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1952-01-01
Technical Paper
520141
WILLIAM G. GUIDE
1952-01-01
Technical Paper
520157
H. W. ANDERSON
1952-01-01
Technical Paper
520168
BEN D. MILLS
1952-01-01
Technical Paper
520186
GEORGE W. PAPEN
This paper discusses the Aircraft Industry requirements for large forgings and extrusions and supports these requirements by analyzing the effect of the trend in performance on aircraft structure, function and production. The paper confirms that large integral structural components satisfy these trends better than a continuation of conventional “bits & pieces” structure. It further concludes that large forgings and extrusions are the most economical methods to produce integral type structure. In addition, detail requirements of large forgings and extrusions relative to physical properties, tolerances and refinements are presented. Statistical studies are presented to indicate the high potential use of large forgings and extrusions.
1952-01-01
Technical Paper
520220
R.M. Schaefer
THE development of the two-stage torque converter with automatic double clutch is presented here. The author covers particularly the substitution of casting for fabrication for several of the units in the transmission.
1952-01-01
Technical Paper
520225
Michael Field, Norman Zlatin
PROCEDURES for increasing the rates of production in production machining are discussed here. The methods fall into two categories: (1) the reduction in time of performing the handling, clamping, rapid traversing, and other machine functions necessary to bring the workpiece to the cutting tool; (2) the reduction in the time necessary actually to machine the metal. This second method is described in detail in the paper.
1952-01-01
Technical Paper
520243
D.J. Reese, F.B. Rote, G.A. Conger
THIS paper presents the results of investigations conducted at the University of Michigan under the sponsorship of the International Nickel Co., Inc., to determine the influence of carbon, silicon, and phosphorus contents and of section size on the mechanical properties of ductile cast iron. Carbon contents in the range of 2.75% to 4.10% had a minor controlling influence on the mechanical properties. Silicon, through its influence on the matrix structure and its solid solution hardening effect, exerts a major effect on the mechanical properties. Increasing the silicon content from 0.1% to 5.0% produces linear increases in tensile and yield stregnths and hardness and decreases in ductility. Increasing the phosphorus content from 0.04 to 0.40% increases hardness and decreases ductility. Ductile iron exhibits moderate section sensitivity, either in the as-cast or fully annealed conditions. With increasing section thickness the properties are all lowered slightly.
1952-01-01
Technical Paper
520083
JOHN J. CHYLE
1952-01-01
Magazine
1952-01-01
Technical Paper
520038
Robert L. Whann
1952-01-01
Technical Paper
520162
C. H. STEVENSON
1952-01-01
Technical Paper
520161
GORDON A. FAIRBAIRN
1952-01-01
Technical Paper
520201
Walter G. Bain
1951-12-01
Magazine
1951-12-01
Standard
AMS2505A
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED ".
1951-12-01
Standard
AMS3076A
Primarily for preservation, during extended periods of shipment and/or storage, of miscellaneous metal parts, tools, subassemblies, and equipment where the compound is readily accessible for removal and removal does not damage the parts.
1951-12-01
Standard
AMS3128B
This specification covers a pigment material in the form of a paste comprising aluminium powder mixed in a suitable binder.
1951-12-01
Standard
AMS6275
This specification has been declared 'NONCURRENT' by the Aerospace Materials Division, SAE, as of August, 1992. Alloy: 94B17 UNS Number: G94171
1951-12-01
Standard
AMS5378A
This specification covers a corrosion and heat resistant cobalt alloy in the form of investment castings.
1951-12-01
Standard
AMS5375A
This specification covers a corrosion and heat resistant cobalt alloy in the form of investment castings.
1951-12-01
Standard
AMS5350B
This specification covers a corrosion and moderate heat-resistant steel in the form of investment castings.
1951-12-01
Standard
AMS2671
This specification covers the engineering requirements for producing brazed joints using metallic copper as the brazing filler metal.
1951-12-01
Standard
AMS5565C
This specification covers a corrosion-resistant steel in the form of welded tubing. This tubing has been used typically for parts, such as fluid-conducting lines not subjected to high pressure, requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 degrees F (427 degrees C) during fabrication may impair corrosion resistance.
1951-12-01
Standard
AMS5360A
This specification covers a corrosion and heat resistant steel in the form of investment castings.
1951-12-01
Standard
AMS5112D
This specification covers a carbon steel in the form of wire supplied as coils, spools, or cut lengths. This wire has been used typically for springs subject to high stress or requiring good fatigue properties up to 200 °F (93 °C), but usage is not limited to such applications.
1951-12-01
Standard
AMS5560C
This specification covers a corrosion-resistant steel in the form of seamless tubing. This tubing has been used typically for parts, such as fluid-conducting lines, not subjected to high pressure and requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 °F (427 °C) during fabrication may impair corrosion resistance.
1951-12-01
Standard
AMS2510B
This specification covers the engineering requirements for finishng aircraft parts and assemblies with an engine gray enamel.
1951-12-01
Standard
AMS5651B
This specification covers a 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.
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