Difference between revisions of "F4U Corsair (History)"
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=== Powerplant === | === Powerplant === | ||
+ | The F4U was powered by a Pratt and Whitney R-2800-8W radial engine. This was the most powerful and largest engine available when the F4U was being developed. An engine that powerful required a large propeller, 13 feet and 4 inches in diameter. The propeller was 3 bladed. | ||
− | === | + | === Wings and Landing Gear === |
+ | Since the F4U was designed as a carrier-based fighter, the wings needed to be foldable, so the plane would take up less room on an aircraft carrier. In order to allow folding wings, the landing gear could not fold into the wings, but would have to fold rearward. But because of the large propeller, rearward folding landing gear would need to be extremely long in order to maintain propeller clearance, threatening the structural stability of the landing gear. To solve this problem, the design was given inverted gull wings, which allowed the length of the landing gear to be reduced. | ||
− | + | The F4U was very aerodynamic for its time. It utilized spot welding in stead of rivets to decrease drag. It was also the first US Navy aircraft to have landing gear that retracted into a fully enclosed wheel well, and the supercharger air intakes were located in the wings, instead of using scoops that protrude from the aircraft. The Corsair also used fabric to cover the parts of the wing aft of the main spar, the ailerons, rudder, and elevators. All of these factors significantly reduced drag, increasing the aerodynamics of the aircraft. Despite this, when using the flaps, the Corsair could still perform carrier landings, as the flaps could be angled at 60° to decrease speed. | |
=== Technical Issues === | === Technical Issues === |
Revision as of 17:23, 26 March 2020
Writing in process... This article is being edited by the member CobraKingII (start date). Other participants are requested to not make any changes while this warning is here. |
Development
Origin
In 1938 the Navy wanted to find a design for a carrier-based fighter with more performance than the Brewster F2A and Grumman F4F. The design contract was given to Vought, based on their proposal, which featured a plane dependent on the Pratt and Whitney R-2800 Double Wasp engine. The design included an inverted gull wing shape. This was necessary because the engine required a large propeller, which needed a large ground clearance. This would require very long landing gear, except the inverted gull wing shape allowed shorter landing gear, while maintaining the necessary ground clearance. The prototype, named XF4U-1 was armed with 4 machine guns, two .50 caliber machine guns in the wings and 2 .30 caliber machine guns on the engine cowling. The XF4U-1 first flew on May 29, 1940, and became the first single engine plane to fly over 400 mph. Before Vought was allowed to produce the plane though, they had to increase its armament, as it was deemed insufficient based on data from Europe. Its armament was changed to six .50 machine guns, and it was ordered into production. A self-sealing fuel tank in the fuselage above the wings caused the cockpit to be moved aft as well. The Navy ordered 584 F4U-1's on April 2, 1941.
Design
Powerplant
The F4U was powered by a Pratt and Whitney R-2800-8W radial engine. This was the most powerful and largest engine available when the F4U was being developed. An engine that powerful required a large propeller, 13 feet and 4 inches in diameter. The propeller was 3 bladed.
Wings and Landing Gear
Since the F4U was designed as a carrier-based fighter, the wings needed to be foldable, so the plane would take up less room on an aircraft carrier. In order to allow folding wings, the landing gear could not fold into the wings, but would have to fold rearward. But because of the large propeller, rearward folding landing gear would need to be extremely long in order to maintain propeller clearance, threatening the structural stability of the landing gear. To solve this problem, the design was given inverted gull wings, which allowed the length of the landing gear to be reduced.
The F4U was very aerodynamic for its time. It utilized spot welding in stead of rivets to decrease drag. It was also the first US Navy aircraft to have landing gear that retracted into a fully enclosed wheel well, and the supercharger air intakes were located in the wings, instead of using scoops that protrude from the aircraft. The Corsair also used fabric to cover the parts of the wing aft of the main spar, the ailerons, rudder, and elevators. All of these factors significantly reduced drag, increasing the aerodynamics of the aircraft. Despite this, when using the flaps, the Corsair could still perform carrier landings, as the flaps could be angled at 60° to decrease speed.
Technical Issues
Design Modifications
Performance
Service
World War 2
United States
Marine Corps
Royal New Zealand Air Force
Captured Corsairs
Korean War
United States
"Football" War
Salvadoran Air Force and Honduran Air Force
Aces
Ira C. Kepford
A member of the famed VF-17 "Jolly Rogers" squadron, Kepford achieved a total of 16 confirmed kills in his F4U-1A.
Roger R. Hedrick
A member of VF-17, and later the Commanding Officer of VF-84, he got 12 confirmed kills in an F4U-1A and F4U-1D.
John T. Blackburn
He was the first Commanding Officer of VF-17, credited with 11 kills in his F4U-1A.
Thomas H. Reidy
A member of VBF-83, he was credited with 10 kills.
US Marine Corps
Gregory "Pappy" Boyington
The Marine Corp's top scoring ace, achieving 22 confirmed kills in an F4U-1A as part of VMF-214.
Kenneth A. Walsh
He had 21 confirmed kills in an F4U-1 and F4U-4, as part of VMF-124. He later was the Operations Officer of VMF-222.
James E. Swett
Serving in VMF-221 he was credited with 8.5 kills in an F4U, sharing one A6M "Zero" kill with another pilot. Before he flew the F4U he became an ace in a day by shooting down 7 planes in one action.
Archie Donahue
He is credited with 12 kills in an F4U while serving in VMF-112.
Variants
- F4U-1 (Corsair Mk I)
- First production version of the Corsair.
- F4U-1A (Corsair Mk II)
- Had a simplified canopy, along with other minor improvements that allowed for easier carrier landings.
- F3A-1 (Corsair Mk III)
- F4U-1 license-built by Brewster. Poor quality caused the contract to be terminated by the Navy.
- F3A-1D (Corsair Mk III)
- F4U-1A license-built by Brewster. Poor quality caused the contract to be terminated by the Navy.
- FG-1A (Corsair Mk IV)
- F4U-1 license-built by Goodyear.
- FG-1D (Corsair Mk IV)
- F4U-1A license-built by Goodyear.
- F4U-1B
- Post-war designation (unofficial) for F4U-1's modified for Fleet Air Arm (Royal Navy) service.
- F4U-1C
- An F4U-1D with four 20 mm cannons replacing the six .50 calibre machine guns.
- F4U-1D (Corsair Mk II)
- Had a new R-2800-8W engine, which was more powerful, allowing for more payload and performance.
- F4U-1P
- Photo reconnaissance variant.
- XF4U-2
- Night fighter variant with two auxiliary fuel tanks.
- F4U-2
- Experimental night fighter based on the F4U-1. The outer right machine gun was removed, so it had a total of five. An airborne intercept (AI) radar was equipped on the outer starboard wing.
- XF4U-3
- A variant designed for the testing of different engines in the F4U airframe.
- FG-3
- XF4U-3 license-built by Goodyear.
- XF4U-3B
- XF4U-3 with slight modifications, built for the FAA.
- XF4U-4
- A variant with a new engine and cowling.
- F4U-4
- Variant with a new 2100 hp dual-stage-supercharged 18-W engine, a four-bladed propeller, and other minor improvements.
- F4U-4B
- F4U-4's with four 20mm cannons instead of machine guns.
- F4U-4E
- Night fighter variant with the APS-4 search radar on the right wingtip. It had four 20 mm cannons instead of machine guns.
- F4U-4N
- Night fighter variant with the APS-6 search radar on the right wingtip. It had four 20 mm cannons instead of machine guns.
- F4U-4K
- Experimental drone variant.
- F4U-4P
- Photo reconnaissance variant of the F4U-4.
- XF4U-5
- A variant with a new engine cowling and other improvements.
- F4U-5
- F4U-4 with a more powerful Pratt and Whitney R-2800-32(E) engine. Other improvements included all-metal wings, a modernized cockpit, and a fully retractable tail wheel.
- F4U-5N
- A variant of the F4U-5 with a radar.
- F4U-5NL
- F4U-5N's equipped with rubber de-icing boots on the leading wing edge and leading tail edge. Made for cold temperatures of winter.
- F4U-5P
- Long-range photo-reconnaissance variant of the F4U-5.
- F4U-6
- A variant made for the Marine Corps with extra armour and oil coolers. It was designed for ground attack.
- AU-1
- Later redesignation of the F4U-6.
- F4U-7
- AU-1 in French service.
- FG-1E
- A Goodyear FG-1 with radar equipment.
- FG-1K
- Drone variant of the Goodyear FG-1.
- FG-3
- Turbo supercharged variant of the FG-1D.
- FG-4
- Goodyear produced F4U-4. It was never delivered.
- F2G-1
- Goodyear modified F4U-1 with a Pratt and Whitney R-4360, Wasp Major 4-row 28-cylinder radial engine. It had manual-folding wings. Never entered service.
- F2G-2
- F2G-1 with hydraulically folding wings and a tailhook for carrier landings. Never entered service.
Specifications
Operators
ArgentinaArgentine Navy operated 26 F4U-5/5N/5NL Corsairs from 1956 to 1968
Brazil
Brazilian Navy operated 30 F4U-1D from 1950 to 1976
Canada
Royal Canadian Navy operated 130 F4U-1D from 1948 to 1960
Chile
Chilean Navy operated 30 F4U-1D and 20 F4U-4 from 1953 to 1978
El Salvador
Air Force of El Salvador operated 25 F4U/FG-1D from 1957 to 1976
France
French Navy operated 69 AU-1 and 94 F4U-7 from 1954 to 1964
Honduras
Honduran Air Force operated 19 from 1956 to 1979
Netherlands
Royal Netherlands Navy operated 35 F4U-1D from 1943 to 1956
New Zealand
Royal New Zealand Air Force operated 368 F4U-1 and 60 FG-1D from 1944 to 1949
United Kingdom
Royal Navy Fleet Air Arm operated 2,012 Corsairs of all types during World War 2, including 95 Corsair I (F4U-1), 510 Corsair II (F4U-1A), 430 Corsair III (F3A-1D), and 977 Corsair IV (FG-1D)
United States
United States Navy and Marine Corps operated Corsairs of all production variants from 1942 to 1953