Armstrong Siddeley Python: Difference between revisions

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m top: One known example still exists, so "is" rather than "was".
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<!-- 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= Python
|image= File:ASPython.jpg
|caption= An Armstrong Siddeley Python during [[National Advisory Committee for Aeronautics|NACA]] wind tunnel testing in 1949
}}{{Infobox Aircraft Engine
|type=[[Gas turbine]] [[turbopropTurboprop]]
|national origin= United Kingdom
|manufacturer= [[Armstrong Siddeley]]
|designer=
|first run= April {{avyear|1945}}
|introduced=
|retired=
|status=
|major applications= [[Westland Wyvern]]
|number built =
|program cost =
|unit cost =
|developed from = [[Armstrong Siddeley ASX]]
|developed into =
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|}
 
The '''Armstrong Siddeley Python''' wasis an early [[United Kingdom|British]] [[turboprop]] engine that was designed and built by the [[Armstrong Siddeley]] company in the mid-1940s. Its main use was in the [[Westland Wyvern]], a [[Aircraft carrier|carrier-based]]-based heavy fighter. The prototypes had used the [[Rolls-Royce Eagle (1944)|Rolls-Royce Eagle]] piston engine, but Pythons were used in production aircraft. In this application, the Python was rated at 4,110 eshp ([[equivalent shaft [[horsepower]] (eshp).
 
==Design and development==
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Lincoln B.2 ''RF403'' had two Pythons similarly installed and was used for high-altitude bombing trials at [[Woomera, South Australia]]. These trials were principally of the ballistic casings for the [[Blue Danube (nuclear weapon)|Blue Danube]] [[Nuclear weapon|atomic weapon]]: the Lincoln was the only available aircraft that could accommodate the large weapon casing, measuring 62 inches diameter x {{convert|24|ft|m}} in length. The Pythons were fitted to increase the [[Flight ceiling|height]] from which tests could be carried out. Maximum release height and speed for the first eleven tests was 275&nbsp;mph and {{convert|34,783|ft|m|abbr=on}} with a bombing error of 61&nbsp;ft.<ref>The National Archives, London, file ES 1/44 E4C Appendix 3 page 1.</ref>
 
==Python Engine on public display==
An Armstrong Siddeley Python is on display at the [[East Midlands Aeropark]] Castle Donington.
 
==Variants==
;ASP.1 (Python 1):reduction gear ratio 0.127:1
;ASP.2 (Python 2):reduction gear ratio 0.135:1
;ASP.3 (Python 3):
 
==Applications==
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|<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
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|ref=''Flight''.<ref>[http://www.flightglobal.com/pdfarchive/view/1954/1954%20-%200979.html Flight Global Archive - 1954] www.flightglobal.com. Retrieved: 3 November 2008</ref>
|type=[[Turboprop]]
|length=123.2 in (3129313 mmcm)
|diameter=54 in (1372137 mmcm)
|weight=3,450 lb (15651,565 kg)
|compressor=axialAxial flow; 14 stages
|combustion=11 combustion chambers
|turbine=axialAxial flow; two stages
|fueltype=
|oilsystem=
|power=4,110 [[eshp]] (3,065 kW) at sea level at 8,000 rpm, including 1,180 lbf (535 kgf[[Kilopond|kp]]) exhaust thrust
|thrust=
|compression=5.35:1
|aircon=52.5 lb/secs (23.8&nbsp; kg/s)
|turbinetemp=
|fuelcon=
|specfuelcon=0.805 lb/hr/(h eshp)
|power/weight=1.2:1
|thrust/weight=}}
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===Bibliography===
{{refbegin}}
* {{cite book|last1=Gunston|first1=Bill|title=World encyclopaedia of aero engines : all major aircraft power plants, from the Wright brothers to the present day|date=1998|publisher=P. Stephens|___location=Sparkford, Nr Yeovil, Somerset, [England]|isbn=978-1852605971|edition=4th}}
* Gunston, Bill. ''World Encyclopedia of Aero Engines''. Cambridge, England. Patrick Stephens Limited, 1998. ISBN 1-85260-597-9
* {{cite book |last=Gunston |first=Bill |title=World Encyclopaedia of Aero Engines |year=1989 |publisher=Patrick Stephens Limited |___location=Cambridge, England |isbn=978-1-85260-163-8 |edition=2nd}}
* {{cite book |title=Jane's all the World's Aircraft 1947 |editor1-last=Bridgman |editor1-first=Leonard |year=1947 |publisher=Sampson Low, Marston & Co |___location=London|pages=4d–5d}}
{{refend}}
 
==External links==
{{commonsCommons category|Armstrong Siddeley Python}}
*[http://1000aircraftphotos.com/Contributions/Braas/9314.htm Image of the Python-engined Lancaster B.Mk.I (FE) ''TW911'']
*[http://www.flightglobal.com/pdfarchive/view/1949/1949%20-%201399.html "Python"] a 1949 ''Flight'' article on the Python
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{{ASaeroengines}}
 
[[Category:Turboprop1940s enginesturboprop 1940–1949engines]]
[[Category:Armstrong Siddeley aircraft engines|Python]]
[[Category:Axial-compressor gas turbine engines]]