Invention Grant
- Patent Title: Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode
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Application No.: US15801105Application Date: 2017-11-01
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Publication No.: US11053888B2Publication Date: 2021-07-06
- Inventor: John C. Vassberg , Mark DeHaan , Dino Roman
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agent Felix L. Fischer
- Main IPC: F02K1/66
- IPC: F02K1/66 ; F04D29/52 ; F04D29/36 ; F02K1/46 ; F02K1/48 ; F02C3/04 ; F01D25/24

Abstract:
An ultrashort nacelle configuration employs a fan cowl having an exit plane and a serrated trailing edge. A variable pitch fan is housed within the fan cowl. The variable pitch fan has a reverse thrust position inducing a reverse flow through the exit plane and into the fan cowl. The serrated trailing edge forms a plurality of vortex generators configured to induce vortices in the reverse flow.
Public/Granted literature
- US20190128214A1 FAN COWL WITH A SERRATED TRAILING EDGE PROVIDING ATTACHED FLOW IN REVERSE THRUST MODE Public/Granted day:2019-05-02
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