WO2023218397A1 - Assembly of a mounting system and rudder, kit for installing hydrofoils comprising such an assembly and method for changing the configuration of a boat comprising such a kit - Google Patents

Assembly of a mounting system and rudder, kit for installing hydrofoils comprising such an assembly and method for changing the configuration of a boat comprising such a kit Download PDF

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Publication number
WO2023218397A1
WO2023218397A1 PCT/IB2023/054880 IB2023054880W WO2023218397A1 WO 2023218397 A1 WO2023218397 A1 WO 2023218397A1 IB 2023054880 W IB2023054880 W IB 2023054880W WO 2023218397 A1 WO2023218397 A1 WO 2023218397A1
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WO
WIPO (PCT)
Prior art keywords
rudder
configuration
boat
supporting plane
mounting
Prior art date
Application number
PCT/IB2023/054880
Other languages
French (fr)
Inventor
Guillaume BONNIOT
Original Assignee
Gb Naval Development
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gb Naval Development filed Critical Gb Naval Development
Publication of WO2023218397A1 publication Critical patent/WO2023218397A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B63B1/26Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type having more than one hydrofoil
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B63B1/28Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B63B1/28Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils
    • B63B1/283Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils movable around a vertical axis, e.g. for steering
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B63B1/28Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils
    • B63B1/30Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils retracting or folding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B83/00Rebuilding or retrofitting vessels, e.g. retrofitting ballast water treatment systems
    • B63B83/30Rebuilding or retrofitting vessels, e.g. retrofitting ballast water treatment systems for improving energy efficiency, e.g. by improving hydrodynamics or by upgrading the power plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/02Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement
    • B63B1/10Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls
    • B63B1/12Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls the hulls being interconnected rigidly
    • B63B1/121Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls the hulls being interconnected rigidly comprising two hulls
    • B63B2001/123Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls the hulls being interconnected rigidly comprising two hulls interconnected by a plurality of beams, or the like members only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B63B1/28Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils
    • B63B2001/281Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type with movable hydrofoils movable about an axis substantially parallel to the flow direction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63BSHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B35/00Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
    • B63B2035/009Wind propelled vessels comprising arrangements, installations or devices specially adapted therefor, other than wind propulsion arrangements, installations, or devices, such as sails, running rigging, or the like, and other than sailboards or the like or related equipment

Definitions

  • the invention relates to the field of installing rudders on boats.
  • the invention thus relates more precisely to a system for mounting a rudder to the hull of a boat, an assembly comprising such a mounting system and a rudder and method for installing a rudder.
  • a solution to this problem is the provision of a rudder comprising a frame and a body mounted sliding in said frame to allow, through this sliding, an adaptation of the depth of the rudder depending on the configuration of the bottom.
  • a sliding assembly makes it possible to adapt the depth of the rudder according to the risks involved, it does not provide protection against an unpredictable obstacle, such as a sandbank or an orphaned rock.
  • support plan installation kits for boats which each include: - two supporting plane arms intended to be fixed on a structural element of the boat and each having a supporting plane intended to be at least partly submerged when the arm equips the boat,
  • rudders each equipped with a supporting plane, for example T-shaped.
  • kits make it possible to transform a “classic” boat into a boat with supporting planes (or, according to its English name which is generally used, “hydrofoils”), or hydrofoils.
  • kits nevertheless have a relatively significant drawback in that they do not allow a rapid transition of the boat from the hydrofoil configuration to the classic configuration. Indeed, if it could be possible to simply dismantle the supporting plane arms to allow passage into a classic configuration, the or each rudder must necessarily be replaced by a classic rudder, that is to say without a supporting plane. Thus, in addition to the difficulty of dismantling the rudder, it is necessary for the boater to have access to one or more rudders without a supporting surface.
  • the invention relates in particular to a system for mounting a rudder to the hull of a boat, the mounting system comprising: a first and a second mounting element by means of which the rudder is intended to be mounted to the hull of the boat, the first and the second mounting element being intended to be mounted movable in rotation with respect to the hull of the boat around a rudder axis which is common to them, the second mounting element being intended to be arranged along the rudder axis under the first mounting element when the boat is afloat, the first element of assembly having a pivot axis along which the rudder is intended to be mounted movable in rotation, the pivot axis being transverse to the rudder axis, and the second mounting element being intended to be assembled to one of the rudder and the hull by elastic interlocking.
  • the invention aims more particularly to facilitate the transition from a hydrofoil configuration to a conventional configuration and to avoid the problems of complete dismantling of the rudder.
  • the invention relates to a mounting system and rudder assembly for mounting the rudder to the hull of a boat from said mounting system, the mounting system and rudder assembly comprising: a first and a second mounting element by means of which the rudder is intended to be mounted to the hull of the boat, the first and the second mounting element being intended to be mounted movable in rotation with respect to the hull of the boat around an axis of rudder which is common to them, a frame mounted on the first and second mounting elements, a rudder body mounted sliding in the frame to allow adjustment of the depth of the rudder.
  • the rudder has a carrier plane, said carrier plane being preferably a T-shaped carrier plane, and the rudder body carries the carrier plane at one of the ends of said rudder body and the rudder body being adapted to be arranged in the reinforcement with either the supporting plane oriented upwards, that is to say above a waterline of the boat, or the supporting plane oriented downwards, that is to say above below a waterline of the boat.
  • rudder can easily switch from a “hydrofoil” configuration, in which the supporting plane is located under the waterline, to a classic configuration, that is to say in which the supporting plane is out of water by a simple change of arrangement of the rudder in the frame.
  • the rudder can be used in both configurations of the boat, thereby eliminating the need for two separate rudders.
  • the second mounting member may be intended to be arranged along the rudder axis below the first mounting member when the boat is afloat, the first mounting member having a pivot pin along which is intended to be mounted movable in rotation the rudder, the pivot axis being transverse to the rudder axis, the second mounting element being intended to be assembled to one of the rudder and the hull by elastic fitting.
  • the second mounting element may be intended to be assembled to the rudder by elastic fitting.
  • the mounting system may further comprise an intermediate part intended to be fixed to the hull, and advantageously to the transom of the hull, and in which the first and the second mounting element are mounted movable in rotation with respect to the intermediate piece around the rudder axis.
  • the first and second mounting elements can be standard elements of a rudder installation kit.
  • the rudder may have a depth portion arranged on one end of the rudder intended to be opposite the hull, and in which said depth portion comprises an element made of deformable material, such as an elastomer which is advantageously a natural or synthetic rubber.
  • the rudder can participate in the elevation of the boat when the latter has a “hydrofoil” configuration.
  • the rudder body carries the supporting plane at the level of one of the ends of said rudder body and the rudder body is adapted to be arranged in the frame with either the supporting plane oriented upwards, c that is to say above a waterline of the boat, or the supporting plane oriented downwards, that is to say below the waterline of the boat.
  • the rudder can equip the boat both when it is configured for “hydrofoil” navigation and when it is configured for “classic” navigation.
  • the invention further relates to a kit for installing supporting planes for a boat, in particular wind-powered, a boat comprising at least one structural element, the kit for installing supporting planes comprising an assembly according to the invention and at least one supporting plane arm intended to be mounted on the structural element and having a supporting plane intended to be at least partly submerged.
  • the invention further relates to a method of mounting a rudder to the hull of a boat from a system according to the invention, the method comprising the following steps of: mounting on the hull of the first and the second element mounting elements movable in rotation with respect to the hull of the boat around a rudder axis which is common to them, the second mounting element being arranged along the rudder axis under the first mounting element when the boat is afloat, mounting the movable rudder in rotation around a pivot axis of the first mounting element, the pivot axis being transverse to the rudder axis, the second mounting element being assembled to one of the rudder and the hull by elastic interlocking.
  • the invention further relates to a method for changing the configuration of a rudder of a boat equipped with a carrier plane installation kit according to the invention, the method for changing the configuration comprising the following steps: removal of the rudder of the frame, passage of the orientation of the rudder from one configuration among a configuration in which the supporting plane oriented upwards and a configuration in which the supporting plane oriented downwards, to another configuration among the configuration in which the supporting plane oriented upwards and the configuration in which the supporting plane oriented downwards, arrangement of the rudder in the frame while maintaining the orientation in which it was passed.
  • a step of modifying a configuration of the at least one supporting plane arm can also be provided in such a way as to change from one configuration to a configuration in which the second supporting plane is at least partly immersed and a configuration in which the second supporting plane is not immersed to the other configuration among the configuration in which the second supporting plane is at least partly immersed and the configuration in which the second supporting plane is not immersed.
  • Figure IA illustrates a rear three-quarter view of a boat equipped with a carrier plan installation kit including two rudder mounting systems according to a first embodiment of the invention, one carrier plan arm of said kit being installed, the other being being installed;
  • Figure IB illustrates a three-quarter side view of the boat shown in the figure
  • Figure 2 schematically illustrates the principle of installing the supporting plane arms of a kit according to the first embodiment of the invention
  • Figure 3 illustrates the support block system used as part of the installation of the support plane arms according to this first embodiment
  • Figure 4A illustrates in a schematic top view the principle of adjusting the inclination of a supporting plane arm according to the first embodiment of the invention
  • Figure 4B illustrates in a schematic side view the principle of adjusting the inclination of a supporting plane arm according to the invention already illustrated in Figure 4A
  • Figure 5A illustrates the mounting system according to the invention of a rudder fitted to the kit of the invention
  • Figure 5B illustrates in partial close-up view the mounting system of Figure 5A showing a combination of a pivot connection and a force fit offering a rudder protection function
  • Figure 5C illustrates in partial close-up view a supporting plane fitted to the rudder and a depth portion of said rudder
  • Figure 5D illustrates in a perspective view the rudder by showing the configuration of each of the ends of
  • FIGS IA and IB illustrate a boat 1, here a catamaran, equipped with an installation kit for supporting planes 22, 32, 45, 55 incorporating a rudder mounting system according to one possibility of the invention so that the latter forms a hydrofoil.
  • the installation kit for supporting planes 22, 32, 45, 55, and therefore the mounting system according to the invention equips a boat 1 of type catamaran, this can be adapted to other types of boats, such as a monohull or a trimaran, as will be shown in the following embodiments.
  • the boat 1 comprises a structural element 15, here one of the connecting arms 15, 16, on which part of the installation kit for supporting planes 22, 32, 45, 55 is installed.
  • An installation kit for supporting planes 22, 32, 45, 55 comprises, as shown in Figure 2: two support blocks 21, 31 each intended to be fixed to the at least one structural element 15 , that is to say one of the connecting arms 15, 16 of the boat 1, two supporting plane arms 22, 32 each having a supporting plane 24, 34 intended to be at least partly immersed, each supporting plane arm 22, 32 being mounted on a support block 21, 31 which is respective to it, two rudders each equipped with a 45, 55 T-shaped supporting plane.
  • the installation kit of supporting planes can also include a control system 17 capable of communicating with a system for modifying the motorized configuration, not shown, and control said system to adapt the arrangement of the supporting plane arms 22, 32.
  • a control system 17 capable of communicating with a system for modifying the motorized configuration, not shown, and control said system to adapt the arrangement of the supporting plane arms 22, 32.
  • the arrangement of the supporting plane arms 22, 32 is adjusted manually by a member of the crew of boat 1.
  • the support block 21, 31 comprises, as shown in Figure 3: two adaptation parts 212A, 212B, shaped to cooperate with the structural element 15, 13 and be fixed to the latter, the adaptation parts providing a plane reference for the supporting plane arm 22, a plate 211 on which the supporting plane arm 22 is mounted, the plate 211 being mounted on the adaptation parts 212A, 212B along the reference plane.
  • two adaptation parts 212A, 212B are provided consisting of two half-shells sandwiching the structural element, that is to say the arm connection 15.
  • the first adaptation part 212A, “top” part has an L shape
  • the second adaptation part 212B, “bottom” part has a U shape in order to best accommodate the lower part of the connecting arm 15.
  • Such a conformation allows the adaptation parts 212A, 212B, from the shape of the portion of the connecting arm 15 which they house, to provide a reference plane, with respect to -screw of the waterline of the boat, for the plate 211 and therefore the supporting plane arm 22 which is mounted on the plate 211.
  • the U shape of the second adaptation part 212B forms a housing so as to stabilize its placement on the connecting arm 15, and that of the first adaptation part 212A.
  • the surface of the first adaptation part 212A which is opposite the deck of the boat defines the reference plane.
  • Each of the first and second adaptation parts is preferably made of a rigid material such as a thermoplastic, a composite material or even wood.
  • said surface of the first adaptation part 212A materializes the reference plane, this plane may not present materiality, since by the provision of a support surface , not necessarily flat, the adaptation part(s) 212A, 212B make it possible to ensure the orientation of the plate 211, and therefore of the supporting plane arm 22, with respect to the waterline of the boat 1.
  • the first adaptation part 212A can have a recess in order to authorize the placement of an adjustment system 213 of the orientation of the supporting plane arm 22 on the plate , said adjustment system 213 comprising a gear assembly to allow height adjustment of the ball joint(s) 215, 216, illustrated in Figures 4A and 4B.
  • the plate 211 has a complementary shape with the adaptation parts 212A, 212B.
  • the plate 211 has a U shape with the two branches of the U which define a housing shaped to receive the adaptation parts 212A, 212B.
  • the fixing of the plate 211 on the adaptation parts 212A, 212B is done by elastic fitting and by translation along the axis of the connecting arm of the boat.
  • the plate 211 thus makes it possible to ensure good fixing of the adaptation parts 212A, 212B on the connecting arm 15.
  • any other assembly such as screwing, riveting or welding can be considered.
  • a removable assembly is to be preferred.
  • Each plate is preferably made of a rigid material such as a thermoplastic, a composite material, wood or even metal and in particular stainless steel.
  • Each support plane arm 22, 32 comprises, as shown in Figures IA and IB, comprises a fixing arm 23, 33 by which the support plane arm 22, 32 is mounted on the plate 211, and a support plane 24, 34 as such which, by being fixed to one end of the fixing arm 23, 33, is intended to be at least partly submerged.
  • the supporting plane 24, 34 is profiled in order to provide a lift force when the boat 1 moves.
  • the support arm 23, 33 and the support plane 24, 34 are distinct from each other, it is possible to provide a one-piece support plane arm 22, 32 with the support arm 23, 33 and the supporting plane 24, 34 which are then formed integral with each other.
  • Each supporting plane arm 22, 32 can be mounted on the corresponding plate 211 from at least two ball joints 215, 216, 217.
  • each plane arm carrier 22, 32 is mounted on the corresponding plate 211 from a first and second ball joints 215, 216 located on either side of the supporting plane arm in order to define a first pivot connection and another ball joint 217 which is arranged at one end of the supporting plane arm 22, 32 which is free from the supporting plane 24, 34 this with a lateral offset to define a second pivot connection with the second ball joint 216.
  • the first ball joint 215 is mounted movable in translation vis- with respect to the plate 211 in order to allow adjustment of the “height” of the first ball joint 215.
  • the third ball joint 217 can be dismountable in such a way as to allow the supporting plane arm to pivot around an axis defined by the first and second ball joints 215, 216 when it is disassembled from the third ball joint 217.
  • a complementary support 214 can be provided, for example arranged on a deck of the boat 1, complementary in order to provide an additional fixing point for the supporting plane arm 22, 32.
  • the supporting plane arm 22, 32 can be fixed to this complementary support 214 from a sliding pivot connection as provided, by example and as illustrated by Figures 4A and 4B, from a strap 214A attaching the supporting plane arm 22, 32 to said complementary support 214.
  • the installation kit for carrier planes 22, 32, 45, 55 also includes two rudders 44, 54 each equipped with a T-shaped carrier plane 45, 55.
  • each of the rudders is extended by a bar 42, 52 which is respective to it.
  • T-shaped supporting plane we mean above that the supporting plane 45, 55 comprises two profiles extending in the extension of one another and on either side of the rudder body thus forming the high bar of a capital “T” with the body of the rudder which forms the body of the T.
  • each rudder 44, 54 is mounted on a respective hull 11, 12 of the boat 1, and more precisely on the transom of said hulls 11, 12, by means of a mounting system 43.
  • the mounting system 43 comprises an intermediate part 431 fixed to the transom, and a first and a second mounting element 432, 433 by means of which the rudder 44, 54 is mounted to the hull 11, 12 of the boat 1, the first and the second mounting element 432, 433 are mounted movable in rotation with respect to the intermediate part 431, and therefore to the hull of the boat, around a rudder axis which is attached to them.
  • the second mounting element 433 is arranged along the rudder axis below the first mounting element 432 when the boat 1 is afloat.
  • the intermediate part 431 is adapted according to the shape of the transom to be equipped.
  • the kit to allow the installation of each rudder, only the intermediate part 431 has to be adapted to the boat 1 to be equipped, the other elements concerning the rudder including in particular the first and second mounting elements can be standardized.
  • the first and second mounting elements 432, 433 can be adapted to the boat 1 which they equip, the first and second mounting elements 432, 433 then being directly mounted on the hull 11, 12 (or in this case at the transom of said hull) around a rudder axis.
  • the first mounting element 432 has a pivot axis 432A along which the rudder 44 is movably mounted in rotation, the pivot axis 432A being transverse to the rudder axis and is, preferably and more precisely, substantially perpendicular to the axis. rudder. More specifically, the first element 432 has on a first portion a through orifice in which the rudder axis passes (lock or needle, depending on the rudder configuration, as discussed below) and on a second portion two others orifices through which the pivot pin 432A passes.
  • the pivot pin 432A is transverse to the rudder pin.
  • the second mounting element 433 is assembled to one of the rudder 44 and the hull 11 (through the intermediate piece 431), here the rudder 44, by elastic fitting.
  • the mounting element 433 can be assembled intermediate piece 431, therefore the hull, by elastic snap-fastening, this elastic snap-fastening then also making it possible to provide a movable assembly in rotation around the rudder axis .
  • the second mounting element 433 has on a first portion a through orifice through which the rudder axis passes and on a second portion comprising two arms each having a cantilevered tongue, the arms together defining a reception space for a rudder fixing member 44 preferably having a relief face.
  • first and second mounting elements 432, 433 are provided in the form of two independent parts, it is also possible, without departing from the scope of the invention, that the first and second elements of assembly 432, 433 are supplied in the form of a single part.
  • first and second elements 432, 433 are mounted in the present embodiment, pivoting around the rudder axis forming the rudder stock, it is also possible that the first and second elements 432, 433 are mounted on the intermediate piece 431, or even the hull, by means of a respective needle, the first and the second element then each forming a femelot.
  • the first element 432 can be mounted removable on the hull, this making the first element 432 free to pivot around the pivot axis 432A and to disengage from the rudder axis, or rudder. In this way, when the user wishes to remove the rudder in order to store it, he can disengage the first element and disengage the second element from its attachment by elastic engagement so as to separate the rudder 44, 54 from the hull 11, 12.
  • the rudder 44 as shown in Figure 5A, comprises: a frame 442 by which the rudder 44 is mounted on the first and second mounting elements 432, 433, rudder body 441 slidably mounted in the frame 442 in order to allow an adjustment of the depth of the rudder 44, a securing system, such as a pin, in the position of the rudder body 441 on the frame 442, not shown.
  • the frame 442 has a first and a second extension, extending towards the shell 11, 12, from which the frame is respectively mounted on the first and the second mounting element 432, 433.
  • the first extension is pivotally mounted around the pivot axis 432A.
  • the second extension forms the fixing member and preferably presents, as shown in Figure 5B and towards the shell 11: two grooves extending on either side of the second extension in a direction parallel to the axis rudder, configured to each accommodate a respective cantilevered tongue of the second mounting element 433, a flush face, to facilitate the introduction of the second member into the reception space defined by the second mounting element.
  • the rudder body 441 has a supporting plane 45 here in a T shape.
  • a supporting plane 45 is linked to the use of a mounting system in the frame of a kit for installing carrier planes 22, 32, 45, 55, such a rudder mounting system 43 is perfectly usable, according to a possibility not included in the scope of the invention, for the assembly of a simple rudder not having a supporting plane or not using a frame 442 since such a mounting system offers both a protective function and ease of handling of the latter, regardless of its configuration.
  • the rudder 44 can comprise a portion of depth 443 arranged on one end of the rudder 44 intended to be opposite the hull and at the front of the latter, in a direction of movement of the boat 1.
  • the depth portion 443 comprises an element made of deformable material, such as an elastomer which can be, for example, a natural or synthetic rubber.
  • Such a depth portion 443 comprising a deformable material, such as an elastomer makes it possible to absorb part of the forces exerted on the rudder 44 when the latter encounters an obstacle.
  • the rudder body 441 has two installation orientations in the frame 442, one with the supporting plane 45 arranged on the bottom of the rudder 44 , that is to say below the waterline of the boat, and the other with the supporting plane arranged on the top of the rudder 44, that is to say above the waterline.
  • the rudder 44 can be used as part of a hydrofoil configuration, that is to say with the supporting plane 45 arranged on the bottom of the rudder 44, as in a classic configuration, that is to say with the supporting plane 45 arranged on the top of the rudder 44.
  • the shape of the rudder body can be adapted with each end 441A, 441B of the body which is configured to provide the guiding function of the boat that is his.
  • the end 441A of the rudder 44 not equipped with a supporting plane can also be provided with a element made of deformable material, such as an elastomer which may be, for example, a natural or synthetic rubber.
  • the bar 42, 52 can be fixed to the frame 442. In this way, it is not necessary to assemble/disassemble it when changing the orientation of the rudder. rudder 44.
  • a method of changing the orientation of the rudder comprising the following steps: disengagement of the second mounting element 433 from its elastic fitting in order to allow pivoting of the frame around the axis of pivot 432A, pivoting of the rudder 44 around the pivot axis 432A in order to bring it to an orientation close to horizontal and removal of the securing system in order to allow the rudder body 441 to slide in the frame 442, removal of the rudder body 441 from the frame 442 and turning of the latter in order to change its orientation, installation of the rudder body 441 in the frame 442 with the new orientation, securing the positioning of the rudder body 441 in the frame 442 by reinstalling the security system.
  • an installation kit for supporting planes 22, 32, 45, 55 can be installed according to an installation method comprising the following steps: fixing the two parts adaptations 212 on the structural element 15, that is to say the connecting arm 15, fixing of each of the plates 211 on the corresponding adaptation part 212 along the reference plane defined by the latter, each adaptation part 212 and the corresponding plate 211 participating in the formation of the corresponding support block 21, 31, mounting of each of the supporting plane arms 22, 32 on the respective plate 211, assembly, for each of the rudders 44, 54 and on the corresponding hull 11, 12, of the first and second mounting elements 432, 433 movable in rotation with respect to the hull 11, 12 of the corresponding boat 1 around a rudder axis which is common to said elements of mounting 432, 433 this by means of the intermediate piece 431, the second mounting element 433 corresponding to said rudder 44, 54 being arranged along the rudder axis under the first mounting element 432 corresponding when the boat 1
  • FIGS. 6A and 6B illustrate the assembly of a supporting plane arm 22 according to a second embodiment.
  • a support plane installation kit 22, 32, 45, 55 according to this second embodiment differs from a support plane installation kit 22, 32, 44, 55 according to the first embodiment in that the supporting plane arm 22 is mounted on the plate 211 from the first and the second ball joint 215, 216 which are both movable in translation with respect to the plate 211, the plate being devoid of third ball joint 217 and in that the supporting plane arm 22 is fixed to the support complementary 214 from a sliding pivot connection provided by a strap 214A attaching the supporting plane arm 22 to said complementary support 214.
  • the first and second ball joint 215, 216 by equipping the end of said supporting plane arm 22, 32 free of the supporting plane, together define an axis of pivoting of the supporting plane arm 22, 32 with respect to the structural element 15.
  • each supporting plane arm 22, 32 is released from the strap 214A which provides the sliding pivot connection to the complementary support 214, said supporting plane arm 22, 32 is able to tilt with respect to the structural element, here the connecting arm 15 and thus be raised out of the water.
  • Such tilting makes it possible to limit the handling constraints of the boat 1 when it is brought ashore for storage or in heavy weather not compatible with a hydrofoil configuration.
  • FIGS 7 to 8B illustrate a monohull boat 1 equipped with a support plane installation kit according to a third embodiment.
  • An installation kit for supporting planes 22, 32, 45, 55 according to this third embodiment differs from an installation kit for supporting planes 22, 32, 45, 55 according to the second embodiment in that a single adaptation part 212 and a single plate 211 are provided forming a single support block on which the two supporting plane arms 22, 32 are mounted, in that the deck 13 of the boat 1 forms the structural element, in that the supporting planes 34 bearing plane arms 22, 32 are T-shaped supporting planes and in that the fixing of the adaptation part on the bridge 13 is obtained by means of a strap 218 passing through the part d adaptation 212 and going around the hull 11.
  • this strap 218, as shown in Figure 7, in this third embodiment in which the support plan installation kit equips a monohull boat 1, can come to bear on the keel 14 in such a way as to improve the fixing the adaptation part on the bridge 13.
  • the adaptation part 212 and the plate 211 extend over the entire width of the bridge 13.
  • FIGS 8A and 8B show the mounting of each of the supporting plane arms 22, 32 on the single plate 211.
  • each arm of plan carrier 22, 32 is mounted on the plate 211 using a first and a second ball joint 215, 216 arranged at one end of the carrier plane arm 22, 32 which is free from the carrier plane by together defining an axis pivoting, which is here provided by means of a pivot 216A connecting the first and second ball joints 215, 216.
  • a pivot 216A as is the case for the second embodiment, is not necessary and the first and second ball joints 215, 216 are capable of providing such mounting without the pivot being necessary.
  • the adjustment system 213 comprises two gears, not referenced, geared together and integral in rotation with respectively the first and second ball joint 215, 216.
  • one of the gears is provided with a pulley intended to be coupled with a winch, not shown, by the use of a belt, not shown.
  • the pulley can be operated manually by a simple rope kept under tension acting as a belt.
  • Each supporting plane arm 22, 32 is also mounted on the plate 211 by means of the complementary support 214 of the supporting plane arm on which the supporting plane arm 22, 32 is mounted by means of a removable sliding pivot connection such as that provided by strap 214A.
  • a sliding pivot connection does not hinder the pivoting of the supporting plane arm 22, 32 when adjusting the height of the first and second ball joints 215, 216 with respect to the plate 211 by means of the adjustment system 213.
  • the complementary support in order to allow stable placement with respect to the plate, has a base having a surface complementary to the upper surface of the plate 211.
  • Figures 9A and 9B respectively illustrate a boat 1 equipped with two rudders 44, 54 according to the invention in a hydrofoil configuration and in a classic boat configuration.
  • each rudder 44, 54, and therefore their body 441 are arranged in the corresponding frame 442, 542 with the supporting plane 45 oriented downwards. , that is to say below the waterline of the boat 1.
  • the supporting plane arms 22, 32 are arranged with their respective supporting plane 24, 34 which is submerged.
  • each rudder 44, 54, and therefore their body 441 are arranged in the corresponding frame 442, 542 with the supporting plane 45 oriented upwards, this is that is to say above the waterline of the boat 1.
  • the supporting plane arms 22, 32 are arranged with their respective supporting plane 24, 34 raised, that is to say outside of the sea.
  • the passage of the boat 1 from one configuration to another can be done according to the following process: removal of each rudder 42, 52 from the corresponding frame 442, 542, changing the orientation of each rudder 42, 52 from one configuration among a configuration in which the supporting plane 45, 55 oriented upwards and a configuration in which the supporting plane 45, 55 oriented downwards, to another configuration among the configuration in which the supporting plane 45, 55 oriented toward the top and the configuration in which the supporting plane 45 faces downwards, arrangement of each rudder 42, 52 in the corresponding frame 44, 54 while maintaining the orientation in which it was passed, passage of each of the plane arms carrying a configuration among a configuration in which the supporting plane 24, 34 corresponding to said arm is at least partly immersed and a configuration in which the supporting plane 24, 34 corresponding to said arm is not immersed in the other configuration among the configuration in which the supporting plane 24, 34 corresponding to said arm is at least partly immersed and the configuration in which the second supporting plane 24, 34 corresponding to said arm is not immersed.

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  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
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  • Water Supply & Treatment (AREA)
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Abstract

The invention relates to an assembly of a mounting system (43) and rudder (44) for mounting the rudder to the hull (11) of a boat (1). The assembly comprises: a frame (442) which is mounted on the hull (11) from a first mounting element and a second mounting element; and a rudder body (441) which is slidably mounted in the frame (442) to allow adjustment of the depth of the rudder (44). The rudder (44) has a hydrofoil (45). The rudder body supports the hydrofoil (45) at one of the ends of said rudder body, and wherein the rudder body is suitable for being arranged in the frame (442) with either the hydrofoil (45) oriented upwards, i.e. above a waterline of the boat (1), or the hydrofoil (45) oriented downwards, i.e. below a waterline of the boat (1).

Description

Titre : Ensemble système de montage et safran, kit d'installation de plans porteurs comprenant un tel ensemble et procédé de changement de configuration d'un bateau comprenant un tel kit Title: Mounting system and rudder assembly, support plane installation kit comprising such an assembly and method of changing the configuration of a boat comprising such a kit
Domaine technique Technical area
L'invention concerne le domaine de l'installation de safran sur les bateaux. The invention relates to the field of installing rudders on boats.
L'invention concerne ainsi plus précisément un système de montage d'un safran à la coque d'un bateau, ensemble comprenant un tel système de montage et un safran et procédé d'installation d'un safran. The invention thus relates more precisely to a system for mounting a rudder to the hull of a boat, an assembly comprising such a mounting system and a rudder and method for installing a rudder.
État de l'art antérieur State of the prior art
Lors de la navigation côtière, il n'est pas rare qu'une partie du bateau, telle que le safran, rencontre un obstacle, tel que le fond ou un rocher ou un objet flottant non identifié. Une telle rencontre peut entrainer un endommagement de ladite partie. During coastal navigation, it is not uncommon for a part of the boat, such as the rudder, to encounter an obstacle, such as the bottom or a rock or unidentified floating object. Such an encounter may result in damage to said part.
Un tel risque est particulièrement présent en ce qui concerne le safran et il y aurait intérêt d'avoir un système permettant de limiter les risques liés aux obstacles côtiers. Such a risk is particularly present with regard to rudder and it would be beneficial to have a system to limit the risks linked to coastal obstacles.
Une solution à ce problème est la fourniture d'un safran comprenant une armature et un corps monté coulissant dans ladite armature pour permettre, par ce coulissement, une adaptation de la profondeur du safran en fonction de la configuration du fond. Néanmoins, si un tel montage coulissant permet d'adapter la profondeur du safran en fonction des risques encourus, il ne permet pas de se prémunir d'un obstacle non prévisible, tel qu'un banc de sable ou un rocher orphelin. A solution to this problem is the provision of a rudder comprising a frame and a body mounted sliding in said frame to allow, through this sliding, an adaptation of the depth of the rudder depending on the configuration of the bottom. However, if such a sliding assembly makes it possible to adapt the depth of the rudder according to the risks involved, it does not provide protection against an unpredictable obstacle, such as a sandbank or an orphaned rock.
Il existe donc un besoin de fournir des systèmes qui permettraient de limiter les risques liés aux obstacles côtiers qui ne nécessitent pas de réglage comme c'est le cas avec un tel montage coulissant. There is therefore a need to provide systems which would make it possible to limit the risks linked to coastal obstacles which do not require adjustment as is the case with such a sliding assembly.
Selon un autre problème de l'art antérieur, il existe des kits d'installation de plans porteurs pour bateau qui comprennent chacun : - deux bras de plan porteur destinés à être fixés sur un élément de structure du bateau et présentant chacun un plan porteur destiné à être au moins en partie immergé lorsque le bras équipe le bateau, According to another problem of the prior art, there are support plan installation kits for boats which each include: - two supporting plane arms intended to be fixed on a structural element of the boat and each having a supporting plane intended to be at least partly submerged when the arm equips the boat,
- un ou plusieurs safrans équipés chacun par un plan porteur, parexemple en T. - one or more rudders each equipped with a supporting plane, for example T-shaped.
De tels kits permettent de transformer un bateau « classique » en bateau à plans porteurs (ou, selon sa dénomination anglaise qui est généralement d'usage, à « hydrofoils »), ou hydroptères. Such kits make it possible to transform a “classic” boat into a boat with supporting planes (or, according to its English name which is generally used, “hydrofoils”), or hydrofoils.
Ces kits présentent néanmoins un inconvénient relativement important en ce qu'ils ne permettent pas un passage rapide du bateau de la configuration hydroptère à la configuration classique. En effet, s'il pourrait être envisageable de simplement démonter les bras de plan porteur pour permettre un passage dans une configuration classique, le ou chaque safran doit nécessairement être remplacé par un safran classique, c'est-à-dire sans plan porteur. Ainsi, outre la difficulté de démontage du safran, il est nécessaire que le plaisancier ait accès à un ou plusieurs safrans dénués de plan porteur. These kits nevertheless have a relatively significant drawback in that they do not allow a rapid transition of the boat from the hydrofoil configuration to the classic configuration. Indeed, if it could be possible to simply dismantle the supporting plane arms to allow passage into a classic configuration, the or each rudder must necessarily be replaced by a classic rudder, that is to say without a supporting plane. Thus, in addition to the difficulty of dismantling the rudder, it is necessary for the boater to have access to one or more rudders without a supporting surface.
Ainsi, il y aurait un intérêt à fournir des éléments d'un tel kit qui permettraient de faciliter ce passage d'un bateau d'une configuration hydroptère à une configuration classique et qui éviterait les problématiques de démontage complet du safran telles que présentées par les kits d'installation de plans porteurs de l'art antérieur. Thus, there would be an interest in providing elements of such a kit which would facilitate the transition of a boat from a hydrofoil configuration to a classic configuration and which would avoid the problems of complete dismantling of the rudder as presented by the installation kits for supporting planes of the prior art.
Exposé de l'invention Presentation of the invention
Dans certaine configuration de l'invention, celle-ci vise à remédier à l'inconvénient ci-dessus et a ainsi pour objet de fournir un système permettant d'offrir une protection des safrans en cas de rencontre d'un obstacle tel qu'un rocher, le fond ou un objet flottant non identifié. In certain configuration of the invention, it aims to remedy the above drawback and thus aims to provide a system making it possible to offer protection to the rudders in the event of encountering an obstacle such as a rock, the bottom or an unidentified floating object.
Dans certaines de ces configurations, l'invention concerne notamment un système de montage d'un safran à la coque d'un bateau, le système de montage comprenant : un premier et un deuxième élément de montage par l'intermédiaire desquels le safran est destiné à être monté à la coque du bateau, le premier et le deuxième élément de montage étant destinés à être montés mobiles en rotation vis-à-vis de la coque du bateau autour d'un axe de gouvernail qui leur est commun, le deuxième élément de montage étant destiné à être à agencé le long de l'axe de gouvernail sous le premier élément de montage lorsque le bateau est à flot, le premier élément de montage présentant un axe de pivot le long duquel est destiné à être monté mobile en rotation le safran, l'axe de pivot étant transversal à l'axe de gouvernail, et le deuxième élément de montage étant destiné à être assemblé à l'un parmi le safran et la coque par emboîtage élastique. In some of these configurations, the invention relates in particular to a system for mounting a rudder to the hull of a boat, the mounting system comprising: a first and a second mounting element by means of which the rudder is intended to be mounted to the hull of the boat, the first and the second mounting element being intended to be mounted movable in rotation with respect to the hull of the boat around a rudder axis which is common to them, the second mounting element being intended to be arranged along the rudder axis under the first mounting element when the boat is afloat, the first element of assembly having a pivot axis along which the rudder is intended to be mounted movable in rotation, the pivot axis being transverse to the rudder axis, and the second mounting element being intended to be assembled to one of the rudder and the hull by elastic interlocking.
L'invention vise plus particulièrement à faciliter le passage d'une configuration hydroptère à une configuration classique et à éviter les problématiques de démontage complet du safran. The invention aims more particularly to facilitate the transition from a hydrofoil configuration to a conventional configuration and to avoid the problems of complete dismantling of the rudder.
L'invention concerne à cet effet un ensemble système de montage et safran pour monter le safran à la coque d'un bateau à partir dudit système de montage, l'ensemble système de montage et safran comprenant : un premier et un deuxième élément de montage par l'intermédiaire desquels le safran est destiné à être monté à la coque du bateau, le premier et le deuxième élément de montage étant destinés à être montés mobiles en rotation vis-à-vis de la coque du bateau autour d'un axe de gouvernail qui leur est commun, une armature montée sur les premier et deuxième éléments de montage, un corps de safran monté coulissant dans l'armature afin d'autoriser un réglage de la profondeur du safran. To this end, the invention relates to a mounting system and rudder assembly for mounting the rudder to the hull of a boat from said mounting system, the mounting system and rudder assembly comprising: a first and a second mounting element by means of which the rudder is intended to be mounted to the hull of the boat, the first and the second mounting element being intended to be mounted movable in rotation with respect to the hull of the boat around an axis of rudder which is common to them, a frame mounted on the first and second mounting elements, a rudder body mounted sliding in the frame to allow adjustment of the depth of the rudder.
Le safran présente un plan porteur, ledit plan porteur étant préférentiellement un plan porteur en T, et le corps de safran porte le plan porteur au niveau de l'une des extrémités dudit corps de safran et le corps de safran étant adapté pour être agencé dans l'armature avec soit le plan porteur orienté vers le haut, c'est-à-dire au-dessus d'une ligne de flottaison du bateau, soit le plan porteur orienté vers le bas, c'est-à-dire au-dessous d'une ligne de flottaison du bateau. The rudder has a carrier plane, said carrier plane being preferably a T-shaped carrier plane, and the rudder body carries the carrier plane at one of the ends of said rudder body and the rudder body being adapted to be arranged in the reinforcement with either the supporting plane oriented upwards, that is to say above a waterline of the boat, or the supporting plane oriented downwards, that is to say above below a waterline of the boat.
De cette manière, avec une telle configuration ; safran peut aisément passer d'une configuration « hydroptère », dans laquelle le plan porteur se trouve sous la ligne de flottaison, à une configuration classique, c'est-à-dire dans laquelle le plan porteur est hors d'eau par un simple changement d'agencement du safran dans l'armature. De plus, avec une telle configuration, le safran peut être utilisé dans les deux configurations du bateau supprimant, de fait, la nécessité de deux safrans distincts. In this way, with such a configuration; rudder can easily switch from a “hydrofoil” configuration, in which the supporting plane is located under the waterline, to a classic configuration, that is to say in which the supporting plane is out of water by a simple change of arrangement of the rudder in the frame. In addition, with such a configuration, the rudder can be used in both configurations of the boat, thereby eliminating the need for two separate rudders.
Le deuxième élément de montage peut être destiné à être agencé le long de l'axe de gouvernail sous le premier élément de montage lorsque le bateau est à flot, le premier élément de montage présentant un axe de pivot le long duquel est destiné à être monté mobile en rotation le safran, l'axe de pivot étant transversal à l'axe de gouvernail, le deuxième élément de montage étant destiné à être assemblé à l'un parmi le safran et la coque par emboîtage élastique. The second mounting member may be intended to be arranged along the rudder axis below the first mounting member when the boat is afloat, the first mounting member having a pivot pin along which is intended to be mounted movable in rotation the rudder, the pivot axis being transverse to the rudder axis, the second mounting element being intended to be assembled to one of the rudder and the hull by elastic fitting.
Le deuxième élément de montage peut être destiné à être assemblé au safran par emboîtage élastique. The second mounting element may be intended to be assembled to the rudder by elastic fitting.
Le système de montage peut comprendre en outre une pièce intermédiaire destinée à être fixée à la coque, et avantageusement au tableau arrière de la coque, et dans lequel le premier et le deuxième élément de montage sont montés mobiles en rotation vis-à-vis de la pièce intermédiaire autour de l'axe de gouvernail. The mounting system may further comprise an intermediate part intended to be fixed to the hull, and advantageously to the transom of the hull, and in which the first and the second mounting element are mounted movable in rotation with respect to the intermediate piece around the rudder axis.
De cette manière seule la pièce intermédiaire peut être spécifique au bateau à équiper les premier et deuxième éléments de montage pouvant être des éléments standard d'un kit d'installation de safran. In this way only the intermediate piece can be specific to the boat to be fitted, the first and second mounting elements can be standard elements of a rudder installation kit.
Le safran peut présenter une portion de profondeur disposée sur une extrémité du safran destinée à être opposée à la coque, et dans laquelle ladite portion de profondeur comprend un élément en matériau déformable, tel qu'un élastomère qui est avantageusement un caoutchouc naturel ou synthétique. The rudder may have a depth portion arranged on one end of the rudder intended to be opposite the hull, and in which said depth portion comprises an element made of deformable material, such as an elastomer which is advantageously a natural or synthetic rubber.
De cette manière, en cas de rencontre d'un objet entraînant le pivotement du safran autour de l'axe de pivot, les risque d'endommagement du safran au niveau de ladite extrémité sont réduits. In this way, in the event of encountering an object causing the rudder to pivot around the pivot axis, the risk of damage to the rudder at said end is reduced.
Par « plan porteur » ou « plans porteurs », il est entendu, ci-dessus et dans le reste de ce document, un élément profilé pour fournir une force de portance au bateau qu'il équipe, de tels éléments sont également connus sous la dénomination « ailes portantes » ou encore « plans sustenteurs », ou, selon la dénomination anglaise plus usuelle « foils » ou « hydrofoils », et équipent les bateaux du type « hydroptère » (ou en anglais « hydrofoil »). By “carrying plane” or “carrying planes”, it is understood, above and in the rest of this document, a profiled element to provide a lift force to the boat that it equips, such elements are also known under the name “wings” bearings” or even “lifting planes”, or, according to the more usual English name “foils” or “hydrofoils”, and equip boats of the “hydrofoil” type (or in English “hydrofoil”).
Avec un tel plan porteur, le safran peut participer à l'élévation du bateau lorsque ce dernier présente une configuration « hydroptère ». With such a supporting plane, the rudder can participate in the elevation of the boat when the latter has a “hydrofoil” configuration.
Conformément à l'invention le corps de safran porte le plan porteur au niveau de l'une des extrémités dudit corps de safran et le corps de safran est adapté pour être agencé dans l'armature avec soit le plan porteur orienté vers le haut, c'est-à-dire au- dessus d'une ligne de flottaison du bateau, soit le plan porteur orienté vers le bas, c'est-à- dire au-dessous de la ligne de flottaison du bateau. In accordance with the invention, the rudder body carries the supporting plane at the level of one of the ends of said rudder body and the rudder body is adapted to be arranged in the frame with either the supporting plane oriented upwards, c that is to say above a waterline of the boat, or the supporting plane oriented downwards, that is to say below the waterline of the boat.
Avec une telle configuration, le safran peut équiper le bateau aussi bien lorsqu'il est configuré pour une navigation « hydroptère » que lorsqu'il est configuré pour une navigation « classique ». With such a configuration, the rudder can equip the boat both when it is configured for “hydrofoil” navigation and when it is configured for “classic” navigation.
L'invention concerne en outre un kit d'installation de plans porteurs pour bateau, notamment à propulsion éolienne, bateau comprenant au moins un élément de structure, le kit d'installation de plans porteurs comprenant un ensemble selon l'invention et au moins un bras de plan porteur destiné à être monté sur l'élément de structure et présentant un plan porteur destiné à être au moins en partie immergé. The invention further relates to a kit for installing supporting planes for a boat, in particular wind-powered, a boat comprising at least one structural element, the kit for installing supporting planes comprising an assembly according to the invention and at least one supporting plane arm intended to be mounted on the structural element and having a supporting plane intended to be at least partly submerged.
L'invention concerne en outre un procédé de montage d'un safran à la coque d'un bateau à partir d'un système selon l'invention, le procédé comprenant les étapes suivantes de : montage sur la coque du premier et du deuxième élément de montage mobiles en rotation vis-à-vis de la coque du bateau autour d'un axe de gouvernail qui leur est commun, le deuxième élément de montage étant agencé le long de l'axe de gouvernail sous le premier élément de montage lorsque le bateau est à flot, montage du safran mobile en rotation autour d'un axe de pivot du premier élément de montage, l'axe de pivot étant transversal à l'axe de gouvernail, le deuxième élément de montage étant assemblé à l'un parmi le safran et la coque par emboîtage élastique. The invention further relates to a method of mounting a rudder to the hull of a boat from a system according to the invention, the method comprising the following steps of: mounting on the hull of the first and the second element mounting elements movable in rotation with respect to the hull of the boat around a rudder axis which is common to them, the second mounting element being arranged along the rudder axis under the first mounting element when the boat is afloat, mounting the movable rudder in rotation around a pivot axis of the first mounting element, the pivot axis being transverse to the rudder axis, the second mounting element being assembled to one of the rudder and the hull by elastic interlocking.
Un tel procédé permet le montage d'un safran à partir d'un système de montage selon l'invention et de bénéficier des avantages qui y sont liés. L'invention concerne en outre un procédé de changement de configuration d'un safran d'un bateau équipé d'un kit d'installation de plan porteurs selon l'invention , le procédé de changement de configuration comprenant les étapes suivantes : retrait du safran de l'armature, passage de l'orientation du safran d'une configuration parmi une configuration dans laquelle le plan porteur orienté vers le haut et une configuration dans laquelle le plan porteur orienté vers le bas, à une autre configuration parmi la configuration dans laquelle le plan porteur orienté vers le haut et la configuration dans laquelle le plan porteur orienté vers le bas, agencement du safran dans l'armature en conservant l'orientation dans laquelle il a été passé. Such a method allows the assembly of a rudder using a mounting system according to the invention and to benefit from the advantages linked thereto. The invention further relates to a method for changing the configuration of a rudder of a boat equipped with a carrier plane installation kit according to the invention, the method for changing the configuration comprising the following steps: removal of the rudder of the frame, passage of the orientation of the rudder from one configuration among a configuration in which the supporting plane oriented upwards and a configuration in which the supporting plane oriented downwards, to another configuration among the configuration in which the supporting plane oriented upwards and the configuration in which the supporting plane oriented downwards, arrangement of the rudder in the frame while maintaining the orientation in which it was passed.
Il peut en outre être prévu une étape de modification d'une configuration de l'au moins un bras de plan porteur de telle manière de faire passer d'une configuration parmi une configuration dans laquelle le deuxième plan porteur est au moins en partie immergé et une configuration dans laquelle le deuxième plan porteur n'est pas immergé à l'autre configuration parmi la configuration dans laquelle le deuxième plan porteur est au moins en partie immergé et la configuration dans laquelle le deuxième plan porteur n'est pas immergé. A step of modifying a configuration of the at least one supporting plane arm can also be provided in such a way as to change from one configuration to a configuration in which the second supporting plane is at least partly immersed and a configuration in which the second supporting plane is not immersed to the other configuration among the configuration in which the second supporting plane is at least partly immersed and the configuration in which the second supporting plane is not immersed.
Brève description des dessins Brief description of the drawings
La présente invention sera mieux comprise à la lecture de la description d'exemples de réalisation, donnés à titre purement indicatif et nullement limitatif, en faisant référence aux dessins annexés sur lesquels : la figure IA illustre une vue de trois-quarts arrière d'un bateau équipé d'un kit d'installation de plans porteurs incluant deux systèmes de montage de safran selon un premier mode de réalisation de l'invention, un bras de plan porteur dudit kit étant installé, l'autre étant en cours d'installation ; la figure IB illustre une vue de trois quarts de côté du bateau illustré sur la figureThe present invention will be better understood on reading the description of exemplary embodiments, given for purely indicative purposes and in no way limiting, with reference to the appended drawings in which: Figure IA illustrates a rear three-quarter view of a boat equipped with a carrier plan installation kit including two rudder mounting systems according to a first embodiment of the invention, one carrier plan arm of said kit being installed, the other being being installed; Figure IB illustrates a three-quarter side view of the boat shown in the figure
IA ; la figure 2 illustre schématiquement le principe d'installation des bras de plan porteur d'un kit selon le premier mode de réalisation de l'invention ; la figure 3 illustre le système de bloc support utilisé dans le cadre de l'installation des bras de plan porteur selon ce premier mode de réalisation ; la figure 4A illustre selon une vue de dessus schématisée le principe de réglage de l'inclinaison d'un bras de plan porteur selon le premier mode de réalisation de l'invention ; la figure 4B illustre selon une vue de côté schématisée le principe du réglage de l'inclinaison d'un bras de plan porteur selon l'invention déjà illustré sur la figure 4A ; la figure 5A illustre le système de montage selon l'invention d'un safran équipant le kit de l'invention ; la figure 5B illustre en vue partielle rapprochée le système de montage de la figure 5A montrant une combinaison d'une liaison pivot et d'un emboîtage en force offrant une fonction de protection du safran ; la figure 5C illustre en vue partielle rapprochée un plan porteur équipant le safran et une portion de profondeur dudit safran ; la figure 5D illustre selon une vue en perspective le safran en montrant la configuration de chacune des extrémités du safran permettant de fournir dans chacune de ses configurations la fonction de guidage qui est la sienne ; la figure 6A illustre selon une vue de dessus le principe de réglage de l'inclinaison d'un bras de plan porteur selon un deuxième mode de réalisation de l'invention ; la figure 6B illustre selon une vue de côté le principe du réglage de l'inclinaison d'un bras de plan porteur selon la variante de l'invention illustrée sur la figure 6A ; la figure 7 illustre un kit d'installation de plans porteurs selon un troisième mode de réalisation équipant un bateau monocoque ; la figure 8A illustre selon une vue de face de trois quarts le montage d'un bras de plan porteur sur une platine mise en œuvre dans le cadre du troisième mode de réalisation de l'invention ; la figure 8B illustre selon une vue de dessous de trois quarts du montage d'un bras de plan porteur illustré sur la figure 8A ; la figure 9A illustre un bateau équipé d'ensemble système de montage et un safran selon l'invention en configuration hydroptère, la figure 9B illustre un bateau équipé d'ensemble système de montage et un safran selon l'invention en configuration « bateau classique ». AI; Figure 2 schematically illustrates the principle of installing the supporting plane arms of a kit according to the first embodiment of the invention; Figure 3 illustrates the support block system used as part of the installation of the support plane arms according to this first embodiment; Figure 4A illustrates in a schematic top view the principle of adjusting the inclination of a supporting plane arm according to the first embodiment of the invention; Figure 4B illustrates in a schematic side view the principle of adjusting the inclination of a supporting plane arm according to the invention already illustrated in Figure 4A; Figure 5A illustrates the mounting system according to the invention of a rudder fitted to the kit of the invention; Figure 5B illustrates in partial close-up view the mounting system of Figure 5A showing a combination of a pivot connection and a force fit offering a rudder protection function; Figure 5C illustrates in partial close-up view a supporting plane fitted to the rudder and a depth portion of said rudder; Figure 5D illustrates in a perspective view the rudder by showing the configuration of each of the ends of the rudder making it possible to provide in each of its configurations its guiding function; Figure 6A illustrates in a top view the principle of adjusting the inclination of a supporting plane arm according to a second embodiment of the invention; Figure 6B illustrates in a side view the principle of adjusting the inclination of a supporting plane arm according to the variant of the invention illustrated in Figure 6A; Figure 7 illustrates a support plane installation kit according to a third embodiment fitted to a monohull boat; Figure 8A illustrates in a three-quarter front view the mounting of a supporting plane arm on a plate implemented within the framework of the third embodiment of the invention; Figure 8B illustrates in a three-quarter bottom view the assembly of a support plane arm illustrated in Figure 8A; Figure 9A illustrates a boat equipped with a mounting system assembly and a rudder according to the invention in a hydrofoil configuration, Figure 9B illustrates a boat equipped with a mounting system assembly and a rudder according to the invention in a “classic boat” configuration .
Des parties identiques, similaires ou équivalentes des différentes figures portent les mêmes références numériques de façon à faciliter le passage d'une figure à l'autre. Identical, similar or equivalent parts of the different figures bear the same numerical references so as to facilitate the transition from one figure to another.
Les différentes parties représentées sur les figures ne le sont pas nécessairement selon une échelle uniforme, pour rendre les figures plus lisibles. The different parts represented in the figures are not necessarily on a uniform scale, to make the figures more readable.
Les différentes possibilités (variantes et modes de réalisation) doivent être comprises comme n'étant pas exclusives les unes des autres et peuvent se combiner entre elles. The different possibilities (variants and embodiments) must be understood as not being exclusive of each other and can be combined with each other.
Exposé détaillé de modes de réalisation particuliers Detailed presentation of particular embodiments
Les figures IA et IB illustrent un bateau 1, ici un catamaran, équipé d'un kit d'installation de plans porteurs 22, 32, 45, 55 incorporant un système de montage de safran selon une possibilité de l'invention afin que ce dernier forme un hydroptère. Figures IA and IB illustrate a boat 1, here a catamaran, equipped with an installation kit for supporting planes 22, 32, 45, 55 incorporating a rudder mounting system according to one possibility of the invention so that the latter forms a hydrofoil.
On notera, bien entendu, que si dans le cadre du présent mode de réalisation, le kit d'installation de plans porteurs 22, 32, 45, 55, et donc le système de montage selon l'invention, équipe un bateau 1 de type catamaran, celui-ci peut être adapté à d'autres types de bateaux, tel qu'un monocoque ou un trimaran, comme cela sera montré dans les modes de réalisation suivants. It will be noted, of course, that if in the context of this embodiment, the installation kit for supporting planes 22, 32, 45, 55, and therefore the mounting system according to the invention, equips a boat 1 of type catamaran, this can be adapted to other types of boats, such as a monohull or a trimaran, as will be shown in the following embodiments.
Le bateau 1 comprend un élément structurel 15, ici l'un des bras de liaison 15, 16, sur lequel est installée une partie du kit d'installation de plans porteurs 22, 32, 45, 55. The boat 1 comprises a structural element 15, here one of the connecting arms 15, 16, on which part of the installation kit for supporting planes 22, 32, 45, 55 is installed.
Un kit d'installation de plans porteurs 22, 32, 45, 55 selon le présent mode de réalisation comporte, comme montré sur la figure 2 : deux blocs supports 21, 31 destinés chacun à être fixé à l'au moins un élément structurel 15, c'est-à-dire l'un des bras de liaison 15, 16 du bateau 1, deux bras de plan porteur 22, 32 présentant chacun un plan porteur 24, 34 destiné à être au moins en partie immergé, chaque bras de plan porteur 22, 32 étant monté sur un bloc support 21, 31 qui lui est respectif, deux safrans chacun équipé d'un plan porteur 45, 55 en T. An installation kit for supporting planes 22, 32, 45, 55 according to the present embodiment comprises, as shown in Figure 2: two support blocks 21, 31 each intended to be fixed to the at least one structural element 15 , that is to say one of the connecting arms 15, 16 of the boat 1, two supporting plane arms 22, 32 each having a supporting plane 24, 34 intended to be at least partly immersed, each supporting plane arm 22, 32 being mounted on a support block 21, 31 which is respective to it, two rudders each equipped with a 45, 55 T-shaped supporting plane.
Il est à noter que, selon une possibilité avantageuse et optionnelle de l'invention, montrée sur la figure 2, le kit d'installation de plans porteurs peut en outre comprendre un système de commande 17 apte à communiquer avec un système de modification de la configuration motorisé, non figuré, et commander ledit système pour adapter l'agencement des bras de plan porteur 22, 32. On notera néanmoins, dans une configuration usuelle de l'invention, l'agencement des bras de plan porteur 22, 32 est ajusté manuellement par un membre de l'équipage du bateau 1. It should be noted that, according to an advantageous and optional possibility of the invention, shown in Figure 2, the installation kit of supporting planes can also include a control system 17 capable of communicating with a system for modifying the motorized configuration, not shown, and control said system to adapt the arrangement of the supporting plane arms 22, 32. Note nevertheless, in a usual configuration of the invention, the arrangement of the supporting plane arms 22, 32 is adjusted manually by a member of the crew of boat 1.
Le bloc support 21, 31 comprend comme le montre la figure 3 : deux pièces d'adaptation 212A, 212B, conformées pour coopérer avec l'élément de structure 15, 13 et être fixées à ce dernier, les pièces d'adaptation fournissant un plan de référence pour le bras de plan porteur 22, une platine 211 sur laquelle est monté le bras de plan porteur 22, la platine 211 étant montée sur les pièces d'adaptation 212A, 212B le long du plan de référence. The support block 21, 31 comprises, as shown in Figure 3: two adaptation parts 212A, 212B, shaped to cooperate with the structural element 15, 13 and be fixed to the latter, the adaptation parts providing a plane reference for the supporting plane arm 22, a plate 211 on which the supporting plane arm 22 is mounted, the plate 211 being mounted on the adaptation parts 212A, 212B along the reference plane.
Comme montré sur la figure 3, dans le présent mode de réalisation, il est prévu deux pièces d'adaptation 212A, 212B consistant en deux demi-coques venant prendre en sandwich l'élément de structure, c'est-à-dire le bras de liaison 15. La première pièce d'adaptation 212A, pièce du « haut », présente une forme en L, tandis que la deuxième pièce d'adaptation 212B, pièce du « bas », présente une forme en U afin de loger au mieux la partie inférieure du bras de liaison 15. Une telle conformation permet aux pièces d'adaptation 212A, 212B, à partir de la forme de la portion du bras de liaison 15 qu'elles logent, de fournir un plan de référence, vis-à-vis de la ligne de flottaison du bateau, pour la platine 211 et donc le bras de plan porteur 22 qui est monté sur la platine 211. Comme montré sur la figure 3, la forme en U de la deuxième pièce d'adaptation 212B forme un logement de manière à stabiliser son placement sur le bras de liaison 15, et celle de la première pièce d'adaptation 212A. On notera que la surface de la première pièce d'adaptation 212A qui est opposée au pont du bateau définit le plan de référence. As shown in Figure 3, in the present embodiment, two adaptation parts 212A, 212B are provided consisting of two half-shells sandwiching the structural element, that is to say the arm connection 15. The first adaptation part 212A, “top” part, has an L shape, while the second adaptation part 212B, “bottom” part, has a U shape in order to best accommodate the lower part of the connecting arm 15. Such a conformation allows the adaptation parts 212A, 212B, from the shape of the portion of the connecting arm 15 which they house, to provide a reference plane, with respect to -screw of the waterline of the boat, for the plate 211 and therefore the supporting plane arm 22 which is mounted on the plate 211. As shown in Figure 3, the U shape of the second adaptation part 212B forms a housing so as to stabilize its placement on the connecting arm 15, and that of the first adaptation part 212A. Note that the surface of the first adaptation part 212A which is opposite the deck of the boat defines the reference plane.
Chacune des première et deuxième pièces d'adaptation est préférentiellement réalisée dans un matériau rigide tel qu'un thermoplastique, un matériau composite ou encore du bois. Each of the first and second adaptation parts is preferably made of a rigid material such as a thermoplastic, a composite material or even wood.
On notera bien entendu, que si dans le présent mode de réalisation, ladite surface de la première pièce d'adaptation 212A matérialise le plan de référence, ce plan peut ne pas présenter de matérialité, puisque par la fourniture d'une surface d'appui, non nécessairement plate, la ou les pièces d'adaptation 212A, 212B permettent d'assurer l'orientation de la platine 211, et donc du bras de plan porteur 22, vis-à-vis de la ligne de flottaison du bateau 1. It will of course be noted that if in the present embodiment, said surface of the first adaptation part 212A materializes the reference plane, this plane may not present materiality, since by the provision of a support surface , not necessarily flat, the adaptation part(s) 212A, 212B make it possible to ensure the orientation of the plate 211, and therefore of the supporting plane arm 22, with respect to the waterline of the boat 1.
Selon une possibilité de l'invention montrée sur la figure 3, la première pièce d'adaptation 212A peut présenter un évidement afin d'autoriser le placement d'un système de réglage 213 de l'orientation du bras de plan porteur 22 sur la platine, ledit système de réglage 213 comprenant un ensemble d'engrenage afin de permettre un réglage d'hauteur de la ou des rotules 215, 216, illustrées sur les figures 4A et 4B. According to one possibility of the invention shown in Figure 3, the first adaptation part 212A can have a recess in order to authorize the placement of an adjustment system 213 of the orientation of the supporting plane arm 22 on the plate , said adjustment system 213 comprising a gear assembly to allow height adjustment of the ball joint(s) 215, 216, illustrated in Figures 4A and 4B.
Conformément à la figure 3, dans le présent mode de réalisation, la platine 211 présente une complémentarité de forme avec les pièces d'adaptation 212A, 212B. Ainsi, la platine 211 présente une forme en U avec les deux branches du U qui définissent un logement conformé pour recevoir les pièces d'adaptation 212A, 212B. La fixation de la platine 211 sur les pièces d'adaptation 212A, 212B se fait par emboîtage élastique et par translation suivant l'axe du bras de liaison du bateau. La platine 211 permettant ainsi d'assurer une bonne fixation des pièces d'adaptation 212A, 212B sur le bras de liaison 15. On notera bien entendu, qu'un tel emboîtage élastique n'est qu'un exemple de montage de la platine 211 sur les pièces d'adaptation, tout autre montage, tel qu'un vissage, un rivetage ou une soudure peuvent être envisagés. On notera néanmoins que dans le cadre de l'invention, un montage démontable est à préférer. In accordance with Figure 3, in the present embodiment, the plate 211 has a complementary shape with the adaptation parts 212A, 212B. Thus, the plate 211 has a U shape with the two branches of the U which define a housing shaped to receive the adaptation parts 212A, 212B. The fixing of the plate 211 on the adaptation parts 212A, 212B is done by elastic fitting and by translation along the axis of the connecting arm of the boat. The plate 211 thus makes it possible to ensure good fixing of the adaptation parts 212A, 212B on the connecting arm 15. It will of course be noted that such elastic fitting is only an example of mounting the plate 211 on the adaptation parts, any other assembly, such as screwing, riveting or welding can be considered. It should nevertheless be noted that in the context of the invention, a removable assembly is to be preferred.
Chaque platine est préférentiellement réalisée dans un matériau rigide tel qu'un thermoplastique, un matériau composite, du bois ou encore du métal et notamment l'inox. Chaque bras de plan porteur 22, 32 comprend, comme montré sur les figures IA et IB, comprend un bras de fixation 23, 33 par lequel le bras de plan porteur 22, 32 est monté sur la platine 211, et un plan porteur 24, 34 en tant que tel qui, en étant fixé à une extrémité du bras de fixation 23, 33, est destiné à être au moins en partie immergé. Le plan porteur 24, 34 est profilé afin de fournir une force de portance lorsque le bateau 1 se déplace. Bien entendu, si dans le présent mode de réalisation, le bras support 23, 33 et le plan porteur 24, 34 sont distincts l'un de l'autre, il est envisageable de fournir un bras de plan porteur 22, 32 monobloc avec le bras support 23, 33 et le plan porteur 24, 34 qui sont alors formés solidaires l'un à l'autre. Each plate is preferably made of a rigid material such as a thermoplastic, a composite material, wood or even metal and in particular stainless steel. Each support plane arm 22, 32 comprises, as shown in Figures IA and IB, comprises a fixing arm 23, 33 by which the support plane arm 22, 32 is mounted on the plate 211, and a support plane 24, 34 as such which, by being fixed to one end of the fixing arm 23, 33, is intended to be at least partly submerged. The supporting plane 24, 34 is profiled in order to provide a lift force when the boat 1 moves. Of course, if in the present embodiment, the support arm 23, 33 and the support plane 24, 34 are distinct from each other, it is possible to provide a one-piece support plane arm 22, 32 with the support arm 23, 33 and the supporting plane 24, 34 which are then formed integral with each other.
Chaque bras de plan porteur 22, 32 peut être monté sur la platine 211 correspondante à partir d'au moins deux rotules 215, 216, 217. Dans ce premier mode de réalisation, comme montré sur les figures 4A et 4B, chaque bras de plan porteur 22, 32 est monté sur la platine 211 correspondante à partir d'une première et deuxième rotules 215, 216 situées de part et d'autre du bras de plan porteur afin de définir une première liaison pivot et d'une autre rotule 217 qui est disposée à une extrémité du bras de plan porteur 22, 32 qui est libre de plan porteur 24, 34 ceci avec un décalage latéral pour définir une deuxième liaison pivot avec la deuxième rotule 216. La première rotule 215 est montée déplaçable en translation vis-à-vis de la platine 211 afin de permettre un réglage de la « hauteur » de la première rotule 215. De cette manière, un réglage de sa hauteur, à partir du système de réglage 213, permet au bras de plan porteur 22, 32 de pivoter autour de la deuxième liaison pivot et ainsi de régler l'orientation des plans porteurs vis-à-vis du bras de liaison 15 et donc du bateau 1. On notera que selon une possibilité de l'invention, la troisième rotule 217 peut être démontable de telle manière à permettre le bras de plan porteur de pivoter autour d'un axe défini par la première et la deuxième rotule 215, 216 lorsqu'il est démonté de la troisième rotule 217. Each supporting plane arm 22, 32 can be mounted on the corresponding plate 211 from at least two ball joints 215, 216, 217. In this first embodiment, as shown in Figures 4A and 4B, each plane arm carrier 22, 32 is mounted on the corresponding plate 211 from a first and second ball joints 215, 216 located on either side of the supporting plane arm in order to define a first pivot connection and another ball joint 217 which is arranged at one end of the supporting plane arm 22, 32 which is free from the supporting plane 24, 34 this with a lateral offset to define a second pivot connection with the second ball joint 216. The first ball joint 215 is mounted movable in translation vis- with respect to the plate 211 in order to allow adjustment of the “height” of the first ball joint 215. In this way, an adjustment of its height, from the adjustment system 213, allows the supporting plane arm 22, 32 to pivot around the second pivot connection and thus to adjust the orientation of the supporting planes with respect to the connecting arm 15 and therefore the boat 1. It will be noted that according to one possibility of the invention, the third ball joint 217 can be dismountable in such a way as to allow the supporting plane arm to pivot around an axis defined by the first and second ball joints 215, 216 when it is disassembled from the third ball joint 217.
Comme également montré sur les figures 4A et 4B, il peut être prévu un support complémentaire 214, par exemple agencé sur un pont du bateau 1, complémentaire afin de fournir un point de fixation supplémentaire du bras de plan porteur 22, 32. Selon cette possibilité, le bras de plan porteur 22, 32 peut être fixé à ce support complémentaire 214 à partir d'une liaison pivot glissante telle que fournie, par exemple et comme illustré par les figures 4A et 4B, à partir d'une sangle 214A attachant le bras de plan porteur 22, 32 audit support complémentaire 214. As also shown in Figures 4A and 4B, a complementary support 214 can be provided, for example arranged on a deck of the boat 1, complementary in order to provide an additional fixing point for the supporting plane arm 22, 32. According to this possibility , the supporting plane arm 22, 32 can be fixed to this complementary support 214 from a sliding pivot connection as provided, by example and as illustrated by Figures 4A and 4B, from a strap 214A attaching the supporting plane arm 22, 32 to said complementary support 214.
Comme montré sur les figures IA et IB, le kit d'installation de plans porteurs 22, 32, 45, 55 selon le présent mode de réalisation comprend également deux safrans 44, 54 chacun équipés d'un plan porteur 45, 55 en T. Afin de permettre de manœuvrer le bateau 1, chacun des safrans se prolonge par une barre 42, 52 qui lui est respective. As shown in Figures IA and IB, the installation kit for carrier planes 22, 32, 45, 55 according to the present embodiment also includes two rudders 44, 54 each equipped with a T-shaped carrier plane 45, 55. In order to allow the boat 1 to be maneuvered, each of the rudders is extended by a bar 42, 52 which is respective to it.
Par plan porteur en T, on entend ci-dessus que le plan porteur 45, 55 comprend deux profiles s'étendant dans le prolongement l'un de l'autre et de part et d'autre du corps de safran formant ainsi la barre haute d'un « T » majuscule avec le corps du safran qui forme le corps du T. By T-shaped supporting plane, we mean above that the supporting plane 45, 55 comprises two profiles extending in the extension of one another and on either side of the rudder body thus forming the high bar of a capital “T” with the body of the rudder which forms the body of the T.
Selon une possibilité de l'invention illustrée sur les figures 5A et 5B, chaque safran 44, 54 est monté sur une coque 11, 12 respective du bateau 1, et plus précisément sur le tableau arrière desdites coques 11, 12, au moyen d'un système de montage 43. Le système de montage 43 comprend une pièce intermédiaire 431 fixée au tableau arrière, et un premier et un deuxième élément de montage 432, 433 par l'intermédiaire desquels le safran 44, 54 est monté à la coque 11, 12 du bateau 1, le premier et le deuxième élément de montage 432, 433 sont montés mobiles en rotation vis-à-vis de la pièce intermédiaire 431, et donc de la coque du bateau, autour d'un axe de gouvernail qui leur est commun. Le deuxième élément de montage 433 est agencé le long de l'axe de gouvernail sous le premier élément de montage 432 lorsque le bateau 1 est à flot. According to one possibility of the invention illustrated in Figures 5A and 5B, each rudder 44, 54 is mounted on a respective hull 11, 12 of the boat 1, and more precisely on the transom of said hulls 11, 12, by means of a mounting system 43. The mounting system 43 comprises an intermediate part 431 fixed to the transom, and a first and a second mounting element 432, 433 by means of which the rudder 44, 54 is mounted to the hull 11, 12 of the boat 1, the first and the second mounting element 432, 433 are mounted movable in rotation with respect to the intermediate part 431, and therefore to the hull of the boat, around a rudder axis which is attached to them. common. The second mounting element 433 is arranged along the rudder axis below the first mounting element 432 when the boat 1 is afloat.
On notera que, selon le principe similaire aux pièces d'adaptation 212A, 212B, la pièce intermédiaire 431 est adaptée en fonction de la forme du tableau arrière à équiper. Ainsi, dans le kit, pour permettre l'installation de chaque safran, seule la pièce intermédiaire 431 a à être adaptée au bateau 1 à équiper, les autres éléments concernant le safran dont notamment les premier et deuxième éléments de montage peuvent être standardisés. Note that, according to the principle similar to the adaptation parts 212A, 212B, the intermediate part 431 is adapted according to the shape of the transom to be equipped. Thus, in the kit, to allow the installation of each rudder, only the intermediate part 431 has to be adapted to the boat 1 to be equipped, the other elements concerning the rudder including in particular the first and second mounting elements can be standardized.
Selon une variante de l'invention les premier et les deuxième éléments de montage 432, 433 peuvent être adaptés au bateau 1 qu'ils équipent, les premier et deuxième éléments de montage 432, 433 étant alors directement montés sur la coque 11, 12 (ou dans le présent cas au tableau arrière de ladite coque) autour d'un axe de gouvernail. According to a variant of the invention, the first and second mounting elements 432, 433 can be adapted to the boat 1 which they equip, the first and second mounting elements 432, 433 then being directly mounted on the hull 11, 12 (or in this case at the transom of said hull) around a rudder axis.
Le premier élément de montage 432 présente un axe de pivot 432A le long duquel est monté mobile en rotation le safran 44, l'axe de pivot 432A étant transversal à l'axe de gouvernail et est, préférentiellement et plus précisément, sensiblement perpendiculaire à Taxe de gouvernail. Plus spécifiquement, le premier élément 432 présente sur une première portion un orifice traversant dans lequel passe l'axe de gouvernail (mèche ou aiguillot, en fonction de la configuration safran, comme cela est discuté ci-après) et sur une deuxième portion deux autres orifices par lesquels passe l'axe de pivot 432A. L'axe de pivot 432A est transversal vis-à-vis de l'axe de gouvernail. The first mounting element 432 has a pivot axis 432A along which the rudder 44 is movably mounted in rotation, the pivot axis 432A being transverse to the rudder axis and is, preferably and more precisely, substantially perpendicular to the axis. rudder. More specifically, the first element 432 has on a first portion a through orifice in which the rudder axis passes (lock or needle, depending on the rudder configuration, as discussed below) and on a second portion two others orifices through which the pivot pin 432A passes. The pivot pin 432A is transverse to the rudder pin.
Le deuxième élément de montage 433 est assemblé à l'un parmi le safran 44 et la coque 11 (au travers de la pièce intermédiaire 431), ici le safran 44, par emboîtage élastique. Bien entendu, selon une variante non illustrée, l'élément de montage 433 peut être assemblé pièce intermédiaire 431, donc la coque, par encliquetage élastique, cet encliquetage élastique permettant alors également de fournir un montage mobile en rotation autour de l'axe de gouvernail. Pour permettre un tel montage élastique, le deuxième élément de montage 433 présente sur une première portion un orifice traversant dans lequel passe l'axe de gouvernail et sur une deuxième portion comprenant deux bras présentant chacun une languette en porte à faux, les bras définissant ensemble un espace d'accueil pour un organe de fixation du safran 44 présentant préférentiellement une face en dépouille. The second mounting element 433 is assembled to one of the rudder 44 and the hull 11 (through the intermediate piece 431), here the rudder 44, by elastic fitting. Of course, according to a variant not illustrated, the mounting element 433 can be assembled intermediate piece 431, therefore the hull, by elastic snap-fastening, this elastic snap-fastening then also making it possible to provide a movable assembly in rotation around the rudder axis . To allow such elastic mounting, the second mounting element 433 has on a first portion a through orifice through which the rudder axis passes and on a second portion comprising two arms each having a cantilevered tongue, the arms together defining a reception space for a rudder fixing member 44 preferably having a relief face.
On notera que si le premier et le deuxième élément de montage 432, 433 sont fournis sous la forme de deux pièces indépendantes, il est également envisageable, sans que l'on sorte du cadre de l'invention, que les premier et deuxième éléments de montage 432, 433 soient fournis sous la forme d'une unique pièce. De même, si les premier et deuxième éléments 432, 433 sont montés dans le présent mode de réalisation, pivotant autour de l'axe de gouvernail formant la mèche de gouvernail, il est également possible que les premier et deuxième éléments 432, 433 soient montés sur la pièce intermédiaire 431, voire la coque, au moyen d'un aiguillot respectif, le premier et le deuxième élément formant alors chacun un femelot. Selon une possibilité non illustrée, le premier élément 432 peut être monté démontable sur la coque, ceci en rendant le premier élément 432 libre de pivoter autour de l'axe de pivot 432A et de se désengager de l'axe de gouvernail, ou mèche. De cette manière, lorsque l'utilisateur souhaite retirer le safran afin de le stocker, il peut désengager le premier élément et déboiter le deuxième élément de sa fixation par emboîtage élastique de manière à désolidariser le safran 44, 54 de la coque 11, 12. It will be noted that if the first and second mounting elements 432, 433 are provided in the form of two independent parts, it is also possible, without departing from the scope of the invention, that the first and second elements of assembly 432, 433 are supplied in the form of a single part. Likewise, if the first and second elements 432, 433 are mounted in the present embodiment, pivoting around the rudder axis forming the rudder stock, it is also possible that the first and second elements 432, 433 are mounted on the intermediate piece 431, or even the hull, by means of a respective needle, the first and the second element then each forming a femelot. According to a possibility not illustrated, the first element 432 can be mounted removable on the hull, this making the first element 432 free to pivot around the pivot axis 432A and to disengage from the rudder axis, or rudder. In this way, when the user wishes to remove the rudder in order to store it, he can disengage the first element and disengage the second element from its attachment by elastic engagement so as to separate the rudder 44, 54 from the hull 11, 12.
Le safran 44, comme le montre la figure 5A, comprend : une armature 442 par laquelle le safran 44 est monté sur les premier et deuxième éléments de montage 432, 433, corps de safran 441 monté coulissant dans l'armature 442 afin d'autoriser un réglage de la profondeur du safran 44, un système de sécurisation, tel qu'une goupille, en position du corps de safran 441 sur l'armature 442, non montré. The rudder 44, as shown in Figure 5A, comprises: a frame 442 by which the rudder 44 is mounted on the first and second mounting elements 432, 433, rudder body 441 slidably mounted in the frame 442 in order to allow an adjustment of the depth of the rudder 44, a securing system, such as a pin, in the position of the rudder body 441 on the frame 442, not shown.
L'armature 442, présente une première et une deuxième extension, s'étendant en direction de la coque 11, 12, à partir desquelles l'armature est respectivement montée sur le premier et le deuxième élément de montage 432, 433. La première extension est montée pivotante autour de l'axe de pivot 432A. La deuxième extension forme l'organe de fixation et présente préférentiellement, comme montré sur la figure 5B et en direction de la coque 11 : deux gorges s'étendant de part et d'autre de la deuxième extension selon une direction parallèle à l'axe de gouvernail, configurées pour accueillir chacune une languette en porte à faux respective du deuxième élément de montage 433, une face en dépouille, pour faciliter l'introduction du deuxième organe dans l'espace d'accueil défini par le deuxième élément de montage. The frame 442 has a first and a second extension, extending towards the shell 11, 12, from which the frame is respectively mounted on the first and the second mounting element 432, 433. The first extension is pivotally mounted around the pivot axis 432A. The second extension forms the fixing member and preferably presents, as shown in Figure 5B and towards the shell 11: two grooves extending on either side of the second extension in a direction parallel to the axis rudder, configured to each accommodate a respective cantilevered tongue of the second mounting element 433, a flush face, to facilitate the introduction of the second member into the reception space defined by the second mounting element.
Avec un tel montage du safran 44 sur la coque du bateau, lorsque le safran rencontre un obstacle, tel que le fond ou un rocher ou un objet flottant non identifié, les efforts s'appliquant sur le safran 44 en raison de cette rencontre vont entraîner un déboitement de la deuxième extension vis-à-vis du deuxième élément de montage 433 et un pivotement du safran 44 autour de l'axe de pivot 432A selon une direction opposée au déplacement du bateau 1 permettant ainsi de limiter les risques d'endommagement du safran 44. With such mounting of the rudder 44 on the hull of the boat, when the rudder encounters an obstacle, such as the bottom or a rock or an unidentified floating object, the forces applying to the rudder 44 due to this encounter will cause a dislocation of the second extension with respect to the second mounting element 433 and a pivoting of the rudder 44 around the pivot axis 432A in a direction opposite to the movement of the boat 1 thus making it possible to limit the risks of damage to the rudder 44.
Dans le cadre du présent mode de réalisation et de l'invention, le corps de safran 441 présente un plan porteur 45 ici en T. Bien entendu, si un tel plan porteur 45 est lié à l'utilisation d'un système de montage dans le cadre d'un kit d'installation de plans porteurs 22, 32, 45, 55, un tel système de montage 43 de safran est parfaitement utilisable, selon une possibilité non comprise dans le cadre de l'invention, pour le montage d'un safran simple ne comportant pas de plan porteur ou n'utilisant pas une armature 442 puisqu'un tel système de montage offre à la fois une fonction de protection et une facilité de manipulation de ce dernier, peu importe sa configuration. In the context of the present embodiment and the invention, the rudder body 441 has a supporting plane 45 here in a T shape. Of course, if such a supporting plane 45 is linked to the use of a mounting system in the frame of a kit for installing carrier planes 22, 32, 45, 55, such a rudder mounting system 43 is perfectly usable, according to a possibility not included in the scope of the invention, for the assembly of a simple rudder not having a supporting plane or not using a frame 442 since such a mounting system offers both a protective function and ease of handling of the latter, regardless of its configuration.
Afin de permettre de régler l'inclinaison des plans porteurs 45, 55 équipant les safrans 44, 54, dans le cadre de l'invention, il est possible de prévoir un système de réglage d'incidence de plan porteur non montré. Un tel système de réglage d'incidence peut être accessible sur la barre 32, 42 associée audit safran 44 ou encore directement accessible sur le safran 44, le réglage se faisant alors soit à terre, soit en relevant le safran 44. In order to allow the inclination of the carrier planes 45, 55 fitted to the rudders 44, 54 to be adjusted, in the context of the invention, it is possible to provide a system for adjusting the incidence of the carrier plane, not shown. Such an angle of attack adjustment system can be accessible on the bar 32, 42 associated with said rudder 44 or even directly accessible on the rudder 44, the adjustment then being made either on the ground or by raising the rudder 44.
Comme montré sur la figure 5C, selon une possibilité de l'invention particulièrement avantageuse dans le cadre d'un tel système de montage, le safran 44 peut comporter une portion de profondeur 443 disposée sur une extrémité du safran 44 destinée à être opposée à la coque et à l'avant de ce dernier, dans un sens de déplacement du bateau 1. La portion de profondeur 443 comprend un élément en matériau déformable, tel qu'un élastomère pouvant être, par exemple, un caoutchouc naturel ou synthétique. Une telle portion de profondeur 443 comprenant un matériau déformable, tel qu'un élastomère, permet d'absorber une partie des efforts s'exerçant sur le safran 44 lorsque ce dernier rencontre un obstacle. As shown in Figure 5C, according to a particularly advantageous possibility of the invention in the context of such a mounting system, the rudder 44 can comprise a portion of depth 443 arranged on one end of the rudder 44 intended to be opposite the hull and at the front of the latter, in a direction of movement of the boat 1. The depth portion 443 comprises an element made of deformable material, such as an elastomer which can be, for example, a natural or synthetic rubber. Such a depth portion 443 comprising a deformable material, such as an elastomer, makes it possible to absorb part of the forces exerted on the rudder 44 when the latter encounters an obstacle.
Selon l'invention, comme cela sera discuté en lien avec les figures 9A et 9B, le corps de safran 441 présente deux orientations d'installation dans l'armature 442, l'une avec le plan porteur 45 agencé sur le bas du safran 44, c'est-à-dire sous la ligne de flottaison du bateau, et l'autre avec le plan porteur agencé sur le haut du safran 44, c'est- à-dire au-dessus de la ligne de flottaison. De cette manière, avec un tel corps de safran 441, le safran 44 peut aussi bien être utilisé dans le cadre d'une configuration hydroptère, c'est- à-dire avec le plan porteur 45 agencé sur le bas du safran 44 que dans une configuration classique, c'est-à-dire avec le plan porteur 45 agencé sur le haut du safran 44. Pour cela, comme cela est montré sur la figure 5D, la forme du corps de safran peut être adapté avec chaque extrémité 441A, 441B du corps qui est configurée pour fournir la fonction de guidage du bateau qui est la sienne. According to the invention, as will be discussed in connection with Figures 9A and 9B, the rudder body 441 has two installation orientations in the frame 442, one with the supporting plane 45 arranged on the bottom of the rudder 44 , that is to say below the waterline of the boat, and the other with the supporting plane arranged on the top of the rudder 44, that is to say above the waterline. In this way, with such a 441 rudder body, the rudder 44 can be used as part of a hydrofoil configuration, that is to say with the supporting plane 45 arranged on the bottom of the rudder 44, as in a classic configuration, that is to say with the supporting plane 45 arranged on the top of the rudder 44. For this, as shown in Figure 5D, the shape of the rudder body can be adapted with each end 441A, 441B of the body which is configured to provide the guiding function of the boat that is his.
On notera que, conformément à la possibilité illustrée sur la figure 5C non reprise sur la figure 5D, l'extrémité 441A du safran 44 non équipée de plan porteur (celle dédiée à la configuration « bateau classique ») peut également être pourvu d'un élément en matériau déformable, tel qu'un élastomère pouvant être, par exemple, un caoutchouc naturel ou synthétique. It will be noted that, in accordance with the possibility illustrated in Figure 5C not shown in Figure 5D, the end 441A of the rudder 44 not equipped with a supporting plane (that dedicated to the "classic boat" configuration) can also be provided with a element made of deformable material, such as an elastomer which may be, for example, a natural or synthetic rubber.
On notera que pour faciliter le réglage de l'orientation du safran, la barre 42, 52 peut être fixée à l'armature 442. De cette manière, il n'est pas nécessaire de la monter/démonter lors du changement d'orientation du safran 44. Note that to facilitate adjustment of the orientation of the rudder, the bar 42, 52 can be fixed to the frame 442. In this way, it is not necessary to assemble/disassemble it when changing the orientation of the rudder. rudder 44.
Selon une telle variante, il peut être prévu un procédé de changement d'orientation du safran comprenant les étapes suivantes : désengagement du deuxième élément de montage 433 de son emboîtage élastique ceci afin de permettre un pivotement de l'armature autour de l'axe de pivot 432A, pivotement du safran 44 autour de l'axe de pivot 432A afin de le mettre à une orientation proche de l'horizontal et retrait du système de sécurisation afin d'autoriser le glissement du corps de safran 441 dans l'armature 442, retrait du corps de safran 441 de l'armature 442 et retournement de ce dernier afin d'en changer l'orientation, installation du corps de safran 441 dans l'armature 442 avec la nouvelle orientation, sécurisation du positionnement du corps de safran 441 dans l'armature 442 par une réinstallation du système de sécurisation. On notera que dans le cadre de l'invention, un kit d'installation de plans porteurs 22, 32, 45, 55 selon ce premier mode de réalisation peut être installé selon un procédé d'installation comprenant les étapes suivantes : fixation des deux pièces d'adaptations 212 sur l'élément de structure 15, c'est-à-dire le bras de liaison 15, fixation de chacune des platines 211 sur la pièce d'adaptation 212 correspondante le long du plan de référence définie par cette dernière, chaque pièce d'adaptation 212 et la platine 211 correspondante participant à la formation du bloc support 21, 31 correspondant, montage de chacun des bras de plan porteur 22, 32 sur la platine 211 respective, montage, pour chacun des safrans 44, 54 et sur la coque 11, 12 correspondante, du premier et du deuxième élément de montage 432, 433 mobiles en rotation vis-à-vis de la coque 11, 12 du bateau 1 correspondante autour d'un axe de gouvernail qui est commun auxdits éléments de montage 432, 433 ceci au moyen de la pièce intermédiaire 431, le deuxième élément de montage 433 correspondant audit safran 44, 54 étant agencé le long de l'axe de gouvernail sous le premier élément de montage 432 correspondant lorsque le bateau 1 est à flot, montage de chaque safran 44, 54 mobile en rotation autour de l'axe de pivot 432A du premier élément correspondant 432, ledit axe de pivot 432A étant transversal à l'axe de gouvernail correspondant, chaque deuxième élément de montage étant assemblé au safran par emboîtage élastique. According to such a variant, a method of changing the orientation of the rudder can be provided comprising the following steps: disengagement of the second mounting element 433 from its elastic fitting in order to allow pivoting of the frame around the axis of pivot 432A, pivoting of the rudder 44 around the pivot axis 432A in order to bring it to an orientation close to horizontal and removal of the securing system in order to allow the rudder body 441 to slide in the frame 442, removal of the rudder body 441 from the frame 442 and turning of the latter in order to change its orientation, installation of the rudder body 441 in the frame 442 with the new orientation, securing the positioning of the rudder body 441 in the frame 442 by reinstalling the security system. It will be noted that in the context of the invention, an installation kit for supporting planes 22, 32, 45, 55 according to this first embodiment can be installed according to an installation method comprising the following steps: fixing the two parts adaptations 212 on the structural element 15, that is to say the connecting arm 15, fixing of each of the plates 211 on the corresponding adaptation part 212 along the reference plane defined by the latter, each adaptation part 212 and the corresponding plate 211 participating in the formation of the corresponding support block 21, 31, mounting of each of the supporting plane arms 22, 32 on the respective plate 211, assembly, for each of the rudders 44, 54 and on the corresponding hull 11, 12, of the first and second mounting elements 432, 433 movable in rotation with respect to the hull 11, 12 of the corresponding boat 1 around a rudder axis which is common to said elements of mounting 432, 433 this by means of the intermediate piece 431, the second mounting element 433 corresponding to said rudder 44, 54 being arranged along the rudder axis under the first mounting element 432 corresponding when the boat 1 is afloat , mounting of each rudder 44, 54 movable in rotation around the pivot axis 432A of the first corresponding element 432, said pivot axis 432A being transverse to the corresponding rudder axis, each second mounting element being assembled to the rudder by elastic interlocking.
Les figures 6A et 6B illustrent le montage d'un bras de plan porteur 22 selon un deuxième mode de réalisation. Un kit d'installation de plans porteurs 22, 32, 45, 55 selon ce deuxième mode de réalisation se différencie d'un kit d'installation de plan porteur 22, 32, 44, 55 selon le premier mode de réalisation en ce que le bras de plan porteur 22 est monté sur la platine 211 à partir de la première et de la deuxième rotule 215, 216 qui sont toutes deux mobiles en translation vis-à-vis de la platine 211, la platine étant dénuée de troisième rotule 217 et en ce que le bras de plan porteur 22 est fixé au support complémentaire 214 à partir d'une liaison pivot glissante fournie par une sangle 214A attachant le bras de plan porteur 22 audit support complémentaire 214. Figures 6A and 6B illustrate the assembly of a supporting plane arm 22 according to a second embodiment. A support plane installation kit 22, 32, 45, 55 according to this second embodiment differs from a support plane installation kit 22, 32, 44, 55 according to the first embodiment in that the supporting plane arm 22 is mounted on the plate 211 from the first and the second ball joint 215, 216 which are both movable in translation with respect to the plate 211, the plate being devoid of third ball joint 217 and in that the supporting plane arm 22 is fixed to the support complementary 214 from a sliding pivot connection provided by a strap 214A attaching the supporting plane arm 22 to said complementary support 214.
Dans ce deuxième mode de réalisation et pour chaque bras de plan porteur 22, 32, la première et la deuxième rotule 215, 216, en équipant l'extrémité dudit bras de plan porteur 22, 32 libre de plan porteur, définissent ensemble un axe de pivotement du bras de plan porteur 22, 32 vis-à-vis de l'élément de structure 15. In this second embodiment and for each supporting plane arm 22, 32, the first and second ball joint 215, 216, by equipping the end of said supporting plane arm 22, 32 free of the supporting plane, together define an axis of pivoting of the supporting plane arm 22, 32 with respect to the structural element 15.
De cette manière, lorsque chaque bras de plan porteur 22, 32 est libéré de la sangle 214A qui fournit la liaison pivot glissant au support complémentaire 214, ledit bras de plan porteur 22, 32 est à même de basculer vis-à-vis de l'élément de structure, ici le bras de liaison 15 et ainsi être relevé hors de l'eau. Un tel basculement permet de limiter les contraintes de manipulation du bateau 1 lorsqu'il est ramené à terre pour son rangement ou en cas gros temps non compatible avec une configuration hydroptère. In this way, when each supporting plane arm 22, 32 is released from the strap 214A which provides the sliding pivot connection to the complementary support 214, said supporting plane arm 22, 32 is able to tilt with respect to the structural element, here the connecting arm 15 and thus be raised out of the water. Such tilting makes it possible to limit the handling constraints of the boat 1 when it is brought ashore for storage or in heavy weather not compatible with a hydrofoil configuration.
Les figures 7 à 8B illustrent un bateau 1 monocoque équipé d'un kit d'installation de plans porteurs selon un troisième mode de réalisation. Un kit d'installation de plans porteurs 22, 32, 45, 55 selon ce troisième mode de réalisation se différencie d'un kit d'installation de plans porteurs 22, 32, 45, 55 selon le deuxième mode de réalisation en ce qu'il est prévu une unique pièce d'adaptation 212 et une unique platine 211 formant un unique bloc support sur lequel sont montés les deux bras de plan porteur 22, 32, en ce que le pont 13 du bateau 1 forme l'élément de structure, en ce que les plans porteurs 34 bras de plan porteur 22, 32 sont des plans porteurs en T et en ce que la fixation de la pièce d'adaptation sur le pont 13 est obtenue au moyen d'une sangle 218 passant par la pièce d'adaptation 212 et faisant le tour de la coque 11. Figures 7 to 8B illustrate a monohull boat 1 equipped with a support plane installation kit according to a third embodiment. An installation kit for supporting planes 22, 32, 45, 55 according to this third embodiment differs from an installation kit for supporting planes 22, 32, 45, 55 according to the second embodiment in that a single adaptation part 212 and a single plate 211 are provided forming a single support block on which the two supporting plane arms 22, 32 are mounted, in that the deck 13 of the boat 1 forms the structural element, in that the supporting planes 34 bearing plane arms 22, 32 are T-shaped supporting planes and in that the fixing of the adaptation part on the bridge 13 is obtained by means of a strap 218 passing through the part d adaptation 212 and going around the hull 11.
On notera que cette sangle 218, comme montré sur la figure 7, dans ce troisième mode de réalisation dans lequel le kit d'installation de plans porteurs équipe un bateau 1 monocoque, peut venir en appui sur la quille 14 de telle manière à améliorer la fixation de la pièce d'adaptation sur le pont 13. La pièce d'adaptation 212 et la platine 211 s'étendent sur toute la largeur du pont 13. It will be noted that this strap 218, as shown in Figure 7, in this third embodiment in which the support plan installation kit equips a monohull boat 1, can come to bear on the keel 14 in such a way as to improve the fixing the adaptation part on the bridge 13. The adaptation part 212 and the plate 211 extend over the entire width of the bridge 13.
Les figures 8A et 8B montrent le montage de chacun des bras de plan porteur 22, 32 sur l'unique platine 211. On peut ainsi voir que dans ce troisième mode de réalisation, d'une manière similaire au deuxième mode de réalisation, chaque bras de plan porteur 22, 32 est monté sur la platine 211 à l'aide d'une première et d'une deuxième rotule 215, 216 agencées à une extrémité du bras de plan porteur 22, 32 qui est libre de plan porteur en définissant ensemble un axe de pivotement, qui est ici fourni au moyen d'un pivot 216A reliant la première et la deuxième rotule 215, 216. Bien entendu, un tel pivot 216A, comme c'est le cas pour le deuxième mode de réalisation, n'est pas nécessaire et les première et deuxième rotules 215, 216 sont aptes à fournir un tel montage sans que le pivot soit nécessaire. Figures 8A and 8B show the mounting of each of the supporting plane arms 22, 32 on the single plate 211. It can thus be seen that in this third embodiment, in a manner similar to the second embodiment, each arm of plan carrier 22, 32 is mounted on the plate 211 using a first and a second ball joint 215, 216 arranged at one end of the carrier plane arm 22, 32 which is free from the carrier plane by together defining an axis pivoting, which is here provided by means of a pivot 216A connecting the first and second ball joints 215, 216. Of course, such a pivot 216A, as is the case for the second embodiment, is not necessary and the first and second ball joints 215, 216 are capable of providing such mounting without the pivot being necessary.
D'une manière identique au deuxième mode de réalisation, la première et la deuxième rotule 215, 216 sont toutes deux mobiles en translation vis-à-vis de la platine 211. Pour ce faire, le système de réglage 213 comprend deux engrenages, non référencés, engrainés ensemble et solidaires en rotation de respectivement la première et la deuxième rotule 215, 216. Comme montré sur la figure 8B, l'un des engrenages est muni d'une poulie destinée à être couplée avec un winch, non montré, par l'utilisation d'une courroie, non montrée. En variante, la poulie peut être actionnée manuellement par un simple cordage maintenu sous tension faisant office de courroie. De cette manière, une manipulation du winch permet d'entrainer en rotation les deux engrenages selon un mouvement contrarotatif ce qui entraine à son tour un déplacement de la première et la deuxième rotule 215, 216 vis-à-vis de la platine 211 qui est opposée l'une de l'autre et donc un pivotement du bras de plan porteur 22, 32. In a manner identical to the second embodiment, the first and the second ball joint 215, 216 are both movable in translation with respect to the plate 211. To do this, the adjustment system 213 comprises two gears, not referenced, geared together and integral in rotation with respectively the first and second ball joint 215, 216. As shown in Figure 8B, one of the gears is provided with a pulley intended to be coupled with a winch, not shown, by the use of a belt, not shown. Alternatively, the pulley can be operated manually by a simple rope kept under tension acting as a belt. In this way, manipulation of the winch makes it possible to rotate the two gears in a counter-rotating movement which in turn causes a movement of the first and second ball joints 215, 216 with respect to the plate 211 which is opposite each other and therefore a pivoting of the supporting plane arm 22, 32.
Chaque bras de plan porteur 22, 32 est également monté sur la platine 211 au moyen du support complémentaire 214 du bras de plan porteur sur lequel est monté le bras de plan porteur 22, 32 au moyen d'une liaison pivot glissant démontable telle que celle fournie par la sangle 214A. Une telle liaison pivot glissant n'entrave pas le pivotement du bras de plan porteur 22, 32 lors du réglage de la hauteur des première et deuxième rotules 215, 216 vis-à-vis de la platine 211 au moyen du système de réglage 213. On notera que dans ce troisième mode de réalisation, afin de permettre un placement stable vis-à-vis de la platine, le support complémentaire présente une embase présentant une surface complémentaire à la surface supérieure de la platine 211. Les figures 9A et 9B illustrent respectivement un bateau 1 équipé de deux safrans 44, 54 selon l'invention dans une configuration hydroptère et dans une configuration bateau classique. Each supporting plane arm 22, 32 is also mounted on the plate 211 by means of the complementary support 214 of the supporting plane arm on which the supporting plane arm 22, 32 is mounted by means of a removable sliding pivot connection such as that provided by strap 214A. Such a sliding pivot connection does not hinder the pivoting of the supporting plane arm 22, 32 when adjusting the height of the first and second ball joints 215, 216 with respect to the plate 211 by means of the adjustment system 213. It will be noted that in this third embodiment, in order to allow stable placement with respect to the plate, the complementary support has a base having a surface complementary to the upper surface of the plate 211. Figures 9A and 9B respectively illustrate a boat 1 equipped with two rudders 44, 54 according to the invention in a hydrofoil configuration and in a classic boat configuration.
On peut voir que dans la configuration hydroptère illustrée sur la figure 9A, conformément à l'invention, chaque safran 44, 54, et donc leur corps 441 sont agencé dans l'armature 442, 542 correspondante avec le plan porteur 45 orienté vers le bas, c'est-à-dire au-dessous de la ligne de flottaison du bateau 1. D'une manière identique les bras de plan porteur 22, 32 sont agencé avec leur plan porteur 24, 34 respectif qui est immergé. It can be seen that in the hydrofoil configuration illustrated in Figure 9A, in accordance with the invention, each rudder 44, 54, and therefore their body 441 are arranged in the corresponding frame 442, 542 with the supporting plane 45 oriented downwards. , that is to say below the waterline of the boat 1. In an identical manner the supporting plane arms 22, 32 are arranged with their respective supporting plane 24, 34 which is submerged.
Dans la configuration classique illustrée sur la figure 9B, conformément à l'invention, chaque safran 44, 54, et donc leur corps 441 sont agencés dans l'armature 442, 542 correspondante avec le plan porteur 45 orienté vers le haut, c'est-à-dire au-dessus de la ligne de flottaison du bateau 1. D'une manière identique les bras de plan porteur 22, 32 sont agencé avec leur plan porteur 24, 34 respectif relevé, c'est-à-dire en dehors de la mer. In the classic configuration illustrated in Figure 9B, in accordance with the invention, each rudder 44, 54, and therefore their body 441 are arranged in the corresponding frame 442, 542 with the supporting plane 45 oriented upwards, this is that is to say above the waterline of the boat 1. In an identical manner the supporting plane arms 22, 32 are arranged with their respective supporting plane 24, 34 raised, that is to say outside of the sea.
Le passage du bateau 1 d'une configuration à l'autre peut se faire selon le procédé suivant : retrait de chaque safran 42, 52 de l'armature 442, 542 correspondante, passage de l'orientation de chaque safran 42, 52 d'une configuration parmi une configuration dans laquelle le plan porteur 45, 55 orienté vers le haut et une configuration dans laquelle le plan porteur 45, 55 orienté vers le bas, à une autre configuration parmi la configuration dans laquelle le plan porteur 45, 55 orienté vers le haut et la configuration dans laquelle le plan porteur 45 orienté vers le bas, agencement de chaque safran 42, 52 dans l'armature correspondante 44, 54 en conservant l'orientation dans laquelle il a été passé, passage de chacun des bras de plan porteur d'une configuration parmi une configuration dans laquelle le plan porteur 24, 34 correspondant audit bras est au moins en partie immergé et une configuration dans laquelle le plan porteur 24, 34 correspondant audit bras n'est pas immergé à l'autre configuration parmi la configuration dans laquelle le plan porteur 24, 34 correspondant audit bras est au moins en partie immergé et la configuration dans laquelle le deuxième plan porteur 24, 34 correspondant audit bras n'est pas immergé. Ce dernier passage d'une configuration à l'autre des bras de plan porteur peut se faire, comme cela est permis dans les modes de réalisation de la présente invention, par un basculement des bras de plan porteur tel que montré sur les figures 9A et 9B. The passage of the boat 1 from one configuration to another can be done according to the following process: removal of each rudder 42, 52 from the corresponding frame 442, 542, changing the orientation of each rudder 42, 52 from one configuration among a configuration in which the supporting plane 45, 55 oriented upwards and a configuration in which the supporting plane 45, 55 oriented downwards, to another configuration among the configuration in which the supporting plane 45, 55 oriented toward the top and the configuration in which the supporting plane 45 faces downwards, arrangement of each rudder 42, 52 in the corresponding frame 44, 54 while maintaining the orientation in which it was passed, passage of each of the plane arms carrying a configuration among a configuration in which the supporting plane 24, 34 corresponding to said arm is at least partly immersed and a configuration in which the supporting plane 24, 34 corresponding to said arm is not immersed in the other configuration among the configuration in which the supporting plane 24, 34 corresponding to said arm is at least partly immersed and the configuration in which the second supporting plane 24, 34 corresponding to said arm is not immersed. This last transition from one configuration to another of the supporting plane arms can be done, as is permitted in the embodiments of the present invention, by tilting the supporting plane arms as shown in Figures 9A and 9B.

Claims

Revendications Claims
1. Ensemble système de montage (43) et safran (44) pour monter le safran à la coque (11) d'un bateau (1), l'ensemble système de montage (43) et safran comprenant : un premier et un deuxième élément de montage (432, 433) par l'intermédiaire desquels le safran (44) est destiné à être monté à la coque (11, 12) du bateau (1), le premier et le deuxième élément de montage (432, 433) étant destinés à être montés mobiles en rotation vis-à-vis de la coque du bateau autour d'un axe de gouvernail qui leur est commun une armature (442) monté sur les premier et deuxième éléments de montage (432, 433), un corps de safran (441) monté coulissant dans l'armature (442) afin d'autoriser un réglage de la profondeur du safran (44), l'ensemble système de montage (43) et safran étant caractérisé en ce que le safran (44) présente un plan porteur (45), ledit plan porteur (45) étant préférentiellement un plan porteur en T, et en ce que le corps de safran (441) porte le plan porteur (45) au niveau de l'une des extrémités dudit corps de safran (441) et le corps de safran (441) étant adapté pour être agencé dans l'armature (442) avec soit le plan porteur (45) orienté vers le haut, c'est- à-dire au-dessus d'une ligne de flottaison du bateau (1), soit le plan porteur (45) orienté vers le bas, c'est-à-dire au-dessous d'une ligne de flottaison du bateau (1). 1. Mounting system (43) and rudder (44) assembly for mounting the rudder to the hull (11) of a boat (1), the mounting system (43) and rudder assembly comprising: a first and a second mounting element (432, 433) by means of which the rudder (44) is intended to be mounted to the hull (11, 12) of the boat (1), the first and the second mounting element (432, 433) being intended to be mounted movable in rotation with respect to the hull of the boat around a rudder axis which is common to them, an armature (442) mounted on the first and second mounting elements (432, 433), a rudder body (441) slidably mounted in the frame (442) in order to allow adjustment of the depth of the rudder (44), the assembly system (43) and rudder being characterized in that the rudder (44 ) has a carrier plane (45), said carrier plane (45) being preferably a T-shaped carrier plane, and in that the rudder body (441) carries the carrier plane (45) at one of the ends of said rudder body (441) and the rudder body (441) being adapted to be arranged in the frame (442) with either the supporting plane (45) oriented upwards, that is to say above a waterline of the boat (1), i.e. the supporting plane (45) oriented downwards, that is to say below a waterline of the boat (1).
2. Ensemble système de montage (43) et safran (44) selon la revendication 1 dans lequel le deuxième élément de montage est destiné à être agencé le long de l'axe de gouvernail sous le premier élément de montage lorsque le bateau (1) est à flot, et dans lequel le premier élément de montage (432) présente un axe de pivot le long duquel est destiné à être monté mobile en rotation le safran (44), l'axe de pivot étant transversal à l'axe de gouvernail, le deuxième élément de montage (433) étant destiné à être assemblé à l'un parmi le safran et la coque par emboîtage élastique. 2. Mounting system assembly (43) and rudder (44) according to claim 1 wherein the second mounting element is intended to be arranged along the rudder axis under the first mounting element when the boat (1) is afloat, and in which the first mounting element (432) has a pivot axis along which the rudder (44) is intended to be rotatably mounted, the pivot axis being transverse to the rudder axis , the second mounting element (433) being intended to be assembled to one of the rudder and the hull by elastic fitting.
3. Ensemble système de montage (43) et safran (44) selon la revendication 2, dans lequel, le deuxième élément de montage (433) est destiné à être assemblé au safran (44) par emboîtage élastique. 3. Mounting system (43) and rudder (44) assembly according to claim 2, wherein, the second mounting element (433) is intended to be assembled to the rudder (44) by elastic fitting.
4. Ensemble système de montage (43) et safran (44) selon l'une quelconque des revendications 2 ou 3, comprenant en outre une pièce intermédiaire (431) destinée à être fixée à la coque (11, 12), et avantageusement au tableau arrière de la coque (11, 12), et dans lequel le premier et le deuxième élément de montage (432, 433) sont montés mobiles en rotation vis-à-vis de la pièce intermédiaire (431) autour de l'axe de gouvernail. 4. Mounting system (43) and rudder (44) assembly according to any one of claims 2 or 3, further comprising an intermediate part (431) intended to be fixed to the hull (11, 12), and advantageously to the transom of the hull (11, 12), and in which the first and the second mounting element (432, 433) are mounted movable in rotation with respect to the intermediate part (431) around the axis of rudder.
5. Ensemble système de montage (43) et safran (44) selon l'une quelconque des revendications 1 à 4, dans lequel le safran (44) présente au moins une portion de profondeur (443) disposée sur une extrémité (441A, 441B) du safran (44) en étant destinée à être opposée à la coque (11, 12), et dans laquelle ladite portion de profondeur (443) comprend un élément en matériau déformable, tel qu'un élastomère qui est avantageusement un caoutchouc naturel ou synthétique. 5. Mounting system assembly (43) and rudder (44) according to any one of claims 1 to 4, in which the rudder (44) has at least one depth portion (443) arranged on one end (441A, 441B ) of the rudder (44) being intended to be opposed to the hull (11, 12), and in which said depth portion (443) comprises an element made of deformable material, such as an elastomer which is advantageously a natural rubber or synthetic.
6. Ensemble système de montage (43) et safran (44) selon la revendication 5, dans laquelle le safran comprend en outre une autre portions de profondeur associées à une autre extrémité (441A) du safran (44), dans lequel chacune de la portion de profondeur et de l'autre portion de profondeur est destinée, dans au moins une configuration du safran (44) à être opposée à la coque (11, 12) et dans lequel l'autre portion de profondeur comprend un autre élément en matériau déformable, tel qu'un élastomère qui est avantageusement un caoutchouc naturel ou synthétique. 6. Mounting system assembly (43) and rudder (44) according to claim 5, in which the rudder further comprises another depth portion associated with another end (441A) of the rudder (44), in which each of the depth portion and the other depth portion is intended, in at least one configuration of the rudder (44) to be opposed to the hull (11, 12) and in which the other depth portion comprises another element made of material deformable, such as an elastomer which is advantageously a natural or synthetic rubber.
7. Ensemble système de montage (43) et safran (44) selon l'une quelconque des revendications 1 à 6 comprenant en outre un système de sécurisation, tel qu'une goupille, en position du safran (44) sur l'armature (442). 7. Mounting system (43) and rudder (44) assembly according to any one of claims 1 to 6 further comprising a securing system, such as a pin, in the position of the rudder (44) on the frame ( 442).
8. Kit d'installation de plans porteurs (22, 32, 45, 55) pour bateau (1), notamment à propulsion éolienne, bateau (1) comprenant au moins un élément de structure (15), le kit d'installation de plans porteurs (22, 32, 45, 55) comprenant un ensemble selon l'une quelconque des revendications 1 à 7 et au moins un bras de plan porteur (22, 32) destiné à être monté sur l'élément de structure (15) et présentant un deuxième plan porteur (24, 34) destiné à être au moins en partie immergé. 8. Kit for installing supporting planes (22, 32, 45, 55) for a boat (1), in particular wind-powered, boat (1) comprising at least one structural element (15), the installation kit for supporting planes (22, 32, 45, 55) comprising an assembly according to any one of claims 1 to 7 and at least one supporting plane arm (22, 32) intended to be mounted on the structural element (15) and having a second supporting plane (24, 34) intended to be at least partly submerged.
9. Procédé de changement de configuration d'un safran d'un bateau équipé d'un kit d'installation de plan porteurs (22, 32, 45, 55) selon la revendication 8, comprenant les étapes suivantes : retrait du safran (42) de l'armature (442), passage de l'orientation du safran (42) d'une configuration parmi une configuration dans laquelle le plan porteur (45) orienté vers le haut et une configuration dans laquelle le plan porteur (45) orienté vers le bas, à une autre configuration parmi la configuration dans laquelle le plan porteur (45) orienté vers le haut et la configuration dans laquelle le plan porteur (45) orienté vers le bas, agencement du safran (42) dans l'armature en conservant l'orientation dans laquelle il a été passé. 9. Method for changing the configuration of a rudder of a boat equipped with a carrier plan installation kit (22, 32, 45, 55) according to claim 8, comprising the following steps: removal of the rudder (42 ) of the frame (442), passage of the orientation of the rudder (42) from one configuration among a configuration in which the supporting plane (45) oriented upwards and a configuration in which the supporting plane (45) oriented downwards, to another configuration among the configuration in which the supporting plane (45) oriented upwards and the configuration in which the supporting plane (45) oriented downwards, arrangement of the rudder (42) in the frame in retaining the orientation in which it was passed.
10. Procédé de changement de configuration d'un safran d'un bateau selon la revendication 9, dans lequel il est en outre prévu une étape de modification d'une configuration de l'au moins un bras de plan porteur (22, 32) de telle manière de faire passer d'une configuration parmi une configuration dans laquelle le deuxième plan porteur (24, 34) est au moins en partie immergé et une configuration dans laquelle le deuxième plan porteur (24, 34) n'est pas immergé à l'autre configuration parmi la configuration dans laquelle le deuxième plan porteur (24, 34) est au moins en partie immergé et la configuration dans laquelle le deuxième plan porteur (24, 34) n'est pas immergé. 10. Method for changing the configuration of a rudder of a boat according to claim 9, in which there is also provided a step of modifying a configuration of the at least one supporting plane arm (22, 32) in such a way as to pass from one configuration among a configuration in which the second supporting plane (24, 34) is at least partly immersed and a configuration in which the second supporting plane (24, 34) is not immersed at the other configuration among the configuration in which the second supporting plane (24, 34) is at least partly immersed and the configuration in which the second supporting plane (24, 34) is not immersed.
PCT/IB2023/054880 2022-05-11 2023-05-11 Assembly of a mounting system and rudder, kit for installing hydrofoils comprising such an assembly and method for changing the configuration of a boat comprising such a kit WO2023218397A1 (en)

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FR2204481A FR3135446A1 (en) 2022-05-11 2022-05-11 System for mounting a rudder to the hull of a boat, assembly comprising such a mounting system and a rudder and method for installing a rudder
FRFR2204481 2022-05-11

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2379425A1 (en) * 1977-02-04 1978-09-01 Anvar Rudder depth control for sailing boat - has rudder tilted inside vertical yoke and operated by twisting tiller
US4218986A (en) * 1978-08-02 1980-08-26 John Hackney Boat rudder accessory
US4406239A (en) * 1978-10-13 1983-09-27 Klaus Enzmann Sailboats, especially catamarans
WO1988008809A1 (en) * 1987-05-13 1988-11-17 Mcmillen Winton P Kick-up rudder assembly
DE202009017432U1 (en) * 2009-12-23 2011-05-05 Enzmann, Klaus J. water craft
WO2012021941A1 (en) * 2010-08-20 2012-02-23 Concepts Ip Pty Ltd Hydrofoil

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2379425A1 (en) * 1977-02-04 1978-09-01 Anvar Rudder depth control for sailing boat - has rudder tilted inside vertical yoke and operated by twisting tiller
US4218986A (en) * 1978-08-02 1980-08-26 John Hackney Boat rudder accessory
US4406239A (en) * 1978-10-13 1983-09-27 Klaus Enzmann Sailboats, especially catamarans
WO1988008809A1 (en) * 1987-05-13 1988-11-17 Mcmillen Winton P Kick-up rudder assembly
DE202009017432U1 (en) * 2009-12-23 2011-05-05 Enzmann, Klaus J. water craft
WO2012021941A1 (en) * 2010-08-20 2012-02-23 Concepts Ip Pty Ltd Hydrofoil

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