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High Energy Flywheel Containment EvaluationA flywheel testing facility is being constructed at the NASA Glenn Research Center. This facility is to be used for life cycle testing of various flywheel rotors. The lifecycle testing consists of spinning a rotor from a low rpm (approx. 20,000 ) to a high rpm (approx. 60,000) and then back to the low rpm. This spin cycle will model that which the rotor will see during use. To simulate the lifetime of the rotor, the spin cycle will be performed tens of thousands of times. A typical life cycle spin test is expected to last six months. During this time the rotor will be spun through a cycle every five minutes. The test will run continuously for the six month period barring a flywheel failure. Since it is not reasonable to have the surrounding area evacuated of personnel for the duration of the testing, the flywheel facility has to be designed to withstand a flywheel rotor failure and insure that there is no danger to any personnel in the adjacent buildings or surrounding areas. In order to determine if the facility can safely contain a flywheel rotor failure an analysis of the facility in conjunction with possible flywheel failure modes was performed. This analysis is intended as a worst case evaluation of the burst liner and vacuum tank's ability to contain a failure. The test chamber consists of a cylindrical stainless steel vacuum tank, two outer steel containment rings, and a stainless steel burst liner. The stainless steel used is annealed 302, which has an ultimate strength of 620 MPa (90,000 psi). A diagram of the vacuum tank configuration is shown. The vacuum tank and air turbine will be located below ground in a pit. The tank is secured in the pit with 0.3 m (12 in.) of cement along the base and the remaining portion of the tank is surrounded by gravel up to the access ports. A 590 kg (1300 lb.) bulkhead is placed on top of the pit during operation and the complete facility is housed within a concrete structure which has 7.5 cm (3 in.) thick walls. A cutaway of the facility is shown.
Document ID
20000120215
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Colozza, Anthony J.
(DYNACS Engineering Co., Inc. Brook Park, OH United States)
Trase, Larry
Date Acquired
September 7, 2013
Publication Date
October 1, 2000
Subject Category
Structural Mechanics
Report/Patent Number
E-12477
NAS 1.26:210508
NASA/CR-2000-210508
Report Number: E-12477
Report Number: NAS 1.26:210508
Report Number: NASA/CR-2000-210508
Funding Number(s)
CONTRACT_GRANT: NAS3-98008
PROJECT: RTOP 344-96-6A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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