Adjustment possible atmospheric pressure wing for flight device of fixed wing

摘要

(57) Abstract The module where it can give impact with the compressed air, the box wing spar (1) is arranged in the front and the rear, it possesses the plate (7) where the aforementioned module, transmits the airtight apex skin and the airtight lower part skin and hydraulic power and at the same time is arranged between module. Each plate (7) has the console on each side. The aforementioned console has extended according to the total length of the wing external form, with airtightness just a little from one which has extensibility two flexible tubes (9), are inserted between two those kind of consoles. When the tube receives pressure, the plate (9), each other is made to move essentially parallel, the wing which has the desirable chamber has. The aerodynamics external form is demarcated by the strong seat (10), the aforementioned seat (10), is locked the seat to joint connecting method the apex skin and by the plate (11) which has the lower part skin (5) and the hinge (14). The onhurou edge of the wing (3), just a little has the tube (15 and 16) which has extensibility with airtightness, when it can add with appropriate method, the onhurou edge (3) designates the tube, as necessary form. The off floor edge (4) is opened.