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Douglas Y1B-7

From Wikipedia, the free encyclopedia
American bomber/observation aircraft
Y1B-7
Y1B-7 of the 31st Bombardment Squadron
General information
TypeBomber/Observation aircraft
ManufacturerDouglas Aircraft Company
Primary userUnited States Army Air Corps
Number built14
History
Manufactured1932
First flight1931
RetiredJanuary 1939

TheDouglas Y1B-7 was a 1930s Americanbomber aircraft. It was the first USmonoplane given theB- 'bomber' designation. The monoplane was more practical and less expensive than thebiplane, and theUnited States Army Air Corps chose to experiment with monoplanes for this reason. At the time the XB-7 was ordered, it was being tested byDouglas Aircraft as an observational plane.

Design and development

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In 1929–1930, theDouglas Aircraft Company designed a new twin-enginedmonoplane observation aircraft to compete with theFokker XO-27, two prototypes of which had been ordered by theUnited States Army Air Corps in July 1929, as Douglas feared that the advanced Fokker would challenge Douglas's role as the major supplier of observation aircraft to the Air Corps. The Douglas proposals resulted in the Air Corps placing an order for two prototypes, theXO-35 andXO-36, on 26 March 1930. The two aircraft were to differ only in the engines fitted, with the XO-35 having gearedCurtiss V-1570-29 Conqueror engines, while the XO-36 used direct-drive V-1570-23, which both produced 600 hp (450 kW) each.[1][2]

The Douglas design hadgull wings mounted high on the aircraft's fuselage, the engines being suspended in streamlinednacelles under the wings by bracing struts. A retractabletailwheel undercarriage was fitted, the mainwheels retracting into the engine nacelles. The fuselage was a semi-monocoque structure with corrugatedduralumin covering, which housed the aircraft's crew of four: a nose gunner/observer, a pilot whose cockpit was situated ahead of the leading edge of the wing, an upper gunner who sat in a cockpit aft of the wing, and a radio operator housed within the fuselage. Armament was two .30 in machine guns.[1][2]

The projected performance of the new twin-engined Douglas and Fokker observation aircraft was much greater than theKeystonebiplanes (theKeystone B-3,B-4,B-5 andB-6) that equipped the Air Corps light bomber squadrons, and both Fokker and Douglas were instructed to complete one of their prototypes as a bomber, with the XO-36 being redesignated theXB-7, with provision to carry up to 1,200 lb (540 kg) of bombs on racks under the fuselage added.[3]

The XO-36 made its first flight at theSanta Monica, California factory of Douglas in spring 1931.[4] On 22 August 1931, the Air Corps placed an order for a small batch of service test aircraft, consisting of seven Y1B-7 bombers and five Y1O-35 observation aircraft. These differed from the prototypes by having smooth fuselage skins rather than the corrugated skins used on the prototype, while the fuselage was 11 in (280 mm) longer to adjust the aircraft'scenter of gravity. A revised fuel system was fitted, with more fuel carried in order to give the two-hour endurance specified by the Air Corps. More powerful Conqueror engines were fitted, with all aircraft using geared engines as used on the XO-35.[3]

Operational history

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The XO-35 was delivered to the Air Corps at its test center atWright Field,Ohio on 24 October 1931, with the XB-7 following in July 1932.[4] The twelve service test aircraft were completed between November 1932 and March 1933.[5] The Y1B-7s equipped the11th and31st Bombardment Squadrons atMarch Field,California,[3] while the Y1O-35s were issued to a number of Squadrons, including the88th Observation Squadron atBrooks Field,Texas.[6] One notable early use of the Y1B-7 was during a May 1933 exercise atFort Knox, where it was able to outrun biplane fighters like theBoeing P-12, showing that the Air Corps needed more modern fighters.[7]

Despite the aircraft's superior performance to the elderly Keystone biplanes, the Douglas monoplane never entered mass production either in the observation or bomber roles because newer, more capable aircraft, such as theMartin B-10, were under development while a change in Air Corps policy meant that it was no longer interested in buying more twin-engined observation aircraft.[8]

In February 1934, US PresidentFranklin D. Roosevelt cancelled allair mail contracts owing to a scandal relating to the award of contracts, thus initiating theAirmail Emergency, where the Air Corps was tasked with carrying the mail until new contracts could be awarded. The O-35s and B-7s were considered some of the most suitable aircraft in the Air Corps inventory for the air mail role, so the six remaining Y1B-7s and the five Y1O-35s, together with the XO-35, were assigned to air mail routes in the western United States, which included hazardous operations over theRocky Mountains, theCascade Range and theSierra Nevada.[9] By the time the Air Corps involvement in air mail flights ended in June 1934, the twelve O-35s and B-7s had flown 1,412 hours on mail flights, while four of the B-7s had been lost as a result of accidents.[10] The last O-35s and B-7s were withdrawn from use in December 1938.[11]

Variants

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XO-35
Prototype twin-engined observation aircraft. Two 600 hp (450 kW) geared Curtiss V-1570-29 engines driving three-bladed propellers. One built.[3]
XO-36
Prototype twin-engined observation aircraft. Two 600 hp (450 kW) direct-drive Curtiss V-1570-23 engines driving two-bladed propellers. Redesignated XB-7. One built.
XB-7
Prototype light bomber, with two direct-drive 600 hp (450 kW) V-1570-23 engines driving two bladed propellers. One built.[3]
Y1O-35
Service test batch of observation aircraft, powered by 650 hp (480 kW) V-1570-39 or 675 hp (503 kW) V-1570-53 engines. Five built.[3]
Y1B-7
Service test batch of bombers, powered by 640 hp (480 kW) V-1570-33 or 675 hp (503 kW) V-1570-53 engines. Seven built.[3]

Operators

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 United States

Specifications (Y1B-7)

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Data from McDonnell Douglas aircraft since 1920 : Volume I[12]

General characteristics

  • Length: 45 ft 11 in (14.00 m)
  • Wingspan: 65 ft (20 m)
  • Height: 11 ft 7 in (3.53 m)
  • Wing area: 621.2 sq ft (57.71 m2)
  • Empty weight: 5,519 lb (2,503 kg)
  • Gross weight: 9,953 lb (4,515 kg)
  • Max takeoff weight: 11,177 lb (5,070 kg)
  • Powerplant: 2 ×Curtiss V-1570-53 Conqueror V-12 liquid-cooled piston engines, 675 hp (503 kW) each
  • Propellers: 3-bladed metal propellers

Performance

  • Maximum speed: 182 mph (293 km/h, 158 kn)
  • Cruise speed: 158 mph (254 km/h, 137 kn)
  • Range: 411 mi (661 km, 357 nmi)
  • Ferry range: 632 mi (1,017 km, 549 nmi)
  • Service ceiling: 20,400 ft (6,200 m)
  • Time to altitude: 10,000 ft (3,000 m) in 8 minutes 42 seconds
  • Wing loading: 16 lb/sq ft (78 kg/m2)
  • Power/mass: 0.135 hp/lb (0.222 kW/kg)

Armament

  • Guns: 2 × 0.30 in (7.6 mm)machine guns
  • Bombs: 1,200 lb (540 kg) of bombs carried beneath the fuselage

See also

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Aircraft of comparable role, configuration, and era

Related lists

References

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Notes

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  1. ^abPelletierAir Enthusiast March/April 2002, pp. 30, 32.
  2. ^abFrancillon 1979, pp. 135–136.
  3. ^abcdefgPelletierAir Enthusiast March/April 2002, p. 32.
  4. ^abFrancillon 1979, p. 137.
  5. ^PelletierAir Enthusiast March/April 2006, pp. 33–34.
  6. ^PelletierAir Enthusiast March/April 2006, p. 34.
  7. ^PelletierAir Enthusiast March/April 2006, pp. 32–33.
  8. ^Francillon 1979, p. 138.
  9. ^PelletierAir Enthusiast March/April 2006, p. 35.
  10. ^Francillon 1979, p. 139.
  11. ^PelletierAir Enthusiast March/April 2006, p.40.
  12. ^Francillon, René J. (1988).McDonnell Douglas aircraft since 1920 : Volume I. London: Naval Institute Press. pp. 119–124.ISBN 0870214284.

Bibliography

[edit]
  • Francillon, René J.McDonnell Douglas Aircraft since 1920. London: Putnam, 1979.ISBN 0-370-00050-1.
  • Pelletier, Alain J. "Bombers as Postmen: Boeing Y1O-35 and Y1B-7".Air Enthusiast, No. 122, March / April 2006, pp. 30–40. ISSN 0143-5450.
  • Wagner, Ray.American Combat Planes. New York: Doubleday, 1982.ISBN 0-930083-17-2.

External links

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