Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Douglas DC-1

From Wikipedia, the free encyclopedia
(Redirected fromDC-1)
Piston airliner
"DC-1" redirects here. For other uses, seeDC-1 (disambiguation).
DC-1
Douglas DC-1 on its handover toTranscontinental & Western Air (Predecessor of Trans World Airlines) in December 1933
RolePrototype airliner
Type of aircraft
ManufacturerDouglas Aircraft Company
First flightJuly 1, 1933
IntroductionDecember,1933
StatusDestroyed
Primary userTranscontinental & Western Air
Number built1
Developed intoDouglas DC-2

TheDouglas DC-1 was the first model of the famous American DC (Douglas Commercial) commercial transport aircraft series. Although only one example of the DC-1 was produced, the design was the basis for theDC-2 andDC-3, the latter being one of the most successful aircraft in the history of aviation.

Design and development

[edit]

Development of the DC-1 can be traced back to the1931 crash of aTWA airliner, aFokker F-10 trimotor in which a wing failed, likely because water had seeped between the layers of the wood laminate and dissolved the glue holding the layers together. Following the accident, theAeronautics Branch of the U.S. Department of Commerce placed stringent restrictions on the use of wooden wings on passenger airliners.[1][2]Boeing developed an answer, the247, a twin-engined all-metalmonoplane with a retractable undercarriage, but their production capacity was reserved to meet the needs ofUnited Airlines, part ofUnited Aircraft and Transport Corporation which also owned Boeing. TWA needed a similar aircraft to respond to competition from the Boeing 247 and they asked five manufacturers to bid for construction of a three-engined, 12-seat aircraft of all-metal construction, capable of flying 1,080 mi (1,740 km) at 150 mph (242 km/h). The most demanding part of the specification was that the airliner would have to be capable of safely taking off from any airport on TWA's main routes (and in particularAlbuquerque, at high altitude and with severe summer temperatures) with one engine non-functioning.[3][4]

Donald Douglas was initially reluctant to participate in the invitation from TWA. He doubted that there would be a market for 100 aircraft, the number of sales necessary to cover development costs. Nevertheless, he submitted a design consisting of anall-metal, low-wing, twin-engined aircraft seating 12 passengers, a crew of two and a flight attendant. The aircraft exceeded the specifications of TWA even with only two engines, principally through the use ofcontrollable pitch propellers.[5] It was insulated against noise, heated, and fully capable of both flying and performing a controlled takeoff or landing on one engine.

Donald Douglas stated in 1935 that the first DC-1 cost $325,000 to design and build.[6]

Operational history

[edit]
DC-1 in TWA markings

Only one aircraft was produced. The prototypefirst flew on July 1, 1933,[7] flown byCarl Cover. It was given the model nameDC-1, or Douglas Commercial Model 1.[8] During a half-year of testing, it performed more than 200 test flights and demonstrated its superiority over the most-used airliners at that time, theFord Trimotor andFokker Trimotor. It was flown across the United States on February 19, 1934, making the journey in the record time of 13 hours 5 minutes.[9]

TWA accepted the aircraft on 15 September 1933 with a few modifications (mainly increasing seating to 14 passengers and adding more powerful engines) and subsequently ordered 20 examples of the developed production model which was named theDouglas DC-2.[10]

The DC-1 was sold toLord Forbes in the United Kingdom in May 1938, who operated it for a few months before selling it inFrance in October 1938. It was then sold toLíneas Aéreas Postales Españolas (L.A.P.E.) inSpain in November 1938 and was also used by theSpanish Republican Air Force as a transport aircraft.[11] It was later operated byIberia Airlines from July 1939 with the nameNegron; it force-landed atMálaga Airport, Spain, on October 4, 1940 and was damaged beyond repair.[10]

Specifications (DC-1)

[edit]

Data from McDonnell Douglas Aircraft since 1920[12]

General characteristics

  • Crew: 2 pilots
  • Capacity: 12 passengers
  • Length: 60 ft 0 in (18.29 m)
  • Wingspan: 85 ft 0 in (25.91 m)
  • Height: 16 ft 0 in (4.88 m)
  • Wing area: 942 sq ft (87.5 m2)
  • Airfoil:root:NACA 2215;tip:NACA 2209[13]
  • Empty weight: 11,780 lb (5,343 kg)
  • Gross weight: 17,500 lb (7,938 kg)
  • Powerplant: 2 ×Wright SGR-1820F3 Cyclone 9-cylinder air-cooled radial piston engines, 690 hp (510 kW) each
  • Propellers: 3-bladed variable-pitch metal propellers

Performance

  • Maximum speed: 210 mph (340 km/h, 180 kn)
  • Cruise speed: 190 mph (310 km/h, 170 kn) at 8,000 ft (2,400 m)
  • Range: 1,000 mi (1,600 km, 870 nmi)
  • Service ceiling: 23,000 ft (7,000 m)

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

[edit]

Notes

[edit]
  1. ^Friedman and Friedman,Aeroplane Monthly May 2001, pp. 34–40.
  2. ^O'Leary,Aeroplane Monthly February 2007, p. 71.
  3. ^Francillon 1979, p. 166
  4. ^Pearcy,Air Enthusiast 1982, p. 60.
  5. ^Smith 1998, p. 10
  6. ^"Douglas Tells Secrets of Speed".Popular Mechanics. February 1935.
  7. ^Gradidge 2006, p. 9
  8. ^"Historical Snapshot: DC-1 Commercial Transport". Boeing. Archived fromthe original on June 4, 2023. RetrievedApril 4, 2022.
  9. ^"Air Power History"(PDF).Air Power History. Vol. 57, no. 1. April 1, 2010. p. 12. Archived fromthe original(PDF) on 2018-11-30.
  10. ^abGradidge 2006, p. 299
  11. ^"Aircraft that took part in the Spanish Civil War".Aircraft of the Spanish Civil War (zi.ku). Archived fromthe original on 2015-02-05. RetrievedFebruary 4, 2011.
  12. ^Francillon 1979, p. 173.
  13. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.

Bibliography

[edit]
  • Francillon, René J. (1979).McDonnell Douglas Aircraft since 1920. London: Putnam.ISBN 0-370-00050-1.
  • Freidman, Herbert M. and Ada Kera Friedman. "The Legacy of the Rockne Crash".Aeroplane, Vol. 29, No. 5, Issue 337, May 2001, pp. 34–40. London: IPC. ISSN 0143-7240.
  • Gradidge, Jennifer M., ed. (2006).DC-1, DC-2, DC-3: The First Seventy Years. Tonbridge: Air-Britain (Historians).ISBN 0-85130-332-3.
  • O'Leary, Michael. "Database: Douglas DC-1 & DC-2".Aeroplane, Vol. 35, No. 2, Issue 406, February 2007, pp. 70–89. London: IPC. ISSN 0143-7240.
  • Pearcy, Arthur. "Douglas Commercial Two".Air Enthusiast, Nineteen, August–November 1982, pp. 60–77. Bromley, UK: Fine Scroll. ISSN 0143-5450.
  • Serrano, José Luis González (March–April 1999). "Fifty Years of DC Service: Douglas Transports Used by the Spanish Air Force".Air Enthusiast (80):61–71.ISSN 0143-5450.
  • Smith, Richard K. (1998).Seventy-Five Years of Inflight Refueling: Highlights 1923–1998(PDF). Air Force History and Museums Program.

External links

[edit]
Civil/Commercial
Military
After-market
Foreign production
Airspeed (United Kingdom)
Kamov (Soviet Union)
GAZ (Soviet Union)
Nakajima (Japan)
Showa (Japan)
Reporting names
Accidents & Incidents
Notable aircraft
Topics
Piston-engined
Jet-engined
Never built
Douglas DC-1 at Wikipedia'ssister projects:
Authority control databases: NationalEdit this at Wikidata
Retrieved from "https://en.wikipedia.org/w/index.php?title=Douglas_DC-1&oldid=1280925173"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp