Skid-type landing gear for a helicopter
The invention relates to a skid-type landing gear ( 1 ) for a helicopter ( 2 ) comprising bow shaped crosstubes ( 10 - 13 ) directed symmetrically towards a left- and a right-hand side of a longitudinal mid axis ( 9 ) of the helicopter ( 2 ) with respective skids ( 14, 15 ) at outboard ends thereof and main beams ( 5 - 8 ) in a fuselage ( 4 ), the crosstubes ( 10 - 13 ) being connected to the main beams ( 5 - 8 ) via supports ( 16 - 23 ) fixed to the main beams ( 5 - 8 ). The skid-type landing gear ( 1 ) is retractable. A method for operating such a skid-type landing gear ( 1 ) for a helicopter ( 2 ) is provided.
1. A skid-type landing gear for a helicopter comprising at least two bow shaped crosstubes directed symmetrically towards a left- and a right-hand side of a longitudinal mid axis of the helicopter with respective skids at outboard ends thereof and main beams in a fuselage, the crosstubes being connected to the main beams via laterally spaced supports fixed to the main beams, wherein at least one crosstube is provided separately for each side of the helicopter, the crosstubes on either side being slidably mounted relative to the supports and in that at least one drive is provided for moving the at least one crosstube per side relative to the supports between a retracted and an extended position.
2. A skid-type landing gear according to claim 1 , wherein the crosstubes have an essentially circular bow shape.
3. A skid-type landing gear according to claim 1 , wherein the supports comprise rollers mounted in rotatable casings of the supports.
4. A skid-type landing gear according to claim 1 , wherein the drive comprises an electric or hydraulic motor.
5. A skid-type landing gear according to claim 1 , wherein the drive comprises a motor-gears unit with a pinion configured to interact with a rack mounted on the crosstubes.
6. A skid-type landing gear according to claim 1 , wherein the crosstubes are lockable in the extended position.
7. A method of operating a skid-type landing gear according to claim 1 with the steps of retracting the at least two bow shaped crosstubes with the respective skids at outboard ends thereof after take-off from an extended position to a flight position and vice versa before landing from a flight position to an extended position.
8. A method according to claim 7 , further comprising the step of locking the crosstubes at least in an extended position.