This paper addresses the packaging considerations and techniques used in the design of a fully integrated VSCF package which is mounted on an engine accessory gearbox. Special design considerations such as vibration, altitude, and temperature in the gearbox area are discussed. A comparison and description of various methods of cooling, such as cold plate, immersion, and spray within a self contained cooling/lubrication system is also presented. The paper describes the integration of microprocessor modules, high power semiconductor arrays, and a high-speed generator, to form a compact, low weight VSCF system.
Packaging the VSCF System for an Aircraft Engine Environment
Sae Technical Papers
Aerospace Congress and Exposition ; 1981
1981-10-01
Aufsatz (Konferenz)
Englisch
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