Invention Grant
- Patent Title: Aircraft engine nacelle inlet having access opening for electrical ice protection system
- Patent Title (中): 飞机发动机舱入口具有电冰保护系统的通道
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Application No.: US12233437Application Date: 2008-09-18
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Publication No.: US07681838B2Publication Date: 2010-03-23
- Inventor: Michael John Layland , Keith T. Brown
- Applicant: Michael John Layland , Keith T. Brown
- Applicant Address: US CA Chula Vista
- Assignee: Rohr, Inc.
- Current Assignee: Rohr, Inc.
- Current Assignee Address: US CA Chula Vista
- Agency: Womble Carlyle
- Main IPC: B64D15/12
- IPC: B64D15/12

Abstract:
An aircraft engine nacelle inlet is provided with an inlet cowling. The inlet cowling includes an inner lip, an outer lip, and a leading edge portion connecting the inner and outer lips. Heating elements are provided proximate the leading edge, either on an inside surface of the cowling or on an outside surface. An inner barrel portion and an outer barrel portion of the nacelle inlet define a space therebetween. Ice protection-related equipment such as controllers, cables, switches, connectors, and the like, may reside in this space. One or more access openings are formed in the outer barrel to enable an operator to gain access to this equipment. The inlet cowling attaches to the inner and outer barrels with its outer lip extending sufficiently far in the aft direction to cover the access opening. When the cowling is removed, the access opening is uncovered, thereby permitting access to the equipment.
Public/Granted literature
- US20090008509A1 AIRCRAFT ENGINE NACELLE INLET HAVING ACCESS OPENING FOR ELECTRICAL ICE PROTECTION SYSTEM Public/Granted day:2009-01-08
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