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Fuel Injector With Shear AtomizerAtomizer for injecting liquid fuel into combustion chamber uses impact and swirl to break incoming stream of fuel into small, more combustible droplets. Slanted holes direct flow of liquid fuel to stepped cylindrical wall. Impact on wall atomizes liquid. Air flowing past vanes entrains droplets of liquid in swirling flow. Fuel injected at pressure lower than customarily needed.
Document ID
19950065196
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Beal, George W. (United Technologies Pratt & Whitney)
Mills, Virgil L. (United Technologies Pratt & Whitney)
Smith, Durward B., II (United Technologies Pratt & Whitney)
Beacom, William F. (United Technologies Pratt & Whitney)
Date Acquired
August 17, 2013
Publication Date
January 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-15398
ISSN: 0145-319X
Report Number: LEW-15398
Accession Number
95B10037
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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