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Detonation-flame arrester devices for gasoline cargo vapor recovery systemsEmpirical data on the deflagration-to-detonation run-up distance for flowing mixtures of gasoline and air in 15.2-cm- (6.0-in.-) diameter piping simulating a vapor recovery system are presented. The quenching capability of eight selected flame control devices subjected to repeated stable detonations was evaluated. The successful detonation-flame arresters were: (1) spiral-wound, crimped aluminum ribbon, (2) foamed nickel-chrome metal, (3) vertically packed bed of aluminum Ballast rings, and (4) water-trap or hydraulic back-pressure valve. Installation configurations for two of the more applicable arresters, the spiral-wound, crimped stainless-steel ribbon and the vertically packed bed of aluminum Ballast rings, were further optimized by a series of parametric tests. The final configuration of these two arresters was demonstrated with repeated detonation tests at conditions that simulated vapor recovery system operation. On these tests, the combustible mixture of gasoline and air continued to flow through the piping for periods up to 120 seconds after the initial detonation had been arrested. There was no indication of continuous burning or reignition occurring on either side of the test arresters.
Document ID
19800013944
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bjorklund, R. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ryason, P. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1980
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-CR-163009
JPL-PUB-80-18
Report Number: NASA-CR-163009
Report Number: JPL-PUB-80-18
Accession Number
80N22431
Funding Number(s)
CONTRACT_GRANT: Z70099-7-74328-H
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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