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Hybrid Thermally Efficient Core (HyTEC) Phase 1 3-Stage Compressor Rig Final Report - Unlimited RightsThe HyTEC Phase 1 3-Stage Compressor Rig project was conducted to mature and validate front-stage aerodynamic technologies in support of HyTEC Phase 2 and GEA’s Compact Core compressor. Building on the prior ERA Phase 2 Baseline Rig, GEA and NASA collaborated on the design and testing of the HyTEC rig, incorporating advanced technologies such as increased radius ratio, higher aerodynamic loading, and advanced casing treatment. The HyTEC test campaign leveraged similar design and instrumentation philosophy, test execution approach, and the same facility (NASA W-7) to enable clear comparison with the legacy ERA rig results. The HyTEC rig was designed to deliver benefits in efficiency, tip loading, operability, and aeromechanics, with success measured against defined TPMs that were anchored to the ERA baseline rig data.
Document ID
20260006262
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
G Scott McNulty
(GE Aerospace Evendale, OH )
Brandon Teitelbaum
(GE Aerospace Evendale, OH )
Mike Paine
(GE Aerospace Evendale, OH )
Arnesha Threatt
(GE Aerospace Evendale, OH )
Kyle Fishleigh
(GE Aerospace Evendale, OH )
Dave Goshorn
(GE Aerospace Evendale, OH )
Krista Mitchell
(GE Aerospace Evendale, OH )
Mitchell Albrecht
(GE Aerospace Evendale, OH )
Date Acquired
July 15, 2026
Publication Date
August 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
E-20439
NASA/CR-20260006262
Funding Number(s)
WBS: 649097.04.03.02.92.01
CONTRACT_GRANT: 80GRC021CA007
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Axial Compressors
Turbomachinery
Small Core
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