fairey Fireflash was an early air-to-air weapon guided by radar beam riding. Developed as "Blue Sky" –

420-693: A derated version of the Red Hawk missile. It was in service briefly before being replaced by the de Havilland Firestreak . Green Cheese was a tactical nuclear anti-ship missile for use with the Gannet. Problems with Gannet led to continued development with the Blackburn Buccaneer but it was cancelled. Fairey Marine Ltd was begun in the late 1940s by Sir Richard Fairey and Fairey Aviation's Managing Director, Mr Chichester-Smith. Both were avid sailing enthusiasts. Utilising techniques developed in

504-514: A design and production factory that specialised in the manufacture of airborne and ground equipment for target aircraft and missile fields including the Tonic towed target, which can be carried and streamed by a Jindivik 3A. In 1957 a miniature camera by the name of WRECISS ( Weapons Research Establishment camera interception single-shot) was designed and developed by the WRE at Woomera and manufactured by

588-420: A finely finished, white-painted body apparently made of seamless tube. About two-thirds of the way back from the nose was fitted a laminated-wood wing of about two feet span, positioned across a diameter of the body, with a root chord of some 18 inches and a quarter-chord sweep of about 50 degrees. In April 1947 Fairey released details of its first guided missile It was an anti-aircraft weapon designed for use in

672-503: A management buy-out from Pearson, listing on the London Stock Exchange in 1988. During the 1990s this company concentrated on expanding its electronics business, acquiring a number of companies, and disposing of the electrical insulator and hydraulic actuator businesses. In 1997, the company acquired Burnfield, of which Malvern Instruments was the most significant company. Servomex plc was acquired in 1999. In July 2000,

756-468: A mechanical overdrive unit for Land Rovers. Vehicles fitted with the unit carried a badge on the rear saying "Overdrive by Fairey", with the Fairey logo (see above). This branch of products effectively ceased in the early 1980s when new product development at Land Rover and a trend for manufacturers to build accessories in-house forced Fairey to drop out of the sector. The American company Superwinch bought

840-707: A range of subsonic and supersonic towed target systems (RADOP) for air-to-air and surface-to-air guided weapon training in Europe, Africa, the Middle East, the Commonwealth and the UK. The parent Fairey Company and its Australian subsidiary were heavily involved guided weapon development. The Weapon Division of Fairey Engineering Ltd was responsible in the UK for the Jindivik Mk 2B Pilotless target aircraft. This had

924-536: A rotaplane (with the rotor free for autorotation and an upward total axial flow through the rotor disc), on the one hand, and a pure helicopter (with the rotor driven, and a downward total axial flow through the rotor disc), on the other hand, that is with a mean axial flow through the rotor disc substantially zero at high forward speed. Bennett's concept described a shaft-driven rotor, with anti-torque and propulsion for translational flight provided by one or more propellers mounted on stub wings. With thrust being provided by

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1008-734: A single manufacturer. The merger of Fairey's aviation interests with Westland Aircraft took place in early 1960 shortly after Westland had acquired the Saunders-Roe group and the helicopter division of the Bristol Aeroplane Company . Westland Aircraft and the Fairey Company announced that they had reached agreement for the sale by Fairey to Westland of the issued share capital of Fairey Aviation, which operated all Fairey's UK aviation interests. Westland acquired all Fairey's aircraft manufacturing business (including

1092-507: A variety of designs, which has led to some of the terminology confusion – other issues including the trademarked Gyrodyne Company of America and the Federal Aviation Administration (FAA) classification of rotorcraft. In recent years, a related concept has been promoted under the name heliplane . Originally used to market gyroplanes built by two different companies, the term has been adopted to describe

1176-542: A warhead. The Stooge required a launching ramp and transport. The missile was extensively tested at Woomera The Malkara missile was designed in Australia by British and Australian companies. It was a heavy wire-guided missile for deployment from vehicles, light naval craft and fixed emplacements. This weapon replaced the Fairey "Orange William" project for the MoS which would later lead to Swingfire . Fairey Engineering had

1260-519: Is working on phase one of that program, a 15-month effort… (it) combines the "gyroplane"… with a fixed-wing business jet. The team was using the Adam A700 , in the very-light-jet class …" There were issues with tip jet noise, and the program was cancelled in 2008. An industry magazine describes the gradual evolution of traditional helicopters as "slow" and lacking revolutionary steps, and non-traditional compounds are still not widespread. "Gyrodyne"

1344-607: The Avro CF-100 . The Canadair Argus used Fairey-designed hydraulic actuators. The company also produced the "Bear Trap" helicopter /ship handling system for the Royal Canadian Navy. In the early 1960s the company undertook the conversion of the Martin Mars flying boats to water-bearing firefighters. Drawing on the parent company's expertise in the design of hydraulic equipment led to local manufacturer of

1428-576: The Fairey III family, the Swordfish , Firefly , and Gannet . It had a strong presence in the supply of naval aircraft, and also built bombers for the RAF. After World War II the company diversified into mechanical engineering and boat-building. The aircraft manufacturing arm was taken over by Westland Aircraft in 1960. Following a series of mergers and takeovers, the principal successor businesses to

1512-818: The Grumman Avenger . The Avro Lancaster conversion programme created the need for plant expansion. The Lancaster was followed in service by the Lockheed Neptune and again the company undertook a share of the repair overhaul and service of these aircraft. The company was engaged in the modification and overhaul of the McDonnell Banshee . Fairey of Canada also developed a component and instrument design and manufacturing organisation. The company began manufacture of Hydro Booster Units which control flight surfaces hydraulically rather than manually. Other flight controls were designed and manufactured for

1596-637: The Jindivik , Meteor, and Canberra drones at Woomera missile test range. Fairey Australasia was the first company to be established at the Weapons Research Establishment (WRE). This was in 1949 when the firm was involved in supporting research trials of the scale model of the Fairey vertical-take-off aircraft. Shortly afterwards the company expanded to manufacture the RTV.l research rockets that were fired in Australia. From this developed

1680-475: The McDonnell XV-1 was developed as a rotorcraft with tip jets to provide vertical takeoff capability. The aircraft also had wings and a propeller mounted on the rear of the fuselage between twin tailbooms with two small rotors mounted at the end for yaw control. The second prototype of XV-1 became the world's first rotorcraft to exceed 200 mph in level flight on 10 October 1956. No more were built and

1764-648: The Pacific War but not completed in time for use by the British Army (who originally ordered it) or for the Royal Navy . The Ministry of Supply requested that the work be completed, and the Stooge was the outcome. It had a length of 7 ft 5.5 in (2.273 m), a span of 6 ft 10 in (2.08 m), a body diameter of 17 in, and weighing 738 lb (335 kg), with a warhead. Propulsion

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1848-734: The Royal Australian Navy Torpedo Establishment (hydraulic servo units), EMI (guidance receivers and amplifiers) and the Commonwealth Aircraft Corporation (magnesium castings). Some parts were also imported from the UK. Assembly was undertaken at Salisbury, South Australia by the Special Projects Division of Fairey. Test firings took place in 1955–56 but by this time the RTV1 was considered obsolete RTV1e

1932-513: The Royal Navy an aircraft capable of true vertical flight. Bennett's innovative design, a new type of rotorcraft that combined key features of the autogyro and helicopter, was tendered to the Air Ministry ( Specification S.22/38 ) as the Cierva C.41 Gyrodyne, but preliminary work was abandoned with the outbreak of World War II . Bennett joined Fairey Aviation in 1945, where he continued

2016-777: The United Kingdom by Avro , in Germany by Focke-Wulf , and in France by Lioré-et-Olivier . On 9 December 1936, Cierva was killed in the Croydon KLM airliner accident when the aircraft in which he was a passenger crashed after taking off in fog. Dr. James Allan Jamieson Bennett was promoted to Chief Technical Officer of the company and remained in the position until leaving in 1939. In addition to making important contributions to autogyro controls while at Cierva Autogyro, Bennett carried through with Cierva's decision to offer

2100-1380: The Westland Wasp and Westland Scout were built at Hayes in the 1960s. Receipt of large UK military contracts in the mid-1930s necessitated acquisition of a large factory in Heaton Chapel Stockport in 1935 that had been used as the National Aircraft Factory No. 2 during World War I. Flight test facilities were built at Manchester's Ringway Airport, the first phase opening in June 1937. A few Hendon monoplane bombers built at Stockport were flown from Manchester's Barton Aerodrome in 1936. Quantity production of Battle light bombers at Stockport/Ringway commenced in mid 1937. Large numbers of Fulmar fighters and Barracuda dive-bombers followed during World War II. Fairey's also built 498 Bristol Beaufighter aircraft and over 660 Handley Page Halifax bombers in their northern facilities . Postwar, Firefly and Gannet naval aircraft were supplemented by sub-contracts from de Havilland for Vampire and Venom jet fighters. Aircraft production and modification at Stockport and Ringway ceased in 1960. On 13 March 1959 Flight reported that Fairey Aviation Ltd

2184-423: The autogyro . The company was set up to further the designs of Juan de la Cierva , a Spanish engineer and pilot, with the financial backing of James George Weir , a Scottish industrialist and aviator. Juan de la Cierva's first British-built autogyro was the C.8 design . It and some other designs were built in conjunction with Avro . The pre-war Cierva C.30 proved popular. Nearly 150 were built under licence in

2268-500: The 1944 Royal Navy specification for a guided anti-aircraft missile known as LOPGAP. In 1947, the Royal Aircraft Establishment took over development work and the missile was renamed RTV1. Several versions of the basic RTV1 were developed. The Fairey Aviation Company of Australasia Pty Ltd was awarded a contract to build 40 RTV1e rockets. The first of which were completed in early 1954. Components were built by

2352-531: The 1950s they produced the larger sailing cruisers, the Atalanta (named after Sir Richard's first son's wife), Titania, Fulmar and the 27-foot (8.2 m) Fisherman motor sailer (based on the Fairey Lifeboat hull) along with the 15 Cinderella (outboard runabout) and the 16'6" Faun (outboard powered family cruiser). In 1937, workers at the Fairey aviation plant formed a brass band . For some sixty years

2436-412: The Air Ministry to build London Heathrow Airport , with no compensation until 1964, caused a severe financial shock which may have hastened the company's end. One notable Hayes-built aircraft type during the late 1930s and World War II was the Swordfish . In 1957, the prototype Fairey Rotodyne vertical takeoff airliner was built at Hayes. After the merger with Westland Helicopters, helicopters such as

2520-829: The Belgian F-16 project. See also Tipsy Nipper . Formed in 1948 the Fairey Aviation Company of Canada Limited and grew from a six-man operation to a major enterprise employing around a thousand people. In March 1949, the company undertook repair and overhaul work for the Royal Canadian Navy on the Supermarine Seafire and the Fairey Firefly and later the Hawker Sea Fury and also undertook modification work on

2604-709: The Belgian authorities and a subsidiary, Avions Fairey was established to produce Fairey aircraft in Belgium The company staff left Belgium ahead of the German invasion of the Low Countries and returned after the war to build aircraft under licence for the Belgian Air Force . With Fairey's financial troubles in the later 1970s, the Belgian government bought Avions Fairey to preserve its involvement in

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2688-805: The Fairey Aviation Co Ltd and its subsequent absorption into the Westland Group in 1960. Production was therefore invested in Fairey Engineering Ltd but by 1962 this had been transformed into a 50/50 joint venture with the British Aircraft Corporation (Holdings) Ltd known as BAC (AT) LTD, with offices at 100 Pall Mall, London SW1 and a share capital of £100. This was separate to the BAC Guided Weapons division. The Fairey company

2772-526: The Fairey Aviation Co of Australasia, at Salisbury, South Australia . In most surface-to-air missile installations the cameras have been mounted in the nose telemetry bay. Although the firing lever must be replaced after each mission, it is estimated that some 30 per cent of the WRECISS can be re-used without repairs and a substantial further proportion can be repaired relatively cheaply. Its film

2856-442: The Fairey Aviation Company of Canada Limited was formed in 1955 at Sidney, Vancouver Island . The plant was located at Patricia Bay Airport. This facility handled mainly repair, overhaul and modification of military and civil aircraft including the conversion of ex-military Avenger aircraft to commercial cropdusting roles. Additionally, the company diversified into designing and manufacturing items of hospital equipment. Following

2940-897: The Fairey Aviation specifically for use on an aircraft carrier was the Fairey Campania a patrol seaplane that first flew in February 1917. In the third report of the Royal Commission on Awards to Inventors, reported in Flight magazine of 15 January 1925, aviation figures prominently. C. R. Fairey and the Fairey Aviation Co. Ltd, was awarded £4,000 for work on the Hamble Baby seaplane. Fairey subsequently designed many aircraft types and, after World War II, missiles . The Propeller Division (Fairey-Reed Airscrews)

3024-575: The Fairey Co. Ltd, and to concentrate general engineering activities in the Stockport Aviation Co. Ltd, whose name would become Fairey Engineering Ltd . Under these changes, the Fairey Co. would become a holding company, with control of policy and finance throughout the group. The government in the late 1950s was determined to rationalise the UK's aero industry. The Ministry of Defence saw the future of helicopters as being best met by

3108-652: The Fairey Company Ltd the entire share capital for £201,163,000. The companies were managed by the National Enterprise Board (NEB). In 1980 The Fairey Group was purchased by Doulton & Co. (part of S Pearson & Son) from the NEB. At the time, Pearson's interests in manufacturing were concentrated in the Doulton fine china business. The engineering interests were strengthened in 1980 by

3192-568: The Fairey Microfilter, which had applications in industries beyond aviation. Yet another Fairey designed and manufactured component was the Safety Ohmmeter. This instrument had many applications in missiles, mining, quarrying and similar fields. The company was appointed agent for RFD Inflatable Marine Survival Equipment. This agency included sales, service inspection and repair of inflatable liferafts. The West Coast Branch of

3276-474: The Fairey VTO Project was used to test the basic configuration of future research craft. Each wing had a large aileron and the vertical fin carried a large rudder. The V.T.O. obtained 900 lbf (4.0 kN) thrust from each Beta nozzle and, for launching, used two solid-fuel boosters of 600 lbf (2.7 kN) each, bringing the total thrust up to 3,000 lbf (13 kN)—obviously more than

3360-546: The Fairey aircraft and those of other manufacturers improved manoeuvrability. Aircraft production was primarily at the factory in North Hyde Road, Hayes (Middlesex), with flight testing carried out at Northolt Aerodrome (1917–1929), Great West Aerodrome (1930–1944), Heston Airport (1944–1947), and finally at White Waltham (1947–1964). Losing the Great West Aerodrome in 1944 by requisition by

3444-651: The Flight Engineer. This led Weir to cease further investment in the company and its development contracts were transferred to Saunders-Roe . Fairey Aviation The Fairey Aviation Company Limited was a British aircraft manufacturer of the first half of the 20th century based in Hayes in Middlesex and Heaton Chapel and RAF Ringway in Cheshire that designed important military aircraft, including

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3528-664: The Gannet AEW.3) and Fairey's 10% investment in the Aircraft Manufacturing Company ( Airco ) Fairey's workforce employed on manufacture of the outer wings of the Airco D.H.121. (later to be the HS 121 Trident ) was transferred to Westland. Fairey received 2,000,000 Westland shares of 5 shillings each and a cash payment of approximately £1.4m. The sale did not include Fairey Air Surveys or the works at Heston which

3612-592: The Government's decision to build three National Aircraft Factories was taken, Crossley Motors Ltd was formed to manage National Aircraft Factory No.2 as it was known. The factory continued to produce aircraft until November 1918. After the First World War the site switched to vehicle production. The factory was taken over by Willys-Knight and Overland Motors for the manufacture of cars and commercial vehicles and retained by them until 30 November 1934 when it

3696-428: The Royal Navy). Apart from installing radio gear the Queen also had some aerodynamic modifications to improve stability, however the first couple of pilotless flights came to quick endings as the drones crashed as soon as they left the catapult launcher on HMS Valiant . In 1960, Fairey announced an agreement between Fairey Engineering Ltd and the Del Mar Engineering Laboratories, Los Angeles, California, to distribute

3780-425: The Second World War, Fairey produced nearly 500 Bristol Beaufighters and nearly 600 Handley Page Halifax (326 B Mk III and 246 B Mk V) Post war they held subcontracts for production of the de Havilland Vampire , and its successor the de Havilland Venom . Fairey imported 50 Curtiss built D-12 engines in 1926, renaming them the Fairey Felix . Fairey's interest in missile production had been kept separate from

3864-434: The Tavistock works and continued making Fairey-designed winches for a few years. The site was Superwinch's European base and manufacturing facility until its closure in 2019, when the US parent company ceased operations and the key assets were sold to the Westin company in San Dimas, California. Year of first flight in brackets As well as producing their own designs, Fairey produced other aircraft under subcontract. During

3948-453: The XV-1 project was terminated in 1957. In 1998, Carter Aviation Technologies successfully flew its technology demonstrator aircraft. The aircraft is a compound autogyro with a high-inertia rotor and wings optimized for high-speed flight. In 2005, the aircraft demonstrated flight at mu-1, with the rotor tip having airspeed equal to the aircraft's forward airspeed, without any vibration or control issues occurring. The high-inertia rotor allowed

4032-475: The acquisition of the four instrumentation and controls businesses of Spectris AG of Germany for £171m was the largest ever made by the company and marked an important strategic addition to the company's instrumentation and controls business. The reshaping of the group was marked with the change of name from Fairey Group to Spectris plc in May 2001. On 27 August 1931, Avions Fairey SA was founded by Fairey engineer Ernest Oscar Tips . Fairey aircraft had impressed

4116-403: The acquisition of the high technology businesses of Fairey, and their merging with Pearson's other engineering interests in 1982. However, these businesses were disposed of in 1986 as part of Pearson wishing to concentrate on core activities; acquired by Williams Holdings they became Williams Fairey Engineering Ltd and then WFEL Ltd . Other parts of the combined Fairey – Doulton group saw

4200-421: The aircraft industry during WWII both men decided that they should produce sailing dinghies and so recruited Charles Currey to help run the company when he came out of the Navy. In the following years, thousands of dinghies were produced by Fairey Marine including the Firefly, Albacore, Falcon, Swordfish, Jollyboat, Flying Fifteen, 505 and International 14's along with the much smaller Dinky and Duckling. Later on in

4284-420: The aircraft to hover for a brief moment during landing, even though the rotor is unpowered, and a prerotating gearbox allows the rotor to be accelerated for an autogyro-style jump takeoff. In 1954, KYB built an aircraft named the Heliplane . The Heliplane was a Cessna 170 B with the wings reduced to stubs, and a rotor powered by tip ramjets. DARPA was funding a project under the "Heliplane" name to develop

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4368-403: The autogyro, but can also drive the rotor to allow vertical takeoff and landing; it then changes to free spinning like an autogyro during cruising flight. In the helicopter, the spinning rotor blades draw air down through the rotor disc ; to obtain forward thrust, the rotor disc tilts forward so that air is also blown backwards. In the autogyro the rotor disc is by contrast tilted backwards; as

4452-460: The company became FBM Babcock Marine Ltd , Spectris plc, and WFEL (formerly Williams Fairey Engineering Limited), the latter manufacturing portable bridges. Founded in 1915 by Charles Richard Fairey (later Sir Richard Fairey) and Belgian engineer Ernest Oscar Tips on their departure from Short Brothers , the company first built under licence or as subcontractor aircraft designed by other manufacturers. The first aircraft designed and built by

4536-429: The crew. The second Gyrodyne prototype was rebuilt as the Jet Gyrodyne and used to develop a pressure-jet rotor drive system later for the Rotodyne transport compound gyroplane. At the tip of each stub wing were rearward-facing propellers which provided both yaw control and propulsion in forward flight. The Jet Gyrodyne flew in 1954, and made a true transition from vertical to horizontal flight in March 1955. This led to

4620-420: The designs of its products, including winch and free-wheeling front hubs for Land Rover vehicles. By the 1970s Fairey was manufacturing a wide range of winches, covering mechanical, hydraulic and electric drive and capstan/drum configurations. Fairey winches formed the bulk of the manufacturer-approved winch options for Land Rover throughout the 1970s and early 1980s. In 1975 Fairey designed and manufactured

4704-559: The development of the C.41 design to create the first gyrodyne , the Fairey FB-1 , that first flew in 1947. In 1943, the Aircraft Department of G & J Weir Ltd. was reconstituted as the Cierva Autogiro Company to develop helicopter designs for the Air Ministry . The post-war Cierva Air Horse was at the time (1948) the world's largest helicopter. The first prototype of the Air Horse crashed killing Alan Marsh , Cierva's manager and chief test pilot John "Jeep" Cable , Ministry of Supply Chief Helicopter Test Pilot, and J. K. Unsworth

4788-511: The end of aircraft production the Heaton Chapel works became Fairey Engineering Ltd and began production of medium and heavy engineering including portable bridges for military and emergency services use, notably the Medium Girder Bridge . Its bridges are in service with the British Army , U.S. Army and many other NATO forces. Fairey Engineering Ltd also made Nuclear Reactor cores and fuelling machines for Dungeness B and Trawsfynydd . The company became Williams Fairey Engineering in 1986, and

4872-537: The failure of the UK parent, Fairey Canada was acquired by IMP Group International . The Australian branch of Fairey Aviation was formed in 1948 as Fairey-Clyde Aviation Co Pty. Ltd , a joint venture with Clyde Engineering and incorporated the aircraft division of CEC. The name was changed in November 1951. Based in Bankstown , Sydney , the factory overhauled aircraft for the Royal Australian Air Force and Royal Australian Navy , converted RAN Firefly AS.5s to Trainer Mark 5 standard. The Special Projects Division built

4956-451: The gyrodyne concept around 2007. Aircraft developed for the project would use a rotor for takeoff and landing vertically, and hovering, together with substantial wings to provide most of the required lift at cruise, combining the large cargo capacity, fuel efficiency, and high cruise speed of fixed-wing aircraft with the hovering capabilities of a helicopter. The project was "…a multi-year $ 40-million, four-phase program. Groen Brothers Aviation

5040-411: The main thrust drives the craft forwards, air flows through the rotor disc from below, causing it to spin and create lift. The gyrodyne is capable of transitioning between these two modes of flight. Typically a gyrodyne also has fixed wings which provide some of the lift during forward flight, allowing the rotor to be offloaded. A computer simulation has suggested an optimum distribution of lift of 9% for

5124-399: The plane and subsequently faced redundancy payments of about £16 million in Belgium. The companies involved were as follows: The Fairey Britten-Norman Aircraft Company was taken over by Pilatus , then a subsidiary of the Oerlikon group in Switzerland. The rescue action was taken by the Government under section 8 of the Industry Act 1972 acquiring from the official receiver of

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5208-450: The propellers at cruise speeds, power would be provided to the rotor only to overcome the profile drag of the rotor, operating in a more efficient manner than the freewheeling rotor of an autogyro in autorotation . Bennett described this flight regime of the gyrodyne as an "intermediate state", requiring power to be supplied to both the rotor and the propulsion system. The Cierva Autogiro Company, Ltd's, C.41 gyrodyne pre-WW2 design study

5292-548: The prototype Fairey Rotodyne , which was developed to combine the efficiency of a fixed-wing aircraft at cruise with the VTOL capability of a helicopter to provide short haul airliner service from city centres to airports. It had short wings that carried two Napier Eland turboprop engines for forward propulsion and up to 40% of the aircraft's weight in forward flight. The rotor was driven by tip jets for takeoff and landing and translational flight up to 80 mph. Despite considerable commercial and military interest worldwide in

5376-428: The prototype Type Y Rotodyne for air transport, British orders were not forthcoming and British Government financial support was terminated in 1962. The division's new parent Westland Helicopters did not see good cause for further investment and the project was stopped. With the end of the Fairey Aviation programs, gyrodyne development came to a halt, although several similar concepts continued to be developed. In 1954,

5460-424: The rotor, and 91% for the wing. However if the rotor is too lightly loaded it can become susceptible to uncontrolled flapping. In Britain , Dr. James Allan Jamieson Bennett , Chief Engineer of the Cierva Autogiro Company, conceived an intermediate type of rotorcraft in 1936, which he named "gyrodyne" and which was tendered to the British Government in response to an Air Ministry specification . In 1939, Bennett

5544-460: The sales agency for all countries outside the US, and was also appointed by the Australian Department of Supply's to assist in the introduction of the Malkara to operational service and to design and produce modifications. The missile was in service with the Royal Armoured Corps , deployed on a special vehicle—the Humber Hornet , made by Wharton Engineering—which carried two rounds on launchers and two rounds stowed. The Hornet could be air-dropped, had

5628-524: The total weight. The Beta I rocket had two jets, one of which could be swivelled laterally and the other vertically, according to signals from an autopilot. The resulting mean thrust line could thus be varied to maintain controlled flight at low airspeeds. Fairey carried out many successful tests, the first of which was from a ship in Cardigan Bay in 1949. Fairey Rocket Test Vehicle 1, formerly known as LOPGAP ("Liquid Oxygen and Petrol Guided Anti-Aircraft Projectile"). The original design can be traced back to

5712-407: Was Ilford Photo SR101 in the form of 0.93in discs punched from 35 mm strip; weight 801; diameter 1.5in; length 1.25in; field of view 186 deg; exposure time 0.3 millisecond; effective relative aperture, approximately f/8. One hundred and ninety-two cameras were made in the initial production run. In 1988 this company was merged into AWA Defence Industries of Australia. Fairey Air Surveys, Ltd,

5796-428: Was about 17 ft in length with a diameter of 10 in. The body was fitted with four wings and four small control vanes. Fairey Australia also displayed an aerodynamic test vehicle, described as a "three-inch winged round". This was a simple projectile, without guidance, to aid investigations into the properties of various wing/body assemblies at high supersonic speeds. The example shown was about 6 ft long, and had

5880-474: Was absorbed into what eventually became Blom Aerofilms. Subsidiary companies were as follows:— Other companies were located in Nigeria, Zambia and the Republic of Ireland. The Fairey factory at Heaton Chapel , Stockport can trace its roots back to when Crossley Bros. Ltd having had by the end of 1916 supplied large numbers of tenders and aero engines to the Royal Flying Corps acquired premises at High Lane, Heaton Chapel to expand production. In 1917, following

5964-400: Was acquired by Fairey. In 1935 the Fairey company received a substantial order for Hendon night bombers and established production lines at the Heaton Chapel factory. The production facilities at Heaton Chapel were incorporated as the Stockport Aviation Company Limited on 11 February 1936 and the Company took a site at Ringway (now Manchester Airport), where test flights were carried out. After

6048-518: Was also involved in the early development of pilotless aircraft which led to the development of radio controlled pilotless target aircraft in Britain and the United States in the 1930s. In 1931, the Fairey "Queen" radio-controlled target was developed, building a batch of three. The Queen was a modified Fairey IIIF floatplane, (a catapult launched aircraft which was used for reconnaissance by

6132-491: Was by four 75 lbf (330 N)-thrust solid-fuel main rockets, but initially four additional booster rockets delivering further 5,600 lb thrust accelerated the Stooge off its 10 ft (3.0 m) long launching ramp. Unlike later designs, the Stooge was intended for high subsonic speeds—and limited ranges. The Stooge consisted of two-stage propulsion, an autopilot, radio control equipment with additional ground unit, and

6216-573: Was fired at an angle of 35 degrees with a maximum altitude of about 12,000 feet. The vehicle was launched by seven solid booster rockets which had a burn time of four seconds, after which the liquid fuel sustainer motor took over. At the 1954 Farnborough Airshow , Fairey Australia displayed a massive missile resembling the RTV-1. The base was formed by a booster unit about 6 ft high and 20 inches in diameter, stabilised by four large and four small fins and housing seven five-inch motors. The main body

6300-599: Was granted as a trademark to the Gyrodyne Company of America in 1950. The company was not involved in gyrodyne development, but instead produced a turbine-engined, remotely piloted drone helicopter, with coaxial rotors , for the United States Navy , designated as the QH-50 DASH . Cierva Autogiro Company The Cierva Autogiro Company was a British firm established in 1926 to develop

6384-477: Was home to the weapon division, which had a contract for research into advanced anti-tank missile systems. Fairey's remaining net worth was approximately £9.5m. In 1977 the Fairey Group went into receivership and was effectively nationalised by the Government. Fairey went into liquidation when it introduced a Britten-Norman Islander production line into its subsidiary company, Avions Fairey, and overproduced

6468-428: Was initially headquartered at 24 Bruton Street , London W1. and later at Reform Road, Maidenhead, with companies across the world. The aircraft ( Douglas Dakotas ) and technical offices were based at White Waltham, Berks, along with a special research laboratory. Here the company undertook the design and development of anti-vibration isolators which were incorporated into camera mountings. Both mapping and geophysical work

6552-813: Was issued a patent from the UK Patent Office , assigned to the Cierva Autogiro Company. On 23 August 1940 the Autogiro Company of America , licensees of the Cierva Autogiro Company, Ltd., filed a corresponding patent application in the United States . On 27 April 1943, US patent #2,317,340 was issued to the Autogiro Company of America. The patents describe a gyrodyne as: a rotary wing aircraft intermediate in type, hereinafter referred to as "gyrodyne", between

6636-579: Was located at the Hayes factory, and used designs based on the patents of Sylvanus Albert Reed . C. R. Fairey first encountered Reed's products in the mid-1920s when investigating the possibilities of the Curtiss D-12 engine. The Curtiss company also manufactured propellers designed by Reed. Another example of utilising the talents of independent designers was the use of flaps, designed by Robert Talbot Youngman ( Fairey-Youngman flaps ) which gave many of

6720-418: Was the beam guidance test vehicle. Radar guidance was provided by a radar unit which projected a narrow beam. Different versions of the test vehicle were created and each was concerned with a different aspect of control, guidance, propulsion and aerodynamics of the complete rocket. The RTV 1e was a two-stage liquid fuel rocket used for research and development into problems associated with beam riding missiles. It

6804-867: Was then taken over by the Kidde portion of the American United Technologies Corporation. in 2000, and became now known as WFEL Ltd. In 2006 the Manchester Evening News reported that private equity investors Dunedin Capital Partners backed a management buy-out of WFEL from UTC which employs 160 people at its factory on Crossley Road, Heaton Chapel. In the post-war period, from the late 1950s onwards, Fairey acquired Mayflower Automotive Products, including their factory in Tavistock , Devon , and with it

6888-600: Was to be reorganised following a proposal to concentrate aircraft and allied manufacturing activities in the United Kingdom into a new wholly owned subsidiary called the Fairey Aviation Co. Ltd . The Board felt that the change, taking effect on 1 April 1959, would enable the Rotodyne and other aircraft work to be handled by a concern concentrating on aviation. It is proposed to change the company's name to

6972-478: Was undertaken. The UK based aircraft were sent out to work all over the world. The company undertook aerial surveys for local authorities within the UK and for many overseas Governments. Maps were also published under the Fairey-Falcon imprint. Over the years the companies names were changed to reflect Fairey ownership and operated into the late 1970s, later becoming Clyde Surveying Services Ltd. Fairey Surveys

7056-468: Was updated and built by Fairey Aviation as the FB-1 Gyrodyne commencing in 1945. Fairey's development efforts were initially led by Bennett, followed by his successor Dr. George S. Hislop . George B.L. Ellis and Frederick L. Hodgess, engineers from the pre-WW2 Cierva Autogiro Company, Ltd., joined Bennett at Fairey Aviation. The first Fairey Gyrodyne prototype crashed during a test flight, killing

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