EP2652436B1 - Zielabschussmaschine - Google Patents

Zielabschussmaschine Download PDF

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Publication number
EP2652436B1
EP2652436B1 EP11796715.8A EP11796715A EP2652436B1 EP 2652436 B1 EP2652436 B1 EP 2652436B1 EP 11796715 A EP11796715 A EP 11796715A EP 2652436 B1 EP2652436 B1 EP 2652436B1
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EP
European Patent Office
Prior art keywords
axis
rotation
target
machine according
arm
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Active
Application number
EP11796715.8A
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English (en)
French (fr)
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EP2652436A1 (de
Inventor
Jean-Michel Laporte
Jean-Marc Fouques
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.)
Laporte Holding SAS
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Laporte Holding SAS
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Publication of EP2652436A1 publication Critical patent/EP2652436A1/de
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Publication of EP2652436B1 publication Critical patent/EP2652436B1/de
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00—Moving targets, i.e. moving when fired at
    • F41J9/16—Clay-pigeon targets; Clay-disc targets
    • F41J9/18—Traps or throwing-apparatus therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00—Moving targets, i.e. moving when fired at
    • F41J9/16—Clay-pigeon targets; Clay-disc targets
    • F41J9/18—Traps or throwing-apparatus therefor
    • F41J9/20—Traps or throwing-apparatus therefor with spring-operated throwing arm
    • F41J9/24—Traps or throwing-apparatus therefor with spring-operated throwing arm cocked by electromechanical means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00—Moving targets, i.e. moving when fired at
    • F41J9/16—Clay-pigeon targets; Clay-disc targets
    • F41J9/18—Traps or throwing-apparatus therefor
    • F41J9/32—Traps or throwing-apparatus therefor characterised by means for obviating the anticipation of the flight path

Definitions

  • the present invention relates to a machine for launching targets for shooting and particularly for the discipline of archery.
  • Target launching devices are also known that are suitable for projecting "clay pigeon" type targets.
  • Such a device is for example known from the US patent US 6,176,229 .
  • These devices generally comprise a rotary launching arm capable of ejecting a target. During launch, the target is placed, by its lower face, on a support surface guiding the ejection of the target. The contact between the target and the bearing surface in combination with the launching arm adjusts the exit path of the target.
  • the present invention makes it possible to very substantially improve the behavior of the target after ejection.
  • a clear improvement in projection distances with same rotating arm power and a better stability in the air of the projected target More precisely, a high gyroscopic effect is observed during the ejection of the target at means of the invention and this even with light targets or even with a wet environment for machines operating in the rain.
  • the present invention particularly implements a bearing surface of the target comprising a portion of offset which is formed in such a way as to remove, advantageously progressively, the point of contact of the target with the bearing surface relative to the throwing arm.
  • the application parameters of the thrust force of the throwing arm on the target during the movement of the latter are modified so as to improve the behavior of the target.
  • the invention relates to a target launching machine having a portion of circular section, said machine comprising a launching arm rotatable about an axis of rotation and a bearing surface of the circular section portion, the bearing surface having an offset portion configured so that the spacing between the trajectory of the throwing arm and the offset portion is increasing in the direction of rotation of the throwing arm.
  • the offset portion is advantageously a concave element whose concavity is oriented towards the throwing arm. More precisely, the concave portion may be in an arc.
  • the target launching machine has a portion of circular section, said machine comprising a launching arm movable in rotation about an axis of rotation and a bearing surface of the portion of circular section, the surface support member having an offset portion configured so that the spacing between the trajectory of the launching arm and the offset portion is increasing in the direction of rotation of the launching arm, and comprising a circular profile portion of offset axis relative to the axis of rotation and parallel to the axis of rotation, characterized in that the offset between the offset axis and the axis of rotation comprises a non-zero component in a primary direction defined by a diameter of the trajectory launching arm located in a vertical plane, said component being disposed relative to the axis of rotation opposite the circular profile portion.
  • the invention relates to a target launching machine more preferably for archery.
  • the present invention is particularly advantageous for machines used in combination with targets made of plastic material and particularly of polymer foam. Indeed, this type of plastic material generates cooperation with the machine different from the clay pigeons. In particular, the risk of blockage is greater because the friction forces with the parts of the machine are higher. On the other hand, while the blockages can sometimes be simply solved by breaking pigeons of clay by means of the throwing arm, such a dislocation releasing the trajectory of the throwing arm is not possible for polymeric foam targets.
  • the target 1 is advantageously of flattened cylindrical shape, advantageously circular, having dimensions of the order of 30 to 150 millimeters in thickness, more preferably for competition targets in particular 245 millimeters in diameter and 50 millimeters in thickness.
  • the target 1 may be a sandwich of several layers of polymer foam, in particular with a denser core layer than the two layers located laterally on either side of the central layer.
  • the target 1 has two faces substantially parallel to each other and a slice corresponding to the thickness of the target. Both faces of the target can be flat or with a relief.
  • the machine may comprise a base that may be a welded structure although it is only a possibility and may be equipped with gripping means such as a handle and wheels for moving the machine.
  • a launch assembly mainly comprising a launch arm 2 rotatably mounted about an axis of rotation 3 defining a launch zone.
  • Conventional actuation means can be used to drive the launching arm 2 in rotation.
  • the launching arm 2 can cooperate with a tensioned spring thanks to a motorization and capable of being expanded on command to operate the projection of the target.
  • a target 1 into the launch zone takes place in the example presented in the figure 1 from a stack 11 of superimposed targets at storage means 10, for example in the form of a column or a cylinder having a plurality of columns for storing a larger number of targets.
  • storage means 10 for example in the form of a column or a cylinder having a plurality of columns for storing a larger number of targets.
  • a selective ejection system is provided so as to remove at least one target 1 from the storage means 10.
  • the target or targets to be projected are transferred via a transfer zone for example comprising a plurality of inclined surfaces having the effect of a slide capable of causing the target or targets 1 to project to the loading area.
  • the loading area is described in more detail below.
  • the loading zone is advantageously located in the lower part, the storage means and the transfer zone 10, 12 being advantageously located in the upper part of the assembly.
  • the target to be sprayed is subjected to the effect of the centrifugal force exerted by the throwing arm 2.
  • the target 1 is a cylindrical element of circular section over its entire thickness.
  • the target 1 is a cylindrical element of circular section over its entire thickness.
  • at least a portion of its section is circular so as to cooperate with the bearing surface 4 more precisely described below.
  • the bearing surface 4 is provided to receive the target 1 to be projected (hereinafter described an embodiment where a target 1 is to be projected but the invention can be addressed to the simultaneous projection of a plurality of targets; in the latter case, the targets are juxtaposed and each resting on the support surface 4, one of the targets being driven by the rotation arm directly and driving the other targets by force transmission).
  • the support surface 4 does not only aim at simply guiding the target 1 during the projection movement involved by the rotation arm 2, but also provides adjustment of the parameters of the application of the force of the arm, by means of a particular configuration of its position relative to the arm.
  • the bearing surface 4 has a portion of offset configured so that the spacing between the trajectory of the launching arm and the offset portion is increasing in the direction of rotation of the throwing arm 2.
  • the entirety of the bearing surface 4 is formed by such an offset portion. This is the case illustrated in the different figures. Other solutions are also possible.
  • a first part, in the direction of rotation of the throwing arm 2, of the bearing surface 4 may have a certain configuration while the offset portion is formed on the end of the path of the target 1 in contact with the support surface 4.
  • the offset portion is made in curvilinear and concave form, the concavity being oriented on the side of the launch arm 2. According to one possibility, the distance between the offset portion and the launching arm 2 increases gradually, with a derivative constant.
  • the offset portion comprises, and more precisely in the case of the figures is constituted, a portion of circular profile. More specifically, the circular profile portion is eccentric relative to the axis of rotation 3 of the throwing arm 2. More specifically, the offset axis 14 of the circular profile portion is parallel to the axis of rotation 3 and located at distance from it.
  • the figure 1 shows a first embodiment of the machine of the invention with a first configuration of the launch arm 2.
  • the launch arm 2 comprises, at its free end, a thrust surface 5 constituting the zone on which the arm 2 applies the projection force to the circular section portion of the target 1.
  • the thrust surface 5 is flat and configured to be applied on the target 1 in parallel with the wafer of the circular section portion of this target 1.
  • the thrust surface 5 extends from the distal end of the throwing arm 2 which then also constitutes the distal end 6 of the thrust surface 5 towards the axis of rotation 3.
  • the length of the thrust surface 5 is indicatively 50% or more of the length of the arm between its distal end 6 and the axis of rotation 3.
  • the fashion realization of the figure 1 has a throwing arm 2 provided with an intermediate portion between the portion at which the pivot is located about the axis of rotation 3 and the portion carrying or constituting the thrust surface 5.
  • This intermediate portion is represented by the elbow 7 at the figure 1 .
  • the formation of such a bend 7 allows to adjust the relative position of the arm 2 and the target 1 in particular in the starting position, that is to say at the beginning of the projection movement.
  • the distance formed by the bend 7 between the direction of the thrust surface 5 and its parallel passing through the axis of rotation 3 may be between 10 and 150 millimeters for a circular profile offset portion of a radius of the order of 500 to 600 millimeters.
  • the bearing surface 4 ensures the optimal positioning of the target 1 relative to the fulcrum exerting the thrust of the throwing arm 2 on the target in question.
  • the bearing surface 4 comprises or consists of a portion of offset itself constituted or having a portion of circular profile in the case shown.
  • the circular profile illustrated has an axis 14 offset relative to the axis 3.
  • the offset portion is formed in the form of a cylinder sector centered on the axis 14.
  • the materials used for the bearing surface 4 do not are not limited; it may be a metal part or plastic. According to an advantageous possibility, the bearing surface 4 is selected so that it offers less friction of the target 1 than the throwing arm 2 via its thrust surface 5.
  • the bearing surface 4 may consist of a portion of bent metal sheet following a concave curvilinear profile advantageously circular.
  • the thrust surface 5 preferably has friction-enhancing means on the target 1 such as relief elements that increase the gripping force or a selection of one or more high-friction materials. such as a portion of elastomer or natural rubber.
  • the movement of the arm 2 is cyclic so that it travels at a 360 ° angle during a launch cycle. More specifically, it operates a mobility powerfully projecting the target 1 according to a first angular sector, preferably less than 180 °. Then, it operates a return to initial position ready for a subsequent projection following a second additional angular sector of the first.
  • the bearing surface 4 is configured to provide contact with the target 1 so as to adjust its positioning.
  • this contact takes place along an angular sector of the order of 90 ° and advantageously less than or equal to 90 °.
  • a primary direction Dp which can, for example, be oriented in a vertical plane and correspond to a reference direction at the beginning of movement.
  • the figure 2 shows the positioning of a target 1 and a launch arm 2 at the primary direction Dp. More specifically, the target is in contact with the support surface 4 located on one side of the primary direction Dp, while the launch arm 2 is located on the other side of the direction Db.
  • the bearing surface 4 on which the target 1 is actually in contact thus begins slightly downstream of Dp relative to the direction of rotation of the throwing arm 2.
  • the direction Db is oriented substantially vertically and constitutes the offset direction between the axis of rotation 3 and the offset axis 14 of the circular profile of the offset portion.
  • the axis 14 is thus parallel and placed above, at a distance relative to the axis 3.
  • the component of this shift oriented along the direction Db is referenced C1.
  • this component is the only component of the offset of the eccentric configuration of the offset portion.
  • the value of this offset may be between 10 and 60% of the radius of the circular profile portion and more preferably substantially 35% of this radius.
  • the Figures 2 to 7 show another embodiment with a different configuration of the throwing arm 2.
  • the throwing arm 2 is configured so that the thrust surface 5 is oriented in a plane including or approaching the axis of rotation 3.
  • the figure 2 illustrates that the direction Dp passes through the axis 3.
  • the offset existing between the axis 3 and the axis 14 comprises a component C1 equivalent position to that described for the embodiment of the figure 1 and a component C2 of direction perpendicular to the component C1, that is to say, in a preferred embodiment, oriented so as to be included in a substantially horizontal plane.
  • the component C1 is of greater length than the component C2.
  • the component C2 may have a length of between 2% and 10% of the radius of the circular profile portion and more preferably a length of about 5% of this radius. According to an additional or alternative possibility, this component C2 is also oriented on the side of the axis of rotation 3 where the circular profile portion, namely towards the left part of the axis of rotation 3 in the configuration of the figures, is located. .
  • the distal end 6 of the thrust surface 5 is in the vicinity of the offset portion at the projection start position, substantially around the primary direction Dp, corresponding to the starting position 8 illustrated in FIG. figure 2 .
  • the distal end 6 tends to move away from the bearing surface 4 as revealed in the successive figures 3 to 7 to a position finalizing the release of the target 1 out of the support surface 4.
  • At least one target 1 is first delivered storage means 10 at which the targets 11 are stacked.
  • a transfer zone 12 ensures the displacement of the target 1 in question towards the loading zone at which the target 1 is brought into contact with the support surface 4 advantageously at the level of the offset portion.
  • a situation equivalent to that presented to the figure 3 is then produced.
  • the effect of gravity is countered by the presence of the bearing surface 4 to maintain the target 1 by its portion of circular section (here following its edge).
  • the target 1 is in contact with the throwing arm 2. Before the start of the projection, the contact of the throwing arm 2 is not necessary but, to avoid shocks, it is advantageous that this contact pre-exists at the beginning of the push.
  • the figure 3 shows this same configuration by illustrating the angle formed between the tangent T to the target 1 (and also tangent to the offset portion at the point of contact of the target 1, the offset portion being here circular profile) relative to the direction Dp of the thrust surface 5.
  • the angle formed between T and Dp is here for example of the order of 65 ° (64.8 ° in the illustration) corresponding to an acute angle involving a relatively inward direction of thrust to the bearing surface 4.
  • a subsequent phase of the rotation of the throwing arm 2 is presented in figure 4 where the direction Db is at the primary direction Dp.
  • the target 1 has then evolved a little along the bearing surface 4 in the direction of rotation of the arm 2.
  • the contact point of the support surface 4 and the target 1 being further apart in this configuration than in FIG. the previous relative to the axis of rotation 3, the angle formed between the tangent T and the direction Db increases.
  • a value of 72.8 ° is recorded in the case of the figure 4 .
  • a final position 9 is reached at which the target 1 reaches the end of the bearing surface 4 so that the projection is obtained out of the machine and there is no contact between the target 1 and the bearing surface 4.
  • the distal end 6 of the thrust surface 5 which comes into contact with the target 1. Due to the particular configuration of the machine of the invention, the finalization of the projection is performed while a clean rotation movement of the high target 1 has been generated. This promotes the stability of the target in space and optimizes the projection distance.
  • the progressive spacing between the offset portion and the throwing arm 5 is configured so as to change the angle between the tangent T and the direction Db from a value less than 90 ° at the beginning of the projection to a value greater than 90 ° at the end of the projection.
  • the cooperation between the launch arm 2 and the target 1 is configured so that the direction of the thrust force at the point of contact between the target 1 and the thrust surface 5 is located according to the diameter of the target 1, at its portion of circular section or above a diameter of the target 1 passing through the point of contact between the target 1 and the thrust surface 5, the opposite of the zone where the bearing surface 4 is in contact with the target 1. That is to say, it is preferable that the point of contact between the target 1 and the thrust surface 5 is furthest from the zone where the bearing surface 4 is in contact with the target 1.
  • the offset portion is adjustable in angular position so as to adjust the output position of the target 1 to be projected.
  • the offset portion may be more or less inclined relative to the rest of the machine so that the end of the offset portion is located higher or lower and more or less inclined according to the vertical.
  • the output of the target 1 is substantially vertical
  • the tangent to the offset portion at the final end of the bearing surface 4 is substantially vertical.
  • a pivot of the bearing surface 4 about its axis 14, in a trigonometric direction, would guide differently the tangent to the bearing surface 4 at the exit zone of the target 1 to incline the projection angle relative to the vertical. In an extreme case, it limits the portion of useful offset (that is to say the length of this portion on which the target 1 is in effective support) so as to produce an ejection at a substantially horizontal angle.
  • the vertical direction is the direction oriented according to the orientation of the gravitational force, the horizontal direction being perpendicular to the vertical direction, along the line of gravity. horizon.
  • the radius of the circular profile of the offset portion is advantageous for the radius of the circular profile of the offset portion to be greater than the length of the arm between its distal end and the axis of rotation 3.
  • the bearing surface 4 operates on the target advantageously located in a plane perpendicular to the direction of rotation of the launching arm 2.
  • the axis of rotation of the launching arm may comprise a vertical component not null and or a non-zero horizontal component.
  • the length of the throwing arm between the axis of rotation 3 and the distal end 6 is of the order of 300 to 450 millimeters.
  • a component C1 of offset between the axis 3 and the axis 14 of the order of 150 to 200 millimeters gives satisfaction.
  • the beginning of the offset zone where the contact of the target 1 and the support surface 4 actually takes place is offset by the order of 10 to 20 ° following the direction of rotation of the throwing arm 2.
  • the end of the bearing surface 4 is advantageously less than 100 ° from the beginning of the surface and preferably in an angular sector less than 90 °.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Sliding-Contact Bearings (AREA)
  • Toys (AREA)
  • Friction Gearing (AREA)
  • Apparatus For Radiation Diagnosis (AREA)

Claims (16)

  1. Zielabschussmaschine (1), die einen Abschnitt mit kreisrundem Querschnitt aufweist, wobei die genannte Maschine einen in Rotation um eine Rotationsachse (3) mobilen Abschussarm (2) und eine Aufstützfläche (4) des Abschnitts mit kreisrundem Abschnitt aufweist,
    wobei die Aufstützfläche (4) einen versetzten Abschnitt aufweist, der derart konfiguriert ist, dass die Beabstandung zwischen der Bahn des Abschussarms (2) und dem versetzten Abschnitt gemäß der Rotationsrichtung des Abschussarms (2) ansteigend ist und einen Abschnitt mit kreisrundem Profil einer Achse (14) umfasst, die relativ zur Rotationsachse (3) versetzt und zur Rotationsachse (3) parallel ist, gekennzeichnet dadurch, dass die Verschiebung zwischen der versetzten Achse (14) und der Rotationsachse (3) eine Komponente (C1) nicht Null gemäß einer primären Richtung umfasst, die durch einen Durchmesser der Bahn des Abschussarms (3) definiert ist, der sich in einer vertikalen Ebene befindet, wobei die genannte Komponente (C1) relativ zur Rotationsachse (3) gegenüber dem Abschnitt mit kreisrundem Profil angeordnet ist.
  2. Maschine gemäß dem voranstehenden Anspruch, bei der der Abschnitt mit kreisrundem Profil einen winkelförmigen Sektor kleiner als oder gleich 90° abdeckt.
  3. Maschine gemäß einem der voranstehenden Ansprüche, bei der die Komponente (C1) gemäß der primären Richtung eine zwischen 10 % und 60 % des Radius des Abschnitts mit kreisförmigem Profil inbegriffene Länge hat.
  4. Maschine gemäß dem voranstehenden Anspruch, bei der die Komponente (C1) gemäß der primären Richtung eine Länge von deutlich 35 % des Radius des Abschnitts des kreisförmigen Profils hat.
  5. Maschine gemäß einem der voranstehenden Ansprüche, bei der die Verschiebung zwischen der versetzten Achse (14) und der Rotationsachse (3) eine Komponente (C2) nicht null gemäß einer sekundären Richtung umfasst, die durch einen Durchmesser der Bahn des Abschussarms (3), der sich in einer horizontalen Ebene befindet, definiert ist.
  6. Maschine gemäß dem voranstehenden Anspruch, bei der die Komponente (C2) gemäß der sekundären Richtung auf der Seite der Rotationsachse (3) ausgerichtet ist, auf der sich der Abschnitt mit kreisförmigem Profil befindet.
  7. Maschine gemäß einem der voranstehenden Ansprüche, bei der die Komponente (C2) gemäß der sekundären Richtung eine zwischen 2 % und 10 % des Radius des Abschnitts mit kreisförmigem Profil inbegriffen ist.
  8. Maschine gemäß dem voranstehenden Anspruch, bei der die Komponente gemäß der sekundären Richtung eine Länge von deutlich 5 % des Radius des Abschnitts mit kreisförmigem Profil hat.
  9. Maschine gemäß einem der voranstehenden Abschnitte, bei der die Länge der Verschiebung zwischen der versetzten Achse (14) und der Rotationsachse (3) zwischen 2 % und 90 % des Radius des Abschnitts mit kreisförmigem Profil inbegriffen ist.
  10. Maschine gemäß einem der voranstehenden Ansprüche, bei der der Abschussarm eine Schubfläche (5) umfasst, die derart ausgerichtet ist, dass sie parallel zur Fläche des Abschnitts mit kreisförmigem Profil des Ziels (1) ist.
  11. Maschine gemäß dem voranstehenden Anspruch, bei der die Schubfläche (5) eben ist.
  12. Maschine gemäß dem voranstehenden Anspruch, bei der die Rotationsachse (3) in der Ebene der Schubfläche (5) inbegriffen ist.
  13. Maschine gemäß Anspruch 10 oder 11, bei der der Abschussarm (2) einen Winkel (7) zwischen der Rotationsachse (3) und der Schubfläche (5) umfasst.
  14. Maschine gemäß Anspruch 10 bis 13, bei der die Schubfläche (5) rutschfeste Mittel umfasst.
  15. Maschine gemäß Anspruch 10 bis 14, bei der der Abschussarm (2) konfiguriert ist, damit das distale Ende (6) der Schubfläche (5) sich in der Nähe des Abschnitts mit kreisrundem Profil in einer Ausgangsposition des Abschusses befindet.
  16. Maschine gemäß einem der voranstehenden Ansprüche, bei der die Aufstützfläche (4) in einer Winkelposition relativ zum Abschussarm (2) anpassbar ist.
EP11796715.8A 2010-12-17 2011-12-16 Zielabschussmaschine Active EP2652436B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1060667A FR2969276B1 (fr) 2010-12-17 2010-12-17 Machine de lancement de cibles
PCT/EP2011/073103 WO2012080489A1 (fr) 2010-12-17 2011-12-16 Machine de lancement de cibles

Publications (2)

Publication Number Publication Date
EP2652436A1 EP2652436A1 (de) 2013-10-23
EP2652436B1 true EP2652436B1 (de) 2015-02-25

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EP11796715.8A Active EP2652436B1 (de) 2010-12-17 2011-12-16 Zielabschussmaschine

Country Status (8)

Country Link
US (1) US9052169B2 (de)
EP (1) EP2652436B1 (de)
CN (1) CN103339464B (de)
CA (1) CA2821369A1 (de)
ES (1) ES2537277T3 (de)
FR (1) FR2969276B1 (de)
RU (1) RU2013132980A (de)
WO (1) WO2012080489A1 (de)

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US9061217B2 (en) * 2013-09-13 2015-06-23 Mattel, Inc. Projectile launcher
FR3016208B1 (fr) * 2014-01-08 2016-02-05 Laporte Holding Dispositif de lancement de cibles pour le tir sportif a depart instantane avec moyens de blocage actifs sur l'arbre de rotation du bras de lancement
US10545011B1 (en) * 2019-02-19 2020-01-28 Subshot, Llc Target disk throwing system
FR3095856B1 (fr) * 2019-05-10 2021-05-21 Laporte Holding Machine de lancement de cibles
US11617934B2 (en) 2019-08-07 2023-04-04 Robert M. SHIRLEY Auto feed hockey puck passing mechanism
US10859349B1 (en) * 2019-12-18 2020-12-08 Cheh-Kang Liu Micro switch adjustment structure of a throwing trap
US11052300B1 (en) * 2020-09-16 2021-07-06 Cheng-Yi Shie Flying disc launcher
US11015896B1 (en) * 2020-10-23 2021-05-25 Franklin Sports, Inc. Flying disc launcher

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Also Published As

Publication number Publication date
CN103339464B (zh) 2015-01-28
ES2537277T3 (es) 2015-06-05
RU2013132980A (ru) 2015-01-27
CA2821369A1 (fr) 2012-06-21
CN103339464A (zh) 2013-10-02
US9052169B2 (en) 2015-06-09
US20130269667A1 (en) 2013-10-17
WO2012080489A1 (fr) 2012-06-21
EP2652436A1 (de) 2013-10-23
FR2969276A1 (fr) 2012-06-22
FR2969276B1 (fr) 2013-09-27

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