EP1963174A1 - Demountable cable cutter - Google Patents

Demountable cable cutter

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Publication number
EP1963174A1
EP1963174A1 EP06841841A EP06841841A EP1963174A1 EP 1963174 A1 EP1963174 A1 EP 1963174A1 EP 06841841 A EP06841841 A EP 06841841A EP 06841841 A EP06841841 A EP 06841841A EP 1963174 A1 EP1963174 A1 EP 1963174A1
Authority
EP
European Patent Office
Prior art keywords
hub
screw
parts
shaft
bore
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
EP06841841A
Other languages
German (de)
French (fr)
Other versions
EP1963174B1 (en
Inventor
Franck Delot
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Delot et Cie SARL
Original Assignee
Delot et Cie SARL
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 Delot et Cie SARL filed Critical Delot et Cie SARL
Publication of EP1963174A1 publication Critical patent/EP1963174A1/en
Application granted granted Critical
Publication of EP1963174B1 publication Critical patent/EP1963174B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/16—Arrangements on vessels of propulsion elements directly acting on water of propellers characterised by being mounted in recesses; with stationary water-guiding elements; Means to prevent fouling of the propeller, e.g. guards, cages or screens
    • B63H5/165—Propeller guards, line cutters or other means for protecting propellers or rudders

Definitions

  • the present invention relates to the field of marine, and more particularly to a rope cutter that can be mounted on a boat propeller shaft.
  • a rope cutter is useful for releasing the propeller shaft when a rope is caught in the shaft and may block the rotation of the propeller.
  • rope used here covers a large number of objects likely to be caught around the tree, including, ropes, orins, cables nets or parts of fishing nets, or herbs, such wire cutter is disclosed in FR2768120.
  • the object of the invention is to provide a cable cutter which has improved mounting facilities and which can meet the problem posed by the propeller shafts mounted on an intermediate chair.
  • such a rope cutter comprising a hub for fixing on a propeller shaft of a boat and a blade carried by said hub, said rope cutter having several parts removable between them so that the shaft of propeller can be introduced radially into the hub.
  • the several parts are two parts that can be disassembled and assembled along an axial plane of the hub. They are advantageously designed to be held by at least one screw arranged so that a first part comprises a housing for supporting the head of said screw and the second portion comprises a threaded zone for engaging said screw.
  • the several parts are two parts that can be disassembled and assembled in two separation planes arranged on either side of an inner bore of the hub, and defining between them an opening at least as wide as the diameter of said bore.
  • the planes may be substantially symmetrical relative to an axial plane of the hub. In addition they can also be parallel to each other and possibly tangent to the bore.
  • the parts may be provided to be held by at least one screw, a first part comprising, facing each other, on either side of the opening, on the one hand a housing for the support of the head of said screw and secondly a threaded zone for engaging said screw, the second part comprising a non-threaded bore for the passage of said screw between the separation planes.
  • the wire cutter advantageously comprises a locking screw screwed into a minus one parts, the locking screw being provided to exert a locking force against the shaft.
  • FIG. 1 is a perspective view of a first embodiment for a rope cutter according to the invention, mounted on a propeller shaft;
  • FIG. 2 is an exploded perspective view of the cable cutter of FIG. 1;
  • FIG. 3 is an exploded plan view of a second embodiment for a cable cutter according to the invention.
  • FIG. 4 is a schematic view of a part of a boat comprising a shaft mounted on an intermediate chair and equipped with two cutters according to the first embodiment, illustrated in Figures 1 and 2.
  • FIG. 1 represents a cable cutter 10 mounted on a propeller shaft 1.
  • the cable cutter is of generally symmetrical shape about an axis X of revolution. As more particularly illustrated in Figure 2, it comprises two parts 11,12 separable along an axial plane P, that is to say including the axis of revolution X. Without the position of Figure 1, when the cutter wire is mounted on the propeller shaft 1, the X axis merges with the axis of revolution of the propeller shaft 1.
  • the two parts form together a hub 2 provided to fit around the propeller shaft 1 and an annular blade 3 extending radially outwardly from and around the hub 2.
  • the blade 3 comprises a substantially circular cutting outer edge, extending over the entire periphery of the blade. This outer edge is made of teeth substantially similar to those of a saw knife.
  • the hub 2 comprises a cylindrical hub bore 5 of diameter substantially identical to a diameter D 1 of the shaft 1.
  • the hub bore is provided for the passage of the shaft 1 through the wire cutter 10.
  • the plane P intersects the hub bore diametrically, so that in each portion 11,12 of the rope cutter 10, a corresponding portion of the hub bore 5 comprises an opening of width substantially equal to the diameter D1 of the shaft.
  • the cutter comprises two openings 14 for receiving the screws 13, pierced in the hub 2, on either side of the bore 5.
  • Each piercing 14 is perpendicular to the plane P. It comprises a first wide zone 141, for receiving the head of the screw 13, a second zone 142 of reduced diameter extends the first to pass the body of the screw. The first zone opens at the periphery of the hub. The second zone of work in the plane P. The first and the second zone are not threaded.
  • a third zone 143, threaded to engage with the screw 13, extends the second zone through the second portion 12.
  • a locking screw 15 is also provided. Its purpose is to avoid the relative movement of the shaft and the rope cutter. It is screwed into a thread 16 passing through the hub 2 between its periphery and the bore 5, in the second part 12.
  • FIG. 3 A second embodiment will now be described for a cable cutter according to the invention, with reference to FIG. 3. This embodiment will only be described in that it differs from the embodiment previously described with reference to FIGS. Figures 1 and 2. Similar elements will be assigned the same references.
  • the cable cutter comprises two parts 21,22, not symmetrical to each other. It comprises a first portion 21 having a shape of "C", and a second complementary portion 22.
  • the branches of C are defined by two planes R parallel to each other and extending tangentially to the bore 5.
  • a first portion substantially semi -cylindrique of the bore 5 is carried by the first portion, and a second complementary portion is carried by the second portion 22.
  • the distance between the parallel planes R is substantially equal to or greater than the diameter Dl of the shaft.
  • a portion of the hub bore 5 carried by the first part 21 thus comprises an opening of width substantially equal to the diameter D1 of the shaft, this opening extending between the planes R.
  • the shaft can be introduced transversely inside the first part 21 in the form of "C", then the second complementary part, comes to reform the cutter in its entirety. This can be done without the need to remove the propeller, as for the embodiment of Figures 1 and 2.
  • a screw 13 allows the assembly and maintenance, between them, parts 21,22.
  • a piercing 14 is provided in the hub 2 to receive the screw 13.
  • the piercing 14 is perpendicular to the planes R. It comprises, at a end of a branch of "C", a first wide zone 141, for receiving the head of the screw 13 and a second zone 142 of reduced diameter which extends the first to allow the body of the screw to pass.
  • the first zone opens at the periphery of the hub.
  • the first and second zones are not threaded.
  • a third zone 144, threaded to engage with the screw 13, is pierced opposite the second zone through the other branch of the "C" shape.
  • the third zone extends between the plane R and the periphery of the hub, respectively of the other branch.
  • a fourth zone 145 is drilled further through the second portion 22, for the adjusted passage of the body of the screw 13, and holding in place this second portion relative to the first
  • FIG. 4 illustrates a part of a boat 30, in the vicinity of a propeller 31 of the boat 30.
  • the boat has a hull 32.
  • a propeller shaft 1 leaves the hull 32 through a sternum 33, and carries the propeller 31 at an end remote from the sternstand 33.
  • a chair 34 Given the outer length of the shaft 1, a chair 34 provides support for the shaft between the stern and the propeller, a first region 36 of the shaft 10 extending between the sternum and the chair, and a second region 37 extending beyond the chair, to the propeller.
  • a first wire cutter 10 is mounted in the first region 36, in the vicinity of the sternstand.
  • a second cutter 10 is mounted in the second region 37.
  • the invention is not limited to the examples that have just been described and many adjustments can be made to these examples without departing from the scope of the invention.
  • the parts are of different shape and number from those of the previously described embodiments.
  • the planes defining the two parts may not be parallel, provided that they define an opening greater than or equal to the diameter of the propeller shaft.
  • the planes can be replaced also by other complementary forms, including for example redents for the mutual interlocking of the parts of the cutter.

Abstract

Cable cutter (10) comprising a hub (2) for attaching it to a boat's screw shaft (1) and a blade (3) carried by said hub, said cable cutter comprising several mutually demountable parts (11, 12) allowing the screw shaft (1) to be inserted radially into the hub (2).

Description

" Coupe-filin démontable " "Removable wire cutter"
La présente invention se rapporte au domaine de la marine, et plus particulièrement à un coupe-filin qui peut être monté sur un arbre d'hélice de bateau. Un tel coupe-filin est utile pour libérer l'arbre d'hélice lorsqu'un filin se prend dans l'arbre et risque bloquer la rotation de l'hélice. On comprendra que le terme filin utilisé ici recouvre un grand nombre d'objets susceptibles de venir se prendre autour de l'arbre, notamment, des filins, des orins, des câbles des filets ou parties de filets de pêche, ou des herbes, Un tel coupe-filin est divulgué par le document FR2768120.The present invention relates to the field of marine, and more particularly to a rope cutter that can be mounted on a boat propeller shaft. Such a rope cutter is useful for releasing the propeller shaft when a rope is caught in the shaft and may block the rotation of the propeller. It will be understood that the term rope used here covers a large number of objects likely to be caught around the tree, including, ropes, orins, cables nets or parts of fishing nets, or herbs, such wire cutter is disclosed in FR2768120.
Cependant, la mise en place d'un tel coupe-filin se fait lors d'une mise en cale du bateau, ce qui est coûteux. Il faut ensuite retirer l'hélice, ce qui implique d'utiliser un arrache-moyeu, et nécessite généralement l'intervention d'un professionnel. En outre, certains arbres d'hélice sont montés sur des chaises. Une telle chaise est fixée dans la coque du bateau et constitue un support intermédiaire pour l'arbre d'hélice. Ainsi, une première partie de l'arbre s'étend depuis l'endroit d'où il sort de la coque jusqu'à la chaise, et une deuxième partie s'étend depuis la chaise jusqu'à l'hélice. Un coupe-filin monté sur la deuxième partie, entre la chaise et l'hélice, comme c'est le cas avec un coupe-filin de l'art antérieur, est inefficace si un filin vient se prendre autour de la première partie de l'arbre d'hélice.However, the implementation of such a rope cutter is done during a boat docking, which is expensive. It is then necessary to remove the propeller, which implies to use a pull-hub, and generally requires the intervention of a professional. In addition, some propeller shafts are mounted on chairs. Such a chair is fixed in the hull of the boat and constitutes an intermediate support for the propeller shaft. Thus, a first part of the tree extends from where it leaves the hull to the chair, and a second part extends from the chair to the propeller. A rope cutter mounted on the second part, between the chair and the propeller, as is the case with a wire cutter of the prior art, is inefficient if a rope is caught around the first part of the wire. propeller shaft.
Le but de l'invention est de proposer un coupe-filin qui présente des facilités de montage amélioré et qui puisse répondre au problème posé par les arbres d'hélice montés sur une chaise intermédiaire.The object of the invention is to provide a cable cutter which has improved mounting facilities and which can meet the problem posed by the propeller shafts mounted on an intermediate chair.
Selon l'invention, un tel coupe-filin comprenant un moyeu de fixation sur un arbre d'hélice d'un bateau et une lame portée par ledit moyeu, ledit coupe-filin comportant plusieurs parties démontables entre elles de sorte que l'arbre d'hélice peut être introduit radialement dans le moyeu. Selon un premier mode de réalisation, les plusieurs parties sont deux parties qui peuvent être démontées et assemblées selon un plan axial de du moyeu. Elles sont avantageusement prévues pour être maintenues par au moins une vis disposée de sorte qu'une première partie comprend un logement pour l'appui de la tête de ladite vis et la deuxième partie comprend une zone filetée pour venir en prise avec ladite vis.According to the invention, such a rope cutter comprising a hub for fixing on a propeller shaft of a boat and a blade carried by said hub, said rope cutter having several parts removable between them so that the shaft of propeller can be introduced radially into the hub. According to a first embodiment, the several parts are two parts that can be disassembled and assembled along an axial plane of the hub. They are advantageously designed to be held by at least one screw arranged so that a first part comprises a housing for supporting the head of said screw and the second portion comprises a threaded zone for engaging said screw.
Selon un deuxième mode de réalisation, les plusieurs parties sont deux parties qui peuvent être démontées et assemblées selon deux plans de séparation disposés de part et d'autre d'un alésage intérieur du moyeu, et définissant entre eux une ouverture au moins aussi large que le diamètre dudit alésage. Les plans peuvent être sensiblement symétriques relativement à un plan axial du moyeu. En outre ils peuvent aussi être parallèles entre eux et éventuellement tangents à l'alésage. Dans ce deuxième mode de réalisation, les parties peuvent être prévues pour être maintenues par au moins une vis, une première partie comprenant en vis-à-vis, de part et d'autre de l'ouverture, d'une part un logement pour l'appui de la tête de ladite vis et d'autre part une zone filetée pour venir en prise avec ladite vis, la deuxième partie comprenant un percement non fileté pour le passage de ladite vis entre les plans de séparation.According to a second embodiment, the several parts are two parts that can be disassembled and assembled in two separation planes arranged on either side of an inner bore of the hub, and defining between them an opening at least as wide as the diameter of said bore. The planes may be substantially symmetrical relative to an axial plane of the hub. In addition they can also be parallel to each other and possibly tangent to the bore. In this second embodiment, the parts may be provided to be held by at least one screw, a first part comprising, facing each other, on either side of the opening, on the one hand a housing for the support of the head of said screw and secondly a threaded zone for engaging said screw, the second part comprising a non-threaded bore for the passage of said screw between the separation planes.
Pour bloquer le coupe-filin relativement à l'arbre, notamment pour qu'il n'aient pas entre eux un mouvement relatif sous les efforts de découpe d'un filin, le coupe filin comprend avantageusement une vis de blocage vissé dans une moins une des parties, la vise de blocage étant prévue pour exercer un effort de blocage contre le l'arbre.To block the thread cutter relative to the shaft, especially so that it does not have a relative movement between them under the cutting forces of a rope, the wire cutter advantageously comprises a locking screw screwed into a minus one parts, the locking screw being provided to exert a locking force against the shaft.
D'autres particularités et avantages de l'invention ressortiront encore de la description ci-après, relative à des exemples non limitatifs. Aux dessins annexés : - la figure 1 est une vue en perspective d'un premier mode de réalisation pour un coupe-filin selon l'invention, monté sur un arbre d'hélice;Other features and advantages of the invention will emerge from the description below, relating to non-limiting examples. In the accompanying drawings: FIG. 1 is a perspective view of a first embodiment for a rope cutter according to the invention, mounted on a propeller shaft;
- la figure 2 est une vue en perspective éclatée du coupe-filin de la figure 1; - la figure 3 est une vue, éclatée et en plan, d'un deuxième mode de réalisation pour un coupe-filin selon l'invention; et,FIG. 2 is an exploded perspective view of the cable cutter of FIG. 1; FIG. 3 is an exploded plan view of a second embodiment for a cable cutter according to the invention; and,
- la figure 4 est une vue schématique d'une partie d'un bateau comprenant un arbre monté sur une chaise intermédiaire et équipé de deux coupes filins selon le premier mode de réalisation, illustré aux figures 1 et 2.FIG. 4 is a schematic view of a part of a boat comprising a shaft mounted on an intermediate chair and equipped with two cutters according to the first embodiment, illustrated in Figures 1 and 2.
La figure 1 représente un coupe-filin 10 monté sur un arbre d'hélice 1. Le coupe-filin est de forme généralement symétrique autour d'un axe X de révolution. Comme plus particulièrement illustré à la figure 2, il comprend deux parties 11,12 séparables selon un plan axial P, c'est-à-dire comprenant l'axe de révolution X. Sans la position de la figure 1, lorsque le coupe-filin est monté sur l'arbre d'hélice 1, l'axe X se confond avec l'axe de révolution de l'arbre d'hélice 1. Tel qu'illustré à la figure 1, une fois assemblées, les deux parties forment ensemble un moyeux 2 prévu pour s'ajuster autour de l'arbre d'hélice 1 et une lame annulaire 3 s'étendant radialement vers l'extérieur, depuis et autour du moyeu 2. La lame 3 comprend un bord extérieur coupant sensiblement circulaire, s'étendant sur toute la périphérie de la lame. Ce bord extérieur est constitué de dents sensiblement analogues à celles d'un couteau scie.FIG. 1 represents a cable cutter 10 mounted on a propeller shaft 1. The cable cutter is of generally symmetrical shape about an axis X of revolution. As more particularly illustrated in Figure 2, it comprises two parts 11,12 separable along an axial plane P, that is to say including the axis of revolution X. Without the position of Figure 1, when the cutter wire is mounted on the propeller shaft 1, the X axis merges with the axis of revolution of the propeller shaft 1. As illustrated in Figure 1, once assembled, the two parts form together a hub 2 provided to fit around the propeller shaft 1 and an annular blade 3 extending radially outwardly from and around the hub 2. The blade 3 comprises a substantially circular cutting outer edge, extending over the entire periphery of the blade. This outer edge is made of teeth substantially similar to those of a saw knife.
Le moyeu 2 comprend un alésage de moyeu 5 cylindrique, de diamètre sensiblement identique à un diamètre Dl de l'arbre 1. L'alésage de moyeu est prévu pour le passage de l'arbre 1 au travers du coupe-filin 10. Le plan P coupe l'alésage de moyeu diamétralement, de sorte que dans chaque partie 11,12 du coupe-filin 10, une portion correspondante de l'alésage de moyeu 5 comprend une ouverture de largeur sensiblement égale au diamètre Dl de l'arbre. Ainsi, l'arbre peut être introduit radialement dans les portions respectives de l'alésage de moyeu 5, de sorte que les deux parties 11,12 peuvent être assemblées radialement autour de l'arbre. Il n'est donc pas utile de retirer l'hélice pour monter un tel coupe- filin.The hub 2 comprises a cylindrical hub bore 5 of diameter substantially identical to a diameter D 1 of the shaft 1. The hub bore is provided for the passage of the shaft 1 through the wire cutter 10. The plane P intersects the hub bore diametrically, so that in each portion 11,12 of the rope cutter 10, a corresponding portion of the hub bore 5 comprises an opening of width substantially equal to the diameter D1 of the shaft. Thus, the shaft can be introduced radially into the respective portions of the hub bore 5, so that the two parts 11,12 can be assembled radially around the shaft. It is therefore not necessary to remove the propeller to mount such a cable cutter.
Deux vis 13 permettent l'assemblage et le maintien, entre elles, des deux parties 11,12. Le coupe-filin comprend deux percements 14 pour recevoir les vis 13, percés dans le moyeu 2, de part et d'autre de l'alésage 5. Chaque percement 14 est perpendiculaire au plan P. Il comprend une première zone large 141, pour recevoir la tête de la vis 13, une deuxième zone 142 de diamètre réduit prolonge la première pour laisser passer le corps de la vis. La première zone s'ouvre en périphérie du moyeu. La deuxième zone d'ouvré dans le plan P. La première et la deuxième zone ne sont pas filetées. Une troisième zone 143, filetée pour venir en prise avec la vis 13, prolonge la deuxième zone au travers de la deuxième partie 12. Une vis de blocage 15 est aussi prévue. Elle a pour but d'éviter le mouvement relatif de l'arbre et du coupe-filin. Elle est vissée dans un filetage 16 traversant le moyeu 2 entre sa périphérie et l'alésage 5, dans la deuxième partie 12.Two screws 13 allow the assembly and maintenance, between them, of the two parts 11,12. The cutter comprises two openings 14 for receiving the screws 13, pierced in the hub 2, on either side of the bore 5. Each piercing 14 is perpendicular to the plane P. It comprises a first wide zone 141, for receiving the head of the screw 13, a second zone 142 of reduced diameter extends the first to pass the body of the screw. The first zone opens at the periphery of the hub. The second zone of work in the plane P. The first and the second zone are not threaded. A third zone 143, threaded to engage with the screw 13, extends the second zone through the second portion 12. A locking screw 15 is also provided. Its purpose is to avoid the relative movement of the shaft and the rope cutter. It is screwed into a thread 16 passing through the hub 2 between its periphery and the bore 5, in the second part 12.
On va maintenant décrire un deuxième mode de réalisation pour un coupe-filin selon l'invention, en référence à la figure 3. Ce mode de réalisation ne sera décrit qu'en ce qu'il diffère du mode de réalisation précédemment décrit en référence aux figures 1 et 2. Les éléments similaires seront affectés des mêmes références.A second embodiment will now be described for a cable cutter according to the invention, with reference to FIG. 3. This embodiment will only be described in that it differs from the embodiment previously described with reference to FIGS. Figures 1 and 2. Similar elements will be assigned the same references.
Dans ce deuxième mode de réalisation, le coupe-filin comprend deux parties 21,22, non symétriques entre elles. Il comprend une première partie 21 ayant une forme de "C", et une deuxième partie complémentaire 22. Les branches du C sont définies par deux plans R parallèles entre eux et s'étendant tangentiellement à l'alésage 5. Une première portion sensiblement semi-cylindrique de l'alésage 5 est portée par la première partie, et une deuxième portion complémentaire est portée par la deuxième partie 22. La distance entre les plans parallèles R est sensiblement égale ou supérieure au diamètre Dl de l'arbre.In this second embodiment, the cable cutter comprises two parts 21,22, not symmetrical to each other. It comprises a first portion 21 having a shape of "C", and a second complementary portion 22. The branches of C are defined by two planes R parallel to each other and extending tangentially to the bore 5. A first portion substantially semi -cylindrique of the bore 5 is carried by the first portion, and a second complementary portion is carried by the second portion 22. The distance between the parallel planes R is substantially equal to or greater than the diameter Dl of the shaft.
Une portion de l'alésage de moyeu 5 portée par la première partie 21 comprend donc une ouverture de largeur sensiblement égale au diamètre Dl de l'arbre, cette ouverture s'étendant entre les plans R. Ainsi, comme illustré à la figure 3 par les flèches F, l'arbre peut être introduit transversalement à l'intérieur de la première partie 21 en forme de "C", puis la deuxième partie complémentaire, vient reformer le coupe-filin dans son intégralité. Ceci peut se faire sans qu'il soit nécessaire de retirer l'hélice, comme pour le mode de réalisation des figures 1 et 2.A portion of the hub bore 5 carried by the first part 21 thus comprises an opening of width substantially equal to the diameter D1 of the shaft, this opening extending between the planes R. Thus, as illustrated in FIG. arrows F, the shaft can be introduced transversely inside the first part 21 in the form of "C", then the second complementary part, comes to reform the cutter in its entirety. This can be done without the need to remove the propeller, as for the embodiment of Figures 1 and 2.
Une vis 13 permet l'assemblage et le maintien, entre elles, des parties 21,22. Un percement 14 est prévu dans le moyeu 2 pour recevoir la vis 13. Le percement 14 est perpendiculaire aux plans R. Il comprend, à une extrémité d'une branche du "C", une première zone large 141, • pour recevoir la tête de la vis 13 et une deuxième zone 142 de diamètre réduit qui prolonge la première pour laisser passer le corps de la vis. La première zone s'ouvre en périphérie du moyeu. La deuxième zone d'ouvré dans un plan R respectif. La première et la deuxième zone ne sont pas filetées. Une troisième zone 144, filetée pour venir en prise avec la vis 13, est percée en vis-à-vis de la deuxième zone au travers de l'autre branche de la forme en "C". La troisième zone s'étend entre le plan R et la périphérie du moyeu, respectifs de l'autre branche. Une quatrième zone 145 est percée autre travers de la deuxième partie 22, pour le passage ajusté du corps de la vis 13, et le maintien en place de cette deuxième partie relativement à la première.A screw 13 allows the assembly and maintenance, between them, parts 21,22. A piercing 14 is provided in the hub 2 to receive the screw 13. The piercing 14 is perpendicular to the planes R. It comprises, at a end of a branch of "C", a first wide zone 141, for receiving the head of the screw 13 and a second zone 142 of reduced diameter which extends the first to allow the body of the screw to pass. The first zone opens at the periphery of the hub. The second area of work in a respective R plane. The first and second zones are not threaded. A third zone 144, threaded to engage with the screw 13, is pierced opposite the second zone through the other branch of the "C" shape. The third zone extends between the plane R and the periphery of the hub, respectively of the other branch. A fourth zone 145 is drilled further through the second portion 22, for the adjusted passage of the body of the screw 13, and holding in place this second portion relative to the first.
Une vis de blocage 15 est aussi prévue dans un filetage 16 à travers le moyeu, dans la première partie 21. La figure 4 illustre une partie d'un bateau 30, au voisinage d'une hélice 31 du bateau 30. Le bateau a une coque 32. Un arbre d'hélice 1 sort de la coque 32 au travers d'un étambot 33, et porte l'hélice 31 à une extrémité distante de l'étambot 33. Compte tenu de la longueur extérieure de l'arbre 1, une chaise 34 assure le soutien de l'arbre, entre l'étambot et l'hélice, une première région 36 de l'arbre 10 s'étendant entre l'étambot et la chaise, et une deuxième région 37 s'étendant au-delà de la chaise, jusqu'à l'hélice.A locking screw 15 is also provided in a thread 16 through the hub, in the first part 21. FIG. 4 illustrates a part of a boat 30, in the vicinity of a propeller 31 of the boat 30. The boat has a hull 32. A propeller shaft 1 leaves the hull 32 through a sternum 33, and carries the propeller 31 at an end remote from the sternstand 33. Given the outer length of the shaft 1, a chair 34 provides support for the shaft between the stern and the propeller, a first region 36 of the shaft 10 extending between the sternum and the chair, and a second region 37 extending beyond the chair, to the propeller.
Grâce aux principes de l'invention, deux coupe-filin 10 tels que décrit précédemment en référence aux figures 1 et 2. Un premier coupe-filin 10 est monté dans la première région 36, au voisinage de l'étambot. Un deuxième coupe-filin 10 est monté dans la deuxième région 37.Thanks to the principles of the invention, two wire cutter 10 as described above with reference to Figures 1 and 2. A first wire cutter 10 is mounted in the first region 36, in the vicinity of the sternstand. A second cutter 10 is mounted in the second region 37.
Bien sûr, l'invention n'est pas limitée aux exemples qui viennent d'être décrits et de nombreux aménagements peuvent être apportés à ces exemples sans sortir du cadre de l'invention. En particulier, il peut être prévues que les parties soient de forme et de nombre différents de celles des modes de réalisation précédemment décrits. Dans le deuxième mode de réalisation, les plans définissant les deux parties, peuvent ne pas être parallèles, pourvu qu'ils définissent une ouverture supérieure ou égale au diamètre de l'arbre d'hélice.Of course, the invention is not limited to the examples that have just been described and many adjustments can be made to these examples without departing from the scope of the invention. In particular, it may be provided that the parts are of different shape and number from those of the previously described embodiments. In the second embodiment, the planes defining the two parts may not be parallel, provided that they define an opening greater than or equal to the diameter of the propeller shaft.
Les plans peuvent être remplacés aussi par d'autres formes complémentaires, comprenant par exemple des redents pour l'emboîtement mutuel des parties du coupe-filin.The planes can be replaced also by other complementary forms, including for example redents for the mutual interlocking of the parts of the cutter.
Dans la disposition de la figure 4, pour améliorer l'efficacité du système, il peut être prévu un troisième coupe-filin, disposé dans la première région, de sorte qu'il y a un coupe-filin de part et d'autre de la chaise. In the arrangement of Figure 4, to improve the efficiency of the system, there may be provided a third wire cutter disposed in the first region, so that there is a wire cutter on both sides of the chair.

Claims

REVENDICATIONS
1. Coupe-filin (10;20) comprenant un moyeu (2) de fixation sur un arbre (1) d'hélice (31) d'un bateau (30) et une lame (3) portée par ledit moyeu, ledit coupe-filin comportant plusieurs parties (11,12;21,22) démontables entre elles de sorte que l'arbre d'hélice peut être introduit radialement dans le moyeu.1. Thread cutter (10; 20) comprising a hub (2) for attachment to a shaft (1) of a propeller (31) of a boat (30) and a blade (3) carried by said hub, said cutter -filin comprising several parts (11,12; 21,22) dismountable between them so that the propeller shaft can be introduced radially into the hub.
2. Coupe-filin selon la revendication 1, caractérisé en ce que les plusieurs parties sont deux parties (11,12) qui peuvent être démontées et assemblées selon un plan (P) axial du moyeu.2. Thread cutter according to claim 1, characterized in that the plurality of parts are two parts (11,12) which can be disassembled and assembled in an axial plane (P) of the hub.
3. Coupe-filin selon la revendication 2, caractérisé en ce que les parties sont prévues pour être maintenues par au moins une vis disposée de sorte qu'une première partie comprend un logement (141) pour l'appui de la tête de ladite vis et la deuxième partie comprend une zone filetée (143) pour venir en prise avec ladite vis.3. Thread cutter according to claim 2, characterized in that the parts are provided to be held by at least one screw arranged so that a first portion comprises a housing (141) for the support of the head of said screw and the second portion comprises a threaded zone (143) for engaging said screw.
4. Coupe-filin selon la revendication 1, caractérisé en ce que les plusieurs parties sont deux parties (11,12) qui peuvent être démontées et assemblées selon deux plans de séparation (R) disposés de part et d'autre d'un alésage intérieur (5) du moyeu (2), et définissant une ouverture au moins aussi large que le diamètre (Dl) dudit alésage (5).4. Thread cutter according to claim 1, characterized in that the several parts are two parts (11,12) which can be disassembled and assembled in two separation planes (R) arranged on either side of a bore interior (5) of the hub (2), and defining an opening at least as wide as the diameter (D1) of said bore (5).
5. Coupe-filin selon la revendication 4, caractérisé en ce que les plans (R) sont sensiblement symétriques relativement à un plan axial du moyeu, parallèles entre eux et tangents à l'alésage.5. Thread cutter according to claim 4, characterized in that the planes (R) are substantially symmetrical relative to an axial plane of the hub, parallel to each other and tangent to the bore.
6. Coupe-filin selon la revendication 4 ou 5, caractérisé en ce que les parties sont prévues pour être maintenues par au moins une vis, une première partie (21) comprenant en vis-à-vis, de part et d'autre de l'ouverture, d'une part un logement (141,142) pour l'appui de la tête de ladite vis et d'autre part une zone filetée (144) pour venir en prise avec ladite vis, la deuxième partie comprenant un percement non fileté (114) pour le passage de ladite vis entre les plans de séparation (R).6. Thread cutter according to claim 4 or 5, characterized in that the parts are provided to be held by at least one screw, a first portion (21) comprising vis-à-vis, on both sides of opening, on the one hand a housing (141,142) for the support of the head of said screw and secondly a threaded zone (144) to engage with said screw, the second portion comprising a non-threaded bore (114) for the passage of said screw between the separation planes (R).
7. Coupe-filin selon l'une des revendications 1 à 6, caractérisé en ce qu'il comprend vissé dans une moins une des partie une vis de blocage sur l'arbre d'hélice (1). 7. Thread cutter according to one of claims 1 to 6, characterized in that it comprises screwed into at least one of the parts a locking screw on the propeller shaft (1).
EP06841841.7A 2005-12-02 2006-12-01 Demountable cable cutter Active EP1963174B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0512278A FR2894224B1 (en) 2005-12-02 2005-12-02 DETACHABLE FILTER CUTTER.
PCT/FR2006/002631 WO2007063227A1 (en) 2005-12-02 2006-12-01 Demountable cable cutter

Publications (2)

Publication Number Publication Date
EP1963174A1 true EP1963174A1 (en) 2008-09-03
EP1963174B1 EP1963174B1 (en) 2013-04-17

Family

ID=36658768

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06841841.7A Active EP1963174B1 (en) 2005-12-02 2006-12-01 Demountable cable cutter

Country Status (6)

Country Link
US (1) US20080293313A1 (en)
EP (1) EP1963174B1 (en)
AU (1) AU2006319021A1 (en)
ES (1) ES2417144T3 (en)
FR (1) FR2894224B1 (en)
WO (1) WO2007063227A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109367748A (en) * 2018-11-28 2019-02-22 大连英蕴科技有限公司 A kind of marine propeller and method

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110070784A1 (en) * 2009-09-24 2011-03-24 Ian Roberts Combination anode and line cutter
US8676804B1 (en) 2011-07-12 2014-03-18 Google Inc. Managing information about entities using observations generated from user modified values
CN104743089B (en) * 2015-04-15 2017-01-04 浙江工业大学 A kind of propeller for vessels twister cutter sweep
KR102105788B1 (en) * 2019-02-26 2020-04-28 한국해양대학교 산학협력단 Hybrid cutting device for cutting foreign matter caught in propeller shaft system

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US67982A (en) * 1867-08-20 Richard harvey hudson
US413819A (en) * 1889-10-29 Pulley
US2281156A (en) * 1939-05-23 1942-04-28 Johnson Emil Drive for shallow water boats
US2346163A (en) * 1941-07-05 1944-04-11 Standard Register Co Combination roll and interchangeable wheel
US4447215A (en) * 1982-07-06 1984-05-08 Govan Donald T Propellor protecting devices
US4507091A (en) * 1983-04-04 1985-03-26 Govan Donald T Propeller protecting devices
GB8531791D0 (en) * 1985-12-24 1986-02-05 Shaw R D Line cutting device
FR2768120B1 (en) * 1997-09-11 2000-03-03 Jean Claude Geron WIRE CUTTER
WO2003013954A1 (en) * 2001-08-08 2003-02-20 Robin David Shaw Cavitation alleviation and line cutting device
US6783411B2 (en) * 2002-04-23 2004-08-31 Allan Walter Pither Propeller protector slipper

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2007063227A1 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109367748A (en) * 2018-11-28 2019-02-22 大连英蕴科技有限公司 A kind of marine propeller and method
CN109367748B (en) * 2018-11-28 2023-11-03 大连英蕴科技有限公司 Ship propeller and method

Also Published As

Publication number Publication date
AU2006319021A1 (en) 2007-06-07
FR2894224A1 (en) 2007-06-08
ES2417144T3 (en) 2013-08-06
US20080293313A1 (en) 2008-11-27
FR2894224B1 (en) 2009-01-16
WO2007063227A1 (en) 2007-06-07
EP1963174B1 (en) 2013-04-17

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