scholarly journals Effect of Local Fluctuation of the High Temperature Strength Properties in Weld Metal on Creep Deformation Behavior of Multi-Layer Welded Joint

2005 ◽  
Vol 54 (2) ◽  
pp. 155-161 ◽  
Author(s):  
Hiromichi HONGO ◽  
Masayoshi YAMAZAKI ◽  
Takashi WATANABE ◽  
Masaaki TABUCHI ◽  
Tatsuhiko TANABE ◽  
...  
1999 ◽  
Vol 48 (2) ◽  
pp. 116-121 ◽  
Author(s):  
Hiromichi HONGO ◽  
Masayoshi YAMAZAKI ◽  
Takashi WATANABE ◽  
Junichi KINUGAWA ◽  
Tatsuhiko TANABE ◽  
...  

Alloy Digest ◽  
1967 ◽  
Vol 16 (4) ◽  

Abstract PRESSURDIE-1 is an air-hardening hot work tool and die steel having high heat resistance and good high temperature strength properties. It is recommended for die casting dies, extrusion and forging dies. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: TS-191. Producer or source: Continental Copper & Steel Industries Inc..


1998 ◽  
Vol 120 (1) ◽  
pp. 172-178 ◽  
Author(s):  
N. Nakazawa ◽  
H. Ogita ◽  
M. Takahashi ◽  
T. Yoshizawa ◽  
Y. Mori

The development of turbine components for the automotive 100 kW ceramic gas turbine has entered the final stage of the seven-year project and is making satisfactory progress toward the goals. We have attained the interim targets of the aerodynamic performances and have been carrying out tests to further improve efficiency. As for ceramic parts, we have changed the material of the turbine rotor to a new one that is excellent in long-sustained and high-temperature strength properties, and have confirmed substantial strength at high temperature through hot-spin tests. After evaluating blade-vibration stress through analyses and experiments, we completed an endurance evaluation at 1200°C (1473 K) TIT (Turbine Inlet Gas Temperature) and a rated speed of 100,000 rpm. We are now carrying out endurance tests at 1350°C (1623 K) TIT. For ceramic stationary parts, we already finished the evaluations at 1200°C TIT and are also conducting an endurance test at 1350°C TIT. Using these parts in a full-assembly test, together with other elements, we confirmed that they cause no functional problem in tests performed at 1200°C TIT level up to the rated speed (100,000 rpm), and are evaluating their performances.


1994 ◽  
Vol 26 (5) ◽  
pp. 342-347
Author(s):  
R. Z. Shron ◽  
I. I. Mints ◽  
N. G. Shul'gina

1992 ◽  
Vol 78 (11) ◽  
pp. 1737-1744 ◽  
Author(s):  
Kazuya MIYAHARA ◽  
Dongsu BAE ◽  
Hidenori SAKAI ◽  
Jun-ichi INAMI ◽  
Yuzo HOSOI

Metals ◽  
2021 ◽  
Vol 11 (1) ◽  
pp. 152
Author(s):  
Marie Kvapilova ◽  
Petr Kral ◽  
Jiri Dvorak ◽  
Vaclav Sklenicka

Cast nickel-based superalloys INC713 LC, B1914 and MAR-M247 are widely used for high temperature components in the aerospace, automotive and power industries due to their good castability, high level of strength properties at high temperature and hot corrosion resistance. The present study is focused on the mutual comparison of the creep properties of the above-mentioned superalloys, their creep and fracture behaviour and the identification of creep deformation mechanism(s). Standard constant load uniaxial creep tests were carried out up to the rupture at applied stress ranging from 150 to 700 MPa and temperatures of 800–1000 °C. The experimentally determined values of the stress exponent of the minimum creep rate, n, were rationalized by considering the existence of the threshold stress, σ0. The corrected values of the stress exponent correspond to the power-law creep regime and suggest dislocation climb and glide as dominating creep deformation mechanisms. Fractographic observations clearly indicate that the creep fracture is a brittle mostly mixed transgranular and intergranular mode, resulting in relatively low values of fracture strain. Determined main creep parameters show that the superalloy MAR-M247 exhibits the best creep properties, followed by B1914 and then the superalloy INC713 LC. However, that each of the investigated superalloys can be successfully used for high temperature components fulfils the required service loading conditions.


2009 ◽  
Vol 386-388 ◽  
pp. 520-524 ◽  
Author(s):  
Taichiro Kato ◽  
Shin-ichi Komazaki ◽  
Yutaka Kohno ◽  
Hiroyasu Tanigawa ◽  
Akira Kohyama

Sign in / Sign up

Export Citation Format

Share Document