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Secondary electric power generation with minimum engine bleedSecondary electric power generation with minimum engine bleed is discussed. Present and future jet engine systems are compared. The role of auxiliary power units is evaluated. Details of secondary electric power generation systems with and without auxiliary power units are given. Advanced bleed systems are compared with minimum bleed systems. A cost model of ownership is given. The difference in the cost of ownership between a minimum bleed system and an advanced bleed system is given.
Document ID
19840001992
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tagge, G. E. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Aircraft Elect. Secondary Power
Subject Category
Mechanical Engineering
Accession Number
84N10059
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19840001988Collected WorksAircraft Electric Secondary Power
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