SCOPUS 정보 검색 플랫폼

Volumn 45, Issue 2, 2002, Pages 193-198

The influence of temperature on the wear mode and deterioration of coatings used for titanium aircarft engine components

(4) Freimanis, A J a Segall, A E b Conway, J C c Whitney, E J c

a BOEING COMPANY (United States)

b WASHINGTON STATE UNIVERSITY (United States)

c PENNSYLVANIA STATE UNIVERSITY (United States)

Author keywords

Coatings; Dovetail; Fretting; Titanium; Wear

Indexed keywords

AIRCRAFT ENGINES; COBALT; COMPRESSORS; INDIUM; JET ENGINES; MOLYBDENUM; NICKEL; PROTECTIVE COATINGS; ROTORS; THERMAL EFFECTS; TITANIUM; TURBOMACHINE BLADES; WEAR OF MATERIALS; COATINGS; COPPER; SEGREGATION (METALLOGRAPHY);

COMPRESSOR BLADES;

TRIBOLOGY; AIRCRAFT ENGINES;

COATING; COMPOSITE; ENGINE; TEMPERATURE EFFECT; TITANIUM; WEAR;

COMPRESSOR BLADES; DOMINANT DETERIORATION MECHANISM; DOVETAIL; FRETTING;

EID: 0035997305 PISSN: 10402004 EISSN: None Source Type: Journal
DOI: 10.1080/10402000208982539 Document Type: Article

Times cited : (25)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.