词条 | Fairey Fulmar | ||||||||||||||||||
释义 |
The Fairey Fulmar was a British carrier-borne fighter aircraft that served with the Fleet Air Arm (FAA) during the Second World War. Fairey Aviation built 600 Fulmars at its Stockport factory between January 1940 and December 1942. The design was based on that of the earlier Fairey P.4/34 that was developed in 1936 as a replacement for the Fairey Battle light bomber. Although its performance (like that of its Battle antecedent) was unspectacular, the Fulmar was a reliable, sturdy aircraft with long range and an effective armament of eight machine guns. It was named after the northern fulmar, a seabird native to the British Isles. Design and developmentThe Fairey P.4/34 was built to Specification P.4/34 as a light bomber capable of being used as a dive bomber, in competition with the Hawker Henley and an unbuilt Gloster design.[1] Despite its high speed of 284 mph, the 300 mph Henley won the competition and was eventually ordered as a target tug.[2] The Fulmar was a version of the P.4/34 adapted for naval use and submitted to meet Specification O.8/38 for a two-crew, observation (reconnaissance) fleet defence fighter. As it was not expected to encounter fighter opposition (Germany, Britain's only potential enemy, possessed no aircraft carriers), manoeuvrability was not considered as important as long range and heavy armament. A navigator/wireless operator was considered essential for the long, ocean flights that would be required. Looking much like the Battle, the Fulmar prototype was aerodynamically cleaner and featured a folding wing that was {{convert|16|in|cm|abbr=on}} shorter.[3] The prototype P.4/34 serial number K5099 first flew on 13 January 1937 at Fairey Aviation's Great West Aerodrome (now covered by London Heathrow Airport), with the Fairey test pilot Chris Staniland at the controls.[4][5] After the first flight tests, the tail was raised by {{convert|8|in|cm|abbr=on}}. The first prototype Fulmar, acting as a "flying mock-up", was powered by a 1,080 hp (810 kW) Rolls Royce Merlin III engine.[5] Performance was poor, the prototype only reaching 230 mph (370 km/h). With the Merlin VIII engine – a variant unique to the Fulmar and with supercharging optimised for low-level flight and aerodynamic improvements, its speed increased to 265 mph (426 km/h) at 7500 ft (2286m), which, owing to the desperate need for modern fighters, was considered adequate.[6][7][8] As a simple derivative of a prototype, the Fulmar promised to be available quickly and an order for 127 production aircraft was placed in mid-1938.[4] The first example flew from Fairey's facility at RAF Ringway near Manchester on 4 January 1940 and the last of 600 Fulmars was delivered from Ringway on 11 December 1942.[9] Fulmar Mk II production began in January 1941, with the first Mk II reaching an operational squadron in March 1941.[10] This mark introduced the more powerful Merlin XXX engine; the airframe had provision for a 60-gallon (273 litre) centre-line drop tank and provision to carry a 250 lb (114 kg) or 500 lb (227 kg) bomb in lieu of the drop tank.[11] Testing of the Fulmar II, at Boscombe Down, in June 1942 showed that the Fulmar could safely drop a 500 lb bomb during 60-degree dives at up to 310 knots.[12] Boscombe Down testing in October 1941 showed that the 60-gallon drop tank extended range to {{convert|1100| mi|km|abbr=on}}.[12] Fulmars were launched from catapults on merchant ships, a convoy defensive plan that was being evaluated at the time.[13] N1854, the first production Fulmar, was later modified to Mk II standard and then used as Fairey's hack, G-AIBE. In June 1959, it reverted to service markings and was seen at Farnborough at the SBAC show on 8 September 1962; its last flight was three months later on 18 December 1962. It is now in the FAA Museum, Yeovilton. Operational historyThe first squadron to be equipped with the Fulmar was No. 806 Squadron FAA in July 1940, and this squadron began operating from {{HMS |Illustrious|R87|6}} shortly afterwards. The Fulmar was inferior in performance to land-based fighters. The Navy had specified a two-seat machine so that the pilot would have the assistance of another crew member in reporting back to the fleet the observations made, which were done using wireless telegraphy (W/T) and navigate over the ocean. The Fulmar was far too large and unwieldy in engagements with single-seat, land-based opposition, as it did in the Mediterranean Theatre. The long range of the Fulmar was useful at times. In the 1941 chase of the {{Ship | German battleship|Bismarck}}, Fulmars acted as carrier-borne spotters, tracking the battleship.[13] First seeing action on Malta convoy protection patrols in September 1940, the sturdy Fulmar was able to achieve victories against its far more agile Italian and German adversaries. By the autumn, Fulmars had shot down ten Italian bombers and six enemy fighters, as well as providing top cover to the Swordfish raid on Taranto. Fulmars played a prominent role in Operation EF, the ill-fated raid on Kirkenes and Petsamo in July 1941. By 1942, the Fulmar was being replaced by single-seat aircraft adapted from land fighters such as the Supermarine Seafire or American single-seaters such as the Grumman Martlet. It saw useful service as a night convoy escort and intruder and was used to train crews for the Fairey Barracuda. Its flight characteristics were considered pleasant, the wide undercarriage provided good deck handling and it had excellent fuel capacity and range. Fulmars were used in long-range reconnaissance after they were withdrawn as fighters. Most Fleet Air Arm fighter aces scored at least some of their victories in Fulmars; Sub Lieutenant Stanley Orr finished the war with twelve confirmed air victories, the third-highest scoring pilot in the FAA. At one time, twenty squadrons of the Fleet Air Arm were equipped with the Fulmar. It flew from eight fleet aircraft carriers and five escort carriers. No. 273 Squadron RAF operated them for some months in 1942 from China Bay, Ceylon, seeing action against Japanese forces during the raid on 9 April 1942, though about half the squadron personnel were Navy.[14] Fulmars destroyed 112 enemy aircraft, which made it the leading fighter type, by aircraft shot down, in the Fleet Air Arm during the Second World War. The Fulmar ended its front line operational career on 8 February 1945, when a Fulmar MK II night-fighter from No. 813 Squadron had a landing accident at the safety barrier on {{HMS|Campania|D48|6}} and was written off.[15] Approximately 100 Fulmars were converted to a night fighter variant but had limited success in this role.[13] The Vichy French captured one Fulmar Mk I, which force-landed while flying a reconnaissance mission over Senegal in March 1941. The Fulmar was repaired and used by the Group de Chasse I/4.[16] Some of the early marks of the aircraft were operated from CAM ships.[17] Variants
First production variant powered by a 1,035 hp (772 kW) (1,275 hp at take off)[6] Rolls-Royce Merlin VIII; 8 × .303 Browning Mk.II (750 rounds per gun),[7] 250 built.
Updated variant powered by a 1,300 hp (970 kW) Merlin XXX[6] with a new propeller and the addition of tropical equipment; 8 × .303 Browning Mk.II (1,000 rounds per gun) or 4 × .50 Browning AN/M2 – part of the last batch[7][18] (170 rounds per gun,[7] in other sources specified 370 rounds per gun), some finished as night fighters, one prototype converted from a Mk.I and 350 built.
Mk.II night fighter with an Air Interception AI Mk. IV radar (1 aircraft) or AI Mk.X radar (other); 4 × .50 Browning AN/M2 – about 50 aircraft (other 8 × .303 Browning Mk.II), total was converted from the Mk.II nearly 100 aircraft.[19] Operators
Surviving aircraftThe only known survivor is N1854, the Fulmar prototype (and first production Mk I) at the Fleet Air Arm Museum. The only known surviving Rolls-Royce Merlin VIII engine is in a private collection in the UK and came from Fulmar Mk I, N1926. Specifications (Mk II){{aircraft specifications|plane or copter?=plane |jet or prop?=prop |ref= |crew=Two |length main= 40 ft 2 in |length alt=12.25 m |span main=46 ft 4¼ in |span alt=14.13 m |height main=14 ft 0 in |height alt=4.27 m |area main=342 ft² |area alt=32 m² |empty weight main=7,015 lb |empty weight alt=3,182 kg |loaded weight main=9,672 lb |loaded weight alt=4,387 kg |max takeoff weight main=10,200 lb |max takeoff weight alt=4,627 kg |engine (prop)=Rolls-Royce Merlin 30 |type of prop=liquid-cooled inline V-12 |number of props=1 |power main=1,300 hp |power alt=970 kW |max speed main=272 mph at 7,250 ft |max speed alt=438 km/h at 2,200 m |range main=780 mi |range alt=1,255 km |ceiling main=27,200 ft |ceiling alt=8,300 m |climb rate main= |climb rate alt= |loading main= 28 lb/ft² |loading alt= 137 kg/m² |power/mass main= |power/mass alt= |armament=
}} See also{{aircontent|related=
|similar aircraft=
|lists=
|see also= }} ReferencesNotes1. ^Mason 1994, p. 306. 2. ^Thetford 1991, p. 152. 3. ^Winchester 2004, p. 85. 4. ^1 Mason 1992, p. 287. 5. ^1 Lumsden 1990, p. 354. 6. ^1 2 Brown 1973, p. 47. 7. ^1 2 3 4 Bussy 2004, p. 0. 8. ^Thetford 1991, p. 157: states 280 mph. Note: Almost all British aircraft could use emergency boost to increase the supercharger intake pressure and increase power at low altitude for short periods of time. The Merlin VIII engine was rated at 1,275 hp at take-off and the use of overboost gained this power rating in combat and 280 mph seems feasible. 9. ^Scholefield 1998, p. 35. 10. ^Brown 1973 {{page needed|date=June 2013}} 11. ^Bussy 2004 {{page needed|date=June 2013}} 12. ^1 Mason 1998, p. 269. 13. ^1 2 Winchester 2004, p. 84. 14. ^"History of No. 273 Squadron." {{webarchive |url=https://web.archive.org/web/20070713080102/http://www.raf.mod.uk/history_old/h273.html |date=13 July 2007 }} RAF History. Retrieved 25 October 2009. 15. ^Brown 1973, p. 41. 16. ^Ovčáčík and Susa 2001, p. 3. 17. ^Ireland 2007, p. 75. 18. ^1 Bussy 2004, p. 7. 19. ^Bussy 2004, p. 37. Bibliography{{Refbegin}}
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