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Continuous inline blending of antimisting keroseneA continuous inline blender was developed to blend polymer slurries with a stream of jet A fuel. The viscosity of the slurries ranged widely. The key element of the blender was a static mixer placed immediately downstream of the slurry injection point. A positive displacement gear pump for jet A was employed, and a progressive cavity rotary screw pump was used for slurry pumping. Turbine flow meters were employed for jet A metering while the slurry flow rate was calibrated against the pressure drop in the injection tube. While using one of the FM-9 variant slurries, a provision was made for a time delay between the addition of slurry and the addition of amine sequentially into the jet A stream.
Document ID
19860020543
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Parikh, P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Yavrouian, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sarohia, V.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
December 31, 1985
Publication Information
Publication: FAA Proceedings of Fuel Safety Workshop
Subject Category
Propellants And Fuels
Accession Number
86N30015
Funding Number(s)
CONTRACT_GRANT: NAS7-917
CONTRACT_GRANT: DTFA03-80-A-00215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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