1. Field of Invention
The present invention relates to fuzes for submunissions of the type which are disbursable by a vehicle such as a projectile or carrier shell, and in particular, to a self-destructing fuze that automatically self-destructs or self-neutralizes the submunition if the primary mode of detonation fails.
2. Description of Related Art
For many years, submunitions included in the family of Improved Conventional Munitions (ICM) employed a simple, low cost point detonating fuze for initiating a main charge upon impact. Reliability of the fuze was in the 95% range, meaning fairly large quantities of subminitions would not function for various reasons. This failure rate of about 5% presents both an environmental and a humanitarian hazard. Unexploded Ordnance (UXO) remained on the battle field indefinitely and with potentially undesirable consequences to friendly troops and/or civilians.
The currently used M223 fuze incorporated unique and effective safety features for personnel and property protection during the manufacturing and loading process. Key among these safety features is a stabilizer ribbon attached to an arming screw that, in its engaged position, locks a detonator-containing slide in an unaligned position, thereby preventing any possible contact of a primary firing pin with the detonator. Upon deployment of the submunition from its carrier (e.g., howitzer projectile) the stabilizer ribbon becomes exposed to the air stream wind resistance and unfurls. The combination of wind resistance, induced spin of the submunition, and/or vibration causes the submunition to rotate relative to the ribbon, causing an arming screw to back out, which in turn releases a spring loaded slide that shifts, allowing the firing pin to align with the detonator. Upon impact, the firing pin, which is typically attached to a small weight, drives into the detonator causing initiation of the main charge.
In the case of projectile carrier, the entire submunition is spinning at a very high rate at ejection and the ribbon's resistance to spinning causes the arming screw to back out. However, a missile is a non-spin carrier so rotation is not available to arm the unit. Instead, the arming screw backs out because of the vibration induced as the submunition descends. That is, a loose fit between the arming screw and weight allows the arming screw to back out, which releases the spring loaded slide to align the firing pin with the detonator.
The failure of the armed submunitions described above results in hazardous duds. Incidence of death and injury to innocent victims from such hazardous duds, coupled with an international moratorium on antipersonnel mines, demonstrates a need to find a solution that would minimize these residuals on the battle field. It would be beneficial to provide a Self-Destruct Fuze (SDF) that, in the event of failure of the fuze in the primary mode, would cause a secondary action to either explode the entire submunition or at least destroy the detonator (e.g., sterilize the submunition, otherwise referred to as sterilization).
U.S. Pat. No. 5,373,790, to Chemiere, et al., discloses a mechanical system for self-destruction of a submunition, having a warhead initiated by a pyrotechnic sequence, a main striker and a priming device composed of a slide movable between a safety position and an armed position, and which has a device for priming the charge. The self-destruction system includes a secondary striker mounted inside a receptacle of the slide, and a control device that releases the secondary striker after a delay. The secondary striker is integral with a holding element held abutting a seat by the urging of an arming spring. The control device of the secondary striker has a corrosive agent stored in a glass ampoule that, when broken by the holding element, chemically attacks the holding element to release it from its seat. When the holding element is released, the arming spring moves the secondary striker to contact the detonator and destroy the munition.
U.S. Pat. No. 4,653,401, to Gatti, discloses a self-destructing fuze having a first striker member movable within the body of the fuze and able to come into contact with a detonator to cause it to explode, and a slide that is movable in a direction substantially orthogonal to the direction in which the first striker member is movable. A second striker member is disposed in the slide, and is movable from a first position in which it elastically deforms a spring and is held at a predetermined distance from the detonator, to a second position in which it comes into contact with the detonator to cause it to explode. The movement of the second striker member is delayed by a section of wire that under a force exerted by the spring is plastically deformed over time. The plastic deformation eventually frees the second striker member allowing its movement to the second position and against the detonator to cause it to explode.
U.S. Pat. No. 5,932,834, to Lyon, et al., discloses an auto-destruct fuze that provides a primary mode detonator and a delayed auto-destruct/self-neutralize mode detonator for a grenade. The mechanics for the primary mode detonator is similar to the M223 fuze. Operation of the auto-destruct/self-neutralize is based on a Liquid Annular Orifice Device (LAOD) that is released from a locked position upon expulsion of the LAOD from a storage container. The LAOD moves slowly under the urging of a spring and eventually releases a clean-up firing pin which activates a clean-up detonator to activate the primary mode detonator and destructs or self-neutralizes the grenade.
U.S. Pat. No. 4,998,476, to RĂ¼denauer, et al., discloses a fuze for a bomblet including a slide having a detonator triggered in response to an impact and which undergoes a transition during the free flight of the bomblet from a safe position into an armed position. The slide also includes a hydraulic or pneumatic cylinder-piston retarding device and a spring biased self-destruct pin which is operatively coupled to the device and has a self-destruct detonator associated therewith. The retarding device is freed upon movement of the slide to the armed position, and releases the movement of the self-destruct pin after a time delay to trigger the self-destruct detonator and, if needed, the primary detonator.
Numerous variations of self-destruct (SD) devices, working in conjunction with proven safety features of the stabilizer ribbon arming screw, and sliding arrangement have been developed with various degrees of success. In one variant, the SD feature centers around a microelectronic battery and circuit with a complicated attendant initiating device. Two other variants employ a critical pyrotechnic delay column to achieve the necessary time lapse. Even if successful, the critical manufacturing process and high costs of these candidates raise long term and expensive productabilty concerns.
U.S. Pat. No. 7,530,313 to Chamlee, et al., discloses a submunition having a slide that houses a self-destruct fuze delay. The delay includes a container filled with an activation fluid, a spring-loaded ampoule breaker to break the container upon deployment of the munition, a spring-loaded self-destruct firing pin to initiate a secondary detonator in close proximity to a primary detonator, and an interlock ball supported by the ampoule breaker that locks the self-destruct firing pin away from the secondary detonator. The ampoule breaker includes a piston and a timing ball, which accesses the activation liquid. The action of the activation liquid on the timing ball over time causes the timing ball to erode until it is forced into the container by the spring-loaded piston. The movement of the piston frees the interlock ball, allowing the spring-loaded self-destruct firing pin to move under force and impact or initiate the secondary detonator. Initiation of the secondary detonator destroys the primary detonator and, depending upon slide location, either sterilizes the submunition, or destroys the entire submunition.
The current self-destruct fuze development still does not consistently meet the overriding human safety requirement to reduce unexploded hazardous duds and unexploded ordinances to at least one percent. Accordingly, it would still be beneficial to provide more reliable and improved self-destruct delay devices or mechanisms for automatically destroying or self-neutralizing submunitions after a time delay to minimize undesirable consequences to friendly troops and/or civilians. All references cited herein are incorporated herein by reference in their entireties.
The preferred embodiments include a self-destruct detonating fuze for a submunition having a longitudinal axis, a main charge and the self-destruct detonating fuze for initiating the main charge upon impact. The exemplary self-destruct detonating fuze includes a self-destruct slide housing holding a first detonator, a movable fuze slide slidingly engaged with the self-destruct slide housing between a safe position and an armed position with the movable fuze slide having a second detonator mounted thereto, and a slide housing holding member permanently engaged with the self-destruct slide housing and holding the self-destruct slide housing in a stationary position relative to the submunition regardless of the position of the movable fuze slide. This stationary self-destruct slide housing includes a delay mechanism, an interlock unit and an activation mechanism. The delay mechanism is offset and substantially orthogonal to the longitudinal axis of the submunition. The delay mechanism includes an energizing source and a self-destruct firing pin, with the self-destruct firing pin aligned with the first detonator and urged toward the first detonator in a first direction by the energizing source to explode the first detonator. The interlock unit is movable between a first position within the self-destruct slide housing, in which the interlock unit abuts the self-destruct firing pin and restrains the self-destruct firing pin away from the first detonator, and a second position within the self-destruct slide housing offset from the first position in a second direction in which the interlock unit allows the energizing source to move the self-destruct firing pin into the first detonator. The activation mechanism is offset from the delay mechanism and supports the interlock unit in the first position against the self-destruct firing pin. The activation mechanism is adapted to shift after a delay and release its support of the interlock unit against the self-destruct firing pin to allow movement of the interlock unit to the second position.
The preferred embodiments also include a self-destruct detonating fuze for a submunition having a longitudinal axis, a main charge and the self-destruct detonating fuze for initiating the main charge upon impact. The self-destruct detonating fuze includes a self-destruct slide housing holding a first detonator, a movable fuze slide slidingly engaged with the self-destruct slide housing between a safe position and an armed position with the movable fuze slide having a second detonator mounted thereto, and a slide housing holding member permanently engaged with the self-destruct slide housing and holding the self-destruct slide housing in a stationary position relative to the submunition regardless of the position of the movable fuze slide. This stationary self-destruct slide housing also includes a delay mechanism, an interlock unit and an activation mechanism. The delay mechanism is offset and substantially orthogonal to the longitudinal axis. The delay mechanism includes an energizing source and a self-destruct firing pin, with the self-destruct firing pin aligned with the first detonator and urged into the first detonator by the energizing source. The activation mechanism is offset from the delay mechanism, and includes a container holding a fluid and a breaking member that breaks the container and accesses the fluid, which erodes the breaking member over a delay and releases a hold against the self-destruct firing pin. The interlock unit is movable between a first position supported by the activation mechanism against the self-destruct firing pin to hold the self-destruct firing pin away from the first detonator, and a second position that releases the hold against the self-destruct firing pin and allows the energizing source to move the self-destruct firing pin into the first detonator. Preferably, the self-destruct slide housing includes a channel between the delay mechanism and the activation mechanism, and the interlock unit includes at least one interlock ball that moves within the channel between the first position and the second position.
While not being limited to a particular theory, the preferred slide housing holding member includes a fuze housing. The fuze housing is fixedly secured to the submunition and covers the stationary self-destruct slide housing. The fuze housing includes a slide housing locking unit extending around and holding the self-destruct slide housing in the stationary position relative to the submunition. It should also be noted that the slide housing holding member preferably further includes an arming screw received within an aperture of the stationary self-destruct slide housing. The aperture is aligned between the arming screw and the second detonator when the movable fuze slide is in the armed position. While not considered a primary function of the arming screw, it is contemplated that the arming screw may also retain the self-destruct slide housing in the stationary position relative to the submunition.
The invention will be described in conjunction with the following drawings in which like reference numerals designate like elements and wherein:
Exemplary embodiments for a stationary self-destruct (SSD) fuze mechanism are described with reference to the figures noted above. Although the preferred SSD fuze is applicable to all the various ICM items, in the interest of brevity, the exemplary SSD fuze mechanisms are generally tailored toward use in the M864, M155 MM projectile which contains 72 submunitions, each with its own SSD fuze. While not being limited to a particular theory, the submunitions typically are disbursed via an expulsion charge that explodes in flight creating ample internal pressure to shear the base plate threads and expel the cargo out the rear of the projectile and into the atmosphere.
In general, as each submunition is disbursed into the atmosphere, the impact of the air stream causes the submunition's stabilizer ribbon to unfurl, allowing an arming screw to back out and a slide to move to its armed position. Upon impact, the firing pin is free to pierce the primary detonator and cause a subsequent main charge explosion, which destroys the submunition. Damaged fuzes and fuzes that arm properly but come into contact with the ground or a target via side impact may fail to initiate the main charge resulting in residual hazardous duds. A hazardous dud is a submunition that still has its fuze attached and its primary detonator present that together could potentially initiate the main charge. A hazardous dud is different than an unexploded ordinance, which is a submunition that has no means of initiation (e.g., primary detonator is missing or destroyed).
The SSD fuze mechanisms of the preferred embodiments incorporate a predetermined time delay (e.g., about 25 seconds minimum to about 5 minutes) that is greater than the foreseeable flight time of the respective submunition, which ends when the submunition reaches the ground or target. This delay allows the primary detonator to initiate the main submunition charge when the submunition strikes the ground or target. The SSD fuze mechanisms destroy the submunition or sterilize the fuze if the submunition fails to explode after it strikes the ground or target. The fuze also retains the positive operation of the M223/M239 fuze, that is, it utilizes the stabilizer ribbon, arming screw and slide to retain the known out-of-line safety features.
Other advantages, characteristics and details of the invention will emerge from the explanatory description thereof provided below with reference to the attached drawings and examples, but it should be understood that the present invention is not deemed to be limited thereto. Toward that end,
As can be seen in
The delay mechanism 22 of the SSD fuze 10 includes a self-destruct (SD) detonator 40 that is arranged in a first channel 42 of the SSD slide housing 14 offset and substantially orthogonal to the longitudinal axis of the submunition and to the arming screw 20. A self-destruct detonator retainer 44 preferable formed of a plastic or metal secured (e.g., by adhesives, crimping, friction, heat) to an inner-cylindrical wall 46 of the channel 42 to seal the self-destruct detonator 40 within the channel. The delay mechanism 22 also includes a compression spring 46 as an energizing source, and a self-destruct (SD) firing pin 48, both preferably formed of metal or other hard material and located within the first channel 42.
The SD firing pin 48 includes a front end 50 proximate the self-destruct detonator 40 and a spring holding rod section 52. While not being limited to a particular theory, the rod section 52 prior to deployment extends through a reduced diameter 54 of the first channel 42 at the second width side wall 39 of the SSD slide housing 14, where it is held in place by a firing pin safety clip 56, as would readily be understood by a skilled artisan. In this arrangement shown in
The interlock unit 26 is shown in
The activation mechanism 24 is offset from the delay mechanism 22 and supports the interlock unit 26 in a position that restricts movement of the SD firing pin 48 toward the SD detonator 40. As will be described in greater detail below, the activation mechanism is adapted to shift after a time delay and release its support of the interlock unit against the self-destruct firing pin to allow movement of the interlock unit to a position that frees the firing pin to explode the SD detonator.
While not being limited to a particular theory, the activation mechanism 24 is located in the second channel 70, which is offset from the first channel 42 that houses the delay mechanism 22. The activation mechanism 24 includes a breakable container 72 (e.g., glass ampoule, ceramic ampoule) that holds a reactant fluid 74. The reactant fluid 74 is preferable a corrosive agent (e.g., acid or liquid solution) that chemically attacks and causes certain materials (e.g. hard plastics) of the interlock unit 26 to erode over time. The container 72 is partially housed in a generally cup-shaped ampoule cup 76 that is a resilient insulator preferably not susceptible to the reactant fluid 74 so that the reactant fluid does not erode the ampoule cup if it inadvertently leaks out of the container. The resilient insulative ampoule cup 76 seals the container 72 and other elements of the activation mechanism 24 discussed below within the second channel 70 of the SSD slide housing 14. In particular, the container 72 is sealed inside the ampoule cup 76 preferably with an epoxy, and then secured inside the second channel 70 as a unit. The ampoule cup 76 also contains the orifice (e.g., ampoule cup aperture 94) through which the timing ball 90 must pass to release the self-destruct firing pin 48, as discussed in greater detail below.
Still referring to
The breaking member 78 is an ampoule breaker that upon release of the SD activation clip 84 is urged by the compression spring 82 into impact with the container 72, causing the container to break and release the reactant fluid 74 into communication with the breaking member. Preferably, the breaking member is a timing ball 90 made of a hard plastic or similar material that is hard enough to break glass or similar fragile material (e.g., ceramic), and that erodes when exposed to the reactant fluid 74. While not being limited to a particular theory, a resilient sleeve 92 centers the timing ball 90 in the second channel 70 and keeps the timing ball aligned between the glass ampoule and the activation pin 80.
The ampoule cup 76 preferably includes a semi-closed end with an aperture 94 facing the timing ball 90. The aperture 94 in the ampoule cup is large enough to allow direct contact between the timing ball 90 and the container 72 (e.g. glass ampoule), but is small enough to still prevent the ball from passing through until the reactant fluid has reduced the diameter. As can best be see in
While not being limited to a particular theory, the activation pin 80 is a generally rod-shaped metal unit that holds the breaking member 78 against the ball guide 92 before deployment. In particular, the activation pin 80 includes an enlarged diameter section 98 that abuts the compression spring 82, and a proximal section 99 between the enlarged diameter section 98 and the timing ball 90. During deployment and after release of the SD activation clip 84, the activation pin 80 is urged by the compression spring 82 toward the fragile container 72, pushing the breaking member 78 at least partially past the ampoule cup aperture 94 at the semi-closed end of the ampoule cup 76 into the container 72, breaking the container and releasing the reactant fluid 74 onto the breaking member 78. Before deployment, the SD activation clip 84 holds the compression spring 82 in a state of tension between the enlarged diameter section 98 of the activation pin 80 and an interior wall 100 of the SSD slide housing 14. Before and during deployment, the enlarged diameter section 98 also abuts and supports the interlock unit 26 to its first position where the interlock unit prevents the self-destruct firing pin 48 from moving into and exploding the self-destruct detonator 40.
As noted above, the breaking member 78, activation pin 80 and compression spring 82 are aligned with the container 72 in the second channel 70 of the SSD slide housing 14, with the second channel being offset from the first channel 42 and in communication with the first channel via the adjoining channel 68. The compression spring 82 is an energizing source mounted in a compressed state inside the second channel 70 between the interior wall 100 of the SSD slide housing 14 and the enlarged diameter section 98 of the activation pin 80. When inserted against the SSD slide housing 14, as shown in
Still referring to
While not being limited to a particular theory, the ampoule cup 76 includes an open end 104 for allowing insertion of the container 72 into the cup where it is sealed in place with epoxy sealant within the interior walls of the ampoule cup and its semi-closed end 106. The semi-closed end 106 of the ampoule cup 76 extends radially inward to define the ampoule cup aperture 94 having a diameter slightly less than the pre-deployment diameter of the breaking member 78, so as to prevent premature passage of the timing ball 90 through the aperture. As can be seen in
The timing ball 90 is both a part of the breaking member 78 that breaks the container 72 upon collision, and a weakened area of the activation mechanism 24 that erodes under chemical attack from the reactant fluid 74 and, after a delay, slips through the ampoule cup aperture 94 and allows the compression spring 82 to move the activation pin 80 beyond its prior abutment of the interlock unit 26. This frees the SD firing pin 48 to overcome the restraint of the interlock unit 26 for release into the SD detonator 40, as set forth in greater detail below. As such, the timing ball 90 is constructed of a material, preferably styrene (e.g., polystyrene) that is both hard enough to break glass or ceramics, and is vulnerable to the reactant fluid 74 (e.g., corrosive agent, acid, solution). In particular, the timing ball 90 is vulnerable to the reactant fluid, in comparison to the other elements of the activation mechanism discussed above, to fail over time over application of the reactant fluid. As can be seen in
The stationary self-destruct fuze self destructs or sterilizes the submunition after a preset delay if the submunition fails to explode upon its impact with the ground or a target all while remaining stationary within the slide housing 14. As discussed above, the SSD slide housing 16, which houses the delay mechanism 22, activation mechanism 24 and interlock unit 26, remains within the fuze housing 30 preferably by slide holding members 28. These members hold the SSD slide housing 14 in a locked position within the fuze housing for reliable, desirable self destruction while permitting the movable fuze slide 16, which holds the primary detonator 18 to shift out after deployment into its armed position. As noted above, the self-destruct fuze 10 self destructs the attached submunition after a preset delay if the submunition fails to explode upon its impact with the ground or a target.
The cover 112 includes a finger bent upright as a backing to retain a fuze slide compression spring 120 against the movable fuze slide 16. The compression spring 120 urges the fuze slide 16 from the safety position to the armed position after deployment. As can be seen in
Still referring to
The anti-backlash ball 122 (
When the movable fuze slide 16 is shifted to its armed position, such that the primary detonator 18 is aligned with the arming screw 20, the ball channel 144 of the SSD slide housing is shifted over the anti-backlash ball port 142 of the movable fuze slide 16. This alignment of the ball channel and anti-backlash ball port allows the anti-backlash ball 122 to fall into the anti-backlash ball port 142 (
As can best be seen in
As steps 204 and 206, the fuze mechanism 12 appears, for example, at
In the case of projectile carrier, the entire submunition is spinning at a very high rate at ejection. While not being limited to a particular theory, the wind resistance of the air stream tends to cause the unfurled stabilizer ribbon to resist the rotational spinning of the submunition 108. This resistance to rotation is transferred to the arming screw 20, causing the arming screw to rotate against the spinning submunition and back out from its pre-deployment position (
It is generally recognized that not all submunitions are spinning projectiles. For example, some missile warheads are non-spin; meaning that rotation is not available to arm a deployed submunition. Here, the arming screw backs out because of the vibration induced as the submunition descends. That is, a loose fit between the arming screw and its housing, along with the screw's weight allows the arming screw to back out, which releases the spring loaded slide to align the firing pin with the detonator, as readily understood by a skilled artisan. Regardless of their spinning characteristics, submunitions are designed so that when the munition is designed to explode (e.g., upon impact with its target), the arming screw 20 with weight inertia initiates the primary detonator 18, causing a chain of explosions through the lead charge 21 and main charge 23 (
However, if the submunition 108 does not function normally, that is, explode upon hitting its target; the reactant fluid 74 continues to erode the timing ball 338 (
As the timing ball 90 erodes to a size small enough to fit through the ampoule cup aperture 94, the force of the activation pin compression spring 82 pulses the timing ball through the aperture at Step 208. As can be seen in
Accordingly, the movement of the timing ball 90 into the container 72 in step 208 releases the self-destruct firing pin 48. At Step 210, the firing pin compression spring 46 drives the released self-destruct (SD) firing pin 48 toward the self-destruct detonator 22, causing the SD firing pin to impact and explode the SD detonator 40. See, for example,
However, if the movable fuze slide 16 is not in the armed position (e.g., the movable fuze slide did not complete its shift to arm and instead remains in the safe position or in a position between its safe an armed position where the primary detonator 18 is not aligned with the main charge as show by example in
It is understood that the method and mechanism for making and using the self-destruct fuze delay device described herein are exemplary indications of preferred embodiments of the invention, and are given by way of illustration only. It other words, the concept of the present invention may be readily applied to a variety of preferred embodiments, including those disclosed herein.
While the invention has been described in detail and with reference to specific examples thereof, it will be apparent to one skilled in the art that various changes and modifications can be made therein without departing from the spirit and scope thereof. For example, the SD fuze delay device is applicable to all the various ICM items including the submunitions of the non-rotating GMLRS/MLRS warheads. Without further elaboration, the foregoing will so fully illustrate the invention that other may, by applying current or future knowledge, readily adapt the same for use under various conditions of service.