LANDING SYSTEM FOR A HELICOPTER ON BOARD A VESSEL

Abstract: Landing system for landing, moving and stationing a helicopter on a vessel, which system comprises a landing deck mounted on the vessel, said deck being provided with an anchorage grid consisting of a large number of openings separated from one another by bridges and a harpoon device fitted on or to be fitted in the helicopter, said harpoon device being provided with number of essentially barb-like elements (30) which are fitted symmetrically around its centre line and are capable of being folded out in the radial direction and which, in the folded-out state, are able to engage behind the bridges forming the boundaries of an opening (6) in the anchorage grid (5) in a manner such that all the bridges forming the boundaries of said opening are subjected to a load, the harpoon device being provided with a pressure ring (32) which can be extended in the downward direction to clamp the grid (5) between said ring and the folded-out barb-like elements (30). The barb-like elements (30) are advantageously fitted on a spear-like device (29), said elements being held in a non-folded-out state by means of elastic devices (31), a sliding device (28) being present which is linked to the piston rod (27) of a piston-and-cylinder unit (25, 26) and which is provided with run-on surfaces (28') which, when the piston rod is pushed outwards, are able to come into contact with the ends of the barb-like elements (30), as a result of which the latter are swung outwards into the said folded-out state.

Description: Title: Landing system for a helicopter on board a vessel The invention relates to a landing system for landing, moving and stationing a helicopter on a vessel, which system comprises a landing deck mounted on the vessel, said deck being provided, essentially in the centre, with an anchorage grid consisting of a large number of openings separated from one another by bridges and a harpoon device fitted or to be fitted in the helicopter at a point on the longitudinal centre line, said harpoon device being capable of being extended downwards, when the helicopter is landing on the deck, in order to enter one of the openings in the anchorage grid and engage behind at least one of the said bridges to anchor the landed helicopter with respect to the deck, and means for towing the helicopter to a parking position. Such a system is at present fairly generally used, in particular on board naval vessels, the anchoring of the landed helicopter on the landing deck by means of the harpoon device being necessary since the helicopter could be thrown off the landing deck by violent sea movements transmitted to the vessel. In the known system, after it has landed on the landing deck and has been temporarily anchored with respect to the grid by means of the harpoon device, the helicopter is towed by means of a set of winches to the parking place, for example in a hangar. This means that personnel are to proceed to the landing deck in order to attach the winching cables to the helicopter, which is very undesirable since the personnel are then exposed to all kinds of dangers. The object of the invention is to provide a landing system of the type mentioned which does not have this disadvantage. This object is achieved in that it has been found that a landed helicopter of the type mentioned can be towed essentially from any landing position to any other position and be guided in the process by arranging for a force to act at a point in the longitudinal centre line of the helicopter so that, since the harpoon device is located at such a point, the anchored helicopter can be towed from the landing position to a parking position by moving the anchorage grid. Consequently, the system according to the invention is characterized in that the anchorage grid is movably mounted in the plane of the landing deck and means are available for moving the grid in a manner such that a towing and guiding force can be exerted on an anchored helicopter during the operation by means of the harpoon device anchored in the grid. Since the harpoon device is provided, in the known landing system, with one claw-type element which engages during anchoring around only one boundary bridge of the opening into which the harpoon device is inserted, said bridge would be too heavily loaded in the system according to the invention when the helicopter is being towed to the parking position. For this reason, the harpoon device in the system according to the invention is preferably provided with a number of essentially barb-like elements which are fitted symmetrically around the centre line and are capable of being folded out in the radial direction and which, in the folded-out state, engage behind the bridges forming the boundaries of an opening in the grid in a manner such that all the bridges forming the boundaries of said opening are subjected to a load. As a result of this, use can be made of a grid having a standard opening shape and bridge shape, with the result that helicopters which are equipped with a conventional harpoon device are also able to land. At the same time, the harpoon device is advantageously provided with a pressure ring which can be extended in the downward direction to clamp the grid between said ring and the folded-out barbs. In this manner, the loading of the frame of the helicopter can be reduced during towing. In an advantageous embodiment of the system according to the invention, the grid is mounted on or in a plate- ype device which is situated essentially in the plane of the landing deck and which can be moved by means of a drive system along a straight path parallel to itself, the grid itself being capable of executing, by means of guiding means, a translation with respect to the plate- type device in the direction perpendicular to the direction of movement of the device or being capable of being rotated with respect to the plate-type device. The invention is explained in more detail with reference to the drawing, wherein Figure 1 shows diagrammatically the parking of a helicopter, Figure 2 shows diagrammatically a movable anchorage grid according to the invention, Figure 3 shows a second embodiment of a movable anchorage grid according to the invention, Figure 4 shows a section through the anchorage grid on an enlarged scale, and Figures 5 and 6 shows a harpoon device according to the invention in longitudinal section, Figure 5& being a section along the line Va-Va. As shown in Figure 1, a helicopter 1 having the side wheels 2 and the forked rear wheel 3 can be towed from the lowermost arbitrary position indicated by broken lines to a position shown at the top in the figure by arranging for a towing force and a guiding force perpendicular thereto to act at the point 4, the point -i describing the path S. At the position of the point 4, the helicopter is provided with a harpoon device. As shown in Figures 2 and 4, the anchorage grid 5 is provided with a large number of round openings 6 which are bounded or separated from one another by bridges 7» The anchorage grid 5 is mounted in a frame 8 so as to move in accordance with the double arrow A, the movement of the grid being capable of being effected by means of a linear movement mechanism, for example the threaded spindle 9 which is rotatably mounted on the frame 8 and with which the plate is engaged by means of the threaded sleeve 10. The spaces at either side of the grid 5 are at the same time always sealed by filler panels 15 which travel concomitantly with the grid. The frame 8 can be moved in accordance with the double arrow B inside a channel-type recess 11 which is provided in the landing deck 12, the plate 8 being guided by rails 13. The frame 8 is coupled to automatically concomitantly travelling filler panels Ik so that the channel 11 is always sealed at the top. Like the panels 15. the filler panels 14 are of the type which is used to seal hatchway openings in a middle deck on board ships, said panels being situated behind one another in one plane and adjacent to one another in the position completely sealing the opening and being situated beneath one another in a somewhat tilted position in the position completely opening the opening at one of the transverse edges of the opening. The plate 8 can be moved back and forth in accordance with B by means of the cable 16 which is wound around the capstan 17 which can be driven by the motor 18. To effect the translation A of the grid 5. the threaded spindle 9 is caused to rotate by means of the cable 19 which is wound round the capstan 20 which can be caused to rotate by means of the planetary gearbox 21, the planetary gearbox being driven by the motor 22. In the embodiment according to Figure 3. use is made of a round anchorage grid 5' which is rotatably received in a plate 8' which can be moved back and forth inside a channel-type recess 11" by means of the cable 16' according to the double arrow B 1 in the same manner as shown for the frame 8 in Figure 2, said recess being provided in the landing deck 12' , the plate being guided by the rails 13'. A rotatable shaft 9' with a worm 10' permanently mounted thereon is provided on the plate 8' , which worm is enmeshed with the grid 5' which is constructed as a worm wheel so that the grid 5* can be rotated by causing the shaft 9 1 to rotate. The rotation of the shaft 9* is effected by means of the cable 19' in the same manner as shown for the threaded spindle 9 in Figure 2. Here *■ again the plate 8' is coupled to automatically concomitantly travelling filler panels 14' so that the channel 11' is always sealed at the top. As shown in Figures 5 and 6, the harpoon device comprises a housing 23 which is attached at its top end by means of a telescopic extension and retraction system, which is not shown, to the helicopter at the bottom thereof. A sleeve-type body 24 is rotatably received inside said housing 23. There is furthermore a cylinder 25 in which a piston 26 is able to move back and forth. said piston being linked to a piston rod 27 which carries a sliding device comprising four leg-type elements 28, each leg-type element 28 having a run-on surface 28* at its bottom end. The sleeve 24 furthermore carries, by means of the screw threads 24', the cross- shaped head 29' of a spear-like device 29 which is provided with four barb-like elements 30 which can be folded out and which are held in the non-folded-out state by means of elastic devices 31- A pressure ring 32 is furthermore provided around the housing 23. Starting from the state shown in Figure 5. the harpoon device is forced downwards out of the helicopter by means of the telescopic extension system mentioned, the spear-like device 2 engaging in an opening 6 of the landing grid 5 and the pressure ring 32 which comes to rest against the bridges 7 during this operation being forced upwards with respect to the housing 23. A pressurized fluid is then admitted, via channels which are not shown, into the space 33 above the piston 26, for example by a signal emitted by the pressure ring, as a result of which the sliding device 28 is lowered, the leg-type elements sliding between the ribs of the cross-shaped head 29' of the spear-like device 29. When this happens, the run-on surfaces 28' come into contact with the ends of the barb-like elements 30, as a result of which said elements are swung outwards and engage behind the bridges 7 of the opening 6 in the grid 5. as shown in Figure 6. A pressurized fluid is then introduced into the chamber 3 between the pressure ring 32 and the housing 23, as a result of which a downwardly directed force is exerted on the pressure ring 3 , with the result that the harpoon device is brought to a virtually vertical position and the grid s clamped between the pressure ring 3 and the folded-out barbs 30. When the harpoon device is released, the pressure in the chamber 34 is removed and a pressurized fluid is introduced into the space 35 beneath the piston 26, as a result of which the sliding device 28 moves upwards with the result that the barb-like elements 30 are released from the bridges 27 because they are folded inwards as a result of the action of the elastic devices 31- Finally, the entire harpoon device is again brought into the starting position from the helicopter by means of the telescopic retraction system. A harpoon device according to the invention can also be constructed in a manner such that it can be pulled, by means of a pilot cable to be operated from the helicopter, into a hollow pin- like device projecting downwards from the bottom of the helicopter and can be secured therein so that the harpoon device essentially forms a separate component which is not permanently connected to the helicopter.

Claims: Claims 1. Landing system for landing, moving and stationing a helicopter on a vessel, which system comprises a landing deck mounted on the vessel, said deck being provided with an anchorage grid consisting of a large number of openings separated from one another by bridges and a harpoon device fitted or to be fitted in the helicopter, said harpoon device being capable of being extended downwards, when the helicopter is landing on the deck, in order to enter one of the openings in the anchorage grid and engage behind at least one of the said bridges to anchor the landed helicopter with respect to the deck, and means for towing the helicopter to a parking position, characterized in that the harpoon device is provided with a number of essentially barb-like elements which are fitted symmetrically round its centre line and which are capable of being folded out in the radial direction and which, in the folded-out state, are able to engage behind the bridges forming the boundaries of an opening in the anchorage grid in a manner such that all the bridges forming the boundary of said opening are subjected to a load. 2. System according to Claim 1, characterized in that the harpoon device is provided with a pressure ring which can be extended in the downward direction to clamp the grid between said ring and the folded-out barb-like elements. 3. System according to Claim 1 or 2, characterized in that the barb-like elements are fitted on a spear-like device which is mounted in the housing, said elements being held in a non-folded- out state by means of elastic devices and a sliding device being present which is linked to the piston rod of a piston- and-cylinder unit fitted in the housing and which is provided with run-on surfaces which, when the piston rod is pushed outwards, are able to come into contact with the ends of the barb-like elements, as a result of which the latter are swung outwards into the said folded- out state. 4. System according to Claim 3. characterized in that the pressure ring is linked to, or forms a single entity with, an axially slidable sheath provided around the housing, an essentially sealed annular chamber which is bounded by a shoulder formed on the sheath at the inside and which can be connected to a source of pressurized fluid being formed between the outside surface of the housing and the inside surface of the sheath so that a force directed towards the free end of the spear-like device is exerted on the sheath by introducing the pressurized fluid into said chamber. 5. System according to Claims 3 or 4, characterized in that four barb-like elements are provided and the sliding device comprises four leg-type elements which are each provided with a run-on surface mentioned, the spear-like device having a shaft which is cross-shaped in section and along which the leg-type elements are guided. 6. System according to Claims 1-5, characterized in that the anchorage grid is movably mounted in the plane of the landing deck and means are available for moving the grid in a manner such that a towing and guiding force can be exerted on the anchored helicopter during the operation by means of the harpoon device anchored in the grid. 7. System according to Claims 6, characterized in that the grid is mounted on or in a plate-type device which is situated essentially in the plane of the landing deck and which can be moved by means of a drive system along a straight path parallel to itself, the grid being capable of executing, by means of guiding means, a translation with respect to the plate-type device in the direction perpendicular to the direction of movement of the device orbeingcapable ofbeingrotatedwith respect to theplate-type device.

Inventors: REIMERING WILHELM ROBERT MARIE, WOLTERS HENK RIJNHOLD, REIMERING, WILHELM, ROBERT, MARIE, WOLTERS, HENK, RIJNHOLD
Applicants: ROTTERDAMSCHE DROOGDOK MIJ, DE ROTTERDAMSCHE DROOGDOK MAATSCHAPPIJ B.V.
Application year: 1990
Main classification: B64F1
IPC codes: B64F1