Invention Grant
- Patent Title: Wing assembly with slats and aircraft
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Application No.: US16896331Application Date: 2020-06-09
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Publication No.: US11591068B2Publication Date: 2023-02-28
- Inventor: Stephen Colavincenzo , Robby Lapointe , Mohammad Tabesh
- Applicant: BOMBARDIER INC.
- Applicant Address: CA Dorval
- Assignee: BOMBARDIER INC.
- Current Assignee: BOMBARDIER INC.
- Current Assignee Address: CA Dorval
- Agency: BCF LLP
- Main IPC: B64C9/26
- IPC: B64C9/26 ; B64C7/00

Abstract:
A wing assembly includes a swept wing body, a leading edge of the wing body extending outward and rearward from a wing root to a wing edge; a first slat selectively movably connected to the wing body; and a second slat selectively movably connected to the wing body, the second slat being disposed outboard of the first slat, a flexible sealing member disposed and connected between the first slat and the second slat; at least a portion of the first slat, at least a portion of the second slat, and at least a portion of the flexible sealing member defining a slat gap therebetween, at least a majority of the slat gap being substantially parallel to a predetermined local airflow direction. An aircraft is also disclosed which includes a fuselage; and two oppositely disposed wing assemblies connected to the fuselage.
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