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Quiet Clean Short-haul Experimental Engine (QCSEE). Composite fan frame subsystem test reportThe element and subcomponent testing conducted to verify the composite fan frame design of two experimental high bypass geared turbofan engines and propulsion systems for short haul passenger aircraft is described. Emphasis is placed on the propulsion technology required for future externally blown flap aircraft with engines located both under the wing and over the wing, including technology in composite structures and digital engine controls. The element tests confirmed that the processes used in the frame design would produce the predicted mechanical properties. The subcomponent tests verified that the detail structural components of the frame had adequate structural integrity.
Document ID
19800006839
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stotler, C. L., Jr. (General Electric Co. Cincinnati, OH, United States)
Bowden, J. H. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-135010
R76AEG233
Accession Number
80N15098
Funding Number(s)
CONTRACT_GRANT: NAS3-18021
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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