Invention Grant
- Patent Title: Aircraft engine apparatus with reduced inlet vortex
- Patent Title (中): 具有减少入口涡流的飞机发动机装置
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Application No.: US122004Application Date: 1998-07-24
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Publication No.: US6129309APublication Date: 2000-10-10
- Inventor: David M. Smith , John Dorris, III
- Applicant: David M. Smith , John Dorris, III
- Applicant Address: MO St. Louis County
- Assignee: McDonnell Douglas Corporation
- Current Assignee: McDonnell Douglas Corporation
- Current Assignee Address: MO St. Louis County
- Main IPC: B64D33/02
- IPC: B64D33/02 ; F02C7/05 ; B64B1/24 ; F02G3/00
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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