The technical field of the invention relates to that of the housings that are intended to be arranged on a vehicle, and in particular on a military vehicle.
It is common to provide a vehicle with a housing, for example a luggage compartment, making it possible to carry additional equipment.
The military vehicles are often provided with such housings which make it possible to carry equipment, provisions or weapons.
A specific housing is the one enclosing a weapon system, for example a missile launching system (these housings enclosing a gun or a missile are often called “POD” in the aeronautical sector).
As an example, patents FR3026479 and FR2394041 describe missile launching housings that are deployable.
The housings generally have a substantially parallelepiped shape comprising a front wall, a rear wall, a lower wall, an upper wall and two side walls.
Generally, the front and rear walls comprise at least one bore to allow air to flow inside the housing in order to reduce the temperature therein.
This venting need is particularly important when the housing encloses a weapon system, such as a missile. Indeed, such weapon system comprises electronic and pyrotechnic components which are sensitive to temperature.
The need for venting the interior of a housing is also important when the housing encloses electronic components or even provisions.
When venting is ensured by natural convection through openings, the problem is to prevent the penetration of fine particles, such as grains of sand, into the housing. Therefore, there are conflicting needs for facilitating the air flow while preventing the penetration of foreign bodies.
Unfortunately, the current solutions which implement fine-mesh gratings are not sufficient to prevent the penetration of sand. Furthermore, these gratings are likely to get clogged when the vehicle moves, thereby limiting the cooling performance for the interior of the housing.
Patent US2014/174283 also describes a container carrying a missile launching system. This container is a 20-foot standardized container of the ISO type, provided with an access door 6, but no particular venting means is described. Patent application US2009/0073077 also describes a device for installing an antenna on a wall of a container. The antenna is attached on an inner wall of the container and is inserted inside one of the venting holes carried by a wall of the container. The holes are covered by a housing which forms an inner cavity in front of the venting holes, the cavity being open at its inner part which comprises slots. As mentioned above, this grating-based closure is not sufficient to prevent the penetration of sand.
The invention aims to provide a housing making it possible to alleviate such disadvantages.
The housing according to the invention makes it possible, with a simple structure, to ensure that the interior of the housing is cooled by natural convection, while preventing the venting holes from getting clogged.
Thus, the invention relates to a housing intended to be arranged on a vehicle, in particular a military vehicle, and having a substantially parallelepiped 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 bore for allwing air to flow inside the housing, the housing being characterized in that at least one of the front or rear walls carries a plate which is arranged outside the housing and at a distance from said wall, the at least one bore of the wall in question being located at the vicinity of an upper edge of said wall, the housing further comprising at least one first slot allowing air to pass between the plate and the wall in question, the slot being located at the vicinity of a lower edge of said wall, the plate also having at least one second dimension that is less than that of said wall in question such that there is at least one second slot constituted by the gap between a lateral edge of the plate and said wall, the housing comprising at least one sheet metal closing the gap between the plate and the wall at an upper edge and at at least one lateral edge of the wall in question.
According to one embodiment, the one or more first slots are carried by the plate and provided at the vicinity of a lower edge of the plate.
According to another embodiment, the plate could have at least one first dimension that is less than that of the wall in question such that at least one first slot is constituted by the gap between a lower edge of the plate and said wall.
Advantageously, the sheet metal could extends, at least on an edge, beyond the plate so as to constitute a baffle.
Preferably, the sheet metal will not extend to the lower edge of the wall.
Advantageously, the plate could comprise a notch cutting a lower corner so as to create a dissymmetry in the plate.
The plate could be an armor steel plate.
According to a particular embodiment, the lower wall of the housing could carry at least one water discharge hole, a panel being arranged below the lower wall and at a distance from the at least one hole, the panel comprising a median part that is parallel to the lower wall and extended by two lateral wings which gradually move away with respect to the lower wall, from the median part.
According to a particular embodiment, the lower wall of the housing could carry at least one water discharge hole intended to be positioned in front of a surface of a recess of the vehicle, the housing comprising at its lower wall inclined planes on either side of the lower wall that carries the holes.
Furthermore, the housing could carry a panel arranged below the lower wall and at a distance from the holes, the panel extending below the inclined planes located on either side of the lower wall.
The invention also relates to a weapon system comprising at least one missile launcher arranged in such a housing.
The invention will be better understood upon reading the following description of particular embodiments, made with reference to the appended drawings in which:
If referring to
The vehicle will be for instance an armored military vehicle provided with a turret and the recess 2 will be provided on the turret. The housing could be secured to the turret and in that case the horizontal part 2a of the recess 2 will simply match with the vehicle chassis. Then, the housing 3 will be arranged at a distance from the vehicle chassis.
The housing 3 could enclose a weapon system, such as a rocket or missile launcher.
This system is not shown in detail. It includes a plate carrying a launcher and in particular the housing 3 can be directed in elevation by pivoting around an aiming axis 4. Traverse is ensured by pivoting the turret itself.
Alternatively, the housing 3 can be fixed with respect to the turret. In that case, it is the weapon system arranged in the housing 3 that will be designed so as to be able to pivot around the aiming axis 4. This pivoting will be coupled to a means making it possible to open the roof 7 of the housing 3 in order to allow the weapon system to exit, with the housing 3 remaining fixed.
To enable firing, for instance firing of the missile, a front wall 5 of the housing is pivotally mounted with respect to the housing. The swiveling axis of the front wall 5 is shown by the chain-dotted line 6. Alternatively, as mentioned above, when the housing 3 is fixed and the roof 7 of the housing 3 opens to allow the weapon system to exit, the front wall 5 remains fixed.
All these structural members are not the subject-matter of the invention and therefore are not described in detail. Reference could be made to patent FR3026479 which describes an embodiment of a launching housing.
The housing 3 has a substantially parallelepiped shape and thus comprises a front wall 5, a rear wall 10, a lower wall (not visible in
The front 5 and rear 10 walls each comprise at least one bore to allow air to flow inside the housing 3. The air flows by forced convection, and it is the movement of the vehicle that ensures that the air flows by entering the housing 3 at the front wall 5 and exiting at the rear door 10.
As it can be particularly seen in
The plate 11 is attached at a distance from the front wall 5 via spacers 12 (here, four cylindrical spacers). The plate 11 is screwed on the spacers 12 which are themselves screwed or welded to the wall 5.
It can be seen in the figures that the wall 5 carries bores 13 which are here constituted by five grooves 13 provided in the wall 5. These grooves are shown in dotted lines in
The grooves 13 are located at the vicinity of an upper edge 5a of the front wall 5.
Of course, the grooves 13 could be replaced with a set of cylindrical bores.
Furthermore, the housing 3 comprises a first slot 14 allowing air to flow between the plate 11 and the wall 5.
This first slot 14 is located at the vicinity of a lower edge 5b of the front wall 5.
As it can be seen in
As it can also be seen in
The housing 3 also comprises a sheet metal 16 which closes the gap 17 between the plate 11 and the front wall 5 at the upper edge 5a of the front wall 5.
This sheet metal 16 also extends along a lateral edge 5c of the front wall 5 and also closes at this emplacement the gap 17 separating the plate 11 and the wall 5. As it can be seen in
Thus, the sheet metal 16 does not extend to the lower edge 5b of the wall 5. This results in a lateral slot 20.
The sheet metal 16 is extended at least at one of its edges, beyond the plate 11, so as to constitute a baffle 16a.
Thus, the sheet metal 16 covers two sides of the plate 11, and it also covers, in the example shown, the cut corner 11e separating the edges 11c and 11d of the plate 11.
The operation of this assembly is as follows.
When the vehicles moves, air enters through the first slot 14 between the plate 11 and the front wall 5. The sheet metal 16 prevents the discharge of air which has to flow towards the grooves 13 carried by the front wall 5. The air enters inside the housing 3 through these grooves 13. The progression of the sand that would be carried to the front wall 5 with the air flow is hindered due to its own mass. It cannot penetrate through the grooves 13. The sand falls by gravity and is discharged through the slot 20.
The excess air is discharged through the second slot 15 which also partially allows the sand to be discharged outwards and prevents the gap 17 from getting clogged.
The profile of the baffle 16a ensures a lateral protection of the plate 11 and channels the incident air flow.
The rear wall of the housing 3 could be equipped with a similar plate 11 mounting. It is not necessary to describe such an arrangement, the figures described and associated with a front wall can be transposed to a rear wall. However, this mounting is not essential, the venting movement taking place preferably from the front to the rear of the housing 3.
However, the plate 11 must necessarily be installed at the wall located forwards in the normal advance direction of the vehicle.
Furthermore, the plate 11 will advantageously be made of armor steel. It will then participate to the protection of the housing 3 against firing of automatic weapons. The front wall 5 could be made of a lightweight alloy, for example aluminum.
This embodiment differs from the preceding one in the dimensions of the plate 11 and the shape of the first slot 14.
In this embodiment, the first slot 14 is a simple lumen parallel to the lower edge 11a of the plate and that is directly drilled in the plate 11. This plate 11 has a length D1 which is thus substantially equal to the respective dimension of the front wall 5.
Here, as in the preceding embodiment, the plate 11 has a second dimension D2 which is less than the respective dimension of the front wall 5. Therefore, there is still a second slot 15 which is constituted by the gap between a lateral edge 11b of the plate and the front wall 5.
This second slot could be omitted, but it is essential that the gap separating the housing 3 from the wall 2a of the recess 2 be large enough to make the lateral discharge of excess air and sand possible.
This embodiment makes it possible to increase the surface of the front wall 5 that is covered by the plate 11, and thus the protection of the housing against firing.
Here, more particularly the notch 21 is positioned at the left lower corner, located on the opposite side relatively to the slot 20.
This notch 21 makes it possible to create a dissymmetry in the air flow inside the gap 17 separating the plate 11 and the wall 5. This dissymmetry results in a vortex air flow inside the gap 17, thereby facilitating the discharge of grains of sand. The notch 21 could be provided as a curve ensuring the dissymmetry of the lower part of the plate 11.
A panel 23 is arranged below the lower wall 18b and at a distance from the holes 22. This panel 23 comprises a median part 23a that is parallel to the lower wall 18b and is extended by two lateral wings 23b and 23c gradually moving away with respect to the lower wall 18b, from the median part 23a.
The panel 23 is attached to the lower wall 18b by spacers 24. This gradual profile upstream and downstream of the holes 22 generates, when the vehicle moves, a Venturi effect that facilitates the discharge of grains of sand that would have succeeded to penetrate into the housing 3 despite the inlet plate 11, or during a (actual or simulated) firing phase.
Furthermore, when the vehicle stops, the holes 22 improve the cooling of the interior of the housing 3 by a natural convection effect, fresh air thus entering the housing 3 through the holes 22 and exiting therefrom at the bores of the front 5 and rear 10 walls.
The lateral wings 23b and 23c of the panel 23 are here planar plate portions forming a constant angle with the lower wall 18b. The wings could also be provided as curved plate portions.
The Venturi effect below the box 19 can be obtained in a different manner.
Thus,
When the vehicle moves forward, the air is channeled between the plane 2a of the recess 2 and the inclined planes 18c and 18d. The converging and then diverging profile of the air flow section, upstream and downstream of the holes 22, generates the desired Ventury effect when the vehicle moves. Thus, the discharge of grains of sand is facilitated.
Such an arrangement is possible when the housing 3 is located near the plane 2a of the recess 2.
Here, unlike the panel described with reference to
Number | Date | Country | Kind |
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1700137 | Feb 2017 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2018/050186 | 1/26/2018 | WO | 00 |