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Transition in Gas Turbine Control System Architecture: Modular, Distributed, and EmbeddedControls systems are an increasingly important component of turbine-engine system technology. However, as engines become more capable, the control system itself becomes ever more constrained by the inherent environmental conditions of the engine; a relationship forced by the continued reliance on commercial electronics technology. A revolutionary change in the architecture of turbine-engine control systems will change this paradigm and result in fully distributed engine control systems. Initially, the revolution will begin with the physical decoupling of the control law processor from the hostile engine environment using a digital communications network and engine-mounted high temperature electronics requiring little or no thermal control. The vision for the evolution of distributed control capability from this initial implementation to fully distributed and embedded control is described in a roadmap and implementation plan. The development of this plan is the result of discussions with government and industry stakeholders
Document ID
20100036217
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Culley, Dennis
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
September 1, 2010
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2010-216806
E-17438
GT2010-23226
Report Number: NASA/TM-2010-216806
Report Number: E-17438
Report Number: GT2010-23226
Meeting Information
Meeting: Turbo Expo 2010
Location: Glasgow, Scotland
Country: United Kingdom
Start Date: June 14, 2010
End Date: June 18, 2010
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 561581.02.08.03.17.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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