초록 ▼

To achieve the required optional conformability and navigability of the hovering motion of the hovering body in a free liquid environment, the hovering body is equipped with a suitable created mechanism for optional control of direction and/or the position of the hovering motion in the form of the b

To achieve the required optional conformability and navigability of the hovering motion of the hovering body in a free liquid environment, the hovering body is equipped with a suitable created mechanism for optional control of direction and/or the position of the hovering motion in the form of the basic jacket suitably equipped with at least one slot jet where the basic jacket is suitably connected to the elongated jacket mechanism for the optional stabilization of the direction and/or the position of the hovering motion suitably equipped with at least one uplift component.

대표청구항 ▼

1. A hovering body, especially a helicopter, comprising an autonomous drive to set the hovering body in hovering motion in a free fluid environment, the body having at least one mechanism for optional control of at least one of a directional motion and a position in free space of the hovering body,

1. A hovering body, especially a helicopter, comprising an autonomous drive to set the hovering body in hovering motion in a free fluid environment, the body having at least one mechanism for optional control of at least one of a directional motion and a position in free space of the hovering body, and the at least one mechanism comprising an elongated basic jacket, which in a direction of its longitudinal axis includes at least one slot jet for controlled ejection of a fluid from an internal environment of the basic jacket into the free fluid environment, the at least one slot jet comprises a cover on its outer side, the cover includes one side connected with the basic jacket and includes another side in the area of its outlet edge set at a distance from the basic jacket, respectively under the cover of the at least one slot jet there is at least one vent passing through the basic jacket, the cover is in the area of the at least one vent set at a distance from the basic jacket for creating outside the at least one vent a turbulizing area which is with the free fluid environment connected by means of an outlet slot between the outlet edge of the cover and the basic jacket, and the aggregate surface of the cross section of the at least one vent under the cover is greater than the surface of the outlet cross section between the outlet edge of the cover and the outer surface of the basic jacket, wherein the basic jacket has a mechanism connected thereto for optional stabilization of at least one of the directional motion and the position in free space of the hovering body, the stabilizing mechanism comprising an elongated jacket closed cover profile where the elongated jacket having connected thereto at least one uplift component, the at least one uplift component having at least one of a convex and a concave surface, wherein the uplift component is configured to produce a force on the elongated jacket when acted upon by a second fluid within the free fluid environment, the uplifting member also having a boarder attack, the boarder attack including a surface area of contact between the uplift component and an external surface of the elongated jacket where the uplifting member mounts to the external surface of the cover profile of the elongated jacket, the surface area includes a continuous curve of inflection points of contact of the uplift component with the outer surface of the elongated jacket, in which in the unrolled shape of the at least one uplift component into a main horizontal plane of symmetry of the basic jacket the ratio of the longitudinal dimension of the boarder attack to a longitudinal dimension of the end place is greater than one, and the mean curve of the traverse profiles, projected on the plane normal to the main horizontal plane of symmetry of the basic jacket makes an arc the angle of whose tangent at the level of the boarder attack is different from the angle of the tangent at the level of the end place of the uplift component.2. The hovering body according to claim 1, wherein the basic jacket together with the elongated jacket form an integral unit.3. The hovering body according to claim 1, wherein the at least one uplift component is by its end place arranged in a distance from the external surface of the elongated jacket.4. The hovering body according to claim 1, wherein the at least one uplift component is equipped with a multi-directional jet connected with the inner space of the basic jacket for the controlled ejection of the fluid from the internal environment of the basic jacket into a free fluid environment.5. The hovering body according to claim 1, wherein the at least one uplift component is by its end place arranged in contact with the external surface of the elongated jacket which is at a distance from the position of contact of the boarder attack of the respective at least one uplift component.6. The hovering body according to claim 2, wherein the at least one uplift component is equipped with a multi-directional jet connected with the inner space of the basic jacket for the controlled ejection of the fluid from the internal environment of the basic jacket into a free fluid environment.7. The hovering body according to claim 3, wherein the at least one uplift component is equipped with a multi-directional jet connected with the inner space of the basic jacket for the controlled ejection of the fluid from the internal environment of the basic jacket into a free fluid environment.8. The hovering body according to claim 5, wherein the at least one uplift component is equipped with a multi-directional jet connected with the inner space of the basic jacket for the controlled ejection of the fluid from the internal environment of the basic jacket into a free fluid environment.9. A hovering arrangement comprising:a body; an autonomous drive coupled to the body and configured to hover the body in a free fluid environment; at least one control mechanism coupled to the body and configured to control at least one of a directional motion and a position in free space of the body, the control mechanism including a basic jacket having an inner space and an external surface, the external surface of the jacket being provided with at least one slot jet to control an ejection of a fluid from the inner space of the jacket to the free fluid environment, the slot jet including a cover and including at least one vent extending from the external surface of the basic jacket to the inner space of the basic jacket, the vent having a cross section, the cover having first and second sides, the first side being connected to the external surface of the basic jacket, the second side being arranged in an area of the vent and separated from the vent to form an outlet slot having a cross section smaller than the cross section of the vent; and a stabilization mechanism coupled to the basic jacket of the control mechanism, the stabilization mechanism including an elongated basic jacket having an inner space and an external surface, the external surface of the elongated jacket being provided with at least one uplift component, the uplift component including a boarder attack, a proximal end, and a distal end, the boarder attack being formed at the proximal end of the uplift component, the boarder attack having a continuous curve of inflection points of contact between the uplift component and the external surface of the elongated jacket, and being configured to couple the uplift component to the external surface of the elongated jacket, wherein the uplift component is configured to produce a force on the elongated jacket when acted upon by a second fluid of the free fluid environment, the force having at least a normal vector with respect to a longitudinal axis of the elongated jacket, wherein the ejection of the fluid from the inner space of the basic jacket to the free fluid environment forms an area of turbulent flow in the free fluid environment adjacent to the outlet slot of the slot jet. 10. The hovering arrangement according to claim 9, wherein the uplift component includes at least one of a concave surface and a convex surface between the distal and the proximal ends.11. The hovering arrangement according to claim 9, wherein the basic jacket and the elongated jacket form an integral unit.12. The hovering arrangement according to claim 9, further comprising a first dimension measuring a linear distance from the boarder attack to the distal end of the uplift component and a second dimension measuring a linear distance along the contact surface of the boarder attack, wherein a ratio between the first and second dimensions is greater than one.13. The hovering arrangement according to claim 9, wherein a mean curve of a normal component relevant to a main horizontal plane of the elongated jacket forms an arc, the arc having a plurality of angles, the angles including a first tangent angle at the boarder attack and a second tangent angle at the distal end, wherein the first tangent angle differs from the second tangent angle.14. The hovering arrangement according to claim 9, wherein the at least one slot jet includes at least one multidirectional jet interconnected with the inner cavity of the basic jacket to control the ejection of the fluid from the inner space of the basic jacket to the free fluid environment, the multidirectional jet being respectively mounted to the distal end of the uplift component.