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Engine component improvement: JT8D and JT9D performance improvementsA feasibility analysis screening method for predicting the airline acceptance of a proposed engine performance improvement modification was developed. Technical information derived from available test data and analytical models is used along with conceptual/preliminary designs to establish the predicted performance improvement, weight and installation characteristics, the cost for new production and retrofit, maintenance cost and qualitative characteristics of the performance improvement concepts being evaluated. These results are used to arrive at the payback period, which is the time required for an airline to recover the investment cost of concept implementation, and to predict the amount of fuel saved by a performance improvement concept. The assumptions used to calculate the payback period and fuel saved are discussed. A summary of the results when the screening method is applied is presented for several representative JT8D and JT9D performance improvement concepts. An example of the input information used to develop the summary results is shown.
Document ID
19780019109
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gaffin, W. O.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1978
Publication Information
Publication: NASA. Langley Res. Center CTOL Transport Technol., 1978
Subject Category
Aircraft Propulsion And Power
Accession Number
78N27052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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