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Analytical fuel property effects. Small combustors. Phase 2 : final report

Author: T G Hill; J D Monty; H L Morton; General Electric Company. Aircraft Engine Business Group.; Lewis Research Center.
Publisher: Lynn, MA : Aircraft Engine Business Group, General Electric, [1985]
Series: NASA contractor report, NASA CR-174848.
Edition/Format:   Book   Microform : National government publication : Microfiche : EnglishView all editions and formats
Summary:
The effects of non-standard aviation fuels on a typical small gas turbine combustor were studied and the effectiveness of design changes intended to counter the effects of these fuels was evaluated. The T700/CT7 turboprop engine family was chosen as being representative of the class of aircraft power plants desired for this study. Fuel properties, as specified by NASA, are characterized by low hydrogen content and  Read more...
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Additional Physical Format: Online version:
Hill, T.G.
Analytical fuel property effects.
(OCoLC)708252503
Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: T G Hill; J D Monty; H L Morton; General Electric Company. Aircraft Engine Business Group.; Lewis Research Center.
OCLC Number: 291101838
Notes: Distributed to depository libraries in microfiche.
"March 1985."
Reproduction Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 1 microfiche : negative.
Description: iv, 39 pages : illustrations.
Series Title: NASA contractor report, NASA CR-174848.
Responsibility: by T.G. Hill, J.D. Monty and H.L. Morton ; prepared for National Aeronautics and Space Administration, Lewis Research Center.

Abstract:

The effects of non-standard aviation fuels on a typical small gas turbine combustor were studied and the effectiveness of design changes intended to counter the effects of these fuels was evaluated. The T700/CT7 turboprop engine family was chosen as being representative of the class of aircraft power plants desired for this study. Fuel properties, as specified by NASA, are characterized by low hydrogen content and high aromatics levels. No. 2 diesel fuel was also evaluated in this program. Results demonstrated the anticipated higher than normal smoke output and flame radiation intensity with resulting increased metal temperatures on the baseline T700 combustor. Three new designs were evaluated using the non standard fuels. The three designs incorporated enhanced cooling features and smoke reduction features. All three designs, when burning the broad specification fuels, exhibited metal temperatures at or below the baseline combustor temperatures on JP-5. Smoke levels were acceptable but higher than predicted.

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