Browse Topic: Beryllium

Items (139)
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by hot isostatic pressing (HIP) (see 8.5).
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of sheet and plate produced by hot rolling beryllium with nominal thicknesses from 0.020 to 1.000 inches (0.51 to 25.4 mm), inclusive (see 8.5).
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot-pressed powder.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot-pressed powder.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from impact-ground beryllium powder consolidated by cold isostatic pressing (CIP) and sintering.
AMS G Titanium and Refractory Metals Committee
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of bar, rod, tubing, and shapes.
AMS G Titanium and Refractory Metals Committee
E-25 General Standards for Aerospace and Propulsion Systems
ACBG Plain Bearing Committee
Manufacturing workpieces with unique material characteristics can provide machining challenges. The metal beryllium is an excellent example. Beryllium is two-thirds the weight of aluminum and six times as stiff as steel. It has a high melting point and a very low range of thermal expansion. Those attributes deliver performance that is crucial in precision applications such as aircraft components, spacecraft, communication satellites and optics. However, beryllium is also hard and brittle and produces powder instead of chips when machined, therefore requiring special machining techniques to avoid cracking. It is also expensive, about $1,500 a pound. And finally, it is toxic and causes severe allergic reactions in those sensitive to it. As such, only a few shops in the United States are the lone providers of parts made from this tricky material. One of those is a California shop that combines a deliberate, highly structured production process; data-driven manufacturing analytics; precise and reliable machine tools; and longtime familiarity with processing beryllium to manufacture parts profitably and safely. Founded in 1954, L.A. Gauge Company in Sun Valley, California, is an ultra-precision machining and optic shop focusing on specialty metal fabrication for the aerospace and defense Industry. The shop regularly holds machining tolerances to within 40 millionths of an inch (1 micron), and polishing tolerances to within billionths of an inch (1 Angstrom).
Manufacturing workpieces with unique material characteristics can provide machining challenges. The metal beryllium is an excellent example. Beryllium is two-thirds the weight of aluminum and six times as stiff as steel. It has a high melting point and a very low range of thermal expansion. Those attributes deliver performance that is crucial in precision applications such as aircraft components, spacecraft, communication satellites and optics. However, beryllium is also hard and brittle and produces powder instead of chips when machined, therefore requiring special machining techniques to avoid cracking. It is also expensive, about $1,500 a pound. And finally, it is toxic and causes severe allergic reactions in those sensitive to it. As such, only a few shops in the United States are the lone providers of parts made from this tricky material.
This specification covers an aluminum alloy in the form of wire, sheet, foil, pig, grains, shot, and chips.
AMS D Nonferrous Alloys Committee
This specification covers beryllium in the form of sheet and plate produced by hot rolling beryllium.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot pressed powder.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot pressed powder.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes from vacuum hot pressed powder.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by cold isostatic pressing (CIP) and sintering.
AMS G Titanium and Refractory Metals Committee
This specification covers an aluminum-beryllium alloy in the form of bars, rods, tubing, and shapes consolidated from powder by extrusion.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by hot isostatic pressing (HIP).
AMS G Titanium and Refractory Metals Committee
ACBG Plain Bearing Committee
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers an aluminum alloy in the form of wire, sheet, foil, pig, grains, shot, and chips.
AMS D Nonferrous Alloys Committee
E-25 General Standards for Aerospace and Propulsion Systems
This specification covers a magnesium alloy in the form of welding wire.
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of welding wire.
AMS D Nonferrous Alloys Committee
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of blocks, blanks or shapes.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by hot isostatic pressing (HIP).
AMS G Titanium and Refractory Metals Committee
ACBG Plain Bearing Committee
Lightweight Materials: Understanding the BasicsB-ASM-04110/1/2012
This book covers the properties, processing, and applications of lightweight materials– aluminum, magnesium, beryllium, titanium, titanium aluminides, engineering plastics, structural ceramics, and composites with polymer, metal, and ceramic matrices. The book begins with a brief history of lightweight materials development during the 20th century, and moves into the basic metallurgy, properties of the available alloys, processing, and applications of each of the lightweight materials. The book's final chapter covers methodologies used in the general materials selection process, specific guidelines for each of the lightweight materials, and the importance of the automotive sector to the lightweight materials industries. Topics include: -Uses of Lightweight Materials - Aluminum Alloys -Magnesium Alloys -Beryllium -Titanium Alloys -Titanium Aluminide Intermetallics -Engineering Plastics -Polymer Matrix Composites -Metal Matrix Composites -Structural Ceramics -Ceramic Matrix Composites -Selection Guidelines for Lightweight Materials This book is intended primarily for technical personnel who want to learn more about lightweight materials. It would be useful to designers, structural engineers, material and process engineers, manufacturing engineers, production personnel, faculty, and students.The book's unique feature is that it provides a single-source reference that covers all of the major types of lightweight materials.
Campbell, F.C.
This specification covers an aluminum alloy in the form of wire, sheet, foil, pig, grains, shot, and chips.
AMS D Nonferrous Alloys Committee
A paper describes how, based on a structural-thermal-optical-performance analysis, it has been determined that a single, large, hollow corner cube (170-mm outer diameter) with custom dihedral angles offers a return signal comparable to the Apollo 11 and 14 solid-corner-cube arrays (each consisting of 100 small, solid corner cubes), with negligible pulse spread and much lower mass. The design of the corner cube, and its surrounding mounting and casing, is driven by the thermal environment on the lunar surface, which is subject to significant temperature variations (in the range between 70 and 390 K). Therefore, the corner cube is enclosed in an insulated container open at one end; a narrow-bandpass solar filter is used to reduce the solar energy that enters the open end during the lunar day, achieving a nearly uniform temperature inside the container. Also, the materials and adhesive techniques that will be used for this corner-cube reflector must have appropriate thermal and mechanical characteristics (e.g., silica or beryllium for the cube and aluminum for the casing) to further reduce the impact of the thermal environment on the instrument’s performance.
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of blocks, blanks or shapes.
AMS G Titanium and Refractory Metals Committee
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from beryllium powder consolidated by hot isostatic pressing (HIP).
AMS G Titanium and Refractory Metals Committee
This specification covers an aluminum-beryllium alloy in the form of bars, rods, tubing, and shapes consolidated from powder by extrusion.
AMS G Titanium and Refractory Metals Committee
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of bar, rod, tubing, and shapes.
AMS G Titanium and Refractory Metals Committee
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