Skid landing gear provided with components having a device for absorbing energy by plastic deformation and/or for limiting stress, and components of this type

Claim 2

Skid landing gear to be fitted to a helicopter comprising a pair of crosspieces pivotally mountable to an undercarriage of a helicopter, each crosspiece including a straight central section and a pair of depending leg sections each having a lower end, each crosspiece being pivotable about a first axis perpendicular to a longitudinal axis of the helicopter, a pair of parallel skids, each being on one side of the helicopter, means for pivotally attaching said skids to the lower ends of the depending leg sections, each means for pivotally attaching having a pivoting axis parallel to said first axis, each said depending leg section being inclined relative to vertical having its lower end more rearwardly of the helicopter than its straight central section, means for absorbing and dissipating energy when acted upon by a force greater than a threshold value by plastic deformation of a component thereof, and means for pivotally interconnecting said means for absorbing and dissipating energy to at least one of said skids and at least one of said depending leg sections, each means for pivotally interconnecting having pivoting axes parallel to said first axis, whereby force exerting on the skid landing gear less than said threshold value is taken up by elastic flexion of said depending leg sections and force exerted on the skid landing gear greater than said threshold value is taken up by said means for absorbing and dissipating energy as the skid landing gear rotates and collapses rearwardly.

Claim 3

The skid landing gear as claimed in claim 1, wherein said means for absorbing and dissipating energy includes shock absorber means for pneumatically absorbing and damping energy when acted upon by a force less than said threshold value.

Claim 4

The skid landing gear as claimed in claim 1, wherein said means for absorbing and dissipating energy includes a cylinder, a rod telescopically mounted in said cylinder, means for moving said rod relative to said cylinder, and means for locking said rod relative to said cylinder in at least one utilization position.

Claim 5

Skid landing gear to be fitted to a helicopter comprising a pair of crosspieces pivotally mountable to an undercarriage of a helicopter, each crosspiece including a straight central section and a pair of depending leg sections each having a lower end, each crosspiece being pivotable about a first axis perpendicular to a longitudinal axis of the helicopter, a pair of parallel skids, each being on one side of the helicopter, means for pivotally attaching said skids to the lower ends of the depending leg sections, each means having a pivoting axis parallel to said first axis perpendicular to the longitudinal axis of the helicopter, each said depending leg section being inclined relative to vertical having its lower end more rearwardly of the helicopter than its straight central section, a lever integral at a lower end thereof with said straight central section of one of said crosspieces, means for absorbing and dissipating energy when acted upon by a force greater than a threshold value by plastic deformation of a component thereof, and means for pivotally interconnecting said means for absorbing and dissipating energy to the other end of said lever and to a structural member in the helicopter, said means for pivotally interconnecting having pivoting axes parallel to said first axis, whereby force exerted on the skid landing gear less than said threshold value is taken up by elastic flexion of said depending leg sections and force exerted on the skid landing gear greater than said threshold value is taken up by said means for absorbing and dissipating energy as the skid landing gear rotates and collapses rearwardly.

Claim 6

Skid landing gear to be fitted to a helicopter comprising a pair of crosspieces pivotally mountable to an undercarriage of a helicopter, each crosspiece including a straight central section and a pair of depending leg sections each having a lower end, each crosspiece being pivotable about a first axis perpendicular to a longitudinal axis of the helicopter, a pair of parallel skids, each being on one side of the helicopter, means for pivotally attaching said skids to the lower ends of the depending leg sections, each means having a pivoting axis parallel to said first axis perpendicular to the longitudinal axis of the helicopter, each said depending leg section being inclined relative to vertical having its lower end more rearwardly of the helicopter than its straight central section, a lever integral at a lower end thereof with said straight central section of one of said crosspieces, means for absorbing and dissipating energy when acted upon by a force greater than a threshold value by plastic deformation of a component thereof, and means for pivotally interconnecting said means for absorbing and dissipating energy to the other end of said lever and to a structural member in the helicopter, said means for pivotally interconnecting having pivoting axes parallel to said first axis, whereby force exerted on the skid landing gear less than said threshold value is taken up by elastic flexion of said depending leg sections and force exerted on the skid landing gear greater than said threshold value is taken up by said means for absorbing and dissipating energy as the skid landing gear rotates and collapses rearwardly.

Claim 7

The skid landing gear as claimed in claim 4, wherein said means for absorbing and dissipating energy includes shock absorber means for pneumatically absorbing and damping energy when acted upon by a force less than said threshold value.

Claim 8

The skid landing gear as claimed in claim 4, wherein said means for absorbing and dissipating energy includes a cylinder, a rod telescopically mounted in said cylinder, means for moving said rod relative to said cylinder, and means for locking said rod relative to said cylinder in at least one utilization position.

Claim 9

Skid landing gear to be fitted to a helicopter comprising a pair of front crosspieces, each mountable to an undercarriage on one side of a helicopter to pivot about an axis substantially parallel to a longitudinal axis of the helicopter, each said front crosspiece having a lower end, a pair of rear crosspieces, each mountable to the undercarriage on one side of the helicopter to pivot about said axis on its respective side, each said rear crosspiece having a lower end and an upper end, said upper end extending past said axis into a body of the helicopter, a pair of parallel skids, each being on one side of the helicopter and being fixed to one front and one rear crosspiece, means for absorbing and dissipating energy when acted upon by a force greater than a threshold value by plastic deformation of a component thereof, and means for pivotally interconnecting said means for absorbing and dissipating energy to said upper ends of said rear crosspieces and to a structural member in the helicopter, said means for pivotally interconnecting having pivoting axes parallel to said axis, whereby force exerted on the skid landing gear less than said threshold value is taken up by elastic flexion of said front and rear crosspieces and force exerted on the skid landing gear greater than said threshold value is taken up by said means for absorbing and dissipating energy as the skid landing gear rotates and collapses laterally outwardly of the helicopter.

Claim 10

Skid landing gear to be fitted to a helicopter comprising a pair of front crosspieces, each mountable to an undercarriage on one side of a helicopter to pivot about an axis substantially parallel to a longitudinal axis of the helicopter, each said front crosspiece having a lower end, a pair of rear crosspieces, each mountable to the undercarriage on one side of the helicopter to pivot about said axis on its respective side, each said rear crosspiece having a lower end and an upper end, said upper end extending past said axis into a body of the helicopter, a pair of parallel skids, each being on one side of the helicopter and being fixed to one front and one rear crosspiece, means for absorbing and dissipating energy when acted upon by a force greater than a threshold value by plastic deformation of a component thereof, and means for pivotally interconnecting said means for absorbing and dissipating energy to said upper ends of said rear crosspieces and to a structural member in the helicopter, said means for pivotally interconnecting having pivoting axes parallel to said axis, whereby force exerted on the skid landing gear less than said threshold value is taken up by elastic flexion of said front and rear crosspieces and force exerted on the skid landing gear greater than said threshold value is taken up by said means for absorbing and dissipating energy as the skid landing gear rotates and collapses laterally outwardly of the helicopter.

Claim 11

The skid landing gear as claimed as claimed in claim 7, wherein said means for absorbing and dissipating energy includes shock absorber means for pneumatically absorbing and damping energy when acted upon by a force less than said threshold value.