共 16 条
- [1] [Anonymous], T ASME
- [3] Reconditioning of gas turbine components by heat treatment [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2001, 123 (01): : 57 - 61
- [5] Solution heat treatment response of a third generation single crystal Ni-base superalloy [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2001, 300 (1-2): : 52 - 60
- [6] ASSESSMENT OF SERVICE INDUCED MICROSTRUCTURAL DAMAGE AND ITS REJUVENATION IN TURBINE-BLADES [J]. METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1988, 19 (08): : 2049 - 2066
- [8] MICROSTRUCTURE, CREEP-PROPERTIES, AND REJUVENATION OF SERVICE-EXPOSED ALLOY 713C TURBINE-BLADES [J]. METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1990, 21 (12): : 3115 - 3125
- [9] Creep life prediction of service-exposed turbine blades [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2006, 433 (1-2): : 305 - 309
- [10] Monkman F.C., 1956, Proc ASTM, V28, P593, DOI [DOI 10.2307/3469318, DOI 10.1016/J.MECHMAT.2004.10.003]