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A simplified fuel control approach for low cost aircraft gas turbinesReduction in the complexity of gas turbine fuel controls without loss of control accuracy, reliability, or effectiveness as a method for reducing engine costs is discussed. A description and analysis of hydromechanical approach are presented. A computer simulation of the control mechanism is given and performance of a physical model in engine test is reported.
Document ID
19730014002
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gold, H. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 26, 1973
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-68229
E-7254
Meeting Information
Meeting: Natl. Air Transportation Meeting
Location: Miami, FL
Country: United States
Start Date: April 24, 1973
End Date: April 26, 1973
Sponsors: Soc. of Automotive Engr.
Accession Number
73N22729
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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