Search Results for aerospace bolting applications

AEREX 350 is a bolt alloy with a combination high temperature creep strength, notch toughness, and thermal stability. It was designed for aerospace bolting applications. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance. Filing Code: Ni-479. Producer or source: SPS Technologies.

Nicrofer 7016 TiNb is an austenitic age-hardening Ni-Cr-Fe alloy containing Ti, Nb, and Al. High tensile strength is combined with good weldability. This aerospace alloy finds applications in rocket exhaust heat exchangers, springs, bellows, and bolts. This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-534. Producer or source: VDM Technologies Corporation.

LESCALLOY 4335+V VAC-ARC is a low-alloy steel with high hardenability and good strength and toughness. It is produced by the vacuum consumable electrode melting process to provide optimum cleanliness and preferred ingot structure. Its uses include aircraft and aerospace components, gears, shafting, bolts and crankshafts. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-390. Producer or source: Latrobe Steel Company.

BRUSH WELLMAN S-65B is a grade of beryllium strengthened by a dispersion of beryllium oxide. It has moderate strength and fairly low ductility (a minimum of 3% elongation). Its uses include optical applications, nuclear reactors, instrumentation, X-ray windows, high-speed computer parts, audio components and aerospace structural applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Be-3. Producer or source: Brush Wellman Inc..

VascoMax T-250 is an ultra-high-strength steel that delivers the high strength (250 ksi tensile strength) and toughness of VascoMax 250 (Alloy Digest SA-142, March 1963). Yet VascoMax T-250 contains no cobalt and less molybdenum (both strategic elements) than the standard grade. In addition, the new grade provides higher ductility and toughness. VascoMax T-250 is recommended for aerospace structures, pressure vessels, shafting, bolts, and fasteners. This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-387. Producer or source: Teledyne Vasco.

Crucible 422 has a structure of tempered martensite to give the alloy high strength. It is useful in the aerospace industry for structurals with high strength/weight ratios. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-1004. Producer or source: Crucible Service Centers.

Ultibron CNS is a high-performance silicon bronze alloy with excellent corrosion resistance. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion resistance as well as forming, machining, and joining. Filing Code: CU-769. Producer or source: Advanced Metals International.

SPS Technologies Aerex 350 is a proprietary high-strength, corrosion-resistant nickel-based superalloy that is suitable for demanding applications up to 730 °C (1350 °F). It has the highest temperature limit of the three SPS superalloys. Like MP35N and MP159, this alloy not only undergoes the multiphase reaction, but also benefits from two additional strengthening mechanisms. Elements are also added to the chemical composition to cause precipitation of the gamma prime phase with higher temperature capability than MP159. Because this alloy is used at even higher temperatures than MP159, elements are added to the chemical composition to also cause the precipitation of eta phase during thermal treatments. This phase contributes to notch toughness at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance. Filing Code: Ni-780. Producer or source: SPS Technologies, Inc.

Marinel 220 is a copper alloy of 18% Ni with high manganese and aluminum. It develops high strength with excellent corrosion resistance. It is the successor alloy to Marinel (see Alloy Digest Cu-602, December 1995). This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming and machining. Filing Code: CU-736. Producer or source: Langley Alloys.

ALLEGHENY Type 216 is an austenitic stainless steel offering superior corrosion resistance, excellent strength properties, and low magnetic permeability. It finds applications in marine engineering, aerospace, and the process industries. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness and fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-243. Producer or source: Allegheny Ludlum Corporation.

Nibron Special is an extra high-strength nickel bronze that is corrosion resistant in both marine environments and industrial media. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as machining and joining. Filing Code: Cu-844. Producer or source: Columbia Metals Ltd.

Altemp X-750 is a precipitation-hardenable nickel-base alloy that is highly resistant to chemical corrosion and oxidation and has excellent stress-rupture and creep properties at temperatures up to 815 deg C (1500 deg F) after suitable heat treatment. The alloy has oxidation resistance up to 980 deg C (1800 deg F). It is typically used in aircraft turbine and structural components. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ni-649. Producer or source: Allegheny Ludlum.

K-KARB (Carbon-Carbon) is a graphitized structural graphite fabricated from a graphitized cloth precursor. The layers of graphitized cloth are laminated and bonded together with a graphitic matrix forming a light weight, high strength graphite. This datasheet provides information on physical properties, tensile properties, and compressive and shear strength as well as fracture toughness. It also includes information on corrosion resistance as well as machining. Filing Code: Cp-2. Producer or source: Kaiser Aerotech.

Inconel alloy MA 758 is a further development of the well-established aerospace superalloy Inconel alloy MA 754 (Alloy Digest Ni-244, March 1990) with an increased chromium content for better resistance to high-temperature corrosives. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as machining, joining, and powder metal forms. Filing Code: Ni-511. Producer or source: Inco Alloys International Inc.

Boehler L080A is a nickel-base alloy with good creep resistance to 805 deg C (1480 deg F). The alloy has excellent oxidation resistance. It is used in the aerospace industry. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, and machining. Filing Code: Ni-656. Producer or source: Böhler-Uddeholm North America.

TIMETAL 21S (Ti-15%Mo-3%Nb-3%Al-0.2Si) offers the good cold formability and weldability of a beta strip alloy, but with greatly improved oxidation resistance and creep strength. Aerospace applications include engine exhaust plug and nozzle assemblies. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming and heat treating. Filing Code: TI-105. Producer or source: Titanium Metals Corporation (Timet). Originally published March 1993, revised October 1998.

Austral Wright 17-4PH (UNS S17400) is a precipitation hardening stainless steel which has extremely high strength and hardness, combined with good ductility and toughness. It has excellent corrosion resistance, approaching that of type 304 austenitic stainless steel. Designers and engineers often choose Austral Wright 17-4PH for its high strength, with corrosion resistance superior to most of the other high strength steels. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: SS-1352. Producer or source: Austral Wright Metals.

Direct Forge 6069 is a Mg-Si-Cu age-hardenable aluminum alloy. Tensile strength in the T-6 condition is approximately 40% higher than that of 6061 alloy with similar corrosion resistance. Applications include light wall bicycle frames and seamless gas cylinders. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as heat treating and joining. Filing Code: AL-374. Producer or source: Northwest Aluminum Company.

SPS Technologies MP159 is a cobalt-nickel multiphase alloy that possesses a unique combination of ultra-high strength, good ductility and toughness, and excellent corrosion resistance. This alloy was developed in response to the need for a fastener alloy that could perform under the higher operating temperatures required for turbine engines and other high performance motors. It has advantages similar to MP35N but can perform in applications up to 593 °C (1100 °F) and is suitable for short term use at even higher temperatures. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: Co-138. Producer or source: SPS Technologies, Inc.

UNILOY 17-4 is a unique stainless steel. It can be annealed (solution treated) to produce a martensite-austenite mixture and then aged to various levels of hardness and strength. It has high mechanical properties including good strength at both sub-zero and elevated temperatures. Its corrosion resistance is excellent. Its many applications include gears, splines, shafts, valves, fasteners and couplings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on corrosion resistance as well as heat treating, machining, and joining. Filing Code: SS-397. Producer or source: Cyclops.