Английская Википедия:Bell 214ST

Материал из Онлайн справочника
Перейти к навигацииПерейти к поиску

The Bell 214ST is a medium-lift, twin-engine helicopter descended from Bell Helicopter's ubiquitous UH-1 Huey series. Though it shares a type number with the somewhat-related Bell 214, the 214ST is larger and of quite different appearance.

Design and development

The Bell 214ST was originally developed as a military project from the Bell 214B BigLifter, specifically for production in Iran and the development by Bell was funded by the Iranian government.[1] The fundamental difference was the replacement of the Model 214's single Lycoming LTC-4 turboshaft engine with two Шаблон:Convert General Electric T700 engines, to improve the helicopter's hot and high performance and improve safety. An interim twin-engine conversion of a Model 214 flew on 15 February 1977 in Texas,[2][3] Testing was successful, and Bell decided to press forward with a definitive twin-engine Bell 214ST, with a fuselage stretched by Шаблон:Convert and a revised main rotor of greater diameter. Iran changed its production plans, with 50 Bell 214A and 350 214STs to be built at the new production plant to be set up at Isfahan, Iran.[4]

Work started on three conforming prototypes in 1978.[5] The overthrow of the Shah in 1979 resulted in the cancellation of Iran's orders. By this time the new helicopter had attracted sufficient interest from other potential customers for Bell to continue with the project and build the 214ST at their Dallas-Fort Worth facility instead. As a result, it was launched as a civil helicopter, rather than a military one.[1][6][7]

Файл:Bell214STSuperTransporterN724HT.JPG
A Bell 214ST of Helicopter Transport Services

The first of the three full 214ST prototypes flew on 21 July 1979.[7] Manufacturing of production 214STs began in 1981. Type certification from the FAA and CAA for visual and instrument flight rules was awarded in 1982.[8] The military variant followed into production with helicopter deliveries commencing in 1982.[2]

The Bell 214ST included major design changes from the Bell 214. The Bell 214ST has a larger, stretched fuselage with seating for 16-18 passengers,[9][10] and two Шаблон:Convert GE CT7-2A engines.[11] The helicopter introduced some ground-breaking innovations for Bell, including a one-hour run-dry transmission, fiberglass rotor blades, elastomeric rotorhead bearings, and the option of either skid or wheeled landing gear.[1] The helicopter has a cockpit door and a large cabin door on each side. The 214ST has a fuel capacity of 435 US gallons (1,650 L). An auxiliary fuel system could be added.[10]

The Model 214ST was the largest helicopter that had been built by Bell at that time[9] (since surpassed by the Bell 525 Relentless)[12] The ST was originally an acronym for "Stretched Twin", but was later changed to "Super Transporter".[9][11] Bell built a total of 96 214STs with production ending in 1993.[13]

The military operators included Iraq (48),[14] Brunei (1), Peru (11), Thailand (9) and Venezuela (4).

Operators

Military operators

Шаблон:BRN
Файл:Iraqi Model 214ST SuperTransport helicopter, 1991.JPEG
An Iraqi Air Force Bell 214ST
Шаблон:PER

Civil operators

Шаблон:CAN
  • Helicopter Transport Services[17]
Шаблон:USA
Шаблон:JPN
Файл:British Caledonian Helicopters Bell 214ST.jpg
A British Caledonian Helicopters Bell 214ST

Former operators

Шаблон:Flaglist
Шаблон:Flag / Шаблон:Flag
Шаблон:THA
Шаблон:UK
Шаблон:VEN

Aircraft on display

United States

Specifications (214ST)

Файл:Bell 214ST orthographical image.svg

Шаблон:Aircraft specs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

External links

Шаблон:Commons category-inline Шаблон:Bell Aircraft Шаблон:Huey family

  1. 1,0 1,1 1,2 Apostolo, Giorgio. The Illustrated Encyclopedia of Helicopters, p. 54. New York: Bonanza Books, 1984. Шаблон:ISBN.
  2. 2,0 2,1 Green, William, Observers Aircraft, p. 228. Frederick Warne Publishing, 1991. Шаблон:ISBN.
  3. Air International October 1982, p. 165.
  4. Air International October 1982, pp. 165–166.
  5. Donald, David, ed. "Bell Model 214ST". The Complete Encyclopedia of World Aircraft. Barnes & Nobel Books, 1997. Шаблон:ISBN.
  6. Lambert Flight International 30 June 1979, p. 2345.
  7. 7,0 7,1 Air International October 1982, p. 166.
  8. 8,0 8,1 Pelletier, Alain J. Bell Aircraft Since 1935. US Naval Institute Press, 1992. Шаблон:ISBN.
  9. 9,0 9,1 9,2 Frawley, Gerard. The International Directory of Civil Aircraft, 2003-2004, p. 44. Aerospace Publications Pty Ltd, 2003. Шаблон:ISBN.
  10. 10,0 10,1 Lambert, M. "Bell 214ST". Jane's All the World's Aircraft 1990-91. Jane's Information Group, 1990. Шаблон:ISBN. (subscription article)Шаблон:Dead link
  11. 11,0 11,1 Green, William. Observers Aircraft, p. 224. Frederick Warne Publishing, 1987. Шаблон:ISBN.
  12. 'Relentless' 525 To Be Largest Bell Helicopter
  13. "Bell 214ST Supertransport" (subscription article)Шаблон:Dead link. Jane's Helicopter Markets and Systems. Jane's Information Group, November 28, 2011.
  14. Timmerman, Kenneth R. The Death Lobby: How the West Armed Iraq. New York: Houghton Mifflin Company, 1991.
  15. 15,0 15,1 Шаблон:Cite web
  16. Шаблон:Cite web
  17. Шаблон:Cite web
  18. Шаблон:Cite web
  19. Шаблон:Cite web
  20. Шаблон:Cite web
  21. Шаблон:Cite web
  22. Шаблон:Cite web
  23. Шаблон:Cite web
  24. Шаблон:Cite web
  25. Шаблон:Cite web
  26. Шаблон:Cite web
  27. Шаблон:Cite web
  28. "F3D Skyknight/124630." Шаблон:Webarchive Flying Leatherneck Aviation Museum. Retrieved: 16 January 2015.