Invention Grant
US6129309A Aircraft engine apparatus with reduced inlet vortex 失效
具有减少入口涡流的飞机发动机装置

Aircraft engine apparatus with reduced inlet vortex
Abstract:
An aircraft engine apparatus with a reduced inlet vortex is provided which utilizes a vortex disruption system that periodically discharges pulses of engine bleed fluid through at least one outlet port opening through the inlet of the engine nacelle to disrupt the engine inlet vortex. The vortex disruption system thereby prevents ingestion of foreign matter into the engine inlet without sacrificing engine power, efficiency, or aircraft cruise performance.
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