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Copper beryllium high strength alloys are less dense than conventional specialty coppers often providing more pieces per pound of input material Copper beryllium also has an elastic modulus 10 to 20 percent higher than other specialty copper alloys Strength resilience and elastic properties make copper beryllium the alloy of choice
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C17200 Beryllium Copper Cube2--C17200 (CDA 172) Beryllium Copper is the most commonly utilized Copper Beryllium alloy and is notable for its highest strength and hardness compared to commercial copper alloys C17200 alloy contains appr 2% of beryllium and achieves its ultimate tensile strength can exceed 200 ksi while the hardness approaches
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Copper Alloy C17510 Mill Hardened Beryllium Copper combines moderate yield strength up to 125 ksi with electrical conductivity from 45 to 60 percent of pure copper Alloys 3 is available in wrought product forms and can be supplied fully hardened by our producing mill Alloy 3 product provides increased thermal conductivity
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Berylco Alloy 25 (UNS C17200) is the most commonly used Beryllium Copper alloy It offers excellent wear resistance and fatigue strength while still providing conductivity at a minimum of 22% IACS In the age hardened condition Berylco Alloy 25 offers the highest strength of any commercial copper base alloy The tensile strength can exceed
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In order to authorize the beryllium–copper alloy for use in high-pressure gaseous hydrogen slow-strain-rate-tensile (SSRT) fatigue life FCG and fracture toughness tests were performed in this study on the precipitation-hardened beryllium–copper alloy in 115-MPa hydrogen gas at room temperature Hydrogen solubility and diffusivity of the
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UNS C17410 (Alloy 174) Beryllium Copper Strips A) UNS C17410 (Alloy 174) Details C17410 (Alloy 174) Beryllium Copper UNS C17410 (CDA 174) Alloy 174 Copper Beryllium strip is a mill hardened alloy designed for use in the automotive appliance and telecommunication markets It provides high yield and fatigue strength with high electrical conductivity and good
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Annealing the copper requires a high temperature Copper melts at 1357Kelvin and annealing generally occurs at greater than half the melting point in degrees K even higher temperature causes faster annealing (but not past the melting temperature of course) Typical temperature to use is 400C or 700F Annealing causes the structure to
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Among wrought copper alloys the composition of C17200 copper is notable for including beryllium (Be) and aluminum (Al) Beryllium is used to permit precipitation hardening (which increases strength) without much effect on electrical conductivity but
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Beryllium copper is a ductile weldable and machinable alloy It can be heat-treated to improve its strength durability and electrical conductivity Because beryllium copper is non-sparkling but physically tough and non-magnetic it is used to make tools that can safely be used in environments where there are explosive vapors and gases such as on oil rigs and coal mines
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Berylco Alloy 25 (UNS C17200) is the most commonly used Beryllium Copper alloy It offers excellent wear resistance and fatigue strength while still providing conductivity at a minimum of 22% IACS In the age hardened condition Berylco Alloy 25 offers the highest strength of any commercial copper base alloy The tensile strength can exceed
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Class 4 copper is available in the annealed condition in this state it can be more readily machined and may be subsequently heat treated to maximum hardness Copper Beryllium alloys derives their high strength through heat treament and in the case of small cross section wroght forms cold working The amount of cold work and the type of heat
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similar for all copper beryllium alloys but at different standard temperatures Figure 1 Response to age-hardening heat treatment for three treating temperatures - Brush Alloy 25 Copper beryllium can be age hardened to varying degrees of strength The term peak aged refers to copper beryllium aged to maximum strength Alloys not
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US2635044A US173239A US17323950A US2635044A US 2635044 A US2635044 A US 2635044A US 173239 A US173239 A US 173239A US 17323950 A US17323950 A US 17323950A US 2635044 A US2635044 A US 2635044A Authority US United States Prior art keywords alloy beryllium stainless steel copper silicon Prior art date 1950-07-11 Legal status
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beryllium copper parts Meet tomorrow's technological challenges Demands for cost quality miniaturisation reliability safety environmental protection and high-end general performance require suitable high-performance alloys such as beryllium copper The available data is to be referred to by the
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