EP3660441B1 - Ausklappvorrichtung eines ausklappbaren elements, insbesondere eines griffs, für ein waffensystem - Google Patents

Ausklappvorrichtung eines ausklappbaren elements, insbesondere eines griffs, für ein waffensystem Download PDF

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Publication number
EP3660441B1
EP3660441B1 EP19207544.8A EP19207544A EP3660441B1 EP 3660441 B1 EP3660441 B1 EP 3660441B1 EP 19207544 A EP19207544 A EP 19207544A EP 3660441 B1 EP3660441 B1 EP 3660441B1
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Prior art keywords
deployable element
deployable
support piece
deploying
deploying device
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EP19207544.8A
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English (en)
French (fr)
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EP3660441C0 (de
EP3660441A1 (de
Inventor
Lucas CHAPIN
Grégory CESAR
Clyde Laheyne
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MBDA France SAS
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MBDA France SAS
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Publication of EP3660441B1 publication Critical patent/EP3660441B1/de
Publication of EP3660441C0 publication Critical patent/EP3660441C0/de
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41C—SMALLARMS, e.g. PISTOLS, RIFLES; ACCESSORIES THEREFOR
    • F41C23/00—Butts; Butt plates; Stocks
    • F41C23/04—Folding or telescopic stocks or stock parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41C—SMALLARMS, e.g. PISTOLS, RIFLES; ACCESSORIES THEREFOR
    • F41C23/00—Butts; Butt plates; Stocks
    • F41C23/16—Forestocks; Handgrips; Hand guards

Definitions

  • the present invention relates to a device for deploying a deployable element for a weapon system.
  • the present invention applies to a weapon system, in particular to a mobile firing station, in particular of the type carried on the shoulder, such as a missile launcher or a launcher. rocket, which requires quick handling, by deploying a gripping element, such as a handle for example.
  • a gripping element such as a handle for example.
  • a handle of such a weapon system has a certain size. Also, to reduce this bulk, in particular during storage and transport of the weapon system when the latter is not in use, it is known to provide a handle which is folded in this situation, while being deployable. Such a deployable handle is capable of being brought from the folded position to a stable deployed position for its use and the handling of the weapon system.
  • a device In order to implement this deployment, a device is known with which an operator must carry out the following operations: press a button to unlock the movement of the handle which is initially locked in the folded position, then move the handle, in particular by rotation, to bring it into the deployed position, and finally lock it in this deployed position before it can be used.
  • the object of the present invention is to remedy this drawback, which is achieved by a deployable element and device for deploying said deployable element according to claim 1. It relates to a device for deploying a deployable element (or capable of being deployed) for a weapon system, making it possible to implement rapid deployment, at least partially automatic, with reduced intervention by an operator.
  • said deployment device comprises a support part, the deployable element is rotatably mounted on said support part and is connected via at least one elastic element to said support part, said element deployable comprises at least one pin, said pin being able to move along a curved guide of the support part and to take one or the other of two stable positions respectively in two housings provided in the support part , these stable positions corresponding respectively to a folded position and a deployed position of the deployable element, and at least said guide and said elastic element are configured to generate an automatic deployment of the deployable element to said deployed position as soon as the the deployable element is subjected to a rotation (from the folded position to the deployed position) whose angle is greater than or equal to a so-called unlocking angle.
  • said deployment device allows rapid deployment of the deployment element, for example a handle of a missile launcher, with reduced intervention by the operator (consisting simply of bringing the deployable element beyond said locking angle) and a partially automatic deployment.
  • Said deployment device also has other advantages.
  • it makes it possible in particular to hold load cases in logistics and to take up all the transverse forces in use, and it comprises a reduced number of components.
  • said guide and said elastic element are configured so that the force of the deployable element on the support piece, generated by the elastic element, is located outside a friction cone created at the point of contact between the deployable element and the support part, that is to say at the point of contact of the pin on the curved guide.
  • the deployable element comprises two pins arranged on either side of said deployable element
  • the support piece comprises two curved guides, and each of said pins is able to move along a said curved guides of the support piece.
  • the curved guide(s) have an arcuate shape between said two housings (defining the stable positions).
  • said deployable element is provided with at least one oblong slot, in which is mounted a pin fixed to the support piece, to allow rotation of the deployable element on said support piece.
  • said deployable element is provided with two oblong slots, in each of which is mounted each time a pin fixed to the support piece.
  • the support part is provided with leaf springs at the level of the ankle(s).
  • said deployable element comprises a bevel between one end of the oblong slot and an edge of said deployable element.
  • said pin is a projecting element whose peripheral edge comprises a substantially semi-circular section.
  • said deployment device can be applied to any type of mechanical element to be deployed (manually in the prior art) on a weapon system.
  • said deployable element corresponds to one of the following elements: a gripping element such as a handle in particular, a stop, a sighting system.
  • the present invention also relates to a weapon system, which comprises at least one deployable element and a device for deploying said deployable element, such as that described above.
  • the present invention can be applied to various weapon systems, and more particularly although not exclusively to mobile, in particular portable, weapon systems.
  • the weapon system corresponds to a missile launcher or a rocket launcher and/or said deployable element corresponds to one of the following elements of this weapon system: a gripping element such as a handle in particular, a stop, a sighting system, preferably with a handle.
  • the device 1 illustrating the invention and represented on the figure 1 is a device for deploying a deployable element 2 (that is to say an element suitable or intended to be deployed) for a weapon system 3, of which only a small part has been represented very schematically on the figure 1 .
  • a deployable element 2 that is to say an element suitable or intended to be deployed
  • the present invention can be applied to various weapon systems, and in particular to portable weapon systems, which require the deployment of a deployable element 2, and this in particular during its use.
  • the weapon system 3 corresponds to a rocket launcher or a missile launcher, in particular an anti-tank missile or a short-range anti-aircraft missile.
  • the deployable element 2 corresponds, for example, to one of the following elements of this weapon system: a gripping element such as a handle in particular, a stop, a sighting system, for example a sight .
  • the deployable element 2 is a handle 4.
  • the deployable handle 4 comprises a usual gripping (or gripping) zone 5, which is able to be taken in hand by an operator (not shown), in particular the operator planning to do operate the weapon system 3.
  • Said deployment device 1 also comprises, as shown in the figure 1 , a support piece 6.
  • This support part 6 can be either a part of the weapon system 3, or an independent part which is intended to be fixed on the weapon system 3 by a usual fixing means.
  • the support piece 6 comprises a plate 7 slightly inclined at its center with respect to a mean plane Pm.
  • the mean plane Pm of the plate 7 is orthogonal to a plane of symmetry P corresponding to a plane of symmetry of the deployment device 1.
  • the support part 6 is also provided with two substantially flat side branches 8 and 9, arranged substantially parallel to the plane of symmetry P, symmetrically with respect to this plane of symmetry P, on either side of the latter.
  • the support piece 6 thus has a shape rider general.
  • the plate 7 can be attached to a part of the weapon system 3 or correspond to a part of the latter.
  • the deployable element 2 is mounted on the support part 6, so as to be able to pivot.
  • the support piece 6 comprises two pegs 10 and 11 ( figure 1 and 2 ) each mounted on one of said branches 8 and 9, respectively on the internal face 8A, 9A of these branches 8 and 9.
  • the support part 6 (visible in its details on the picture 2 ) is shown in thin line to illustrate a transparency allowing to see the details of the deployable element 2 mounted on this support part 6, in order to simplify the understanding of the deployment device 1.
  • the internal adjective is determined towards the plane of symmetry P, on either side of said plane of symmetry P, as illustrated by arrows I1 and I2 on the figure 2 , and the external adjective is defined in reverse.
  • the superior adjective is determined according to the meaning (illustrated by an arrow E on the figures 1 to 3 ) of the deployable element 2 towards the support part 6, and the lower adjective is determined according to the direction opposite to the direction E.
  • each of said oblong slots 12 and 13 is formed in an upper part of a branch 14, 15 of the deployable element 2.
  • the two branches 14 and 15 planes are provided, on either side of the plane of symmetry P, at the upper part of the deployable element 2, as shown in the figures 3 and 4 .
  • the deployable element 2 is linked via at least one elastic element 16 to said support piece 6.
  • the elastic element 16 is a spring 17.
  • This spring 17 comprises a loop 17A, 17B at each of its longitudinal ends, as shown in particular on the figures 5 and 6 .
  • These loops 17A and 17B surround pins 18 and 19.
  • Pin 18 is inserted into holes 20 ( picture 2 ) made in the support piece 6, and the pin 18 is inserted into holes 21 ( picture 3 ) practiced in the deployable element 2.
  • the deployable element 2 comprises two pins 22 represented on the figure 1 , 3 and 4 , which are arranged on either side of the deployable element 2, on the outer faces 14A and 15A ( picture 3 ) of the branches 14 and 15 of the deployable element 2. Only the pin 22 of the branch 15 is visible on these figure 1 , 3 and 4 .
  • the support piece 6 further comprises two guides 23 and 24 curves.
  • the curved guides 23 and 24 represent, respectively, sections of a part of the peripheral edge of the branches 8 and 9 of the support part 6, as shown in the figure 2 .
  • Each of the curved guides 23 and 24 comprises a part 23A, 24A having the shape of an arc of a circle.
  • This part 23A, 24A is defined between two housings, a housing 23B, 24B and a housing 23C, 24C.
  • These housings 23B, 24B, 23C, 24C correspond to rounded recesses made in the peripheral edge of the branches 8 and 9, on either side of the arcuate part 23A, 24A.
  • Each pin 22 is able to move along the associated curved guide 23, 24 of the support part 6 and to take one or the other of two stable positions, respectively, in one or the other of the two housings (housing 23B, 24B on the one hand and housing 23C, 24C on the other hand) provided in the support part 6.
  • the support part 6 is provided with leaf springs 30 and 31 at the level of the pins 10 and 11, as represented on the picture 2 .
  • Each spring blade 30 and 31 is formed in a branch 8, 9 of the support part 6. These spring blades 30 and 31 facilitate the insertion of the pins 10 and 11 (which can thus be pushed slightly outwards) in the oblong slots 12 and 13 of the support piece 6, and thus facilitate the mounting of the deployable element 2 on the support piece 6.
  • the deployable element 2 comprises, on each of the branches 14 and 15, a bevel 27 between an upper end 28 of the oblong slot 12, 13 and an upper edge 29 of the deployable element 2.
  • These bevels 27, of which only one is visible on the figure 4 also facilitate the insertion of the pins 10 and 11 into the oblong slots 12 and 13 and thus the mounting of the deployable element 2 on the support part 6.
  • each pin 22 is a projecting element, the upper peripheral edge of which comprises a section 25 substantially in a semicircle. The rest of its peripheral edge is not an arc of a circle, and is provided with a beveled zone 26.
  • each pin 22 can also simply correspond to a projecting cylindrical section.
  • the deployment device 1, and in particular at least said guide 23, 24 curve and said elastic element 16 are configured (that is to say formed and arranged) so as to generate an automatic deployment of the deployable element 2 until to said deployed position P2 ( Picture 9 ), and this as soon as the deployable element 2 is subjected in the direction illustrated by an arrow H1 on the figure 7 (from the folded position P1 to the deployed position P2), to a rotation whose angle is greater than or equal to an unlocking angle ⁇ 0 ( figure 8 ).
  • This rotation (or pivoting) is generated by an operator who presses, preferably manually, on the deployable element 2 in the direction illustrated by the arrow H1 on the figure 7 .
  • the unlocking angle ⁇ 0 defines a unlocked position P3 (shown on the figure 8 ) of the deployable element 2. From this unlocking position P3, the end of the deployment up to the deployed position P2 of the figure 9 is carried out automatically, in the direction illustrated by an arrow H2 on the figure 8 .
  • the deployment device 1, and in particular the curved guides 23 and 24 and the elastic element 16 are configured so that the force F1 of the deployable element 2 on the support part 6, which is generated by the elastic element 16, is always located outside a friction cone C, as shown in the figures 5 and 6 respectively in an intermediate position P4 (corresponding for example to the unlocking position) and in the deployed position P2.
  • This friction cone C is created, in the usual way, at the point of contact PC between the deployable element 2 and the support part 6, that is to say at the point of contact of each pin 22 on the guide 23, 24 associated curve.
  • This point of contact PC therefore moves during the rotation of the deployable element 2 with respect to the support part 6, as illustrated by an arrow J on the figure 5 .
  • the friction cone C has a generatrix F2 which is defined along a direction normal to the tangent of the curve (of the guide 23, 24 curve) at the point of contact PC.
  • the friction cone C has an angle ⁇ with respect to the generatrix F2.
  • the force F1 it is defined from the point of contact PC parallel to the direction of the elastic element 16 (spring 17).
  • the deployment device 1 and in particular the curved guides 23 and 24 and the elastic element 16 are configured so that the following inequality is always satisfied: N. ⁇ ,
  • ⁇ ( figure 6 ) is the angle between on the one hand said force F1 of the deployable element 2 on the support piece 6, generated by the elastic element 16, and on the other hand the generatrix F2 of said friction cone C.
  • N is a safety factor which is greater than 1.
  • the operation of the deployment device 1, as described above, is as follows.
  • the deployable element 2 namely the handle 4, being in the folded state P1, as represented on the figure 7 , an operator pushes or pulls on the deployable element 2 in the direction illustrated by the arrow H1.
  • the deployment device 1 generates an automatic deployment of the deployable element 2 in the direction illustrated by the arrow H2, until it is brought into the deployed position P2 represented on the figure 9 .
  • the pin 22 is located in the housing 24C, the deployed position P2 is stable and no final locking is necessary.
  • deployment means the displacement, by pivoting (or rotation on an arc of a circle) of the deployable element 2, from the folded position P1 to the deployed position P2.
  • the deployable element 2 can be brought back by an operator from the deployed position P2 to the folded position P1, in particular for transporting the weapon system.
  • said deployment device 1 generates rapid deployment of the deployment element 2, for example a handle 4, with reduced operator intervention (consisting simply of bringing the deployable element beyond said locking angle ) and partially automatic deployment.
  • the deployment device 1 therefore allows quick handling of the weapon system 3, for example a mobile firing station carried on the shoulder or any other element requiring the integration of a quick and compact grip.
  • the deployment device 1 also makes it possible to achieve automatic positioning of the deployable element 2, in the deployed position P2, in which the weapon system 3 will be used, with a reduction in the number of movements of the operator which uses it.
  • the deployment device 1 makes it possible, by its design, to take up all the (transverse) forces on the plane normal to the axis of the deployable element 2, during its use.
  • the deployment device 1 makes it possible to block the deployable element 2 in the event of shocks, so to avoid inadvertent deployment.
  • the number of components of the deployment device 1 is reduced, and this by more than 50% compared to a usual device. This reduction in the number of components also makes it possible to reduce the cost of the deployment device 1.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)

Claims (14)

  1. Ausklappbares Element und Ausklappvorrichtung des ausklappbaren Elements für ein Waffensystem, wobei die Ausklappvorrichtung (1) ein Stützteil (6) umfasst, wobei das ausklappbare Element (2) drehbar auf dem Stützteil (6) angebracht ist und mithilfe mindestens eines elastischen Elements (16) mit dem Stützteil (6) verbunden ist, wobei das ausklappbare Element (2) mindestens einen Stift (22) umfasst, wobei der Stift (22) geeignet ist, sich entlang einer gekrümmten Führung (23, 24) des Stützteils (6) zu bewegen und jeweils in zwei Aufnahmen (23B, 24B; 23C, 24C), die im Stützteil (6) vorgesehen sind, die eine oder die andere von zwei stabilen Positionen (P1, P2) einzunehmen, wobei diese stabilen Positionen jeweils einer eingezogenen Position (P1) und einer ausgeklappten Position (P2) des ausklappbaren Elements (2) entsprechen,
    dadurch gekennzeichnet, dass mindestens die Führung (23, 24) und das elastische Element (16) dazu ausgelegt sind, ein automatisches Ausklappen des ausklappbaren Elements (2) bis zur ausgeklappten Position (P2) zu erzeugen, sobald das ausklappbare Element (2) ausgehend von der eingezogenen Position (P1) zur ausgeklappten Position (P2) einer Drehung unterzogen wird, deren Winkel größer oder gleich einem als Entriegelungswinkel (00) bezeichneten Winkel ist.
  2. Ausklappbares Element und Ausklappvorrichtung nach Anspruch 1,
    dadurch gekennzeichnet, dass die Führung (23, 24) und das elastische Element (16) zum Erzeugen des automatischen Ausklappens derart ausgelegt sind, dass die Kraft (F1) des ausklappbaren Elements (2) auf das Stützteil (6), die von dem elastischen Element (16) erzeugt wird, sich außerhalb eines Reibungskegels (C) befindet, der am Kontaktpunkt (PC) zwischen dem ausklappbaren Element (2) und dem Stützteil (6) geschaffen wird.
  3. Ausklappbares Element und Ausklappvorrichtung nach Anspruch 2,
    dadurch gekennzeichnet, dass mindestens die Führung (23, 24) und das elastische Element (16) zum Erzeugen des automatischen Ausklappens derart ausgelegt sind, dass die folgende Ungleichung erfüllt ist: N . β < α
    Figure imgb0003
    wobei in der Ungleichung:
    - β der Winkelwert des Reibungskegels (C) in Bezug auf seinen Generator (F2) ist;
    - α der Winkel zwischen der Kraft (F1) des ausklappbaren Elements (2) auf das Stützteil (6), die von dem elastischen Element (16) erzeugt wird, und dem Generator (F2) des Reibungskegels (C) ist; und
    - N ein Sicherheitskoeffizient größer als 1 ist.
  4. Ausklappbares Element und Ausklappvorrichtung nach einem der vorstehenden Ansprüche,
    dadurch gekennzeichnet, dass das ausklappbare Element (2) zwei Stifte (22) umfasst, die auf beiden Seiten des ausklappbaren Elements (2) eingerichtet sind, dadurch, dass das Stützteil (6) zwei gekrümmte Führungen (23, 24) umfasst, und dadurch, dass jeder der Stifte (22) geeignet ist, sich entlang einer der gekrümmten Führungen (23, 24) des Stützteils (6) zu bewegen.
  5. Ausklappbares Element und Ausklappvorrichtung nach einem der vorstehenden Ansprüche,
    dadurch gekennzeichnet, dass die gekrümmte(n) Führung(en) (23, 24) eine Kreisbogenform (23A, 24A) zwischen den Aufnahmen (23B, 24B; 23C, 24C) aufweisen.
  6. Ausklappbares Element und Ausklappvorrichtung nach einem der vorstehenden Ansprüche,
    dadurch gekennzeichnet, dass das ausklappbare Element (2) mit mindestens einem länglichen Schlitz (12, 13) versehen ist, in dem ein am Stützteil (6) befestigter Dübel (10, 11) angebracht ist, um die Drehung des ausklappbaren Elements (2) auf dem Stützteil (6) zu erlauben.
  7. Ausklappbares Element und Ausklappvorrichtung nach Anspruch 6,
    dadurch gekennzeichnet, dass das ausklappbare Element (2) mit mindestens zwei länglichen Schlitzen (12, 13) versehen ist, bei denen in jedem jeweils ein am Stützteil (6) befestigter Dübel (10, 11) angebracht ist.
  8. Ausklappbares Element und Ausklappvorrichtung nach einem der Ansprüche 6 und 7,
    dadurch gekennzeichnet, dass das Stützteil (6) an dem oder den Dübeln (10,11) mit Federblättern (30, 31) ausgestattet ist.
  9. Ausklappbares Element und Ausklappvorrichtung nach einem der vorstehenden Ansprüche,
    dadurch gekennzeichnet, dass das ausklappbare Element (2) eine Abschrägung (27) zwischen einem Ende (28) des länglichen Schlitzes (12, 13) und einem Rand (29) des ausklappbaren Elements (2) umfasst.
  10. Ausklappbares Element und Ausklappvorrichtung nach einem der vorstehenden Ansprüche,
    dadurch gekennzeichnet, dass der Stift (22) ein vorstehendes Element ist, dessen Umfangsrand einen im Wesentlichen halbkreisförmigen Abschnitt (25) umfasst.
  11. Ausklappbares Element und Ausklappvorrichtung nach einem der vorstehenden Ansprüche,
    dadurch gekennzeichnet, dass das ausklappbare Element (2) einem der folgenden Elemente entspricht: einem Griffelement (4), einem Anschlag, einem Visiersystem.
  12. Waffensystem,
    dadurch gekennzeichnet, dass es mindestens ein ausklappbares Element (2) und eine Ausklappvorrichtung (1) des ausklappbaren Elements (2) nach einem der Ansprüche 1 bis 11 umfasst.
  13. Waffensystem nach Anspruch 12,
    dadurch gekennzeichnet, dass es einem der folgenden Elemente entspricht: einem Flugkörperstartgerät, einem Raketenstartgerät.
  14. Waffensystem nach einem der Ansprüche 12 und 13,
    dadurch gekennzeichnet, dass das ausklappbare Element (2) einem der folgenden Elemente des Waffensystems (3) entspricht: einem Griffelement (4), einem Anschlag, einem Visiersystem.
EP19207544.8A 2018-11-28 2019-11-06 Ausklappvorrichtung eines ausklappbaren elements, insbesondere eines griffs, für ein waffensystem Active EP3660441B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1871885A FR3089002B1 (fr) 2018-11-28 2018-11-28 Dispositif de déploiement d’un élément déployable, en particulier une poignée, pour un système d’arme

Publications (3)

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EP3660441A1 EP3660441A1 (de) 2020-06-03
EP3660441B1 true EP3660441B1 (de) 2023-07-12
EP3660441C0 EP3660441C0 (de) 2023-07-12

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US (1) US11549779B2 (de)
EP (1) EP3660441B1 (de)
ES (1) ES2951565T3 (de)
FR (1) FR3089002B1 (de)
IL (1) IL283113B1 (de)
WO (1) WO2020109686A1 (de)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019133450A1 (en) 2017-12-27 2019-07-04 Magpul Industries Corp. Foldable firearm

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US601840A (en) * 1898-04-05 mcclean
US1340996A (en) * 1918-09-19 1920-05-25 Frank A Williams Gun-sight
US3327422A (en) * 1965-10-23 1967-06-27 Harris Gerald Bipod for attachment to a firearm
US6571502B1 (en) * 2001-12-20 2003-06-03 Smith & Wesson Corp. Electronically fired revolver utilizing a latch mechanism between trigger and hammer to implement firing
WO2009009663A2 (en) * 2007-07-11 2009-01-15 Hinds Richard A Jr Gun with internally stored bipod
US8599097B2 (en) * 2008-05-15 2013-12-03 Air Systems, Inc. Collapsible portable stand with telescoping support and integral storage case
US10429144B2 (en) * 2015-02-05 2019-10-01 Far League S.R.L. Automatic submachine gun for exploiting recoil comprising two opposing levers for the hammer, one associated with single-shot firing mode and the other with burst firing mode

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US20210396487A1 (en) 2021-12-23
WO2020109686A1 (fr) 2020-06-04
US11549779B2 (en) 2023-01-10
IL283113A (en) 2021-06-30
IL283113B1 (en) 2024-09-01
EP3660441C0 (de) 2023-07-12
ES2951565T3 (es) 2023-10-23
FR3089002A1 (fr) 2020-05-29
FR3089002B1 (fr) 2020-11-27
EP3660441A1 (de) 2020-06-03

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