CuAl10Fe3Mn2 (CW306G) is a wrought alloy of high strength, also at increased temperatures. The strength properties of cold formable wrought alloys are primarily dependent on the deformation grade. Tensile strength, yield strength and hardness rise according to the increasing cold forming grade. Elon

Material CuZn40Pb2, mat. No. CW617N, is an unhardenable wrought alloy.High hardness and strength parameter are achievable by cold forming only. Thermal and electrical conductivity are lower than for CuZn40. Machinability is improved by Pb-addition. Corrosion resistance to water, several saline solut

CuZn40Mn1Pb1 (CW720R former identification: CuZn40MnPb) is an unhardenable copper alloy. High hardness and strength parameter are achievable by cold forming only. Manganes increases corrosion resistance and sliding qualities. Improved machinability by Pb-addition. Processing properties: warm forming

Wire fom copper alloy for general purposes.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.4 - 8.47 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus20.0 °C96 - 97 GPaHardness, Vickers20.0 °C95 - 130 [-]Shear modulus23.0 °C40 GPaTypical for Wrought Copper BrassThermalPropertyTem

Wire fom copper alloy for general purposes.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.4 - 8.47 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus20.0 °C96 - 97 GPaHardness, Vickers20.0 °C145 [-]Shear modulus23.0 °C40 GPaTypical for Wrought Copper BrassThermalPropertyTemperat

The nickel-alloyed cryogenic material X8Ni9, materia number 1.5662 is used in pressure vessel construction. Application for refrigerators, gearbox parts and components in machine and apparatus engineering which are exposed to temperatures up to -200 °C.PropertiesGeneralPropertyTemperatureValueDensit

The nickel-alloyed cryogenic material 12Ni14, material number 1.5637 is used for pressure vessel construction. Application for boilers as well as for aircraft industry components and in refrigerator construction which are exposed to temperatures up to -100 °C. and have to show high toughness.Propert

Copper alloy profiles and bars for general purposes.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.4 g/cm³MechanicalPropertyTemperatureValueElastic modulus20.0 °C102 GPaHardness, Brinell20.0 °C120 [-]Hardness, Vickers20.0 °C125 [-]Shear modulus20.0 °C37 GPaThermalPropertyTemperatureValueCo

Wire fom copper alloy for general purposes.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.4 g/cm³MechanicalPropertyTemperatureValueElastic modulus20.0 °C102 GPaHardness, Brinell20.0 °C100 - 145 [-]Hardness, Vickers20.0 °C100 - 180 [-]Shear modulus20.0 °C37 GPaThermalPropertyTemperatureValu

Material CuNi18Zn19Pb1, mat. No. CW408J is an alloy of high strength and hardness. To the comparabel mark CuNi18Zn19Pb1, mat. No. 2.0790, acc. to DIN 17663 : 1983-12 applies: Strength is further increasable due to the high strain hardening capability. The material does not embrittle at low temperat

Material CuNi12Zn30Pb1, mat. No. CW406J is an alloy of high strength and hardness. To the comparabel mark CuNi12Zn30Pb1, mat. No. 2.0780, acc. to DIN 17663 : 1983-12 applies: Strength is further increasable due to the high strain hardening capability. The material does not embrittle at low temperat

CuZr, mat. No CW120C, is counted among hardenable, low alloyed copper alloys. To the comparable make CuZr, mat. No 2.1580, acc. to DIN 17666 : 1983-12 applies: The strength properties of CuZr are not as favorable as for CuCrZr but it very well meets high requirements to tempering strength and creep

CuZr, mat. No CW120C, is counted among hardenable, low alloyed copper alloys. To the comparable make CuZr, mat. No 2.1580, acc. to DIN 17666 : 1983-12 applies: The strength properties of CuZr are not as favorable as for CuCrZr but it very well meets high requirements to tempering strength and creep

CuZr, mat. No CW120C, is counted among hardenable, low alloyed copper alloys. To the comparable make CuZr, mat. No 2.1580, acc. to DIN 17666 : 1983-12 applies: The strength properties of CuZr are not as favorable as for CuCrZr but it very well meets high requirements to tempering strength and creep

Wire fom copper alloy for general purposes.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.4 - 8.44 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus20.0 °C102 GPaHardness, Vickers20.0 °C130 [-]Poisson's ratio20.0 °C0.34 [-]Shear modulus23.0 °C40 GPaTypical for Wrought Copp

CuZn40Mn2Fe1(former identification: CuZn40Mn2) is an unhardenable copper alloy. High hardness and strength parameter are achievable by cold forming only. Tensile strength and Brinell hardness are higher than at CuZn31Si1 (CW708R). Manganese increases corrosion resistance and sliding qualities. CuZn4

CuZn40Mn2Fe1(former identification: CuZn40Mn2) is an unhardenable copper alloy. High hardness and strength parameter are achievable by cold forming only. Tensile strength and Brinell hardness are higher than at CuZn31Si1 (CW708R). Manganese increases corrosion resistance and sliding qualities. CuZn4

Application: general purpose wire, springs, fastenersPropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.3 g/cm³MechanicalPropertyTemperatureValueElastic modulus20.0 °C135 GPaElongation20.0 °C2 %Tensile strength20.0 °C1150 MPaYield strength Rp0.220.0 °C1000 MPaThermalPropertyTemperatureValueCom

Steel 34CrNiMo6 is suitable for high-stress components (also large forged parts) with high heat-treatment cross-sections and good toughness properties in aircraft, heavy vehicle and machine construction (e.g. propeller shafts, connecting rods, gearbox shafts). Lowest working temperature -40 °C The s

Steel 30CrNiMo8 is suitable for high-stress components (also large forged parts) with high heat-treatment cross-sections and good toughness properties in aircraft, heavy vehicle and machine construction (e.g. propeller shafts, connecting rods, gearbox shafts). Furthermore for large forged parts (e.g