CHASE 75W-25 Re

Alloy Digest ◽  
1965 ◽  
Vol 14 (9) ◽  

Abstract CHASE 75 W-25 Re is a tungsten-rhenium ultra-high temperature alloy recommended for temperatures up to 5000 F. It is used for power and electron tube components, heat exchangers, thermocouples and thermocouple protection tubes, nuclear reactor and power generation components and in general any high temperature application requiring high strength and ductility. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, and joining. Filing Code: W-10. Producer or source: Chase Brass & Copper Company Inc..

Alloy Digest ◽  
2001 ◽  
Vol 50 (8) ◽  

Abstract TIMETAL 829 is a Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si near-alpha titanium alloy that is weldable and has high strength and is a creep resistant high temperature alloy. The major application is as gas turbine engine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on forming and heat treating. Filing Code: TI-118. Producer or source: Timet.


Alloy Digest ◽  
1960 ◽  
Vol 9 (4) ◽  

Abstract NI-RESIST DUCTILE IRONS are a group of austenitic nickel-alloyed cast irons having high strength and ductility combined with heat and corrosion resistance. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness. It also includes information on high temperature performance as well as heat treating and joining. Filing Code: CI-28. Producer or source: International Nickel Company Inc..


Alloy Digest ◽  
1960 ◽  
Vol 9 (2) ◽  

Abstract C.D.C. Manganese Alloy No. 772 offers a combination of high strength and ductility. It has a high temperature coefficent of expansion, high electrical resistivity, low thermal conductivity, and high vibration damping constant. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mn-1. Producer or source: Chicago Development Corporation. Originally published July 1953, revised February 1960.


Alloy Digest ◽  
1965 ◽  
Vol 14 (1) ◽  

Abstract AISI No. 618 is a general purpose, high temperature alloy steel that can be hardened to high strength and hardness levels. It maintains good hot hardness. This datasheet provides information on composition, physical properties, hardness, and elasticity as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-172. Producer or source: Alloy steel mills and foundries.


1990 ◽  
Vol 186 ◽  
Author(s):  
A.J.S. Chowdhury ◽  
T. Sheppard

AbstractThe phases responsible for high temperature strength and ductility of Al-Fe based alloys, specifically Al-Fe-Mo alloys, have yet to be unambiguously identified. The phases appear to vary slightly under different experimental and processing conditions. This poses some queries concerning the reproducibility of mechanical properties of these alloys. In this paper an attempt is made to address these points and focus on the structure-property relationships of Al-Fe-Mo and Al-Fe-V rapidly solidified powder alloys.


Alloy Digest ◽  
1966 ◽  
Vol 15 (3) ◽  

Abstract Chase 50Re-50Mo is a rhenium-molybdenum high temperature alloy recommended for temperatures up to 4200 F where high strength at elevated temperature combined with high ductility are required. The alloy retains remarkable ductility even in the recrystallized condition, is weldable, and can be formed into shapes with far less chance of failure than pure molybdenum. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, and joining. Filing Code: Mo-7. Producer or source: Chase Brass & Copper Company Inc..


Alloy Digest ◽  
1993 ◽  
Vol 42 (6) ◽  

Abstract P/M RENE 95 is a high strength, high temperature alloy used for rotating jet turbine components. Supersolvus P/M Rene 95 provides even higher temperature creep and stress-rupture resistance than standard Rene 95. Both are available as-HIP performs. A typical application is a high pressure turbine disc. This datasheet provides information on composition and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating and powder metal forms. Filing Code: Ni-434. Producer or source: Crucible Compaction Metals.


Alloy Digest ◽  
1966 ◽  
Vol 15 (9) ◽  

Abstract Pyromet 860 is a high temperature alloy with an unusual combination of strength and ductility in the 1350 F range. It is a precipitation hardening alloy recommended for turbine parts and other high temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-117. Producer or source: Carpenter Technology Corporation.


Alloy Digest ◽  
1957 ◽  
Vol 6 (10) ◽  

Abstract CROLOY 15-15N is a super strength iron-base austenitic steel for high temperature application under extreme pressure conditions. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-62. Producer or source: Babcock & Wilcox Company.


Alloy Digest ◽  
1971 ◽  
Vol 20 (5) ◽  

Abstract COPPER ALLOY No. 715 is a copper nickel alloy having high strength and ductility and excellent resistance to corrosion, particularly by saline waters. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Cu-232. Producer or source: Copper and copper alloy mills.


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