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State of the NASA Aeropropulsion Discipline Input from the Glenn Research CenterPROBLEM: Current power turbines are designed for single operating speed, and performance degrades rapidly as power turbine speed decreases. OBJECTIVES: Demonstrate 50 improvement in efficient operational capability using a Variable Speed Power Turbine concept. (Refer to figure lower left, where the goal is to raise efficiency from the current technology line to the green line which represents the AVSPOT VSPT goal.APPROACH: Conduct RD required to advance the technology readiness level of VSPT technology to TRL 4Partner with DoD and leverage DOD AVSPOT contract to share government cost (5050) of contracted efforts to GE and PW for VSPT TRL 45 demonstration.
Document ID
20170004517
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Reddy, D. R.
(NASA Glenn Research Center Cleveland, OH United States)
Schmidt, George
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
May 10, 2017
Publication Date
April 6, 2017
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
GRC-E-DAA-TN40593
Meeting Information
Meeting: NESC Propulsion Technical Discipline Team (TDT) Face-to-Face Meeting
Location: Huntsville, AL
Country: United States
Start Date: April 4, 2017
End Date: April 6, 2017
Sponsors: NASA Marshall Space Flight Center
Funding Number(s)
WBS: WBS 432938.08.01.03.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
power turbine
variable-speed
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