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Title:
WING ROOT HIGH-LIFT SYSTEM WITH MOBILE FUSELAGE WING
Document Type and Number:
WIPO Patent Application WO/2019/164385
Kind Code:
A8
Abstract:
Wing root high-lift system with mobile fuselage wing, installed on airplanes at the root of the wings. The invention serves to increase lift and optimize load distribution of the airplane during all flight phases. It consists of two wing root separation surfaces (3) that prevent air flowing from the fuselage to the wings in order to increase lift at the wing root, two fuselage partitions (5) which complement the work of said wing root separation surfaces, a new mobile fuselage wing (6) which serves to provide additional lift and, at the same time, serves to control and optimize the load distribution of the airplane during all flight phases in order to improve the performance of the airplane and save substantial amounts of fuel.

Inventors:
MAHFAD HICHAM (MA)
Application Number:
PCT/MA2019/000001
Publication Date:
February 20, 2020
Filing Date:
January 08, 2019
Export Citation:
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Assignee:
MAHFAD HICHAM (MA)
International Classes:
B64C3/00; B64C5/08; B64C5/10; B64C23/00; B64C39/08
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