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Electric Thrust Reverser Actuation Systems
Technical Paper
2002-01-2950
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
All classes of airplane actuation systems have unique system level characteristics. This paper discusses key systems aspects of electric T/R actuation such as safety, power, controls, and maintainability, from an large airplane perspective, principally by comparing electric T/R actuation systems to equivalent hydraulic and pneumatic actuation. Enabling technology with which to implement system level requirements are discussed. The system issues are presented for a typical large airplane cascade T/R.
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