EP3579945B1 - Gehäuse zur anordnung an einem fahrzeug und waffenanlage mit solch einem gehäuse - Google Patents
Gehäuse zur anordnung an einem fahrzeug und waffenanlage mit solch einem gehäuse Download PDFInfo
- Publication number
- EP3579945B1 EP3579945B1 EP18707079.2A EP18707079A EP3579945B1 EP 3579945 B1 EP3579945 B1 EP 3579945B1 EP 18707079 A EP18707079 A EP 18707079A EP 3579945 B1 EP3579945 B1 EP 3579945B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- wall
- plate
- housing
- edge
- housing according
- 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.)
- Active
Links
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims 3
- 239000004576 sand Substances 0.000 description 11
- 238000009423 ventilation Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 5
- 125000006850 spacer group Chemical group 0.000 description 5
- 238000011144 upstream manufacturing Methods 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 238000010304 firing Methods 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000008094 contradictory effect Effects 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910001234 light alloy Inorganic materials 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
- F42B39/20—Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
- F42B39/26—Packages or containers for a plurality of ammunition, e.g. cartridges
Definitions
- the technical field of the invention is that of boxes which are intended to be placed on a vehicle, and in particular a military vehicle.
- a particular casing is the one containing a weapon system, for example a missile launching system (these casings containing a gun or a missile are often referred to as “POD” in the aeronautical field).
- a weapon system for example a missile launching system
- POD missile launching system
- the boxes generally have a substantially parallelepiped shape comprising a front wall, a rear wall, a bottom wall, an upper wall and two side walls.
- the front and rear walls have at least one hole to allow the circulation of air in the housing in order to reduce the temperature inside thereof.
- a weapon system such as a missile.
- a weapon system comprises electronic and pyrotechnic components which are sensitive to temperature.
- the need for ventilation of the interior of a box is also present when the box contains electronic components or even food.
- the box according to the invention makes it possible, with a simple structure, to ensure the internal cooling of the box by natural convection, while preventing the clogging of the ventilation orifices.
- the subject of the invention is a box intended to be placed on a vehicle, in particular a vehicle military, and having a substantially parallelepipedal shape comprising a front wall, a rear wall, a lower wall, an upper wall and two side walls, the front and rear walls each comprising at least one hole to allow the circulation of air to the inside the case, case characterized in that at least one of the front or rear walls carries a plate which is arranged outside the case and at a distance from the said wall, the hole or holes in the wall in question being arranged ) in the vicinity of an upper edge of said wall, the housing further comprising at least a first slot allowing the passage of air between the plate and the wall in question, which slot is located in the vicinity of a lower edge of said wall, the plate also having at least a second dimension less than that of the wall considered so that there is at least a second slot constituted by the interval between a lateral edge of the pl aque and said wall, the housing comprising at least one sheet closing the space between the plate and the wall at
- the first slot or slots are carried by the plate and arranged in the vicinity of a lower edge of the plate.
- the plate may have at least a first dimension less than that of the wall considered such that at least a first slot is formed by the gap between a lower edge of the plate and said wall.
- the sheet may be extended at least on one edge beyond the plate so as to constitute a deflector.
- the sheet will not extend to the lower edge of the wall.
- the plate may include a notch cutting a lower angle so as to create an asymmetry of the plate.
- the plate may be an armored steel plate.
- the bottom wall of the casing may carry at least one water evacuation hole, a panel being arranged below the bottom wall and at a distance from the hole(s), panel comprising a central parallel part to the lower wall and extended by two side wings which gradually move away from the lower wall starting from the middle part.
- the lower wall of the casing may carry at least one water evacuation hole intended to be positioned facing a surface of a recess in the vehicle, the casing comprising at the level of its wall lower inclined planes on either side of the bottom wall carrying the holes.
- the casing may also carry a panel arranged below the bottom wall and at a distance from the holes, the panel extending below the inclined planes located on either side of the bottom wall.
- the invention also relates to a weapon system comprising at least one missile launcher disposed in such a casing.
- a vehicle 1 carries at a recess 2 a housing 3 according to the invention.
- the vehicle will for example be an armored military vehicle equipped with a turret and the recess 2 will be arranged on the turret.
- the housing may be integral with the turret and the horizontal part 2a of the recess 2 will in this case simply correspond to the chassis of the vehicle.
- the box 3 will then be placed at a distance from the chassis of the vehicle.
- the box 3 may contain a weapon system, such as a missile or rocket launcher.
- This system is not shown in detail. It comprises a plate carrying a launcher and the case 3 is in particular orientable in elevation by pivoting around a pointing axis 4. Pointing in bearing is ensured by the pivoting of the turret itself.
- the box 3 can be fixed relative to the turret.
- the weapon system arranged in the housing 3 which will be designed so as to be able to pivot around the pointing axis 4. This rotation will be coupled to a means making it possible to open the roof 7 of the box 3 to allow the exit of the weapon system, the box 3 remaining fixed.
- a front wall 5 of the casing is pivotally mounted with respect to the casing.
- the chain line 6 represents the pivot axis of the front wall 5.
- the box 3 has a substantially parallelepipedal shape and it therefore comprises a front wall 5, a rear wall 10, a bottom wall (not visible on the picture 1a ), an upper wall 7 and two side walls 8 and 9.
- the front 5 and rear 10 walls each have at least one hole to allow the circulation of air inside the housing 3.
- the air circulates by forced convection and it is the movement of the vehicle which ensures the circulation of air. air which enters the box 3 through the front wall 5 and leaves it through the rear wall 10.
- FIG. 1b shows a side view of the box 3.
- the box 3 has a bottom wall 18 which is not flat but which comprises a front part 18a and a rear part 18b substantially parallel and separated by a front connection plane 18c.
- This configuration materializes a rear box 19 which allows in particular to house the means for motorizing the deployment of the casing 3 containing the weapon system.
- a rear inclined plane 18d connects the rear part 18b of the lower wall to the rear wall 10.
- THE figures 2a and 2b show a first embodiment of the front part of the case 3.
- the front wall 5 carries a plate 11 which is arranged outside the box 3 and at a distance d from the front wall 5.
- the plate 11 is fixed at a distance from the front wall 5 by means of spacers 12 (here four cylindrical spacers). Plate 11 is screwed onto spacers 12 which are themselves screwed or welded to wall 5.
- the wall 5 carries holes 13 which here consist of five grooves 13 made in the wall 5. These grooves are shown in dotted lines on the figure 2a because they are hidden by plate 11.
- the grooves 13 are arranged near an upper edge 5a of the front wall 5.
- grooves 13 could be replaced by a set of cylindrical holes.
- the box 3 includes a first slot 14 allowing the passage of air between the plate 11 and the wall 5.
- This first slot 14 is located near a lower edge 5b of the front wall 5.
- plate 11 has a first dimension D1 which is less than the corresponding dimension of front wall 5.
- first slot 14 is formed by the gap between a lower edge 11a of plate 11 and said front wall 5.
- the plate 11 has a second dimension D2 which is less than the dimension corresponding to the front wall 5. There is therefore a second slot 15 which is formed by the gap between a side edge 11b of the plate 11 and the front wall 5.
- the box 3 also comprises a sheet 16 which closes the space 17 between the plate 11 and the front wall 5 at the level of the upper edge 5a of the front wall 5.
- This sheet 16 also extends along a side edge 5c of the front wall 5 and also closes at this level the space 17 separating the plate 11 and the wall 5. As can be seen in the figure 2b , the sheet 16 does not extend beyond the lower edge 11a of the plate 11.
- the sheet 16 does not extend as far as the lower edge 5b of the wall 5. This results in a lateral slot 20.
- the sheet 16 is extended at least on one of its edges, beyond the plate 5, so as to constitute a deflector 16a.
- the sheet 16 thus covers two sides of the plate 11, and it also covers, in the example drawn, the cut corner 11e separating the edges 11c and 11d of the plate 11.
- the air When driving the vehicle, the air enters through the first slot 14 between the plate 11 and the front wall 5.
- the sheet 16 prevents the evacuation of the air which is forced to flow towards the grooves 13 worn by the front wall 5.
- the air is introduced into the casing 3 by these grooves 13.
- the sand which would be led towards the front wall 5 with the flow of air is hindered in its progression by its own mass. It cannot penetrate through the grooves 13.
- the sand falls by gravity and is evacuated through the slot 20.
- the excess air is evacuated through the second slot 15 which also partly allows the evacuation of the sand to the outside and prevents the clogging of the space 17.
- the profile of the deflector 16 provides lateral protection for the plate 11 and channels the incident air flow.
- the rear wall of the housing 3 could be equipped with a similar mounting plate 11. It is not necessary to describe such a configuration, the figures described and associated with a front wall can be transposed for a rear wall. This assembly is however not essential, the ventilation movement being carried out in a privileged way from the front to the rear of the case 3.
- the plate 11 must on the other hand be installed at the level of the wall which is situated forwards in the normal direction of progression of the vehicle.
- the plate 11 will advantageously be made of shielded steel. It will then contribute to the protection of the box 3 against the firing of automatic weapons.
- the front wall 5 may be made of a light alloy, for example aluminum.
- This mode differs from the previous one only by the dimensions of the plate 11 and by the shape of the first slot 14.
- the first slot 14 is a single slot parallel to the lower edge 11a of the plate and which is drilled directly into the plate 11.
- This plate 11 has a length D1 which is therefore substantially equal to the corresponding dimension of the wall before 5.
- the plate 11 has here, as in the previous mode, a second dimension D2 which is less than the corresponding dimension of the front wall 5. There is therefore always a second slot 15 which is formed by the interval between a side edge 11b of the plate and the front wall 5.
- This second slot could be omitted but it is necessary that the space separating the casing 3 from the wall 2a of the recess 2 be sufficient to allow the lateral evacuation of excess air and sand.
- This embodiment makes it possible to increase the surface covered by the front wall 5 by the plate 11, and therefore the protection of the casing against shots.
- FIG 4 shows a third embodiment of the invention, a mode which differs from the first embodiment only by the presence on the plate 11 of a triangular notch 21 which is provided at the level of a lower angle and which intersects this lower angle .
- the notch 21 is here more particularly positioned at the level of the lower left corner, located opposite the slot 20.
- This notch 21 makes it possible to create an asymmetry in the flow of the air inside the space 17 separating the plate 11 and the wall 5. This asymmetry results in a vortex flow of the air in the space 17 which favors the evacuation of the grains of sand.
- the notch 21 could be made in the form of a rounding ensuring the asymmetry of the lower part of the plate 11.
- the figure 4 can be associated with figure 2b , the sectional view being identical for these two embodiments.
- FIG 5 shows, enlarged and in partial section, the lower part of the box 19 which is visible at the figure 1b .
- the lower wall 18b carries holes 22 allowing the evacuation of water from the box 19.
- a panel 23 is arranged below the lower wall 18b and at a distance from the holes 22.
- This panel 23 comprises a middle part 23a which is parallel to the lower wall 18b and which is extended by two side wings 23b and 23c which move away gradually from the bottom wall 18b from the middle part 23a.
- the panel 23 is fixed to the lower wall 18b by spacers 24.
- This progressive profile upstream and downstream of the holes 22 creates, during the rolling of the vehicle, a Venturi effect which makes it possible to facilitate the ejection of the few grains of sand which, despite the entry plate 11, or during a firing phase (real or simulated), would have nevertheless succeeded in penetrating into the box 3.
- the holes 22 make it possible, when the vehicle is stationary, to improve the cooling of the interior of the casing 3 by a natural convection effect, the fresh air then enters the casing 3 through the holes 22 and comes out. at the level of the holes in the front 5 and rear 10 walls.
- the side wings 23b and 23c of the panel 23 are here flat plate portions forming a constant angle with the bottom wall 18b.
- the wings could also be made in the form of curved plate portions.
- venturi effect below box 19 can be obtained in different ways.
- FIG. 6 thus shows, in a way analogous to the figure 1b , a side view of the box 3.
- the bottom wall 18 of the box 3 is positioned close to the plane 2a of the recess 2.
- the rear part 18b of the bottom wall 18, which also forms the bottom of the box 19, is delimited by the plane front connection 18c and the rear inclined plane 18d which have substantially symmetrical inclinations with respect to a vertical plane.
- the air is channeled between the plane 2a of the recess 2 and the inclined planes 18c and 18d.
- the converging then diverging profile of the air passage section, upstream and downstream of the holes 22, creates, when the vehicle is running, the desired Venturi effect. This facilitates the ejection of the grains of sand.
- FIG 7 shows another embodiment in which the casing 3 is at a relatively large distance from the plane 2a of the recess 2.
- a panel 23 is arranged below the bottom wall 18b and at a distance holes 22. Panel 23 attaches to bottom wall 18b by spacers 24.
- the panel 23 is here flat and parallel to the bottom wall 18b.
- the panel is longer than the bottom wall 18b. It cooperates with the inclined planes 18c and 18d which extend upstream and downstream the lower wall 18b so as to form an air passage section which has a convergent profile upstream of the holes 22, then diverges downstream of the holes 22
- the desired Venturi effect is created, which makes it possible to facilitate the ejection of the grains of sand.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
- Vehicle Step Arrangements And Article Storage (AREA)
- Body Structure For Vehicles (AREA)
Claims (11)
- - Gehäuse (3) zur Anordnung an einem Fahrzeug, vor allem an einem Militärfahrzeug, mit einer etwa parallelepipedischen Form, aufweisend eine vordere Wand (5), eine hintere Wand (10), eine untere Wand (18), eine obere Wand (7) und zwei seitliche Wände (8, 9), wobei die vordere Wand und die hintere Wand jeweils mindestens eine Bohrung (13) aufweisen, um die Zirkulation der Luft im Inneren des Gehäuses zu gestatten, wobei das Gehäuse dadurch gekennzeichnet ist, dass mindestens eine von der vorderen (5) oder hinteren (10) Wand eine Platte (11) trägt, die außerhalb des Gehäuses (3) und von der Wand beabstandet angeordnet ist, wobei die Bohrung(en) (13) der entsprechenden Wand (5) in der Nähe eines oberen Randes (5a) der Wand angeordnet ist/sind, wobei das Gehäuse (3) im Übrigen mindestens einen ersten Schlitz (14) aufweist, der den Durchgang der Luft zwischen der Platte (11) und der entsprechenden Wand (5) gestattet, wobei der Schlitz in der Nähe eines unteren Randes (5b) der Wand (5) lokalisiert ist, wobei die Platte (11) ebenfalls mindestens eine zweite Abmessung (D2) hat, die kleiner als die der entsprechenden Wand (5) derart ist, dass es mindestens einen zweiten Schlitz (15) gibt, der von dem Intervall zwischen einem seitlichen Rand (11b) der Platte (11) und der Wand (5) gebildet ist, wobei das Gehäuse mindestens ein Blech (16) aufweist, das den Raum (17) zwischen der Platte (11) und der Wand (5) im Bereich eines oberen Randes (5a) und mindestens eines seitlichen Randes (5c) der entsprechenden Wand verschließt.
- - Gehäuse nach Anspruch 1, dadurch gekennzeichnet, dass der oder die erste(n) Schlitz(e) (14) von der Platte (11) getragen werden und in der Nähe eines unteren Randes (11a) der Platte eingerichtet sind.
- - Gehäuse nach Anspruch 1, dadurch gekennzeichnet, dass die Platte (11) mindestens eine erste Abmessung (D1) hat, die kleiner als die der entsprechenden Wand (5) ist, so dass mindestens ein erster Schlitz (14) vom Abstand zwischen einem unteren Rand (11a) der Platte (11) und der Wand (5) gebildet wird.
- - Gehäuse nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass das Blech (16) mindestens über einen Rand jenseits der Platte (11) derart verlängert ist, dass ein Abweiser (16a) gebildet wird.
- - Gehäuse nach Anspruch 4, dadurch gekennzeichnet, dass sich das Blech (16) nicht bis zum unteren Rand (5b) der Wand (5) erstreckt.
- - Gehäuse nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass die Platte (11) eine Kerbe (21) aufweist, die eine untere Ecke derart schneidet, dass eine Asymmetrie der Platte (11) entsteht.
- - Gehäuse nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass die Platte (11) eine Stahlpanzerplatte ist.
- - Gehäuse nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass die untere Wand (18b) mindestens ein Wasserableitungsloch (22) trägt, wobei eine Tafel (23) unterhalb der unteren Wand (18b) und von dem oder den Löchern (22) beabstandet angeordnet ist, wobei die Tafel einen mittleren Teil (23a) aufweist, der parallel zu der unteren Wand (18b) ist und von zwei seitlichen Flügeln (23b, 23c) verlängert wird, die sich nach und nach von der unteren Wand (18b) ab dem mittleren Teil (23a) entfernen.
- - Gehäuse nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass die untere Wand (18b) mindestens ein Wasserableitungsloch (22) trägt, das einer Oberfläche (2a) einer Vertiefung des Fahrzeugs zugewandt ist, wobei das Gehäuse (3) im Bereich seiner unteren Wand (18b) geneigte Ebenen (18c, 18d) beiderseits der unteren Wand (18b) aufweist, die die Löcher (22) tragen.
- - Gehäuse nach Anspruch 9, dadurch gekennzeichnet, dass das Gehäuse (3) eine Tafel (23) trägt, die unterhalb der unteren Wand (18b) und von den Löchern (22) beabstandet angeordnet ist, wobei sich die Tafel (23) unterhalb der geneigten Ebenen (18c, 18d) erstreckt, die sich beiderseits der unteren Wand (18b) befinden.
- - Waffensystem, dadurch gekennzeichnet, dass es mindestens einen Raketenwerfer umfasst, der in einem Gehäuse (3) nach einem der vorangehenden Ansprüche angeordnet ist.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1700137A FR3062717B1 (fr) | 2017-02-07 | 2017-02-07 | Boitier destine a etre dispose sur un vehicule et systeme d'arme comprenant un tel boitier. |
PCT/FR2018/050186 WO2018146395A1 (fr) | 2017-02-07 | 2018-01-26 | Boîtier destiné à être disposé sur un véhicule et système d'arme comprenant un tel boîtier |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3579945A1 EP3579945A1 (de) | 2019-12-18 |
EP3579945B1 true EP3579945B1 (de) | 2023-03-22 |
Family
ID=59296885
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18707079.2A Active EP3579945B1 (de) | 2017-02-07 | 2018-01-26 | Gehäuse zur anordnung an einem fahrzeug und waffenanlage mit solch einem gehäuse |
Country Status (7)
Country | Link |
---|---|
US (1) | US11193732B2 (de) |
EP (1) | EP3579945B1 (de) |
ES (1) | ES2946585T3 (de) |
FI (1) | FI3579945T3 (de) |
FR (1) | FR3062717B1 (de) |
PL (1) | PL3579945T3 (de) |
WO (1) | WO2018146395A1 (de) |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2394041A1 (fr) | 1977-06-09 | 1979-01-05 | Saint Gobain | Etuvage de bandes continues de fibres isolantes |
US7610726B2 (en) | 2005-05-05 | 2009-11-03 | Tapco International Corporation | Housing assembly |
DE102006025214B3 (de) * | 2006-05-29 | 2007-11-08 | Reel Reinheimer Elektronik Gmbh | Anordnung einer Antenne an einem Container |
ES2437177T3 (es) * | 2009-03-30 | 2014-01-09 | Director General, Defence Research & Development Organisation | Sistema de lanzamiento de misiles móvil y método del mismo |
CA2763183A1 (en) | 2012-01-05 | 2013-07-05 | Pumpwell Solutions Ltd. | Vent cover |
DE102012025314B4 (de) * | 2012-12-22 | 2016-04-07 | Diehl Bgt Defence Gmbh & Co. Kg | Flugkörperbehälter |
DE202014003420U1 (de) | 2014-04-24 | 2014-06-02 | Walter Reitz | Einteilige Wetterschutzhaube mit Dichtung und "unsichtbarer" Befestigung |
FR3026479B1 (fr) | 2014-09-26 | 2016-09-02 | Nexter Systems | Lance missile |
AR114811A1 (es) * | 2018-02-27 | 2020-10-21 | Orica Int Pte Ltd | Sistema de transporte y entrega de materiales explosivos reconfigurables |
-
2017
- 2017-02-07 FR FR1700137A patent/FR3062717B1/fr active Active
-
2018
- 2018-01-26 FI FIEP18707079.2T patent/FI3579945T3/fi active
- 2018-01-26 PL PL18707079.2T patent/PL3579945T3/pl unknown
- 2018-01-26 EP EP18707079.2A patent/EP3579945B1/de active Active
- 2018-01-26 ES ES18707079T patent/ES2946585T3/es active Active
- 2018-01-26 US US16/483,135 patent/US11193732B2/en active Active
- 2018-01-26 WO PCT/FR2018/050186 patent/WO2018146395A1/fr unknown
Also Published As
Publication number | Publication date |
---|---|
ES2946585T3 (es) | 2023-07-21 |
FI3579945T3 (fi) | 2023-05-25 |
PL3579945T3 (pl) | 2023-05-02 |
US20200271414A1 (en) | 2020-08-27 |
US11193732B2 (en) | 2021-12-07 |
EP3579945A1 (de) | 2019-12-18 |
WO2018146395A1 (fr) | 2018-08-16 |
FR3062717B1 (fr) | 2021-01-01 |
FR3062717A1 (fr) | 2018-08-10 |
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