Modifications that Improve Performance of a Double Annular Combustor at Simulated Engine Idle Conditions PDF Download
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Author: Donald F. Schultz
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Languages : en
Pages :
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Author: Donald F. Schultz
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Donald F. Schultz
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Category : Aircraft gas-turbines
Languages : en
Pages : 36
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Author: Donald F. Schultz
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 40
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Author: Donald F. Schultz
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Category :
Languages : en
Pages :
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A test program was undertaken to determine if variable combustor geometry could be used to reduce exhaust emissions of a low-pressure-ratio jet engine operating at ground idle conditions. Three techniques for varying combustor geometry were simulated. Other techniques evaluated were radial fuel staging and the use of preheated fuel. When simulated variable combustor geometry was employed with radial fuel staging, combustion efficiency at a fuel-air ratio of 0.01 was increased from 77 to 95 percent, and exhaust emissions of unburned hydrocarbons and carbon monoxide were significantly reduced.
Author:
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Category :
Languages : en
Pages : 382
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Author:
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Category : Aeronautics
Languages : en
Pages : 310
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Category : Aeronautics
Languages : en
Pages : 994
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Category : Aeronautics
Languages : en
Pages : 920
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Category : Astronautics
Languages : en
Pages : 714
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Author: United States. National Aeronautics and Space Administration
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Category : Aeronautics
Languages : en
Pages : 774
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