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Beryllium Copper Alloy
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Beryllium Copper Sheet
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Tellurium Copper Alloy
DIN. 2.1247 CuBe2 Half Hard Rolled Strips On Coil 0,10x8mm
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xName | Half Hard Rolled Strips | Max Coil Wt. | 2T |
---|---|---|---|
Thinnest Thick. | 0,10mm | Width | 8mm |
Standard | ASTM B194, SAE J463, J461 | Hardness | 300-360HV |
Safe Handling | No Special Health Risk. | Machining Property | Good |
Surface | Bright/Polished | Flatness | Good |
State | Half Hard Rolled | ||
High Light | Half Hard Rolled C17200 Beryllium Copper,DIN. 2.1247 C17200 Beryllium Copper,Half Hard Rolled Beryllium Copper Strip |
CuBe2 (DIN. 2.1247) Half Hard Rolled Strips On Coil 0,10x8mm With High Strength
Product Normal Description:
Product Name: Half hard rolled strips
Grade: CuBe2(DIN. 2.1247)
Standard: ASTM B194, SAE J463, J461
Product Specification: 0,10mmx8mm
State: Half hard rolled
Product Brand: CUBERYLLIUM®
Chemical Composition of CuBe2 (DIN. 2.1247) Alloys:
Beryllium(Be): 1.80-2.00%
Cobalt(Co) + Nickel(Ni): 0.20% Min
Cobalt(Co) + Nickel(Ni) + Iron(Fe): 0.60% Max
Lead: 0.02% Max
Copper(Cu): Balance
Note: Copper plus additions equal 99.5% Minimum.
Temper Designations of CuBe2 (DIN. 2.1247) Strip:
Cuberyllium Designation | ASTM | Mechanical and Electrical Properties of Copper Beryllium Strip | ||||||
Designation | Description | Tensile Strength (Mpa) |
Yield Strength 0.2% offset | Elongation Percent | HARDNESS (HV) |
HARDNESS Rockwell B or C Scale |
Electrical Conductivity (% IACS) |
|
A | TB00 | Solution Annealed | 410~530 | 190~380 | 35~60 | <130 | 45~78HRB | 15~19 |
1/2 H | TD02 | Half Hard | 580~690 | 510~660 | 12~30 | 180~220 | 88~96HRB | 15~19 |
H | TD04 | Hard | 680~830 | 620~800 | 2~18 | 220~240 | 96~102HRB | 15~19 |
HM | TM04 | Mill hardened |
930~1040 | 750~940 | 9~20 | 270~325 | 28~35HRC | 17~28 |
SHM | TM05 | 1030~1110 | 860~970 | 9~18 | 295~350 | 31~37HRC | 17~28 | |
XHM | TM06 | 1060~1210 | 930~1180 | 4~15 | 300~360 | 32~38HRC | 17~28 |
Tipical Uses of CuBe2(DIN. 2.1247) Alloys:
Oil & Gas - Instrument Housings, Flex Shafts, MWD & LWD Components, Bearings, Bushings, Valve Components, Pump Shafts
Automotive - Plastic Molds, Electronic Components, RWMA Tooling
Electrical - Spring Connectors, Current Carring Navigational Instruments, Contact Bridges, Clips, Relay Parts, Electrical Switch and Relay Blades
Aerospace - Landing Gear Bushings, Aircraft Components, Cryogenics
Fasteners - Bolts, Screws, Retaining Rings, Lock Washers, Belleville Washers, Roll Pins, Fasteners, Washers
Other Industrial - Flexible Metal Hose, Non Sparking Safety Tools, Shafts, Pump Parts, Rolling Mill Parts, Bearings, Bushings, Valve Seats, Valve Stems, Wear Plates on Heavy Equipment, Springs, Electrochemical
Specifications of CuBe2 (DIN. 2.1247) Alloys:
Strip | ASTM B194 |
Bar | ASTM B196 |
Wire | ASTM B197 |
Plate | ASTM B194 |
Sheet | ASTM B194 |
Tube | ASTM B643 |
Product Photo of CuBe2 (DIN. 2.1247) Strips:
Key Technology of Beryllium Copper(Heat treatment)
Heat treatment is the most important process for this alloy system. While all copper alloys are hardenable by cold working, beryllium copper is unique in being hardenable by a simple low temperature thermal treatment. It involves two basic steps. The first is called solution annealing and the second, precipitation or age hardening.
Solution Annealing
For the typical alloy CuBe2Pb) the alloy is heated between 720°C and 860°C. At this point the contained beryllium is essentially “dissolved” in the copper matrix (alpha phase). By rapidly quenching to room temperature this solid solution structure is retained. The material at this stage is very soft and ductile and can be readily cold worked by drawing, forming rolling, or cold heading. The solution annealing operation is part of the process at the mill and is not typically used by the customer. Temperature, time at temperature, quench rate, grain size, and hardness are all very critical parameters and are tightly controlled by ohmalloy.
Age Hardening
Age hardening significantly enhances the material’s strength. This reaction is generally carried out at temperatures between 260°C and 540°C depending on alloy and desired characteristics. This cycle causes the dissolved beryllium to precipitate as a beryllium rich (gamma) phase in the matrix and at the grain boundaries. It is the formation of this precipitate which causes the large increase in material strength. The level of mechanical properties attained is determined by the temperature and time at temperature. It should be recognized that beryllium copper has no room temperature aging characteristics.
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