Browse Topic: Corrosion resistant alloys

Items (6,499)
This specification covers an aluminum alloy in the form of sheet and plate, alclad two sides, 0.188 to 1.000 inch (4.775 to 25.400 mm), inclusive, in thickness, supplied in the annealed (O) condition (see 8.5).
AMS D Nonferrous Alloys Committee
The industrial world focuses on developing eco-friendly, natural fibres such as reinforcing lightweight, inexpensive compounds in modern days. Basalt, a rare phenomenon, derives its origins from molten volcanic rocks, which is essential for their cost-effectiveness and offers different glass fibre properties. High mechanical strength, outstanding wear resistance, and exceptional durability in a variety of environmental conditions are all displayed by basalt fibres. These fibres are ideal for reinforcing polymer composites because of their mechanical properties at high temperatures. Furthermore, basalt fibres are appropriate for long-term applications because they resist corrosion and degradation while maintaining structural integrity over time. This article provides a brief overview of basalt fibres as a substitute for glass fibres and as composite materials. Additionally, attempts are being made to draw attention to the expanding field of basalt fibre research. In the review, studies
Chidambaranathan, BibinRaghavan, SheejaSoundararajan, GopinathArunkumar, S.Ashok Kumar, R.Rajesh, K.
This specification covers an aluminum alloy in the form of sheet and plate alclad two sides, over 0.187 to 1.000 inch (over 4.750 to 25.40 mm) in nominal thickness, supplied in the -T3/-T351 temper (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.187 inch (1.02 to 4.75 mm), inclusive, in nominal thickness (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Basalt-based products are known to provide substantial wear and corrosion resistance even in harsh environments. This paper aims to explore the stir casting technique as an efficient way to reinforce basalt particulates into Aluminium (AA7075). The properties such as hardness, ultimate tensile strength with corrosion behaviour of the composites were evaluated and compared with as-cast AA7075 fabricated under the same conditions. It is evident from the results that an increase in basalt particulate content significantly increases the ultimate tensile strength of 216 MPa and hardness of 123 VHN. The mechanism of bonding between basalt particulate and aluminum alloy at the interface was studied using scanning electron microscopy (SEM). AA7075 matrix composites exhibited better corrosion resistance and they showed enhancement in thermal and mechanical properties.
Vallimanalan, A.Murali, M.Mahendran, R.Manivannan, S.
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 0.499 inch (0.51 to 12.67 mm), inclusive, in nominal thickness alclad two sides (see 8.5).
AMS D Nonferrous Alloys Committee
This SAE Aerospace Standard (AS) defines the requirements for air cycle air conditioning systems used on military air vehicles for cooling, heating, ventilation, and moisture and contamination control. General recommendations for an air conditioning system, which may include an air cycle system as a cooling source, are included in MIL-E-18927E and JSSG-2009. Air cycle air conditioning systems include those components which condition high temperature and high pressure air for delivery to occupied and equipment compartments and to electrical and electronic equipment. This document is applicable to open and closed loop air cycle systems. Definitions are contained in Section 5 of this document.
AC-9 Aircraft Environmental Systems Committee
This specification covers an aircraft-quality, corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a precision cold-rolled corrosion- and heat-resistant nickel alloy in the form of sheet and strip over 0.005 to 0.015 inch (0.13 to 0.38 mm), inclusive, in nominal thickness and foil up to 0.005 inch (0.13 mm), inclusive, in nominal thickness (see 8.4).
AMS F Corrosion and Heat Resistant Alloys Committee
This procurement specification covers aircraft-quality solid rivets and tubular end rivets made from a corrosion-resistant steel of the type identified under the Unified Numbering System as UNS S34700.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers aircraft quality retaining rings of the spiral wound type with uniform rectangular cross-sections and made from a corrosion resistant austenitic iron base alloy of the type identified under the Unified Numbering System as UNS S30200, and of spring temper condition.
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers closely-wound helical coil, screw thread inserts made from an age hardenable nickel base alloy formed wire of the type identified under the Unified Numbering System as UNS N07750. The inner surface of the insert coil, after assembly into a screw thread tapped hole, provides internal threads of standard 60° Unified Form.
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a corrosion- and heat-resistant nickel alloy in the form of wire up to and including 0.563 inches (14.30 mm) in diameter.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of sheet 0.040 to 0.249 inches (1.02 to 6.32 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers an aluminum alloy in the form of alclad sheet over 0.039 to 0.126 inches (0.99 to 3.20 mm), inclusive, in nominal thickness with a fine-grain core of ASTM No. 6 or finer (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of alclad coiled sheet from 0.010 to 0.128 inch (0.25 to 3.25 mm), inclusive, in thickness supplied in the -T4 temper (see 8.5).
AMS D Nonferrous Alloys Committee
This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivets.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers solid rivets and hollow end rivets made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 80 ksi single shear strength at room temperature.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers retaining rings of the spiral wound type with uniform rectangular cross-section, made of a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, work strengthened and heat treated to a tensile strength of 185 to 240 ksi at room temperature.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable, nickel base alloy of the type identified under the Unified Numbering System as UNS N07041 and of 155 ksi tensile strength at room temperature, with maximum test temperature of parts at 1400 °F.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers split cotter pins with optional ends (see Figure 1), made to metric dimensions and made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S32100.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers split cotter pins with optional ends (see Figure 1), made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S32100.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers aircraft-quality solid rivets and tubular end rivets made from a corrosion- and heat-resistant nickel alloy of the type identified under the Unified Numbering System as UNS N06002.
E-25 General Standards for Aerospace and Propulsion Systems
This procurement specification covers aircraft-quality solid rivets made from a corrosion- and heat-resistant cobalt alloy of the type identified under the Unified Numbering System as UNS R30605.
E-25 General Standards for Aerospace and Propulsion Systems
Items per page:
1 – 50 of 6499