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HIGH TEMPERATURE TENSILE FRACTURE BEHAVIOR OF ORIENTED DD100 SINGLE CRYSTAL SUPERALLOY

Author C.D. Zhou1 , 2) , J.X. Yu1) , X.P. Dong1) , Y.H. Zhang1) , C.Q. Sun3) and T.F. Li4) 1) The State Education Commission Open Research Laboratory for High Temperature Materials and Testing , Shanghai Jiao Tong University , Shanghai 200030 , China2) Shanghai Enhanced Lab of Ferrometallurgy , Shanghai University , Shanghai 200072 , China3) Institute of Aeronautical Materials , Beijing 100095 , China 4) Institute of Corrosion and Protection of Metals , The Chinese Academy of Sciences , Shenyang 110015 , ChinaManuscript received 18 October 1998

金属学报(英文版)

An investigation has been made on the tensile fracture behavior of oriented single crystal DD100 superalloy at 850. The appearance of the fracture surface of DD100 reflects the glide plane decohension fracture mechanism, which is different from the fracture of oriented DD100. The tensile strength and elongation are lower than the oriented DD100. Oxygen in air has little effect on the strength of DD100 but reduces the tensile elongation obviously. Oxygen does not affect the fracture mode of DD100 but strongly accelerates the process of fracture.

关键词: single crystal superalloy , null , null

HREM STUDY OF GRAIN BOUNDARY PHASES IN Fe-Ni-Co-Nb-Ti SUPERALLOY

R.M. Wang , C.Z. Li , S. W. Zhang and M.G.Yan(1)Institute of Aeronautical Materials , Beijing 100095 , China 2)Laboratory of Atomic Imaging of Solids , Institute of Metal Research , Chinese Academy of Sciences , Shenyang 110015 , China 3)Beijing Laboratory of Electron Microscopy , Chinese Academy of Sciences , Beijing 100080 , China Manuscript received 26 August 1996)

金属学报(英文版)

The microstructures of the grain boundary phases in Fe-Ni-Co-Nb-Ti superalloy have been studied by high resolution electron microscopy (HREM).Besides the Laves phase,three other grain boundary phases have been found and analyzed. The ε phase particles are needle-like with some stacking faults along the(0001) direction. The dominant phase at the grain boundaries is the orthorhombic phase that is also rod-like. High reselution image also confirms the existence of the triclinic phase at the grain boundaries that is irregular and scarce.

关键词: :high resolution electron microscopy , null , null

STUDY ON THE THREESTAGE CREEP OF THE DD3SINGLE CRYSTAL SUPERALLOY

Author X.A. Zhang1) , H.Q. Xia1) , Z.T. Wu1) , Y.F. Han1) , R. Shi2) and G.X. Hu2) \= 1) Mechanical Properties Laboratory , Beijing Institute of Aeronautical Materials , Beijing 100095 , China2) The State Education Commission Open Research Laboratory for High Temperature

金属学报(英文版)

Materials and Testing, Shanghai Jiao Tong University, Shanghai 200030, ChinaManuscript received 18 October 1998 The threestage creep behavior of DD3 single crystal superalloy had been studied. The results show that the creeprupture properties of DD3 single crystal satisfy the requirements for high performance turbine blade application. The influence of crystal orientation on the creeprupture property of DD3 single crystal was tested and discussed. An engineering criterion to evaluate the regimes of secondary and tertiary creep is proposed, and this method gives a reasonable result for practical applications. The fractography and TEM micrography of the tested specimens had been studied, and it is determined that the glidecontrolled creep is the basic creep mechanism of DD3 single crystal at intermediate temperature, but the thermally activated processes become dominant at higher temperature.

关键词: threestage creep curve , null , null , null

LOW CYCLE FATIGUE AND CREEPFATIGUE BEHAVIOROF A HIGH TEMPERATURE ALLOY ON SMOOTH ANDNOTCHED SPECIMENS

Author H.J. Shi1) , S.L. Liu2) , Y.H. He1) and Z.X. Duan2) 1) Department of Engineering Mechanics , Tsinghua University , Beijing 100084 , China2) Laboratory of Material Mechanical Properties , Beijing Institute of Aeronautical Materials , Beijing 100095 , ChinaManuscript received 18 October 1998

金属学报(英文版)

A series of low cycle fatigue and creepfatigue tests on smooth specimens and notched specimens were performed with a high temperature alloy used in the manufacture of aeroengine turbine discs. The cyclic stressstrain behavior and fracture characteristics of the notched specimens were emphatically investigated. A comparison of fatigue behavior between smooth and notched specimens was done and lifetime of notched specimens was evaluated. At the same temperature, the fatiguecreep lives of the smooth specimens are far greater than that of the notched specimens.

关键词: low cycle fatigue , null , null , null

Microstructure and Tensile Properties of Spray-deposited IC6 Alloy

Guofa MT , Zhou LI , Shifan TIAN , Xanguo ZHAO and Zhiping LUO (Institute of Aeronautical Materials , Beijing 100095 , China)Songyan ZENG and Qingchun LI(School of Materials Science and Engineering , Harbin Institute of Technology , Harbin 150001 , China)

材料科学技术(英文)

The microstructure and mechanical properties of a Ni3Al based Ni-Al-Mo superalloy-IC6 which possesses low impurity content and high density by spray deposition technique have been studied.The results indicate that the IC6 alloy has good tensile strength and elongation both at room and intermediate temperatures

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CONSOLIDATION BEHAVIOR OF MECHANICALLY ALLOYED γ-TiAl

LI Chenggong , YANG Wanhong , LUO Zhiping(Institute of Aeronautical Materials , Beijing 100095 , China FROES F H , FREFER A) Institute of Materials and Advanced Processing , College of Mines , University of Idaho , Moscow. ID83843-3026. USA

金属学报(英文版)

Use of mechanically alloying for preparation of Ti-35at.%Al results in significant reduction in crystal size, so the ductility of alloy can be improved Consolidation of Mechanically alloyed γ -TiAl is difficult because of its poor workability. The present paper will discuss recent studies on consolidation behavior by using different methods, such as explosive compaction, hot isostatic pressing, and rapid omnidirectional compaction, etc.. The microstructure and property of the samples are evaluated.

关键词: : mechanical alloying , null , null , null

ORIENTATION VARIANT SELECTION AND ITS EFFECTING FACTORS IN TITANIUM SHEET

Z.S. Zhu , N.P.Chen , J.L. Gu and M.G. Yan(1)Institute of Aeronautical Materials , P.O. Box 8115 , Beijing 100095 , China 2)Department of Materials Science and Engineering , Tsinghua University , Beijing 100084 , China Manuscript received 26 August 1996)

金属学报(英文版)

By means of crystallite orientation distribution function (ODF) analysis, the influence on orientation variant selection of cold rolling reductions, recrystallization annealing and cooling rates during α→β→α cyclic phase transformation treatments in cold rolled titanium sheet has been investigated. The results show that, cold rolling reduction and annealing treatment both have a great effect on the formation of phase transformation textures.No variant selection occurs in cold rolled and recrystallization annealed titanium sheet which resulte in a more randomly distributed texture.The phase transformation texture formed α→β→α transformation is inherited after 3 cycles of α→β→α phase transformation. The cooling rates during phase transformation have little effect on orientation variant selection.

关键词: :texture , null , null , null , null

CRACK GROWTH, FRACTURE FEATURE AND RUPTURE LIFEDURING CYCLIC CREEP OF SUPERALLOY GH2132

Author M.F. Geng1) , T. Wang1) and X.A. Zhang2) 1) Department of Special Metal Materials and Products , Luoyang Ship Material Research Institute , Luoyang 471039 , China2) Mechanical Properties Laboratory , Beijing Institute of Aeronautical Materials , Beijing 100095 , China Manuscript received18 October 1998

金属学报(英文版)

The effects of cyclic loading on crack growth, fracture feature and rupture life of superalloy GH2132 have been studied in the present paper. The crack growth tests were carried out at 550 on compact tension specimens under a wide range of load levels and various periods of hold time, and the fracture surfaces were examined on a scanning electron microscope. The results show that, for both static and cyclic creep, Stage-I of crack growth is related with initial test stress, during which the crack extension is about 0.5mm, and that the final effect of cyclic loading on rupture life depends on the counteraction of its two reversed effects on crack growth rate before and after the point n=0.2.

关键词: cyclic creep , null , null , null , null , null

CORROSION PROTECTION OF Al CATHODES IN ZINC ELECTROLYSIS

F. Lu and WJ. van Ooij( Beijing Institute of Aeronautical Materials , P.O. Box 81-5 , Beijing 100095 , China)( Department of Materials Science and Engineering , University of Cincinnati , Cincinnati , OH 45221-0012 , U.S.A.)

金属学报(英文版)

Zn-Al couple's galvanic coeeosion was a serious problem in acdic ainc sulfate solution .In this paper, a new pretreatment or a coating for Al was developed and tested to protect the Al effectively form corrosion when connected to pure Zinc at electroplating potential,and exposed to an acdic sulfate solution.Corrosion measurement techniques(Galvanic corrosion and DC)were used to investigate galvanic corrosion between Al cathode and Zn anode.It was found out that Al alloy purity and electroplating potential have a large effect on galvanic corrsion between Zn-Al couples.EIS,salt spray test and immersion test were performed to evaluate the method for Al cathodes in zinc electrolyte,BTSE silane pretreatment and polyurethane coating displayed better corrosion protection.Calculation showed the Al dissolution rate is small enough for Al cathode to be used in zinc plants.BTSE treatment or BTSE plus polyurethane coating has the best corrosion performance,and willprotect the Al cathode effectively in zinc electrolysis

关键词: Al-Zn couple , null

Microstructure of Laser Remelted Ni-base Alloy Coating on Stainless Steel

Yang GAO (Beijing Institute of Aeronautical Material , Beijing 100095 , China)Yong LIANG and Changxu SHI (Institute of Metal Research , Chinese Academy of Sciences , Shenyang 110015 , China)

材料科学技术(英文)

A 5 kW CW CO2 gas laser was used to produce NiCrBSi superalloy coatings. Powders were preplaced by plasma-spraying. The microstructure and chemical composition of the coating have been studied by SEM, XRD and HREM. The results show the coating microstructure is fine dendrites, composed of γ matrix, γ' and boride (NiB) eutectic, the lattice parameter of the γ matrix is 0.3572 nm and there is a metallurgical bonding in interface.

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