Rotorcraft having at least one undercarriage with at least one inclined wheel, and a method

1. A rotorcraft having an airframe having a front and a rear, the airframe carrying at least one rotor that contributes to providing the rotorcraft with lift and/or propulsion, the rotorcraft having at least one undercarriage towards the front of the airframe,

wherein the at least one undercarriage comprises at least one inclined wheel undercarriage, the inclined wheel undercarriage having an undercarriage leg carrying at least one axle, the at least one axle carrying at least two wheels,

the undercarriage leg having a center of gravity that is located at a location when the at least two wheels touch the ground during a landing,

a vertical plane passing through the location and orthogonal to a pitching axis of the rotorcraft when the rotorcraft is not turning on the ground,

the at least two wheels not being in contact with any other wheel, the at least two wheels presenting non-zero camber when the at least two wheels touch the ground and independently of forces exerted by the airframe on the inclined wheel undercarriage, the at least two wheels having a negative camber and being arranged transversely on either side of the undercarriage leg and wherein for each wheel a first distance lies orthogonally between a top of the wheel and the vertical plane and a second distance lies between the vertical plane and a surface of the wheel in contact with the ground, the second distance being greater than the first distance.

2. The rotorcraft according to claim 1 ,

wherein each of the at least two wheels rotates in a rolling plane, and the rolling plane presents an angle of inclination lying in the range 65 degrees to 85 degrees relative to the ground when each of the at least two wheels touches the ground and independently of forces exerted by the airframe on the inclined wheel undercarriage.

3. The rotorcraft according to claim 1 ,

wherein, for a first length lying transversely between two respective tops of the at least two wheels, and for a second length lying between two respective surfaces of the at least two wheels in contact with the ground, the second length is different from the first length, the first length and the second length being non-zero.

4. The rotorcraft according to claim 3 ,

wherein the second length is greater than the first length.

5. The rotorcraft according to claim 1 ,

wherein each of the at least two wheels has an inflated tire.

6. The rotorcraft according to claim 1 ,

wherein the at least one undercarriage comprises a plurality of undercarriages, at least one of the plurality of undercarriages including at least one inclined wheel undercarriage.

7. A rotorcraft comprising:

an airframe having a front and a rear and carrying at least one rotor that contributes to providing the rotorcraft with lift and/or propulsion;

an undercarriage towards the front of the airframe and comprising at least one inclined wheel undercarriage,

the inclined wheel undercarriage having an undercarriage leg carrying at least one axle, the at least one axle carrying at least two wheels, the undercarriage leg having a center of gravity that is located at a location when the at least two wheels touch the ground during a landing,

a vertical plane passing through the location and orthogonal to a pitching axis of the rotorcraft when the rotorcraft is not turning on the ground,

the at least two wheels not being in contact with any other wheel, the two wheels presenting non-zero camber when the at least two wheels touch the ground and independently of forces exerted by the airframe on the inclined wheel undercarriage, the at least two wheels angled inwardly from top to bottom of the wheel, the at least two wheels comprising a first wheel and a second wheel, the first wheel is arranged on a first side of the undercarriage leg and the second wheel is arranged transverse to the first wheel on a second side of the undercarriage leg such that for each wheel a first distance lies orthogonally between the top of the wheel and the vertical plane and a second distance lies between the vertical plane and the bottom of the wheel in contact with the ground, the second distance being greater than the first distance.

8. The rotorcraft according to claim 7 , wherein each of the at least two wheels rotates in a rolling plane, and the rolling plane presents an angle of inclination lying in the range 65 degrees to 85 degrees relative to the ground when each of the at least two wheels touches the ground and independently of forces exerted by the airframe on the inclined wheel undercarriage.

9. The rotorcraft according to claim 7 , wherein, for a first length lying transversely between two respective tops of the at least two wheels, and for a second length lying between two respective surfaces of the at least two wheels in contact with the ground, the second length is different from the first length, the first length and the second length being non-zero.

10. The rotorcraft according to claim 9 , wherein the second length is greater than the first length.

11. The rotorcraft according to claim 7 , wherein each of the at least two wheels has an inflated tire.

12. The rotorcraft according to claim 7 , wherein the at least one undercarriage comprises a plurality of undercarriages, with each of the plurality of undercarriages including at least one inclined wheel undercarriage.

13. A rotorcraft comprising:

an airframe having a front and a rear;

a rotor supported by the airframe, the rotor contributing to providing the rotorcraft with lift and/or propulsion;

an inclined wheel undercarriage supported by the airframe and disposed towards the front of the airframe, the inclined wheel undercarriage having an undercarriage leg and at least two wheels connected transversely to the undercarriage leg on either side of the undercarriage leg, the undercarriage leg having a center of gravity located at a location when the at least two wheels touch the ground during a landing,

a vertical plane passing through the location and orthogonal to a pitching axis of the rotorcraft when the rotorcraft is not turning on the ground,

the at least two wheels negatively cambered and having a top and a surface in contact with the ground, the at least two wheels not being in contact with each other, wherein for each wheel a first distance lies orthogonally between the top of the wheel and the vertical plane and a second distance lies between the vertical plane and a mid-point of the surface of the wheel in contact with the ground, the second distance being greater than the first distance.

14. The rotorcraft according to claim 13 , wherein each of the at least two wheels rotates in a rolling plane, and the rolling plane presents an angle of inclination lying in the range 65 degrees to 85 degrees relative to the ground when each of the at least two wheels touches the ground and independently of forces exerted by the airframe on the inclined wheel undercarriage.

15. The rotorcraft according to claim 13 , wherein, for a first length lying transversely between two respective tops of the at least two wheels, and for a second length lying between two respective surfaces of the at least two wheels in contact with the ground, the second length is different from the first length, the first length and the second length being non-zero.

16. The rotorcraft according to claim 15 , wherein the second length is greater than the first length.

17. The rotorcraft according to claim 13 , wherein each of the at least two wheels has an inflated tire.

18. The rotorcraft according to claim 1 , wherein the at least one undercarriage comprises a plurality of undercarriages, with each of the plurality of undercarriages including at least one inclined wheel undercarriage.