초록 ▼

An aerodynamic body that can be adjusted relative to a main wing of an aircraft by an adjusting device is provided. A gap between the aerodynamic body and another aerodynamic body or a component of the fuselage or the main wing is formed on one lateral end and said and the gap is variable due to the

An aerodynamic body that can be adjusted relative to a main wing of an aircraft by an adjusting device is provided. A gap between the aerodynamic body and another aerodynamic body or a component of the fuselage or the main wing is formed on one lateral end and said and the gap is variable due to the adjustability of the aerodynamic body. The body features a gap bridge-over device with a shell part that extends along the gap and overlaps the outer shell of the aerodynamic body in the wingspread direction on the front side thereof so that the shell part can be telescopically moved relative to this aerodynamic body in the wingspread direction. An airfoil for an aircraft with a main wing and a plurality of aerodynamic bodies that are arranged adjacent to one another transverse to the chord direction is also provided.

대표청구항 ▼

1. An airfoil for an aircraft including at least one aerodynamic body that can be adjusted relative to a main wing of the aircraft by means of an adjusting device, wherein a gap between the at least one aerodynamic body and another aerodynamic body or a component of the fuselage or the main wing is

1. An airfoil for an aircraft including at least one aerodynamic body that can be adjusted relative to a main wing of the aircraft by means of an adjusting device, wherein a gap between the at least one aerodynamic body and another aerodynamic body or a component of the fuselage or the main wing is formed on one lateral end and said gap is variable due to the adjustability of the at least one aerodynamic body, featuring a gap bridge-over device with a shell part that extends along the gap and overlaps an outer shell of the at least one aerodynamic body in a wingspread direction on the front side thereof in such a way that the shell part can be telescopically moved relative to the at least one aerodynamic body in the wingspread direction wherein: the gap bridge-over device features a coupling rib that is connected to the shell part, the coupling rib having a first side opposite a second side, and a first coupling device for coupling the first side of the coupling rib to a structural component of the at least one aerodynamic body and a second coupling device, andthe first coupling device features at least one first connecting part that extends transverse to a chord direction and at least one second connecting part that extends transverse to a chord direction, the at least one first connecting part spaced apart from the at least one second connecting part in the chord direction,said at least one first connecting part is coupled to the first side of the coupling rib by means of an articulated connection that is constrained to extend substantially along a longitudinal direction of the at least one first connecting part and the at least one first connecting part is extendable along the longitudinal direction of the at least one first connecting part in order to displace the shell part in the wingspread direction,said at least one second connecting part is coupled to the first side of the coupling rib by means of an articulated connection that is constrained to extend substantially along a longitudinal direction of the at least one second connecting part and the at least one second connecting part is extendable along the longitudinal direction of the at least one second connecting part in order to displace the shell part in the wingspread direction,said at least one first connecting part is formed as a rod which is guided for telescopic linear movement in the longitudinal direction of the at least one first connecting part and in the wingspread direction on the at least one aerodynamic body,said at least one second connecting is formed as a rod which is guided for telescopic linear movement in the longitudinal direction of the at least one second connecting part and in the wingspread direction on the at least one aerodynamic body, andthe second coupling device includes at least two connecting rods that are arranged spaced apart from one another in the chord direction, each of the at least two connecting rods including a first end and a second end, the first end of each of the at least two connecting rods including an articulation to couple the first end of each of the at least two connecting rods to the at least one aerodynamic body and the second end of each of the at least two connecting rods including an articulation to couple the second end of each of the at least two connecting rods to the second side of the coupling rib. 2. The airfoil according to claim 1, wherein the shell part is positioned outside a skin of the at least one aerodynamic body. 3. The airfoil according to claim 1, wherein the shell part is positioned inside a skin of the at least one aerodynamic body. 4. The airfoil according to claim 1, wherein a sealing device is arranged on the gap bridge-over device. 5. The airfoil according to claim 1, wherein the second coupling device features a pressing device between a supporting component of the at least one aerodynamic body and the coupling rib such that the pressing device presses the gap bridge-over device outward and away from an interior of the at least one aerodynamic body. 6. The airfoil according to claim 4, wherein the sealing device is arranged on a first side of the gap bridge-over device that lies opposite of a second side of the gap bridge-over device, and the second side of the gap bridge-over device overlaps an adjacent skin of the at least one aerodynamic body. 7. The airfoil according to claim 4, wherein the sealing device is, referred to the coupling rib, arranged on the shell part and on a side that is positioned near an overlapping region. 8. The airfoil according to claim 5, wherein the pressing device features a telescopic rod that is prestressed in the direction toward the outer side of the at least one aerodynamic body. 9. An airfoil for an aircraft with a main wing and a plurality of aerodynamic bodies that are arranged adjacent to one another transverse to a chord direction and can be adjusted relative to the main wing by means of an adjusting device, wherein a gap is formed between the facing ends of outer shells of the aerodynamic bodies and said gap is variable due to the adjustability of the aerodynamic bodies, featuring a gap bridge-over device that includes a coupling rib having a first side opposite a second side, a first coupling device and a second coupling device, the first coupling device including at least one first connecting part that extends transverse to a chord direction and at least one second connecting part that extends transverse to a chord direction, and the at least one first connecting part is coupled to the first side of the coupling rib by means of an articulated connection that is constrained to extend substantially along a longitudinal direction of the at least one first connecting part and the at least one first connecting part is extendable along the longitudinal direction of the at least one first connecting part, and the second coupling device is coupled to the second side of the coupling rib, the second coupling device including at least two connecting rods that are arranged spaced apart from one another in the chord direction, each of the at least two connecting rods including a first end and a second end, the first end of each of the at least two connecting rods including an articulation to couple the first end of each of the at least two connecting rods to one of the aerodynamic bodies and the second end of each of the at least two connecting rods including an articulation to couple the second end of each of the at least two connecting rods to the second side of the coupling rib,wherein the at least one first connecting part is formed as a rod which is guided for telescopic linear movement in the longitudinal direction of the at least one first connecting part and in a wingspread direction on one of the plurality of aerodynamic bodies. 10. The airfoil according to claim 9, wherein the gap bridge-over device features: a shell part that at least sectionally extends along a contour of the outer shells of the aerodynamic bodies on the gap,the coupling rib connected to the shell part,the first coupling device for coupling the coupling rib to a first aerodynamic body of the plurality of aerodynamic bodies in an articulated fashion, andthe second coupling device for coupling the coupling rib to a second aerodynamic body of the plurality of aerodynamic bodies positioned adjacent to first aerodynamic body in an articulated fashion. 11. An aircraft with an airfoil according to claim 9. 12. The airfoil according to claim 10, wherein the second coupling device features a pressing device between a supporting component of the second aerodynamic body and the coupling rib such that the pressing device presses the gap bridge-over device outward and away from an interior of the second aerodynamic body. 13. The airfoil according to claim 10, wherein: a gap bridge-over device with a coupling device is respectively arranged on the first aerodynamic body and the second aerodynamic body and can be telescopically moved thereon, andsaid coupling device features a pressing device between a supporting component of the second aerodynamic body and the coupling rib. 14. An airfoil for an aircraft with a main wing and an aerodynamic body with an aerodynamically active profile that can be adjusted relative to the main wing by means of an adjusting device and is arranged adjacent to a component of a fuselage or the main wing transverse to a chord direction, wherein a gap is formed between one end of an outer shell of the aerodynamic body and the component of the fuselage or the main wing and said gap is variable due to the adjustability of the aerodynamic body, featuring a gap bridge-over device that includes a coupling rib having a first side opposite a second side, a first coupling device and a second coupling device, the first coupling device including a first connecting part that extends transverse to the chord direction and the first connecting part is coupled to the first side of the coupling rib by means of an articulated connection that is constrained to extend substantially along the longitudinal direction of the first connecting part and is extendable along the longitudinal direction of the first connecting part, the second coupling device is coupled to the second side of the coupling rib, the second coupling device including at least two connecting rods that arc arranged spaced apart from one another in the chord direction, each of the at least two connecting rods including a first end and a second end, the first end of each of the at least two connecting rods including an articulation to couple the first end of each of the at least two connecting rods to the aerodynamic body and the second end of each of the at least two connecting rods including an articulation to couple the second end of each of the at least two connecting rods to the second side of the coupling rib,wherein the first connecting part .s formed as a rod which is guided on the aerodynamic body for telescopic linear movement along a longitudinal axis of the rod, the longitudinal axis extending in a wingspread direction. 15. The airfoil according to claim 14, wherein the gap bridge-over device features: a shell part that at least sectionally extends along a contour of the outer shell of the aerodynamic body on the gap, andthe coupling rib connected to the shell. 16. The airfoil according to claim 14, wherein: a gap bridge-over device with a coupling device is respectively arranged on the first aerodynamic body and the component and can be telescopically moved thereon, andsaid coupling device features a pressing device between a supporting component of the second aerodynamic body and the coupling rib. 17. The airfoil according to claim 15, wherein the first or second coupling device features a pressing device between a supporting component of the component or the aerodynamic body and the coupling rib such that the pressing device presses the gap bridge-over device outward and away from the interior of the second aerodynamic body or the component.