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CURRENT
2017-07-20
Standard
AMS4975N
This specification covers a titanium alloy in the form of bars, wire, flash welded rings 3.00 inches (76.2 mm) and under in nominal diameter or least distance between parallel sides and 16 in2(103 cm2) and under in cross-sectional area and stock of any size for flash welded rings (see 8.4).
CURRENT
2017-07-20
Standard
AMS4976K
This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal diameter or least distance between parallel sides and 9 in2 (58 cm2) and under in cross-sectional area and forging stock of any size (see 8.5).
CURRENT
2017-07-20
Standard
AMS5862M
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 4.0 inches (102 mm) and under in nominal thickness (see 8.5).
2017-07-19
WIP Standard
G17AB
This specification covers a titnaium alloy in the form of forgings 4.4 inches (111.76 mm) and under in nominal diameter or least distance between parallel sides and forging stock of any size.
CURRENT
2017-07-19
Standard
AMS5825H
This specification covers a corrosion resistant steel in the form of welding wire.
CURRENT
2017-07-17
Standard
AMS2482E
This specification establishes the requirements for a hard aluminum oxide coating, impregnated or codeposited with polytetrafluoroethylene (PTFE) on aluminum alloys.
CURRENT
2017-07-14
Standard
AMS4044N
This specification covers an aluminum alloy in the form of sheet and plate from .008 to 2.000 inches, incl (0.20 to 50.80 mm, incl) in thickness, supplied in the annealed (O) condition (see 8.4).
CURRENT
2017-07-14
Standard
AMS4368
This specification covers discontinuously reinforced aluminum alloy (DRA) metal matrix composites (MMC) made by mechanical alloying of 6061B aluminum powder and SiC particulate, which is then consolidated by Hot Isostatic Pressing (HIP) into shapes between 12 to 100 in2 (0.008 to 0.065 m2) cross-section inclusive. Tensile property response to heat treatment has been demonstrated on samples of 1 in2 (645 mm2) maximum cross section (see 8.9).
CURRENT
2017-07-11
Standard
AMS2631E
This specification covers the procedure for ultrasonic inspection of wrought titanium and titanium alloy products 0.25 inch (6.4 mm) and over in cross-section (thickness) or diameter.
2017-07-10
Technical Paper
2017-28-1969
Senthil Ram Nagapillai Durairaj, Thulasirajan Ganesan, Praveen Chakrapani Rao
Abstract Magnesium alloy current being used for automotive sector and are being significantly used for manufacturing engine block as offering higher power to weight ratio to the vehicle. In this context, the magnesium alloy has been used in the replacement of aluminium alloy for the starter housing which in turn increase the power to weight ratio of the motor. Considering the operation condition of starter motor in the engine of the vehicles, the starter motor is being exposed to the harsh environment, where its system is being tested for Noise, Vibration and Harshness. In this paper, the magnesium alloy housing is used to study the vibration and noise developed in the starter motor and the same is compared with the noise and vibration of the motor when it being used with Aluminium alloy Housing. First, the vibration study is carried out for the housing part alone to capture the resonant frequency of the both housing alloy say, Aluminium and Magnesium.
2017-07-10
Technical Paper
2017-28-1986
Dinesh Paulraj, S.S.M Abdul Majeed, R Rajendran
Abstract In this study, the TiO2 nano particles are incorporated with A356 aluminium to form a Metal Matrix Composite (MMC) to be utilized in aerospace, marine, military and automotive applications. Stir casting method was used for producing the metal matrix composites. A356 aluminium was reinforced with various weight percentage (wt%) of TiO2 under 10 minutes holding time and 450 rpm stirring speed. Mechanical properties such as tensile strength and hardness of the Metal Matrix Composite were tested. Using Scanning electron microscope the surface morphology and composition of the manufactured specimens were studied. Energy dispersive spectroscopic analysis was carried out to study the elemental composition of the MMC. The mechanical tests reveal that there is a significant enhancement in the properties of the composites with 1.5 wt% of TiO2.
2017-07-10
WIP Standard
AMS5596M
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, foil, and plate 1.00 inch (25.4 mm) and under in thickness (see 8.5).
CURRENT
2017-07-07
Standard
AMS7510/1C
This specification covers one type of samarium-cobalt permanent magnet.
CURRENT
2017-07-07
Standard
AMS4031J
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 2.000 inches (0.51 to 50.80 mm), inclusive, in nominal thickness, supplied in the annealed (O) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper.
2017-07-06
WIP Standard
AMS7464D
This specification covers premium quality bolts and screws made from a low-alloy, heat-resistant steel and having threads of UNJ (MIL-S-8879) form.
2017-07-06
WIP Standard
AMS2376E
This specification covers procedures for approval of premium quality forgings, usually serialized, the stock from which such forgings are produced, and the controls to be exercised in producing the forgings and forging stock.
2017-07-04
WIP Standard
AMS5122K
This specification covers a carbon steel in the form of strip.

This material hs been used typically for washers and other stamped parts requiring a smooth finish and only slight or no forming, but usage is not limited to such applications.

2017-07-04
WIP Standard
AMS7301J
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2017-07-04
WIP Standard
AMS5328E
This specification covers a low alloy steel in the form of investment castings.
2017-07-04
WIP Standard
AMS5315E
This specification covers a ductile (nodular) iron in the form of sand castings.
2017-07-04
WIP Standard
AMS5316E
This specification covers a ductile (nodular) iron in the form of sand castings.
2017-07-04
WIP Standard
AMS7311H
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.
2017-07-04
WIP Standard
AMS5115J
This specification covers a carbon steel in the form of wire supplied as coils of wire or as finished springs. Primarily for springs, such as valve springs, subject to moderate stresses and requiring good fatigue properties.
2017-07-03
WIP Standard
AMS5061H
This specification has been declared "NONCURRENT "by the Aerospace Materials Division, SAE, as of February 2009. It is recommended, therefore, that this specification not be specified for new designs.
2017-07-03
WIP Standard
AMS5042N
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
2017-07-03
WIP Standard
AMS5031G
This specification covers a low-carbon steel in the form of covered welding electrodes.
Viewing 1 to 30 of 10672

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