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Viewing 19231 to 19260 of 19611
Technical Paper
1942-01-01
T. P. Wright
Technical Paper
1942-01-01
Eugene E. Wilson
Technical Paper
1942-01-01
H. N. Cowan, J. B. Kendrick
Technical Paper
1942-01-01
DONALD U. KUDLICH
MANY of the differences between engineering and production units arise from the fact that the former are too far from the product which they have conceived to appreciate its deficiencies, and the latter are not qualified by experience to improve upon it. As a result, changes intended to correct a defect have bred others which, in turn, have necessitated additional modifications. By the assignment of a third group, an engineering liaison, which is familiar with design requirements to observe the assembly and test, and other production phases of aircraft engines, the correction of basic faults and the elimination of unnecessary changes in design or procedures, have been possible. Examples of typical troubles and other methods of correction are cited in this paper.
Standard
1942-01-01
This specification covers the procedure to be used for spraying metallic parts with aluminum and the properties of the coating.
Standard
1942-01-01
This specification provides requirements and procedures for air-pressure leak testing of parts.
Standard
1942-01-01
This specification provides requirements and procedures for air-pressure leak testing of parts.
Standard
1942-01-01
null, null
This specification covers leather tanned with chromium salts and retanned with vegetable tanning material.
Standard
1942-01-01
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September, 2002. Alloy: CNS UNS Number: S63005
Standard
1942-01-01
This specification covers a corrosion and heat resistant steel in the form of bars, forgings, and forging stock.
Standard
1942-01-01
This specification provides requirements and procedures for air-pressure leak testing of parts.
Standard
1942-01-01
This specification provides requirements and procedures for air-pressure leak testing of parts.
Standard
1942-01-01
This specification provides requirements and procedures for gas-pressure leak testing of parts.
Standard
1941-11-01
This specification covers a high-carbon steel in the form of bars.
Standard
1941-11-01
This specification covers a corrosion and heat-resistant steel in the form of welded tubing.
Standard
1941-11-01
This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing.
Standard
1941-11-01
No scope available.
Standard
1941-11-01
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard
1941-11-01
No scope available.
Standard
1941-11-01
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.
Standard
1941-11-01
This specification covers a low alloy steel in the form of wire supplied as coils, spools, and straight lengths.
Standard
1941-11-01
This specification covers piston rings fabricated from cast iron.
Standard
1941-11-01
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
Standard
1941-11-01
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
Standard
1941-11-01
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
Standard
1941-11-01
This specification covers a corrosion and heat resistant steel in the form of seamless tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication, and also for parts requiring oxidation resistance up to 1500 degrees F (816 degrees C) but useful at that temperature only when stresses are low; usage is not limited to such applications.
Standard
1941-11-01
This specification covers the requirements for electrodeposited cadmium on metal parts.
Viewing 19231 to 19260 of 19611

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