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An aircraft landing gear includes a leg having a strut receiving a telescopic rod to slide on a sliding axis, the strut being hinged to an aircraft structure and being capable of pivoting about a pivot axis that is highly offset from the sliding axis. The landing gear further includes a connection s

An aircraft landing gear includes a leg having a strut receiving a telescopic rod to slide on a sliding axis, the strut being hinged to an aircraft structure and being capable of pivoting about a pivot axis that is highly offset from the sliding axis. The landing gear further includes a connection structure essentially comprising two panels connecting two axially separate points of the strut to a common axis structure extending along the strut pivot axis. In the gear-down position, the panels are one above the other, the top panel being connected to the strut via a high attachment which is rigid in twisting, while the bottom panel is connected to the strut via a low attachment which tolerates twisting, thereby enabling the strut to warp to some extent when the aircraft is turning while taxiing.

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1. An aircraft landing gear comprising a leg ( 11 ) constituted by a strut ( 12 ) in which a telescopic shock-absorber rod ( 13 ) slides along a sliding axis (Z), the free end of the rod being hinged to a rocker beam ( 14 ) carrying a wheel set having multiple axles, said strut being hinged to a str

1. An aircraft landing gear comprising a leg ( 11 ) constituted by a strut ( 12 ) in which a telescopic shock-absorber rod ( 13 ) slides along a sliding axis (Z), the free end of the rod being hinged to a rocker beam ( 14 ) carrying a wheel set having multiple axles, said strut being hinged to a structure of the aircraft and being capable of being pivoted by an associated connection structure about a substantially horizontal axis (X) that is highly offset from the sliding axis (Z) of the telescopic rod ( 13 ) which is vertical in the gear-down position, wherein the connection structure ( 100 ) is essentially constituted by two panels ( 101 , 102 ) connecting two axially separated points of the strut ( 12 ) to a common axis structure ( 103 ) extending along the pivot axis (X) of said strut, in such a manner that in the gear-down position said panels are disposed one above the other, with a top panel ( 101 ) which is connected to the strut ( 12 ) via a high attachment ( 105 ) which is rigid in twisting, and with a bottom panel ( 102 ) which is connected to the strut ( 12 ) via a low attachment ( 106 ) which tolerates twisting, thereby allowing the strut ( 12 ) to warp to some extent when the aircraft is turning while taxiing. 2. The landing gear according to claim 1, wherein the top panel ( 101 ) and the bottom panel ( 102 ) both extend in respective planes each containing the pivot axis (X) of the strut ( 12 ), the plane of the top panel ( 101 ) being substantially orthogonal to the sliding axis (Z) of the telescopic rod ( 13 ). 3. The landing gear according to claim 1, wherein the top and bottom panels ( 101 , 102 ) are constituted by plane pieces with stiffened margins. 4. The landing gear according to claim 1, wherein the high attachment ( 105 ) between the top panel ( 101 ) and the strut ( 12 ) is constituted by a fixed connection ( 105 . 1 ). 5. The landing gear according to claim 1, wherein the high attachment ( 105 ) between the top panel ( 101 ) and the strut ( 12 ) is constituted by a totally rigid connection ( 105 . 2 ) achieved by welding to or by being formed integrally with said strut. 6. The landing gear according to claim 1, wherein the high attachment ( 105 ) between the top panel ( 101 ) and the strut ( 12 ) is constituted by a connection ( 105 . 3 ) that is hinged about an axis contained in the plane of said panel and extending parallel to the pivot axis (x) of said strut. 7. The landing gear according to claim 1, wherein the low attachment ( 106 ) between the bottom panel ( 102 ) and the strut ( 12 ) is constituted by a connection ( 106 . 1 , 106 . 2 ) that is hinged about an axis contained in the plane of said panel and extending parallel to the pivot axis (X) of said strut. 8. The landing gear according to claim 1, wherein the low attachment ( 106 ) between the bottom panel ( 102 ) and the strut ( 12 ) is constituted by a swivel connection ( 106 . 3 ) associated with a stub axle ( 115 ) projecting from said strut. 9. The landing gear according to claim 1, wherein the low attachment ( 106 ) between the bottom panel ( 102 ) and the strut ( 12 ) is constituted by a restrained connection ( 106 . 4 ) to at least one lug ( 118 ) projecting from said strut. 10. The landing gear according to claim 1, wherein the high and low attachments ( 105 , 106 ) are provided level with sliding bearing surfaces ( 21 , 22 ) for the telescopic rod ( 13 ) in the strut ( 12 ) when the rod is in its pushed-in position corresponding to supporting the aircraft on the ground. 11. The landing gear according to claim 1, wherein the common axis structure ( 103 ) is a separate part including the pivot bearings ( 104 ) enabling the strut ( 12 ) to pivot about its pivot axis (X), said separate part being fixed to the top and bottom panels ( 101 , 102 ) via lugs that are secured thereto and/or to said panels. 12. The landing gear according to claim 1, wherein the common axis structure ( 103 ) is integral with one of the panels ( 101 ). 13. T he landing gear according to claim 1, wherein the common axis structure ( 103 ) includes a panel portion ( 120 ) that is fixed to the top panel ( 101 ) and/or to the bottom panel ( 102 ), said panel portion being coplanar with and extending the associated panel.