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#http://www.digplanet.com/wiki/Turbo-Union_RB199 |
#http://www.digplanet.com/wiki/Turbo-Union_RB199 |
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#https://images.search.yahoo.com/search/images;_ylt=AwrBT8k5hZJXR.wAX7NXNyoA;_ylu=X3oDMTEyY3M1aWxwBGNvbG8DYmYxBHBvcwMxBHZ0aWQDVUkyQzJfMQRzZWMDc2M-?p=Turbo-Union+RB199+Aircraft+Turbofan+Jet+Engine&fr=yset_chr_cnewtab |
#https://images.search.yahoo.com/search/images;_ylt=AwrBT8k5hZJXR.wAX7NXNyoA;_ylu=X3oDMTEyY3M1aWxwBGNvbG8DYmYxBHBvcwMxBHZ0aWQDVUkyQzJfMQRzZWMDc2M-?p=Turbo-Union+RB199+Aircraft+Turbofan+Jet+Engine&fr=yset_chr_cnewtab |
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+ | #http://www.rolls-royce.com/Images/rb199_tcm92-6699.pdf |
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[[Category:Engineering]] |
[[Category:Engineering]] |
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[[Category:UK]] |
[[Category:UK]] |
Revision as of 18:42, 27 July 2016
The engine
The Turbo-Union RB199 is an aircraft turbofan jet engine designed and built in the early 1970s by Turbo-Union, a joint venture between the firms Rolls-Royce, MTU and Fiat-Avio. The RB199's sole production application is the Panavia Tornado.
The stats
- Made in: 1972
- Type: terbofan
- Length: 3,600 millimetres (142 in)
- Diameter: 720 millimetres (28.3 in)
- Dry weight: 976 kilograms (2,151 lb)
- Compressor:
- Combustors:
- Turbine: Single stage HP, Single stage IP, 2-stage LP
- Maximum thrust:
- Overall pressure ratio:
- Specific fuel consumption:
- Thrust-to-weight ratio:
- First made in: 1972
- Nationality: Joint British\Italian\W. German.
Links
- https://en.wikipedia.org/wiki/Turbo-Union_RB199
- http://www.mepcsa.com/Products---Services/RB199.aspx
- http://dictionary.sensagent.com/turbo%20union%20rb199/en-en/
- https://runnymedemeccanoguild.org.uk/gallery/sections/members,pete-wood,tornado-gr1-ids,turbounion-rb199-triple-spool-turbofan-engine
- http://www.digplanet.com/wiki/Turbo-Union_RB199
- https://images.search.yahoo.com/search/images;_ylt=AwrBT8k5hZJXR.wAX7NXNyoA;_ylu=X3oDMTEyY3M1aWxwBGNvbG8DYmYxBHBvcwMxBHZ0aWQDVUkyQzJfMQRzZWMDc2M-?p=Turbo-Union+RB199+Aircraft+Turbofan+Jet+Engine&fr=yset_chr_cnewtab
- http://www.rolls-royce.com/Images/rb199_tcm92-6699.pdf