Skid landing gear and an aircraft provided with such landing gear

1. A landing gear comprising a first longitudinal bearing skid and a second longitudinal bearing skid together with a first transverse crossbar and a second transverse crossbar each connected to the first and second skids in order to connect each longitudinal bearing skid to an airframe of an aircraft, wherein the landing gear includes at least one resilient fastener device together with at least one blocking means and at least one centering means per crossbar, the fastener device for the associated crossbar including connection means for connecting the associated crossbar to the airframe and slide means for allowing the associated crossbar to slide relative to the connection means while landing on sloping terrain, the blocking means being independent and acting to block the sliding of the associated crossbar relative to the connection means after landing on sloping terrain, the centering means acting in flight to position the associated crossbar in a predetermined position relative to the connection means, wherein the blocking means comprise a stationary portion suitable for being fastened to the airframe and a movable portion secured to the associated crossbar, the stationary portion and the movable portion co-operating by interfering shapes after a landing.

2. The landing gear according to claim 1 , including at least one lateral abutment arranged on at least one of the transverse crossbars to limit the movement of the crossbar relative to the connection means during a landing on sloping terrain.

3. The landing gear according to claim 1 , wherein at least one given crossbar comprises a central portion that is secured to a first portion fastened to the first skid and a second portion fastened to the second skid, the centering means comprising the central portion, the central portion presenting an arc of given radius (R) about a center of curvature (Co), the center of curvature (Co) being above the given crossbar when the landing gear is resting on horizontal ground.

4. The landing gear according to claim 1 , wherein the centering means comprise transverse return means and a lever secured to the associated crossbar, the transverse return means tending to move the lever in order to position the associated crossbar in the predetermined position.

5. The landing gear according to claim 1 , wherein the stationary portion includes catches and the movable portion includes teeth suitable for co-operating with the catches.

6. The landing gear according to claim 1 , wherein the connection means comprise a fastener structure suitable for being fastened to the airframe, the slide means comprise a stationary wheel and a movable wheel co-operating with the fastener structure to connect the associated crossbar to the airframe, the associated crossbar passing between the stationary wheel and the movable wheel.

7. The landing gear according to claim 6 , wherein the fastener structure supports a stationary axle for the stationary wheel and a movable axle for the movable wheel, wherein the movable axle slides in at least one slot extending in elevation in the fastener structure above the stationary wheel.

8. The landing gear according to claim 7 , wherein the slide means include elevation return means for returning the movable wheel and suitable for pressing the movable wheel against the associated crossbar.

9. An aircraft comprising an airframe and landing gear, the landing gear being provided with a first longitudinal bearing skid and a second longitudinal bearing skid, together with first and second transverse crossbars connecting together each of the first and second skids in order to connect each longitudinal bearing skid to the airframe, wherein the landing gear includes at least one resilient fastener device together with at least one blocking device and at least one centering means per crossbar, the fastener device for fastening the associated crossbar including connection means for connecting the associated crossbar to the airframe and slide means for allowing the associated crossbar to slide relative to the airframe during a landing on sloping terrain, the blocking device being independent to block sliding of the associated crossbar relative to the airframe following a landing on sloping terrain, the centering means acting in flight to position the associated crossbar in a predetermined position relative to the airframe, wherein the blocking device comprises a stationary portion suitable for being fastened to the airframe and a movable portion secured to the associated crossbar, the stationary portion and the movable portion co-operating by interfering shapes after a landing.

10. The aircraft according to claim 9 , including at least one lateral abutment arranged on at least one of the transverse crossbars to limit the movement of the crossbar relative to the connection means during a landing on sloping terrain.

11. The aircraft according to claim 9 , wherein at least one given crossbar comprises a central portion that is secured to a first portion fastened to the first skid and a second portion fastened to the second skid, the centering means comprising the central portion, the central portion presenting an arc of given radius (R) about a center of curvature (Co), the center of curvature (Co) being above the given crossbar when the landing gear is resting on horizontal ground.

12. The aircraft according to claim 9 , wherein the centering means comprise transverse return means and a lever secured to the associated crossbar, the transverse return means tending to move the lever in order to position the associated crossbar in the predetermined position.

13. The aircraft according to claim 9 , wherein the connection means comprise a fastener structure suitable for being fastened to the airframe, the slide means comprise a stationary wheel and a movable wheel co-operating with the fastener structure to connect the associated crossbar to the airframe, the associated crossbar passing between the stationary wheel and the movable wheel.

14. A landing gear comprising a first longitudinal bearing skid and a second longitudinal bearing skid together with a first transverse crossbar and a second transverse crossbar each connected to the first and second skids in order to connect each longitudinal bearing skid to an airframe of an aircraft, wherein the landing gear includes at least one resilient fastener device together with at least one blocking means and at least one centering means per crossbar, the fastener device for the associated crossbar including connection means for connecting the associated crossbar to the airframe and slide means for allowing the associated crossbar to slide relative to the connection means while landing on sloping terrain, the blocking means being independent and acting to block the sliding of the associated crossbar relative to the connection means after landing on sloping terrain, the centering means acting in flight to position the associated crossbar in a predetermined position relative to the connection mean; wherein at least one given crossbar comprises a central portion that is secured to a first portion fastened to the first skid and a second portion fastened to the second skid, the centering means comprising the central portion, the central portion presenting an arc of given radius (R) about a center of curvature (Co), the center of curvature (Co) being above the given crossbar when the landing gear is resting on horizontal ground.

15. The landing gear according to claim 14 , including at least one lateral abutment arranged on at least one of the transverse crossbars to limit the movement of the crossbar relative to the connection means during a landing on sloping terrain.

16. The landing gear according to claim 14 , wherein the centering means comprise transverse return means and a lever secured to the associated crossbar, the transverse return means tending to move the lever in order to position the associated crossbar in the predetermined position.

17. The landing gear according to claim 14 , wherein the blocking means comprise a stationary portion suitable for being fastened to the airframe and a movable portion secured to the associated crossbar, the stationary portion and the movable portion co-operating by interfering shapes after a landing, and wherein the stationary portion includes catches and the movable portion includes teeth suitable for co-operating with the catches.

18. The landing gear according to claim 14 , wherein the connection means comprise a fastener structure suitable for being fastened to the airframe, the slide means comprise a stationary wheel and a movable wheel co-operating with the fastener structure to connect the associated crossbar to the airframe, the associated crossbar passing between the stationary wheel and the movable wheel.

19. The landing gear according to claim 18 , wherein the fastener structure supports a stationary axle for the stationary wheel and a movable axle for the movable wheel, wherein the movable axle slides in at least one slot extending in elevation in the fastener structure above the stationary wheel.

20. The landing gear according to claim 19 , wherein the slide means include elevation return means for returning the movable wheel and suitable for pressing the movable wheel against the associated crossbar.