AMS Specifications Titanium

Description: This specification defines the procedures and requirements for fusion welding titanium and titanium alloys and the properties of such weldments.

Description: This specification establishes the engineering requirements for producing an electrolytic conversion (anodic) coating on titanium and titanium alloys and the properties of the coating.

Description: This specification defines the procedures and requirements for fusion welding titanium and titanium alloys and the properties of such weldments.

Description: This specification covers procedures for identifying wrought products of tanium and titanium alloys.

Description: These alloys are commonly referred to as commercially pure (C.P.) titanium with the level of impurities and mechanical properties increasing slightly from ERTi-1 to ERTi-4. C.P. Grade 2 titanium (ERTi-2) is the most widely used titanium alloy for industrial applications because

• Applications: Aerospace / Aircraft (AQ), Pressure Vessel (PVQ)
• Features: Non-ferrous - Any Type, Other, Pure / Very Low Alloy, Refractory / Reactive (UNS R), Specialty / Other, Titanium / Titanium Alloy
• Shape / Form: Wire / Shaped Wire

Description: Specifications AWS A5.16 Classes ERTi-1, 2, 3 and 4/AMS 4951D Shielding Gas Argon is the recommended shielding gas, however an argon-helium mixture will give greater penetration although at the expense of arc stability. Description Washington Alloy Commercial Pure Titanium is a

Description: Armite Lubricants Graphite Petrolatum Anti-Seize Compound meets specification SAE-AMS-2518 Rev D. This anti-seize compound is safe to use in contact with austenitic corrosion-resistant steels, titanium, nickel and cobalt alloys, and related corrosion resistant metals and alloys.

• Flash Point: 200.12 F
• Density / Specific Gravity (@15.6°C, 60°F): 1.25 specific gravity
• Type: Anti-Seize / Thread Compound
• Composition / Chemistry: Graphite, Synthetic / Semi-synthetic

Description: Requirements for aerospace resistance spot and seam welding of aluminum, magnesium, steel, nickel, cobalt, titanium, and their alloys. Intended to replace MIL-W-6858D and AMS-W- 6858A. ANSI Approved. approx. 44 pages,11 figures, 13 tables. ISBN 978-0-87171-064-2

Description: requirements for coatings of autocatalytic nickel boron deposited from aqueous solutions onto substrates for engineering use. The specification classifies these coatings into two types: 1.2.1 Type 1 coatings have a boron content of 0.1 to less than 3.5 mass percent with the balance nickel.

Description: corrosion resistance and good strength. Also available in other stainless and nickel alloy grades (i.e. 321, 600 etc.). Normally available in commercial specifications (i.e. ASTM-A-269); Occasionally available in other specs. (i.e. Mil-T-8504, AMS-5570). Primarily stocked in annealed

• Outside Diameter / Size: 0.0313 to 3 inch
• Maximum Inside Diameter / Size: 2.93 inch
• Wall Thickness: 0.75 inch
• Features: Aluminum, Brass / Bronze, Copper, Hastelloy®, Stainless Steel, Steel, Titanium, Welded and Drawn (W&D)

Description: Through a network of facilities worldwide, Lubrication Sciences International provides Dicronite dry lubrication. Dicronite dry lubrication reduces friction and wear with an extremely low coefficient of friction (0.030) in a very thin film (0.5 microns) that is extremely stable under a wide

• Industry Served: Aerospace, Automotive, Castings / Cast Metal, Chemical / Material Processing, Electronics, Energy / Utilities, Food & Beverage, Machine Tools, Maintenance / MRO, Marine, Medical / Healthcare, Military Specification, OEM / Industrial, Oil & Gas, Process Equipment
• Materials: Aluminum, Carbide, Ceramic, Copper / Copper Alloys, Iron / Cast Iron, Metal, Nickel / Nickel Alloys, Plastic, Stainless Steel, Steel / Steel Alloys, Titanium
• Functions & Features: Conductive, Friction Reducing / Low Friction, Mold Release / Nonstick, VOC Compliant
• Services: Degreasing, Inspection / Monitoring, New / OEM Parts, Recoating / Refinishing, Ultrasonic Cleaning

Description: services include flow, vacuum leak, and an ultrasonic C-scan. Assemblies can be certified to AMS, AWS and Mil specifications. Consultation services are available to help you design your part for successful vacuum brazing services.

• Applications / Industry: Aerospace / Avionics, Heat Sinks / Thermal Management, Honeycomb Structures, Medical Devices / Health Care, Process Equipment (Heat Exchangers, Tanks, etc.), Specialty / Other, Tubing Assembly / System
• Services: Brazing
• Materials: Carbide / Hardmetal, Carbon (Graphite, Diamond, etc.), Ceramics / Ceramic-to-Metal, Copper / Copper Alloy, Dissimilar Materials, Refractory Metal, Steel - Carbon / Alloy, Steel - Stainless, Titanium Alloy
• Additional Services: Design Assistance, High Volume Production, Low to Mid Volume Production, Testing and Inspection

Description: (Commercially Pure Titanium: Grade 2) (40A) Strip, Coil, Foil, Wire, ASTM B265 GR2, AMS 4902, ASTM F67, MIL-T-9046CP3 APPLICATIONS Bellows aircraft structural honeycomb gaskets aircraft skin heat exchanger parts TITANIUM GRADE 2 DESCRIPTION Commercially Pure Titanium

• UNS Number: 50,400
• Tensile Strength (UTS, Break): 50,000 psi
• Yield Strength (YS): 40,000 to 65,000 psi
• Elongation: 20 %

Description: Ti 15-3-3-3 Strip, Coil, Foil & Wire, AMS 4914 APPLICATIONS Airframe structures Ducting Honeycombs Hydraulic tubing Springs Fasteners DESCRIPTION Titanium Alloy 15-3-3-3 is a metastable beta titanium alloy that offers substantial weight reductions over other engineering

• UNS Number: 58,153
• Tensile Strength (UTS, Break): 102,000 to 180,000 psi
• Yield Strength (YS): 100,000 to 170,000 psi
• Elongation: 5 to 12 %

Description: Titanium alloy 8A1-1Mo-1V filler metal is for gas-metal-arc and gas tungsten arc welding of base metals of similar analysis.

• Specifications: AMS
• Applications: Aerospace / Aircraft (AQ)
• Type: Light Alloy
• Features: Non-ferrous - Any Type, Other, Refractory / Reactive (UNS R), Titanium / Titanium Alloy

Description: Alloy 263 is a Ni-Co-Cr-Mo-Ti-Al precipitation-hardenable alloy. 263 is furnished in the solution-treated condition unless otherwise specified. It exhibits high strength, corrosion resistance, excellent formability, ductility, and weldability. This alloy is normally used for applications up to

• Overall Thickness: 0.177 to 0.24 inch
• Specifications: AMS, UNS
• Features: Alloy, Aluminum / Aluminum Alloy (UNS A), Cobalt / Cobalt Alloy, Copper, Brass or Bronze Alloy (UNS C), Corrosion Resistant, Heat Resistant / Hot Work, Nickel / Nickel Alloy (UNS N), Non-ferrous - Any Type, Refractory / Reactive (UNS R), Titanium / Titanium Alloy
• Processing, Temper & Finish: Hardened / Heat Treated