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Viewing 169981 to 170010 of 173232
1942-01-01
Standard
AMS4017
This specification covers an aluminum alloy in the form of sheet and plate.
1942-01-01
Standard
AMS4088
This specification covers an aluminum alloy in the form of seamless, drawn tubing.
1942-01-01
Standard
AMS2601A
This specification provides requirements and procedures for gas-pressure leak testing of parts.
1942-01-01
Technical Paper
420102
W. G. OVENS
RESULTS of a study of a Mitsubishi Kinsei engine taken from a crashed Japanese plane are presented in this paper. The engine was made available to the author by the Experimental Engineering Section of the Army Air Force Materiel Center, Wright Field, O. The following are among the conclusions drawn by Mr. Ovens: The engine “is undoubtedly a highly dependable, even though not highly developed, piece of equipment, probably produced under time and tooling limitations which we would consider nearly impossible.” The designers “did a very ingenious job of combining what they apparently believed to be the most desirable features of a number of foreign engines - proved features all - into a composite design that ‘has to work the first time,’ and probably did.”
1942-01-01
Technical Paper
420123
SIDNEY OLDBERG, THOMAS M. BALL
THE Junkers 211B engine follows the usual German practice of very large displacements and conservative mean effective pressures and rotative speeds. However, the relative light weight per unit of displacement results in a net weight per horsepower that is not far above its competitors. Fully automatic devices which control propeller speed, manifold pressure, mixture ratio, spark advance, and supercharger gear ratio follow the German policy of removing all possible distractions from the pilot. This is one of three large liquid-cooled engines known to be produced in quantity in Germany; it powers an impressive percentage of the Luftwaffe. While of external appearance and displacement that resemble the Daimler-Benz DB-601 engine, the fundamental construction, detail design practice, and metallurgy of the Junkers 211B are surprisingly different.
1942-01-01
Standard
AMS4140
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 materials which may have been widely used previously 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.
1942-01-01
Standard
AMS3226
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for hose, packings, bushings, grommets, and seals in contact with hot, petroleum-base lubricating oils and glycol-type coolants from -40 degrees to +100 degrees C (-40 degrees to +212 degrees F).
1941-12-01
Magazine
1941-11-01
Standard
AS54
No scope available.
1941-11-01
Standard
AMS7310
This specification covers piston rings fabricated from cast iron.
1941-11-01
Standard
AS41
No scope available.
1941-11-01
Standard
AMS6254A
No scope available.
1941-11-01
Standard
AMS6252A
No scope available.
1941-11-01
Standard
AMS6253A
No scope available.
1941-11-01
Standard
AMS6240A
ABSTRACT
1941-11-01
Standard
AMS6292A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
1941-11-01
Standard
AMS6290A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. These products have been used typically for carburized parts which require low minimum core hardness and allow a wide hardness range in sections 0.375 in. (9.50 mm) and under in nominal thickness, but usage is not limited to such applications. The core may or may not be machinable after hardening.
1941-11-01
Standard
AMS4380
ABSTRACT
1941-11-01
Standard
AMS4350A
This specification covers a magnesium alloy in the form of extruded bar rods, wire, tubing, and profiles. These products have been used typically for low-strength parts requiring rigidity and low density, but usage is not limited to such applications. Special care is necessary to prevent corrosion.
1941-11-01
Standard
AMS4424A
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of August, 1992. It is recommended, therefore, that this specification not be specified for new designs.
1941-11-01
Standard
AMS4422A
This specification covers a magnesium alloy in the form of sand castings.
1941-11-01
Standard
AMS4420A
This specification covers a magnesium alloy in the form of sand castings.
1941-11-01
Standard
AMS4210A
This specification covers an aluminum alloy in the form of sand castings.
1941-11-01
Standard
AMS4240
This specification covers an aluminum alloy in the form of sand castings.
1941-11-01
Standard
AMS4006
This specification covers an aluminum alloy in the form of sheet and plate.

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