Aluminum Metal Matrix Composite

Description: Aluminum Metal Matrix Composite Tubing

Description: Nomenclature System for Aluminum Metal Matrix Composite Materials

Description: AM 162 H minimizes stress from vibration on leads, solder joints & substrates, increases fatigue life of electronic packages, reduced section thickness and adjusts for platform requirements. Plus, EB Weldable, TIG weldable, DIP and Vacuum brazing & machines like aluminum, can be coated like

• Features: Beryllium / Beryllium Alloy, Non-ferrous - Any Type, Other / Miscellaneous Nonferrous (UNS M)
• Applications: Electronics / RF-Microwave
• Type: Metal Matrix Composite, Refractory / Reactive (UNS R)

Description: METAL MATRIX COMPOSITES (MMC): CONTINUOUS SILICON CARBIDE FIBER REINFORCED/6061 ALUMINUM

Description: METAL MATRIX COMPOSITES (MMC): CARBON (GRAPHITE) FIBER REINFORCED/ALUMINUM, GENERAL SPECIFICATION FOR

Description: LM-13 aluminum alloys reinforced with B\u2084C particles (5, 10, 15 wt. %) were prepared by gravity die casting. The samples were characterized on the basis of microstructure, microhardness, XRD and SEM. The microhardness tests indicated increased hardness values of the metal

Description: CoorsTek combines materials into composites to solve complex problems. Each composite is tailored to take advantage of the different materials' strengths. The resulting product exhibits better properties than the individual materials would have. A composite begins with a

• Features: Other

Description: A non-beryllium metal matrix composite, SupremEX™ B-135H consists of boron carbide at 35% volume fraction in a 1050 aluminum matrix, and has a closely matched coefficient of thermal expansion to AlBeMet 162 over the standard tactical temperature range (-50 - 50

• Applications: Aerospace / Aircraft (AQ), Electronics / RF-Microwave
• Type: Metal Matrix Composite
• Features: Non-ferrous - Any Type

Description: Cemented Carbides and Cermets BHCM13 M-14 Graphite and Carbon-Carbon Composites BHCM14 M-15 Ultrahard Materials: Diamond and Boron Nitride BHCM15 M-16 Aluminum Matrix Composites BHCM16 M-17 Electron Tubes and Vacuum Equipment BHCM17 M-18 Honeycomb Structures BHCM18 M-19

Description: This specification covers a dilute aluminum/TiB 2 metal matrix composite in the form of sand castings.

Description: This specification covers a dilute aluminum/TiB 2 metal matrix composite in the form of investment castings.

Description: This specification covers a dilute aluminum/TiB 2 metal matrix composite in the form of investment castings.

Description: "impossible" for more than 30 years with its innovative metal-to-ceramic, metal-to-composite, and metal-to-metal bonding solutions. PA&E's numerous "explosive" technologies such as Explosive Bonding can join otherwise incompatible materials without compromising

• Function / Performance: Abrasion / Erosion Resistant, Blast Mitigation / Armor, Conductive / Electrical, Corrosion / Chemical Resistant (Rust Preventive), Heat Resistant / High Temperature, Impact Resistant, Magnetic, Non-magnetic, Wear / Tribology
• Cladding / Overlay Material: Aluminum, Braze, Carbide / Hardmetal, Composite / Metal Matrix, Copper / Copper Alloy, Nickel / Nickel Alloy, Precious Metal (Gold, Silver), Refractory Metal, Solder, Steel - High Carbon / Alloy, Steel - Stainless, Steel - Tool, Titanium Alloy
• Surfacing Process: Explosive Bonding, Hardening / Heat Treatment
• Features: North America, Northwest US Only, Specialty / Other, United States Only

Description: Cemented Carbides and Cermets BHCM13 M-14 Graphite and Carbon-Carbon Composites BHCM14 M-15 Ultrahard Materials: Diamond and Boron Nitride BHCM15 M-16 Aluminum Matrix Composites BHCM16 M-17 Electron Tubes and Vacuum Equipment BHCM17 M-18 Honeycomb Structures BHCM18 M-19

Description: Duocel® aluminum foam is a true metal skeletal structure. It is not a sintered, coated, or plated product. Its purity is typically that of the parent alloy metal, with no voids, inclusions, or entrapments. The matrix of cells and ligaments is completely repeatable,

• Bulk Density: 11.8 lbs/ft³
• Tensile Strength: 180 psi
• Tensile Modulus (E): 14.6 ksi
• Thermal Conductivity: 40.21413332649231 BTU-in/hr-ft²-F

Description: CoorsTek provides USP Class VI compliant technical ceramic components and subassembly services to leading electrosurgical instrument manufacturers. See how our advanced ceramic components provide superior stiffness and dielectric strength to help build the medical devices of today and tomorrow.

• Density: 3.6999976648298842 to 6.0999961501249444 g/cc
• Thermal Conductivity: 2 to 30 W/m-K
• Coeff. of Thermal Expansion (CTE): 8.2 to 10 µm/m-C
• MOR / Flexural Strength: 51,923.1884898765 to 249,463.363694379 psi

Description: use in metal clad electric band and strip heaters. TYPES RS-DA & RS-DM can be readily cut with a knife or scissors. Joints can be made by wetting both surfaces with water (with a sponge or brush) and promptly pressing the two surfaces together. Thickness greater than 1/8" can be made by

• Thickness / Wall Thickness: 0.04 inch
• Length: 18 inch
• Diameter: 24 inch
• Max Use / Curie Temperature: 1,200 C

Description: use in metal clad electric band and strip heaters. TYPES RS-DA & RS-DM can be readily cut with a knife or scissors. Joints can be made by wetting both surfaces with water (with a sponge or brush) and promptly pressing the two surfaces together. Thickness greater than 1/8" can be made by

• Thickness / Wall Thickness: 0.04 inch
• Length: 18 inch
• Diameter: 24 inch
• Max Use / Curie Temperature: 1,200 C

Description: use in metal clad electric band and strip heaters. TYPES RS-DA & RS-DM can be readily cut with a knife or scissors. Joints can be made by wetting both surfaces with water (with a sponge or brush) and promptly pressing the two surfaces together. Thickness greater than 1/8" can be made by

• Thickness / Wall Thickness: 0.12 inch
• Length: 36 inch
• Diameter: 48 inch
• Max Use / Curie Temperature: 1,200 C

Description: Cemented Carbides and Cermets BHCM13 M-14 Graphite and Carbon-Carbon Composites BHCM14 M-15 Ultrahard Materials: Diamond and Boron Nitride BHCM15 M-16 Aluminum Matrix Composites BHCM16 M-17 Electron Tubes and Vacuum Equipment BHCM17 M-18 Honeycomb Structures BHCM18 M-19

Description: These shapes are derived by consolidating the aluminum-beryllium powder formed during hot isostatic pressing (HIP) and cold isostatic pressing (CIP), followed by extrusion. AM 162 Extrusions nominally contains 62% weight beryllium and 38% aluminum. Because of its light weight and

• Applications: Aerospace / Aircraft (AQ)
• Nonferrous: Aluminum / Aluminum Alloy (UNS A), Beryllium / Beryllium Alloy
• Shape / Form: Bar Stock, Rod / Round Bar Stock, Semi-finished Shape / Mill Stock, Sheet
• Features: Light Alloy, Metal Matrix Composite, Non-ferrous - Any Type, Refractory / Reactive (UNS R)

Description: well suited for use in high vacuum and reducing environments where silica cannot be tolerated, such as power metal and MIM furnaces with H2 atmospheres. They also have high electrical resistivity at elevated temperatures allowing them to be used in direct contact with resistance heating

• Length: 12 inch
• Width / O.D.: 12 inch
• Max Use / Curie Temperature: 1,650 C
• Coeff. of Thermal Expansion (CTE): 0.000007 µm/m-C

Description: metal-lined hoop-wrapped COPVs (CGA Type II), (3) plastic-lined composite pressure vessels (CPVs) with a nonload-sharing liner (CGA Type IV), and (4) an all-composite, linerless COPV (undefined Type). This guide also has relevance to COPVs used at cryogenic temperatures. 1.3 The

Description: metal-lined hoop-wrapped COPVs (CGA Type II), 3) plastic-lined composite pressure vessels (CPVs) with a nonload-sharing liner (CGA Type IV), and 4) an all-composite, linerless COPV (undefined Type). This guide also has relevance to COPVs used at cryogenic temperatures. 1.3 The

Description: Cemented Carbides and Cermets BHCM13 M-14 Graphite and Carbon-Carbon Composites BHCM14 M-15 Ultrahard Materials: Diamond and Boron Nitride BHCM15 M-16 Aluminum Matrix Composites BHCM16 M-17 Electron Tubes and Vacuum Equipment BHCM17 M-18 Honeycomb Structures BHCM18 M-19

Description: we machine include: Alumina, Sapphire, Aluminum Nitride, Silicon Nitride, Silicon Carbide, MMC(Metal Matrix Composites)*2, CMC(Ceramic Matrix Composites), Zirconia, Steatite, Silicon, Glasses (TEMPAX Float®, Corning Glass ULE®, Fused Quartz / Fused Silica

• Machining Capabilities: Broaching, CNC Machining, Deep Hole Drilling, Drilling, Milling, Screw Machining, Surface Grinding, Turning, Wire EDM
• Services: CAD / CAM Support, High Volume Production, Just-in-Time Delivery, Low Volume Production, Prototype Services
• Materials: Ceramics, Composites, Glass, Glass Ceramics, Quartz, Ultra-hard Materials
• Features: East Asia / Pacific Only, Other

Description: Aremco offers a broad range of machinable and fully-dense ceramic materials for applications in which high temperature insulation, thermal shock resistance and high dielectric strength are required. Aremcolox™ and Super-Heat ceramics include compositions based on alumina, alumino-silicates, boron

• Density: 2.4358300762478375 g/cc
• Max Use / Curie Temperature: 1,204.4444444444443 C
• Thermal Conductivity: 40 W/m-K
• MOR / Flexural Strength: 18,200 psi

Description: and packaging material integrated circuit substrate, electrolytic cell lining, metal matrix composite reinforcement body, active armor material, heat sink and heating element of high temperature furnace. In the electronics and power industries, insulating ceramics, such as

• Density: 3.8999975386044725 g/cc
• MOR / Flexural Strength: 47,862.15698787501 psi
• Compressive / Crushing Strength: 290,073.678714394 psi
• Material Type: Alumina / Aluminum Oxide

Description: 250 nanometers (0.150 to 0.250 microns). Applications Magnetic media filler: Video tapes, audio tapes, data storage devices Polishing abrasive Structures: Metal matrix composites, ceramic bodies

• Compound / Abrasive Type: Aluminum Oxide
• Grading System: Micron Graded
• Type: Polishing
• Form: Powder

Description: Aluminum Nitride, Silicon Carbide, Silicon Nitride, and Zirconia. We are very passionate about machining newly developed or extremely hard materials. We even machine CMC(Ceramic Matrix Composites)* for applications in space. We employ a variety of CNC machining centers including

• Diameter: 1" - 3", 3" - 6", 6" - 48", Less than 1"
• CNC Machining: 3-axis Machining, 5-axis Machining, Deep Hole Drilling, Drilling, Milling, Screw Machining, Turning, Wire EDM
• Additional Services: Assembly Services, CAD / CAM Support, Design Assistance, High Volume Production, Just-in-Time Delivery, Low Volume Production, Prototype Services
• Materials: Ceramics, Glass, Glass Ceramics, Hardened Metals, Ultra-hard Materials

Description: for aerospace applications. VICTREX PEEK polymers may successfully replace metals such as aluminum, titanium, magnesium, brass, corrosion-resistant (CRES) or stainless steel and specialty alloys because it offers a unique combination of mechanical, thermal and tribological properties,

• Tensile Strength (Break): 100 to 110 psi
• Tensile Modulus: 3.7 ksi
• Elongation: 15 to 45 %
• Use Temperature: 350 to 365 F

Description: *2CMC(Ceramic Matrix Composites): A fiber-reinforced ceramic composed of SiC fibers and SiC matrix. It is light-weight, high-temperature strength, and high durability material developed as a next-generation material for aero-engines.

• Materials: Alumina (Al₂O₃), Composite, Glass Ceramic, Metal Carbide / Hard Metal (WC, TiC), Nitride (AlN, BN), Porous Ceramic, Sapphire, SiAlON (Al₂O₃-Si₃N₄), Silicate / Fused Silica, Silicon Carbide (SiC), Silicon Nitride
• Services: Ceramic Part Fabrication, Material Selection, Materials Development / R&D, Testing / Inspection
• Features: East Asia / Pacific Only
• Process: Grinding, Machining

Description: metal, rubber, footwear, leather, apparel, fabric, tape paper products, pharmacy and so on Standard( including but not limited to below): ASTM B565 Shear Aluminum Products Test er ASTM C273 Shear - Sandwich Materials - Flatwise Tester ASTM D1002 Lap Shear Testing for Adhesively Bonded

• Force / Load Capacity: 4,410 lbs
• Test Speed: 0.003937007874015741 to 19.68503937007871 in/min
• Display / User Interface: Application Software, Computer Interface
• Mechanical Test: Shear / Torsion

Description: liner thicknesses less than 2.3 mm (0.090 in.), and fiber loadings in the composite overwrap greater than 60 percent by weight. In COPVs, the composite overwrap thickness will be of the order of 2.0 mm (0.080 in.) for smaller vessels, and up to 20 mm (0.80 in.) for larger ones. 1.2