General Considerations in the Design of Combustion Chambers for Aircraft and Industrial Gas Turbines 640009
This paper reviews those requirements that are common in the design of all gas turbines combustion equipment. Where necessary, a distinction is made between the demands of industrial and aircraft chambers. The problem of designing equipment for long life and low pressure loss, in a size compatible with the overall engine, is discussed in detail, and the application of combustor characteristics and design factors to the demands of new aircraft and industrial turbines are anticipated.
Citation: Clarke, J. and Jackson, S., "General Considerations in the Design of Combustion Chambers for Aircraft and Industrial Gas Turbines," SAE Technical Paper 640009, 1964, https://doi.org/10.4271/640009. Download Citation
Author(s):
J. S. Clarke, S. R. Jackson
Affiliated:
Joseph Lucas, Ltd
Pages: 20
Event:
SAE World Congress & Exhibition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Gas turbines
Combustion chambers
Combustion and combustion processes
Aircraft
Design processes
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