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Volumn 155, Issue 1-2, 2010, Pages 13-17

Gas turbine engine test of RCL® catalytic pilot for ultra-low NO x applications

Author keywords

Catalytic; Catalytic pilot; Combustion; Low NOx; Rich Catalytic Lean burn

Indexed keywords

BASELOAD; CATALYTIC; CATALYTIC COMBUSTION; CATALYTIC PILOT; CO EMISSIONS; COMBUSTION STABILITY; COMBUSTION TECHNOLOGY; COMBUSTOR ACOUSTICS; ENGINE CONTROL; ENGINE TESTING; ENHANCED REACTIVITY; FLAME TEMPERATURES; FURTHER DEVELOPMENT; GAS TURBINE ENGINE; HIGHER TEMPERATURES; LONG TERM; LOW NOX; NATURAL GAS APPLICATIONS; PRE-REACTIONS; PREMIXED; PRIMARY ZONES; RICH CATALYTIC/LEAN-BURN; TRANSIENT BEHAVIOR;

EID: 77956061068     PISSN: 09205861     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.cattod.2010.05.029     Document Type: Conference Paper
Times cited : (14)

References (26)
  • 13
    • 77956057112 scopus 로고
    • U.S. Patent, Dec. 30 Pat. # 3,928,961
    • W.C. Pfefferle, U.S. Patent, Dec. 30, 1975, Pat. # 3,928,961.
    • (1975)
    • Pfefferle, W.C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.