Invention Grant
- Patent Title: Aircraft engine protection device
- Patent Title (中): 飞机发动机保护装置
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Application No.: US12840935Application Date: 2010-07-21
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Publication No.: US08756909B2Publication Date: 2014-06-24
- Inventor: Donna Avery
- Applicant: Donna Avery
- Applicant Address: US NJ Teaneck
- Assignee: The CTFOT Group LLC
- Current Assignee: The CTFOT Group LLC
- Current Assignee Address: US NJ Teaneck
- Agency: Leason Ellis LLP
- Main IPC: F02C7/05
- IPC: F02C7/05 ; F02C7/055

Abstract:
A jet engine intake guard includes an engine sleeve located within the nacelle of the engine; a primary deflection screen located at a front portion of the sleeve and having a first circular frame formed of a tubular fabric member and a plurality of fiber yarn strings disposed across the diameter of the primary frame and attached to one another in a tri-axel weave pattern. The guard also includes a secondary deflection screen located behind the primary deflection screen in the direction of air flow through the engine and having a second circular frame formed of a tubular fabric member and a plurality of fiber yarn strings disposed across the secondary frame and attached to one another in a tri-axel weave pattern. The guard further includes a capture basket located between the primary and secondary deflection screens. The capture basket has a first wall located toward the primary deflection screen, a center portion and a second wall located toward the secondary deflection screen. In a preferred embodiment the entire guard is made of woven carbon fiber.
Public/Granted literature
- US20110016845A1 AIRCRAFT ENGINE PROTECTION DEVICE Public/Granted day:2011-01-27
Information query
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