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Title: Experimental clean combustor program, alternate fuels addendum, phase 2. Final report

Technical Report ·
OSTI ID:7318528

The characteristics of current and advanced low-emissions combustors when operated with special test fuels simulating broader range combustion properties of petroleum or coal derived fuels were studied. Five fuels were evaluated; conventional JP-5, conventional No. 2 Diesel, two different blends of Jet A and commercial aromatic mixtures - zylene bottoms and naphthalene charge stock, and a fuel derived from shale oil crude which was refined to Jet A specifications. Three CF6-50 engine size combustor types were evaluated; the standard production combustor, a radial/axial staged combustor, and a double annular combustor. Performance and pollutant emissons characteristics at idle and simulated takeoff conditions were evaluated in a full annular combustor rig. Altitude relight characteristics were evaluated in a 60 degree sector combustor rig. Carboning and flashback characteristics at simulated takeoff conditions were evaluated in a 12 degree sector combustor rig. For the five fuels tested, effects were moderate, but well defined. (GRA)

Research Organization:
General Electric Co., Cincinnati, OH (USA)
DOE Contract Number:
NAS3-18551
OSTI ID:
7318528
Report Number(s):
N-76-22398; NASA-CR-134972; R-76AEG268
Country of Publication:
United States
Language:
English