Overpressure door for aircraft
An aircraft, overpressure technology, applied in the direction of affecting the air flow flowing through the surface of the aircraft, aircraft accessories, aircraft parts, etc., can solve the problems of external flow obstruction, achieve the effect of reducing weight, optimizing structural size, and improving aerodynamic efficiency
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[0036] The present invention involves such as figure 1 and 2 An axial overpressure door 1 for an aircraft is shown schematically. This overpressure door 1 comprises a hatch 2 comprising an inner surface 2A and an outer surface 2B and is pivotable about an axis of rotation 4 via a standard hinge 5 relative to a compartment 6, only a part 7 of the outer wall of the compartment 6 being Shows. The hatch cover 2 can be in the closed position (in figure 2 indicated in ) and open position (in figure 1 indicated in ) to pivot between. Since said overpressure door 1 is of the axial type, the axis of rotation 4 is aligned (within limits) with the external flow generated by the relative movement of the aircraft in the air during flight. The external stream is in figure 1 Indicated by arrow E. Thus, the directions of the flow E and the axis of rotation 4 are substantially parallel.
[0037] This overpressure door 1 is thus mounted on the cabin 6 of the aircraft or of the aircr...
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