Packaging the VSCF System for an Aircraft Engine Environment

811088

10/01/1981

Event
Aerospace Congress and Exposition
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/811088
Pages
12
Citation
Pollard, D., and Krajci, G., "Packaging the VSCF System for an Aircraft Engine Environment," SAE Technical Paper 811088, 1981, https://doi.org/10.4271/811088.
Additional Details
Publisher
Published
Oct 1, 1981
Product Code
811088
Content Type
Technical Paper
Language
English