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MEMS-Based Spinning NozzleA nozzle body and assembly for delivering atomized fuel to a combustion chamber. The nozzle body is rotatably mounted onto a substrate. One or more curvilinear fuel delivery channels are in flow communication with an internal fuel distribution cavity formed in the nozzle body. Passage of pressurized fuel through the nozzle body causes the nozzle body to rotate. Components of the nozzle assembly are formed of silicon carbide having surfaces etched by deep reactive ion etching utilizing MEMS (micro-electro-mechanical systems) technology. A fuel premix chamber is carried on the substrate in flow communication with a supply passage in the nozzle body.
Document ID
20030053080
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
External Source(s)
LEW-17110-1
Authors
Robert S Okojie
(Glenn Research Center Cleveland, United States)
Date Acquired
August 21, 2013
Publication Date
February 4, 2003
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-6,513,730
Patent Application
US-Patent-Appl-SN-816722
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