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The specifications contained in this SAE Standard pertain to high-tension ignition cable used in road vehicle engine ignition systems.
This specification covers a corrosion-resistant steel in the form of investment castings.
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
This specification covers a corrosion-resistant steel in the form of investment castings.
This specification covers a low-expansion iron-nickel-cobalt alloy in the form of wire.
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose.
This specification covers a low-alloy steel in the form of welding wire.
This specification covers a synthetic rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
This specification covers an aluminum-killed carbon steel in the form of sheet and strip.
This specification covers a titanium alloy in the form of forgings 3.000 inches (76.20 mm) and under in nominal cross-sectional thickness and of stock for forging of any size.
This specification covers a synthetic rubber in the form of a soft wall, smooth bore, collapsing-type hose.
This specification covers a synthetic rubber in the form of a nonrigid, smooth bore, noncollapsing-type hose.
This specification establishes the engineering requirements for producing chemical-film coatings on aluminum and aluminum alloys and the properties of such coatings.
This specification covers a corrosion and heat resistant nickel alloy in the form of investment castings.
This specification covers a corrosion and heat resistant iron alloy in the form of covered welding electrodes.
The electrical cranking system components, which include the battery, cables, and cranking motor, must be carefully selected to provide the necessary speed to start an engine under the most severe climatic conditions for which the system is intended. Engine cranking loads increase with cold temperatures, therefore, the initial selection of these components needs to consider low-temperature engine torque requirements. To insure an adequate electrical cranking system is obtained, it is important that proper test procedures are used for obtaining the cranking load requirements of the engine.
This report is intended to provide the information to estimate the accessory load of a typical heavy truck or bus. The components covered include: air compressors, alternators, refrigerant compressors, engine cooling fans and power steering pumps. The values show an estimate of the average power requirements and duty cycles for these accessories. This report does not address loads required for engine operation. Required systems include those needed for engine performance such as fuel pumps and electronic control modules (ECM).
This specification covers a stable, nonvolatile, petroleum-base compound in a form suitable for application by dipping at 170 to 210 °F (77 to 99 °C).
This SAE Recommended Practice is intended to apply to lamps, batteries, heaters, radios, and similar equipment for operation with mobile or automotive diesel engines. Twenty-four V systems have long been used for heavy-duty services because 24 V permit operating 12 V systems in series-parallel. Thirty-two V systems have been used for marine, railroad-car lighting, and other uses. Generators, storage batteries, starting motors, lighting, and auxiliary electrical equipment shall be for nominal system ratings of 12, 24, or 32 V as determined by the power requirements of the application. It is recommended that no intermediate voltages be considered. The combination of a 24 V starting motor and two 12 V batteries connected in series for cranking is considered practical where it can be adapted to the installation. The batteries are reconnected in parallel for charging from a 12 V generator/alternator and for operating lights and other auxiliary equipment, or charged separately and used
This SAE Aerospace Information Report (AIR) outlines a recommended procedure for evaluation of the vibration environment to which the gas turbine engine powerplant is subjected in the helicopter installation. This analysis of engine vibration is normally demonstrated on a one-time basis upon initial certification, or after a major modification, of an engine/helicopter configuration. This AIR deals with linear vibration as measured on the basic case structure of the engine and not, for example, torsional vibration in drive shafting or vibration of a component within the engine such as a compressor or turbine airfoil. In summary, this AIR discusses the engine manufacturer’s "Installation Test Code" aspects of engine vibration and proposes an appropriate measurement method.
This specification covers a solvent-dispersed, corrosion-inhibiting compound packaged in aerosol cans.
This SAE Recommended Practice applies to mobile, construction type, crane and cable excavator hand and foot controls. It should not be construed to limit the use of, or to apply to combination controls, automatic controls, or any other special operating control requirements.
The purpose of this SAE Standard is to provide a standardized test procedure for generating engine performance maps. An engine performance map is a listing of engine fuel flow rates versus torque or power obtained at specific engine speeds and loads. Engine performance maps as specified by this code can be used in fuel economy simulation programs. This document is applicable to both four-stroke spark ignition (SI) and compression ignition (CI) engines, naturally aspirated and pressure charged, with or without charge air cooling.
This specification establishes the performance, qualification, acceptance limits, and identification for aeronautical engine high tension spark igniters.
SAE data file format for exchanging controlled periodic overload data. The object of this SAE Standard is to provide a simple, common methodology for exchanging the data from periodic overload fatigue tests. These tests consist of a single large fatigue cycle followed by a larger number of smaller cycles. The overloads are fully reversed fatigue cycles while the smaller cycles share a common mean and amplitude.
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