High-lift device
OwnerOlivier LAMAILLEinventor
Life of this patent
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Abstract
The present invention relates to the field of aeronautics and more particularly to a high-lift device and an aerodyne comprising such a high-lift device.
Claims16
Device located at an aerodyne jet engine or engine [FIG. 7] [FIG. 10], said device being capable of generating an airflow from inlet ports [FIG. 2] (2), and or a jet engine or an engine, said airflow being directed by channels and controlled by a turbine (3) located in a wing profile, said device comprising a chamber which surrounds the jet engine of an airplane (FIG. 8:
- 15), mobile winglets upstream from the thrust reversers and winglets downstream [FIG. 9], (FIG. 10:
- 16), said winglets being designed such that movement thereof makes it possible to direct the airflow generated by the engine or jet engine from the chamber (15) to a high-lift device located at the wings.
Aerodyne comprising a high-lift device according to any one of the preceding claims.
Airplane security device (ASD), comprising at least three parts, including a fuselage equipped with two ailerons, stabilisers, and four motors (theta device) (FIG. 44).
Aileron of symmetrical convex shape capable of being integrated in the body of a wing of an airplane or a glider [FIG. 21]:
- (24) FIG. 19:
- according to FIG. 22;
- or FIG. 23].
Airplane cradle whereon the structure of the wings is mounted, characterised by a biconvex shape of the hollow part located at the root of the wings accommodating the ailerons of a rescue module.
Stabiliser device (FIG. 47 or FIG. 48) located at the rear end of the fuselage characterised by the conical shape thereof and the shaft thereof allowing it to accommodate mobile stabilisers having the same base, comprising two symmetrically opposite ailerons equipped with flight control surfaces, off-centred with respect to the centre of the cone, thus positioned at the fin, which enables it to be integrated in the vertical tail, to decrease the drag.
Device [FIG. 35] [FIG. 40] allowing the passage of a shaft which connects an arm and fan assembly to a fuselage structure [FIG. 37], said arms being capable of pivoting on a shaft (x) via electric motors not shown, the device optionally comprising or comprising:
- four fans housed inside a compartment, each fan being composed of a hollow arm of cylindrical shape, assembled perpendicularly to the arm,
- a cylindrical base comprising on the flank at least one hole enabling the assembly of the constituent elements of this device [FIG. 39].
Aerodyne comprising any one of the devices claimed above or a combination of these devices.
Dependencies are inferred from the claim text.