NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Water Misting and Injection of Commercial Aircraft Engines to Reduce Airport NOxThis report provides the first high level look at system design, airplane performance, maintenance, and cost implications of using water misting and water injection technology in aircraft engines for takeoff and climb-out NOx emissions reduction. With an engine compressor inlet water misting rate of 2.2 percent water-to-air ratio, a 47 percent NOx reduction was calculated. Combustor water injection could achieve greater reductions of about 85 percent, but with some performance penalties. For the water misting system on days above 59 F, a fuel efficiency benefit of about 3.5 percent would be experienced. Reductions of up to 436 F in turbine inlet temperature were also estimated, which could lead to increased hot section life. A 0.61 db noise reduction will occur. A nominal airplane weight penalty of less than 360 lb (no water) was estimated for a 305 passenger airplane. The airplane system cost is initially estimated at $40.92 per takeoff giving an attractive NOx emissions reduction cost/benefit ratio of about $1,663/ton.
Document ID
20040035576
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Daggett, David L.
(Boeing Commercial Airplane Group Seattle, WA, United States)
Hendricks, Robert C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2004
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2004-212957
E-14397
C/EA-BQ130-Y04-002
Report Number: NASA/CR-2004-212957
Report Number: E-14397
Report Number: C/EA-BQ130-Y04-002
Funding Number(s)
CONTRACT_GRANT: NASA Order C-74711-A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available