MAGAZINE, CARTRIDGE AND METHOD FOR VARIABLE PROJECTILE CLUSTER DENSITY OF A COUNTERMEASURE
20190178613 ยท 2019-06-13
Inventors
Cpc classification
B64D7/00
PERFORMING OPERATIONS; TRANSPORTING
F41F1/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B5/15
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41F7/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41A21/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D1/02
PERFORMING OPERATIONS; TRANSPORTING
F42B12/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F42B5/15
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41F1/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D7/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A magazine for storing and launching countermeasures arranged in cartridges, comprising a plurality of longitudinal cartridge cases forming the magazine, where the magazine comprises a tilting means adapted to tilt the cartridge cases, such that the openings of the cartridge cases can be directed in a selected direction, and where a countermeasure comprises multiple projectiles, and where the magazine is adapted to launch a first countermeasure and a second countermeasure, where the projectile cluster density of the first countermeasure is lower than the projectile cluster density of the second countermeasure. The advantage of the invention is that a countermeasure can be directed towards an incoming object and can be adapted for the distance to the object before it is launched.
Claims
1-15. (canceled)
16. A magazine (2) for storing and launching countermeasures (5) arranged in cartridges (12), comprising a plurality of longitudinal cartridge cases (6) forming the magazine (2), wherein: the cartridge cases (6) are arranged to each other in a slidable manner in a longitudinal direction, the magazine (2) comprises a tilting means adapted to tilt the cartridge cases (6), such that an opening (14) of a cartridge case (6) can be directed in a selected direction, a countermeasure (5) comprises multiple projectiles (11), the magazine (2) is adapted to launch a first countermeasure (40) and a second countermeasure (41), and the projectile cluster density of the first countermeasure (40) is lower than the projectile cluster density of the second countermeasure (41).
17. Magazine according to claim 16, wherein the magazine (2) is adapted to launch a third countermeasure (42), wherein the projectile cluster density of the third countermeasure is higher than the projectile cluster densities of the first and the second countermeasure (41).
18. Magazine according to claim 17, wherein the magazine (2) comprises at least two different types of cartridges (43, 44), wherein a first cartridge type (43) is provided with a fixed choke (46) having a first diameter and a second cartridge type (44) is provided with a fixed choke (47) having a second diameter, wherein the first diameter is larger than the second diameter.
19. Magazine according to claim 18, wherein the magazine (2) comprises at third cartridge type (45) provided with a fixed choke (48) having a third diameter, wherein the third diameter is smaller than the first and the second diameter.
20. Magazine according to claim 19, wherein the second countermeasure (41) is adapted to be launched before the first countermeasure (40).
21. Magazine according to claim 20, wherein the third countermeasure (42) is adapted to be launched before the second countermeasure (41).
22. Magazine according to claim 16, wherein the magazine (2) comprises a plurality of cartridges (12), wherein a cartridge comprises an adjustable choke (17) adapted to be set to a desired diameter.
23. Magazine according to claim 22, wherein the adjustable choke (17) comprises a plurality of wedge shaped elements (25) adapted to be moved along a longitudinal direction of the cartridge (12) in order to adjust the diameter of the choke (17).
24. Magazine according to claim 23, wherein a wedge shaped element (25) is moved by an actuator (27) positioned in the recoil plate (8) of a cartridge (12).
25. Magazine according to claim 22, wherein the adjustable choke (17) comprises a sleeve (29) having a conical front portion (31) adapted to be moved along a longitudinal direction of the cartridge (12) in order to adjust the diameter of the choke (17).
26. Magazine according to claim 25, wherein the magazine (2) is adapted to set the adjustable choke (17) of a first cartridge to a first diameter and to set the adjustable choke (17) of a second cartridge to a second diameter, wherein the second diameter is smaller than the first diameter, before the countermeasures are launched.
27. Magazine according to claim 26, wherein the projectiles (11) are spherical or multifaceted and that the diameter of a projectile is in the range between 1-8 mm.
28. A cartridge (12) adapted to be used in a magazine (2) according to claim 16, comprising cartridge (12) comprises an adjustable choke (17) adapted to be set to a desired diameter, wherein the adjustable choke (17) comprises a plurality of wedge shaped elements (25) adapted to be moved along a longitudinal direction of the cartridge (12) in order to adjust the diameter of the choke (17).
29. A method for launching a countermeasure (5) from a magazine (2), wherein the magazine comprises a tracking system comprising an active position sensor adapted to detect the position of an incoming object, wherein the countermeasure (5) is arranged in a cartridge case (6), wherein the magazine (2) comprises a plurality of cartridge cases (6), wherein the method comprises the steps of: launching a second countermeasure (41) having a predefined projectile cluster density, and thereafter launching a first countermeasure (40) having a lower projectile cluster density.
30. An aircraft comprising at least one magazine according to claim 16.
Description
BRIEF DESCRIPTION OF DRAWINGS
[0033] The invention will be described in greater detail in the following, with reference to the embodiments that are shown in the attached drawings, in which
[0034]
[0035]
[0036]
[0037]
[0038]
[0039]
MODES FOR CARRYING OUT THE INVENTION
[0040] The embodiments of the invention with further developments described in the following are to be regarded only as examples and are in no way to limit the scope of the protection provided by the patent claims. References such as longitudinal, horizontal, vertical, forward, rearward, sideway, etc. refer to directions of an aircraft flying forwards in a normal orientation. For a magazine used on ground, directions may also be referred to as forward, rearward, sideway, left, right, etc.
[0041] An aircraft 1 in the form of a helicopter, shown in
[0042] Since the helicopter may hover or may fly upwards, downwards, forwards or sideways and with varying speeds, the desired launch direction will also depend on the actual flight direction of the helicopter as well as on the relative azimuth and elevation angle to an incoming object. The launch direction will also depend on the actual mounting position on the helicopter. Preferably, several magazines are mounted in different positions on a helicopter in order to cover different launch directions. In this way, it will be possible to launch countermeasures in most directions from the helicopter, such that the flight direction of the helicopter is not important in order to direct the countermeasure to a desired position.
[0043] A magazine 2 is described in more detail with reference to
[0044] The magazine 2 comprises a plurality of cartridge cases 6 arranged in a matrix with a number of rows and a number of columns. A suitable number of rows may e.g. be 4-8 and a suitable number of columns may e.g. be 5-12, depending on the size of a cartridge. A cartridge case is designed with a longitudinal body, preferably having a square or rectangular cross-section. The cross-section of a cartridge may e.g. be 11 or 1*2 inches and the length may e.g. be 8 inches. A cartridge case is adapted to receive a countermeasure 5 stored in a cartridge 12. The countermeasure cartridge 12 is attached to the cartridge case in a known way. The countermeasure cartridge 12 is further connected to a launch system of the aircraft, comprising a firing control. The countermeasure cartridge may either be connected directly to the launch system of the aircraft, or is connected to an electronic control unit of the magazine, which in turn is connected to the launch system of the aircraft. The interface between the countermeasure cartridge and the electronic control unit of the aircraft may be a mechanical system, which can only launch the countermeasure, or it may be an electrical interface, comprising two way communication between the countermeasure cartridge and the aircraft.
[0045] A countermeasure is in this example provided with a plurality of small projectiles or pellets, which may be spherical or may be multifaceted. The projectiles are preferably made from metal, and preferably a heavy metal such as lead, steel, tungsten or bismuth. The projectiles may also be made from a synthetic or ceramic material. The projectiles are launched with a predefined projectile cluster density. Preferably, at least two countermeasures are launched consecutively, having two different projectile cluster densities. The projectile cluster density of consecutive countermeasures can be varied in different ways.
[0046] One possibility is to use countermeasures with fixed chokes having different diameters. A countermeasure having a choke with an appropriate diameter can then be launched at a selected moment. Another possibility is to use countermeasures with an adjustable choke. The choke can then be adjusted to a desired diameter before the countermeasure is launched.
[0047] The actual projectile cluster density of a countermeasure is selected in dependency of the distance to an incoming object and/or of the type of the incoming object. In this way, it is possible to launch a countermeasure having a relatively high projectile cluster density if the incoming object is relatively far away, and to launch a countermeasure having a lower projectile cluster density if the incoming object is closer. By varying the projectile cluster density in dependency of the distance to the incoming object, the likelihood of hitting the incoming object with a sufficient amount of projectiles will increase.
[0048] The aircraft, the vehicle or the ground system comprises a tracking system adapted to detect and track an incoming flying object, e.g. a shell from a handheld shell launcher. The tracking system may be positioned in the magazine or in the aircraft and comprises an active position sensor that is adapted to detect the position and speed of an incoming object and the distance to the incoming object. When an incoming object has been detected, the tracking system tilts the magazine in a direction towards the incoming object and a fine tracking function will then continuously follow the incoming object by fine adjusting the magazine direction. In this way, the launch openings of the cartridge cases will be directed towards the incoming object. The tracking system will further continuously track the distance to the incoming object and will determine the required projectile cluster density for the countermeasures depending on the distance to the incoming object. The control system may either select between countermeasures having fixed chokes in order to determine which countermeasure to use, or the system may adjust the choke of a countermeasure having an adjustable choke. The magazine will thus be ready to launch a countermeasure when the incoming object has reached a predefined position and distance.
[0049] The tracking system may be integrated in the magazine and the active position sensor may be positioned in a cartridge case in the magazine. It is also possible to position the active position sensor on the outside of the magazine. The active position sensor is adapted to detect and to follow a flying incoming object. A suitable and robust sensor may be a radar, a lidar or a vision system. It is also possible to use one type of sensor for the detection of the position of the incoming object and another sensor for the fine tracking of the incoming object. In this case, the fine tracking function may use an optical system.
[0050] The active position sensor is connected to an electronic control unit adapted to control the tilting means of the magazine in dependency of the signal from the active position sensor. When the tracking system detects an incoming object, the electronic control unit will control the magazine to point in the general direction of the incoming object and the fine tracking function will then fine adjust the direction of the magazine to point directly to the incoming object. The electronic control unit is also connected to an external control system, e.g. of an aircraft, and receives information regarding the flight parameters of the aircraft. The electronic control unit will also send information regarding an incoming object to the control system of the aircraft. The electronic control unit will further control the projectile cluster density of a countermeasure that is to be launched.
[0051] The magazine 2 comprises a base 7, which is the base of the magazine and is used to mount the magazine to e.g. an aircraft by the use of an attachment means. The base is also used to absorb the recoil force created when a countermeasure is launched. The base will absorb and distribute the created force over the entire base area of the base.
[0052] Each cartridge case 6 is attached to the base with a flexible joint 16, e.g. a ball joint, such that the cartridge case can be tilted in two directions, At the bottom of each cartridge case, a recoil plate 8 is arranged which is used to attach each cartridge case to the base through the flexible joint. The recoil plate will also transfer the recoil force from a countermeasure to the base when a countermeasure is launched. A cartridge case 6 is attached to a recoil plate 8 in a removable way, such that a countermeasure cartridge 12 can be inserted in the cartridge case. Since the cartridge cases are interconnected to each other to form the magazine, it is possible that all cartridge cases are removed at the same time as one unit when countermeasure cartridges are to be replaced. The flexible joint of one cartridge case will be arranged at a fixed position and will be mounted to the base in a fixed way. This cartridge case will be referred to as the tilt control cartridge case. This cartridge case will be provided with a tilting means which will tilt the magazine in a desired direction.
[0053] A cartridge case 6 comprises a cavity 13, adapted to store a countermeasure cartridge 12 and is provided with an opening 14 at the front of the cartridge case. The countermeasure cartridges 12 are connected to a launch control unit (not shown) for feeding launch signals to the countermeasure cartridges. When a countermeasure has been launched, the countermeasure cartridge can be replaced with a new countermeasure cartridge by removing the remains of the launched countermeasure cartridge from the cartridge case and by inserting a new countermeasure cartridge into the cartridge case.
[0054] The base of the magazine is further provided with means that allows the flexible joint of the other cartridge cases to move somewhat along the x-axis and the z-axis. This will allow the distance between two flexible joints to vary. When the cartridge cases are tilted, the flexible joints will have to move slightly away from each other due to the relative geometric change between the cartridge cases. Depending on the required tilt angle for the magazine, it would e.g. also be possible to attach each flexible joint to the base with a resilient means such as rubber. It is important that the flexible joints bear against the base, since the recoil force from the recoil plate is transferred through the flexible joint to the base. Other interconnecting methods are also possible.
[0055] A magazine 2 positioned in a resting or idle position 50 is shown in
[0056] The cartridge cases of the magazine are adapted to be tilted from the resting position 50, shown in
[0057] The magazine 2 shown in
[0058] When an incoming object is identified, and the distance to the incoming object is within a predefined range, two or more countermeasures are launched at the incoming object. The control system determines when and which countermeasure is to be launched in order to be able to destroy the incoming object. A countermeasure having a relatively high projectile cluster density is e.g. launched at a first moment when the incoming object is at an outer limit of the range. With a relatively high projectile cluster density, there is a fair chance that enough projectiles will hit the incoming object, which will cause the incoming object to detonate. When the incoming object is closer, a countermeasure having a lower projectile cluster density may be launched. The lower projectile cluster density will give a wider spread of projectiles which will increase the likelihood of hitting the incoming object with enough projectiles. A wider spread of particles is of advantage when the incoming object is closer since the tolerances in aiming and launching will affect the ability to hit exactly at the desired position. Preferably, two, three or more countermeasures having different projectile cluster densities are launched in a consecutive order with a small time delay.
[0059] The magazine 2 shown in
[0060] One advantage of the inventive magazine is that the openings of the cartridge cases can be directed towards an incoming object. By being able to point directly towards an incoming object, it is possible to use countermeasures that can disarm or destroy the incoming object. Often, countermeasures can only disturb active incoming objects but have no effect on passive incoming objects. The inventive magazine will allow e.g. a helicopter to protect itself from passive shells in an efficient and cost-effective way.
[0061] In
[0062] The cartridge comprises an outer wall 18 which preferably is circular or square, even if other shapes are possible. The outer wall is provided with a bottom 19 which comprises a squib 20 adapted to ignite the explosive charge 21 of the countermeasure. The cartridge further comprises an inner wall 22 housed inside the outer wall. The inner wall is circular and holds the small metal projectiles 11 of the countermeasure 5. The small metal projectiles may be spherical or multifaceted having a diameter of between 1 to 8 mm. The inner wall is preferably made from a metal. The front section 34 of the inner wall is provided with longitudinal slits 23 arranged in parallel to the centre axis 15 of the cartridge, which will create flexible tongues 24 at the front section of the inner wall. The length of the slits is e.g. in the range of to 1/10 of the length of the cartridge. The number of tongues is preferably four but could also be six or eight. The width of the slits is such that the tongues will bear against each other when the tongues are in their innermost position.
[0063] The cartridge is further provided with wedge-shaped elements 25 arranged between the outer wall and the tongues, at the front section of the inner wall. The wedge-shaped elements are slidable in a direction parallel with the centre axis 15 of the cartridge.
[0064] In
[0065] A wedge-shaped element may in one example cover up to a fourth of the circumference of the cartridge opening, and may extend over up to 90 degrees of the opening. The actuator is preferably positioned at the base of the cartridge, in the recoil plate of the cartridge case, and acts on the pull rod through a connection means. It would also be possible to position an actuator at the front of the cartridge which is adapted to push the wedge-shaped element downwards. In another example, the wedge-shaped elements may be combined into a wedge-shaped ring which is provided with a thread and which is arranged between the outer wall and the inner wall. By rotating the ring with an actuator, the wedge-shaped element is moved inwards or outwards.
[0066] In
[0067] In
[0068] The adjustable choke of the cartridge is adjusted by rotating the sleeve downwards, such that the conical front portion bends the tongues inwards, thereby reducing the diameter of the adjustable choke 17. The projectile cluster density of the cartridge will now be higher when compared with an unadjusted cartridge. The sleeve is rotated by an actuator 32 which is provided with a toothed wheel 33 which acts on teeth on the outside of the sleeve. The actuator may be positioned at the bottom of the cartridge, at the recoil plate 8 of the cartridge case or may be positioned at the front of the cartridge. When the inner wall is circular and the outer wall is square or rectangular, there is space in the corners of the cartridge case for the actuator.
[0069] The adjustable choke can be provided with two positions, one forward, unadjusted position and one rearward, adjusted position. In this case, the adjustable choke is provided with a first position having a first projectile cluster density and a second position, having a second projectile cluster density which is higher than the first projectile cluster density. The two positions are preferably adapted for two different distances to an incoming object. The first position is used for objects that are relatively close, while the second position is used for objects farther away.
[0070] The adjustable choke may also be provided with more than two predefined positions, or may be continuously variable between the most forward and the most rearward position. When an incoming object is detected and the distance to the object is determined, the adjustable choke of a cartridge is adjusted for the determined distance before the countermeasure is launched.
[0071] When an incoming object is detected by the tracking system of the aircraft, the cartridge cases are tilted in the direction of the incoming object, i.e. such that the centre axis of a cartridge case points in the direction of the incoming object. A fine tracking function of the tracking system will then continuously follow the incoming object and will continuously fine adjust the tilt angle of the cartridge cases to point directly at the incoming object. The distance to the incoming object will also be monitored continuously, such that a countermeasure having an appropriate projectile cluster density can be prepared. The tracking system may comprise an additional fine tracking sensor that is adapted to track a detected object. When the incoming object reaches a predefined position in relation to the aircraft, two or more countermeasures are launched directly towards the incoming object in order to eliminate and destroy the incoming object. By first launching a countermeasure having a relatively high projectile cluster density adapted for a longer distance, and later a second countermeasure having a lower projectile cluster density adapted for a shorter distance, the likelihood of destroying the incoming object is increased.
[0072] Depending on the speed of, the angle to and the distance to the incoming object, it is also possible to point the cartridge cases with an offset angle, such that the cartridge cases are directed to a position in front of the incoming object. This will compensate for the time delay when launching a countermeasure until the countermeasure reaches the incoming object.
[0073] The tracking system of the magazine is adapted to detect and follow an incoming object. The tracking system will in such an example be provided with an active position sensor such as a radar or lidar. It is also possible to integrate a vision system in the tracking system. A vision system can be used to identify the type of the incoming object and also to detect the position and speed of the incoming object. A vision system may also be used to detect objects on the ground, such that a hostile detected object can be eliminated by launching e.g. a shell or the like.
[0074] The invention is not to be regarded as being limited to the embodiments described above, a number of additional variants and modifications being possible within the scope of the subsequent patent claims. The magazine may be mounted to both moving vehicles of all kinds and may also be mounted in a stationary manner, either fixed on e.g. a building or on a movable stand.
REFERENCE SIGNS
[0075] 1: Aircraft [0076] 2: Magazine [0077] 3: Direction of launch [0078] 4: Launch sector [0079] 5: Countermeasure [0080] 6: Cartridge case [0081] 7: Base [0082] 8: Recoil plate [0083] 10: Ball joint [0084] 11: Projectiles [0085] 12: Cartridge [0086] 13: Cavity [0087] 14: Opening [0088] 15: Centre axis [0089] 16: Flexible joint [0090] 17: Adjustable choke [0091] 18: Outer wall [0092] 19: Bottom [0093] 20: Squib [0094] 21: Charge [0095] 22: Inner wall [0096] 23: Slit [0097] 24: Tongue [0098] 25: Wedge-shaped element [0099] 26: Pull rod [0100] 27: Actuator [0101] 28: Outer thread [0102] 29: Sleeve [0103] 30: Inner thread [0104] 31: Conical front portion [0105] 32: Actuator [0106] 33: Toothed wheel [0107] 34: Front section [0108] 40: First countermeasure [0109] 41: Second countermeasure [0110] 42: Third countermeasure [0111] 43: First cartridge [0112] 44: Second cartridge [0113] 45: Third cartridge [0114] 46: First fixed choke [0115] 47: Second fixed choke [0116] 48: Third fixed choke [0117] 50: Resting position 51: Active position