GB1007120A - - Google Patents

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Publication number
GB1007120A
GB1007120A GB1007120DA GB1007120A GB 1007120 A GB1007120 A GB 1007120A GB 1007120D A GB1007120D A GB 1007120DA GB 1007120 A GB1007120 A GB 1007120A
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GB
United Kingdom
Prior art keywords
turbine
duct
low pressure
compressor
high pressure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Application number
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English (en)
Publication of GB1007120A publication Critical patent/GB1007120A/en
Active legal-status Critical Current

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  • Engine Equipment That Uses Special Cycles (AREA)
GB1007120D Active GB1007120A (enrdf_load_stackoverflow)

Publications (1)

Publication Number Publication Date
GB1007120A true GB1007120A (enrdf_load_stackoverflow)

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ID=1754909

Family Applications (1)

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GB1007120D Active GB1007120A (enrdf_load_stackoverflow)

Country Status (1)

Country Link
GB (1) GB1007120A (enrdf_load_stackoverflow)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4222234A (en) * 1977-07-25 1980-09-16 General Electric Company Dual fan engine for VTOL pitch control
GB2264751A (en) * 1992-03-04 1993-09-08 Snecma Jet propulsion engine.

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4222234A (en) * 1977-07-25 1980-09-16 General Electric Company Dual fan engine for VTOL pitch control
GB2264751A (en) * 1992-03-04 1993-09-08 Snecma Jet propulsion engine.
GB2264751B (en) * 1992-03-04 1996-01-24 Snecma Propulsion engine

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