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Development of Advanced Low Emission Injectors and High-Bandwidth Fuel Flow Modulation ValvesParker Hannifin Corporation developed the 3-Zone fuel nozzle for NASA's Environmentally Responsible Aviation Program to meet NASAs target of 75 LTO NOx reduction from CAEP6 regulation. The nozzle concept was envisioned as a drop-in replacement for currently used fuel nozzle stem, and is built up from laminates to provide energetic mixing suitable for lean direct injection mode at high combustor pressure. A high frequency fuel valve was also developed to provide fuel modulation for the pilot injector. Final testing result shows the LTO NOx level falling just shy of NASAs goal at 31.
Document ID
20150023047
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Mansour, Adel
(Parker-Hannifin Corp. Mentor, OH, United States)
Date Acquired
December 15, 2015
Publication Date
November 1, 2015
Subject Category
Fluid Mechanics And Thermodynamics
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2015-218899
GRC-E-DAA-TN26080
E-19154
Funding Number(s)
CONTRACT_GRANT: NNC11CA09C
WBS: WBS 338881.02.26.03.04.05.09
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
control
combustor
injectors
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