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    737/CFM56-7 Aircraft Engine Systems (2006)
    In:  CASI
    Details
    Publication Date: 2018-06-06
    Description: The configuration of the propulsion system engine externals must meet many airplane requirements such as cost, thrust, weight, range and systems power extraction. On the 737-700 several program requirements also played a major role in the development of the engine externals. These program goals were increased range, same cost as a 1994 737-300, 15% reduction in maintenance costs from the 737-300, and a propulsion package that appeared as if it was designed by one company. This presentation will show how these requirements shaped the design of the engine externals for the 737-700/CFM56-7B.
    Keywords: Aircraft Propulsion and Power
    Type: Seals/Secondary Fluid Flows Workshop 1997; Volume I; 397-434; NASA/CP-2006-214329/VOL1
    Format: application/pdf
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