Combustion chamber for axial flow gas turbines
United States Patent 2742762
US Patent References:
Starting up system for heat producing and consuming plants
- - 2227666
Secondary combustion air distribution control for bridge wall furnaces
- - 2471101
Air nozzle and porting for combustion chamber liners
- - 2510645
Combustor with sectional housing and liner
- - 2547619
Combustion chamber for gas turbines with circumferentially arranged pulverized solidfuel and air nozzles
- - 2601390
Starting up system for heat producing and consuming plants
- - 2227666
Secondary combustion air distribution control for bridge wall furnaces
- - 2471101
Air nozzle and porting for combustion chamber liners
- - 2510645
Combustor with sectional housing and liner
- - 2547619
Combustion chamber for gas turbines with circumferentially arranged pulverized solidfuel and air nozzles
- - 2601390
Inventors:
Kuhring, Malcolm S.
Publication Date:
04/24/1956
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Export Citation:
Assignee:
NAT RES COUNCIL
Primary Class:
International Classes:
F23R3/06; F23R3/10; F23R3/04
US Patent References:
| 2631429 | Cooling arrangement for radial flow gas turbines having coaxial combustors |
Foreign References:
| GB650462A | ||||
| GB650528A |