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 covers procedures for identifying wrought products of tanium and titanium alloys.

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: 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: Universal 321 is a titanium stabilized filler metal used with the gas metal arc and gas tungsten arc processes. Universal 321 stabilized weldments are often subjected to severe corrosive and high temperature service such as; aircraft exhaust manifolds, cabin heaters, fire walls and pressure

• Tensile Strength (UTS, Break): 95,000 psi
• Yield Strength (YS): 65,000 psi
• Elongation: 40 %
• Specifications: AMS

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