Английская Википедия:Armstrong Siddeley Viper

Материал из Онлайн справочника
Версия от 19:45, 2 февраля 2024; EducationBot (обсуждение | вклад) (Новая страница: «{{Английская Википедия/Панель перехода}} {{short description|1950s British turbojet aircraft engine}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Use dmy dates|date=February 2018}} {{Use British English|date=February 2018}} {|{{Infobox Aircraft Begin |name= Viper |image= File:Rolls-Royce Viper 1.jpg |caption= Pr...»)
(разн.) ← Предыдущая версия | Текущая версия (разн.) | Следующая версия → (разн.)
Перейти к навигацииПерейти к поиску

Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English

The Armstrong Siddeley Viper is a British turbojet engine developed and produced by Armstrong Siddeley and then by its successor companies Bristol Siddeley and Rolls-Royce Limited. It entered service in 1953 and remained in use with the Royal Air Force, powering its Dominie T1 navigation training aircraft until January 2011.[1]

Design and development

The design originally featured a seven-stage compressor based on their Adder engine — the Viper is in effect a large-scale Adder.

Like the similar J85 built in United States, the Viper was originally developed as an expendable engine for production versions of the Jindivik target drone. Like the J85, the limited-life components and total-loss oil systems were replaced with standard systems for use in crewed aircraft.[2]

Because it was initially developed as an expendable engine, the Viper was subject to many recurring maintenance issues. This led to the development of the first Power by the Hour program in which operators would pay a fixed hourly rate to Bristol Siddeley for the continual maintenance of the engines.[3]

In the 1970s, Turbomecanica Bucharest and Orao Sarajevo acquired the license for the Viper engine, which propelled various Romanian and Yugoslav built aircraft.[4][5]

Variants

Файл:RR Viper 202.jpg
Rolls-Royce Viper in RAF Museum Cosford

Data from:Jane's All the World's Aircraft 1955-56,[6] Jane's all the World's Aircraft 1959-60,[7] Jane's All the World's Aircraft 1962-63[8]

ASV.1
Short life design study; Шаблон:Convert.
ASV.2
Developed short life version, first run in April 1951; Шаблон:Convert.
ASV.3
(Mk.100) Short life for missile/target applications, flight-tested in the tail of an Avro Lancaster November 1952; Шаблон:Convert.
ASV.4
Short life for missile/target applications first run in 1952, Шаблон:Convert.
ASV.5
(Mk. 101) Extended life version for crewed aircraft.[6]
ASV.6
Short life for missile/target applications; Шаблон:Convert.
ASV.7
ASV.7/R
ASV.7 with re-heat; Шаблон:Convert.
ASV.8
(became Viper 8 and Mk.102); Long-life version rated at Шаблон:Convert for Jet Provost T Mk.3.
ASV.9
(became Viper 9 and Mk.103) Similar to ASV.8 with improved turbine materials; Шаблон:Convert.
ASV.10
Long-life version with re-designed Sapphire-style compressor first run in January 1956; Шаблон:Convert.
ASV.11
(became Viper 11 and Mk.200) ASV.10 with increased mass-flow; Шаблон:Convert.
ASV.12
(became Viper 12) up-rated ASV.11 with higher JPT and rated at Шаблон:Cvt
Viper 8
(Mk.102 / Mk.104): Engines for the Hunting-Percival Jet Provost TMk.3 (Mk.102) and GAF Jindivik Mk.102B target drone (Mk.104).
Viper 9
(Mk.103): Powered the Bell X-14 and Handley Page HP 115 among others.
Viper 11
(Mk.200): Powered the Hunting-Percival Jet Provost TMk.4(Mk202) and GAF Jindivik Mk.3 among others.
Viper 12
see ASV.12 above
Viper 20
(Mk.500 series): Powered the Hawker Siddeley HS.125 and Piaggio-Douglas PD.808 among others.
Viper 22
Built under licence by Piaggio for the Aermacchi MB.326
Mk.100
see ASV.3 above
Mk.101
see ASV.5 above
Mk.102
see ASV.8 above
Mk.103
see ASV.9 and Viper 9 above
Mk.104
see ASV.12 above
Mk.200
see Viper 11 above
Mk.201
Mk.202
see Viper 11 above
Mk.204
Mk.301
Mk.521
Mk.522
Mk.525
Mk.601
Mk.632
Built under licence by Turbomecanica and Orao, as the non-afterburning engine for the IAR-93 Vultur A/MB versions, Soko J-22 Orao 1 version, IAR-99 Standard/Șoim versions, and Soko G-4 Super Galeb.
Mk.633
Built under licence by Turbomecanica and Orao, as the afterburning engine for the IAR-93 Vultur B version, and Soko J-22 Orao 2 version.
M.D.30 Viper
Engines licence-built and developed by Dassault Aviation[6][9]
M.D.30R Viper
Шаблон:Cvt with afterburner.[10]

Applications

Шаблон:Columns-list

Specifications (Viper ASV.12)

Шаблон:Jetspecs

See also

Шаблон:Aircontent

References

Notes

Шаблон:Reflist

Bibliography

  • Шаблон:Cite book
  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. Шаблон:ISBN
  • Smith, Tom. "Expendable to Indispensable: The Story of a Classic Turbojet - The Viper". Air Enthusiast, No. 55, Autumn 1994, pp. 37–55. Шаблон:ISSN

External links

Шаблон:Commons category


Шаблон:ASaeroengines Шаблон:Bristol aeroengines Шаблон:RR aeroengines

Партнерские ресурсы
Криптовалюты
Магазины
Хостинг
Разное

  1. ↑ Dominie T1 Шаблон:Webarchive www.raf.mod.uk. Retrieved: 14 October 2009
  2. ↑ Gunston 1989, p.20.
  3. ↑ Шаблон:Cite web
  4. ↑ About Turbomecanica
  5. ↑ INCAS - IAR 93 and SOKO /VTJ - J - ORAO Specifications
  6. ↑ 6,0 6,1 6,2 Шаблон:Cite book
  7. ↑ Шаблон:Cite book
  8. ↑ Шаблон:Cite book
  9. ↑ Шаблон:Cite book
  10. ↑ Шаблон:Cite book
Источник — http://wikihandbk.com/ruwiki/index.php?title=Английская_Википедия:Armstrong_Siddeley_Viper&oldid=13248653