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Development of a multiplane multispeed balancing system for turbine systemsA prototype high speed balancing system was developed for assembled gas turbine engine modules. The system permits fully assembled gas turbine modules to be operated and balanced at selected speeds up to full turbine speed. The balancing system is a complete stand-alone system providing all necesary lubrication and support hardware for full speed operation. A variable speed motor provides the drive power. A drive belt and gearbox provide rotational speeds up to 21,000 rpm inside a vacuum chamber. The heart of the system is a dedicated minicomputer with attendant data acquisition, storage and I/O devices. The computer is programmed to be completely interactive with the operator. The system was installed at CCAD and evaluated by testing 20 T55 power turbines and 20 T53 power turbines. Engine test results verified the performance of the high speed balanced turbines.
Document ID
19850014089
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Martin, M. R.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
September 5, 2013
Publication Date
July 19, 1984
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
MTI-84TR39
NAS 1.26:174750
NASA-CR-174750
Accession Number
85N22400
Funding Number(s)
CONTRACT_GRANT: NAS3-20609
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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