AU2398156A - Improvements in and relating to combustion systems for axial-flow gas turbine engines and ramjet engines - Google Patents

Improvements in and relating to combustion systems for axial-flow gas turbine engines and ramjet engines

Info

Publication number
AU2398156A
AU2398156A AU23981/56A AU2398156A AU2398156A AU 2398156 A AU2398156 A AU 2398156A AU 23981/56 A AU23981/56 A AU 23981/56A AU 2398156 A AU2398156 A AU 2398156A AU 2398156 A AU2398156 A AU 2398156A
Authority
AU
Australia
Prior art keywords
engines
relating
axial
gas turbine
flow gas
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.)
Expired
Application number
AU23981/56A
Other versions
AU212714B2 (en
Inventor
Amos Stokes and Robert William Oliver Papworth Morris
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors Ltd
Filing date
Publication date
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Application granted granted Critical
Publication of AU212714B2 publication Critical patent/AU212714B2/en
Publication of AU2398156A publication Critical patent/AU2398156A/en
Expired legal-status Critical Current

Links

AU23981/56A 1956-12-14 Improvements in and relating to combustion systems for axial-flow gas turbine engines and ramjet engines Expired AU212714B2 (en)

Publications (2)

Publication Number Publication Date
AU212714B2 AU212714B2 (en) 1957-06-20
AU2398156A true AU2398156A (en) 1957-06-20

Family

ID=

Similar Documents

Publication Publication Date Title
AU212714B2 (en) Improvements in and relating to combustion systems for axial-flow gas turbine engines and ramjet engines
AU2398156A (en) Improvements in and relating to combustion systems for axial-flow gas turbine engines and ramjet engines
AU209851B2 (en) Improvements in or relating to fuel systems of gas turbine engines
AU1961056A (en) Improvements in or relating to fuel systems of gas turbine engines
AU241031B2 (en) Improvements in and relating to fuel systems for gas turbine engines
AU5221059A (en) Improvements in and relating to fuel systems for gas turbine engines
AU233288B2 (en) Improvements in or relating to fuel systems for gas turbine aircraft engines
AU233299B2 (en) Improvements in or relating tothe operation of gas turbine engines and to fuel compositions for use in said engines
AU240768B2 (en) Improvements in or relating to fuel systems for gas turbine engines
AU162785B2 (en) Improvements in or relating to fuel systems for gas turbine engines
AU163023B2 (en) Improvements in or relating to fuel systems for gas turbine engines
CA531868A (en) Air inlet for airplane gaseous combustion turbine engines
AU206661B2 (en) Improvements in blades for gas turbine engines
AU215390B2 (en) Improvements in or relating to jet propulsion gas turbine engines
AU5219759A (en) Improvements in or relating to fuel systems for gas turbine aircraft engines
AU4112758A (en) Improvements in or relating tothe operation of gas turbine engines and to fuel compositions for use in said engines
AU225774B2 (en) Improvements in or relating to combustion apparatus of gas turbine engines orthe like
AU5219859A (en) Improvements in or relating to fuel systems for gas turbine engines
AU207378B2 (en) Improvements in or relating to axial flow compressors and gas turbine engines including such compressors
CA524435A (en) Continuous flow internal combustion engines and in particular aircraft ram-jets
AU204387B2 (en) Combustion systems for gas turbine engines
AU2712054A (en) Improvements in or relating to fuel systems for gas turbine engines
AU2528254A (en) Improvements in or relating to fuel systems for gas turbine engines
AU213686B2 (en) Improvements in and relating to liquid fuel systems for monofuel type gas turbines
AU1701556A (en) Improvements in blades for gas turbine engines