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Self-Adjusting Liquid Injectors for CombustorsA class of self-adjusting injectors for spraying liquid oxidizers and/or fuels into combustion chambers has been proposed. The proposed injectors were originally intended for use in rocket-engine combustion chambers, but could also be used to improve control over flows of liquid propellants in other combustion chambers. The basic idea of the proposed injectors is to use simple mechanisms, inside the injectors themselves, to adjust inlet areas so as to keep injection pressure drops at or near optimum values through out wide throttling ranges. These mechanisms would be actuated by the very pressure drops that they are intended to regulate.
Document ID
20100036541
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Trinh, Huu
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Myers, William
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
October 1, 2010
Publication Information
Publication: NASA Tech Briefs, October 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
MFS-32518-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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