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2015-02-03
WIP Standard
AS5188B
No scope available.
2015-02-03
WIP Standard
J518/4
This document standardizes the design of connector blocks used for joining SAE J518-1/ISO 6162-1 (Code 61) flange heads with other SAE J518-1/ISO 6162-1 (Code 61) flange heads with straight, elbow, and tee geometries. The blocks specified in this document are designed to provide for very compact installations. As a result, the tap depths specified in this document do not conform to those specified in SAE J518-1/ISO 6162-1 to allow for a minimal bend radius in the elbow and tee configurations. This document specifies both inch and metric configurations
2015-02-03
WIP Standard
J1942/1
Effective August 28, 1991, the SAE replaced the USCG as the listing agency for Marine Hose Assemblies. The previous USCG list was discontinued as of December 31, 1992, and is being replaced by this SAE listing, J1942-1. All products appearing on the USCG list as of December 31, 1992, may be carried over to the SAE J1942-1 provided they meet the new test requirements listed in SAE J1942. If your products comply, you may retain your listings with no additional testing. (Please note that the USCG has the authority to request and inspect your test results at their discretion.) The following list consists of hose data provided as of May 2003, and is for convenience in determining acceptability of nonmetallic flexible hose assemblies intended for usage under 46 CFR 56.60-25(c). Where the maximum allowable working pressure (MAWP) or type of fitting is not specified, use the manufacturer's recommended MAWP or type of fitting.
2015-01-28
Standard
AMS2430T
This specification covers the requirements for automatic shot peening of surfaces of parts by impingement of media, including metallic, glass, or ceramic shot.
2015-01-26
Standard
AS7119B
This document has been declared "CANCELLED" as of January 2015 and has been superseded by PRI AC7119. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7119. Cancelled specifications are available from SAE. This Aerospace Standard (AS) establishes the requirements for suppliers of Electronics Printed Circuit Boards to be accredited by Nadcap. Nadcap accreditation is granted in accordance with SAE AS7003 after demonstrating compliance with the requirements herein. These requirements may be supplemented by additional requirements specified by Nadcap Electronics Task Group. Using the audit checklist (AC7119) will ensure that accredited Electronics Printed Circuit Boards suppliers meet all of the requirements in this standard and all applicable supplementary standards.
2015-01-26
Standard
AMS2419D
This specification covers the engineering requirements for electrodeposition of cadmium-titanium on metal parts and the properties of the deposit.
2015-01-22
Standard
AS1371A
This standard covers all-metal, self-locking, prevailing torque nuts made of corrosion resistant steel.
2015-01-22
Standard
AS17845A
SCOPE IS UNAVAILABLE.
2015-01-22
WIP Standard
AS4461C
This standard is applicable to manual soldering and machine soldering processes utilizing controlled soldering devices, for electrical connections for wiring and cabling used in aerospace vehicles. Description of a component or device herein is not to be construed as authorizing the use of the component or device.
2015-01-20
WIP Standard
ARP6402B
The purpose of this document is to provide certain basic considerations and design criteria for installation of LED landing, runway turnoff, and taxiing light systems for night operation. Criteria for recognition lights are also included.
2015-01-20
Standard
AMS7848D
This specification covers a tantalum alloy in the form of bars and rods up through 3.5 inches (88.9 mm), inclusive.
2015-01-15
Standard
ARP1833B
The purpose of this standard is to provide the missile hydraulic and pneumatic component designer with information learned, tested and substantiated in correction of problems and failures experienced with seals that are subject to the unique requirements of missile static storage and subsequent dynamic operational conditions.
2015-01-15
Standard
AMS4987E
This specification covers a titanium alloy in the form of forgings 4.00 inches (101.6 mm) and under in nominal cross-sectional thickness and of forging stock of any size.
2015-01-15
Standard
AMS4520L
This specification covers a copper alloy in the form of strip. This strip has been used typically for rolled, split bushings, but usage is not limited to such applications.
2015-01-14
Standard
AMS7849E
This specification covers tantalum in the form of sheet, strip, plate, and foil up through 0.1875 inch (4.75 mm), inclusive.
2015-01-14
Standard
AMS7912D
This specification covers an aluminum-beryllium alloy in the form of bars, rods, tubing, and shapes consolidated from powder by extrusion.
2015-01-14
Technical Paper
2015-26-0019
Werner Bick, Cagri Cevik, Christoph Steffens
Abstract In order to minimize the development and production costs in the automotive industry, despite steadily increasing variety of models and applications offered by the OEMs, the pressure on standardization of components and production processes is increasing continuously. As a direct consequence, modular engine families are already established with high degrees of common parts and kits as well as standardized interfaces for all vehicle platforms by most manufacturers these days. At the same time, the world adopted and announced massive legal demands concerning the reduction of CO2 emissions for the entire vehicle fleet. In addition to the optimization of the combustion process, the exhaust gas aftertreatment and thermal management, the use of improved and more resilient materials for higher reduction of mechanical friction leads to a significant amount of the realized lowering in fuel consumption respective CO2 emissions.
2015-01-14
Technical Paper
2015-26-0029
Suresh Kumar Kandreegula, Umashanker Gupta, Swapnil Vyas
Abstract Proper sealing of an engine is very important parameter in an engine design. Even small amount of gas leakage from the engine can affect the overall performance of the engine during operation. There are two important factors in enhancing the efficiency of the sealing of the gasket are right tightening torque of bolts & gasket design. In this study, both the distribution of the contact pressure on the gasket, and the stresses of the cylinder head at different loading conditions, such as cold assembly, hot assembly, cold start, and hot firing, is simulated by commercial tool, based on the finite element method (FEM). The results shows that the efficiency of the sealing of the cylinder head gasket depends on the tightening torque of the hold-down bolts, without taking into consideration any thermal load resulting from the temperature distribution in the cylinder head.
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