This invention relates to the art of fuses, and more particularly, to fuses for armaments such as missiles and bombs.
It is desired that missiles and bombs explode only when specified conditions are met, such as upon reaching their targets. Otherwise, it is desired that such missiles and bombs can be handled safely. Thus, it is necessary for a missile or bomb to contain a fuse that can differentiate between motions resulting from normal handling, or even severe accidental drops, and between the motions that indicate a need to set off an explosion, e.g., launch or impact. In addition, it is desirable that the operational readiness, as well as the state of the fuse, be testable with the result being perceivable by a human being.
I have recognized that a highly reliable fuse for explosives and armaments can be achieved, in accordance with the principles of the invention, by employing a micro mechanical device that operates to disrupt a relatively low impedance bypass circuit coupled in parallel with a relatively high impedance trigger mechanism. The removal of the electrical bypassing is performed as a result of the movement of the micro mechanical device to enable detonation under prescribed conditions. In accordance with an aspect of the invention, the electrical bypassing is removed by having at least one low impedance electrical bridge that is part of the bypass circuit break when the micro mechanical device is subjected to prescribed trigger activation forces, which are typically large forces, such as are generated during launch or impact.
In one embodiment of the invention, the micro mechanical device is a micro-electrical mechanical system (MEMS) device and the bridge is at least one spring that is part of the MEMS device and also part of the bypass circuit. Breaking the at least one spring disrupts the bypass circuit, permitting current to pass through the high impedance trigger mechanism enabling detonation. In another embodiment of the invention, the bridge is a separate element from the MEMS device and motion of the MEMS device due to the trigger activation forces cause the MEMS device to move such that it breaks the bridge disrupting the bypass circuit, permitting current to pass through the high impedance trigger mechanism enabling detonation.
After moving so as to disrupt the bypass circuit, the MEMS device may be latched into its new position to prevent it from causing any other damage to the trigger, e.g., by moving around therein.
Motion of multiple MEMS devices may be required to fully remove the bypass circuit, which may be implemented as multiple parallel connections. Advantageously, the redundancy provided by employing multiple MEMS devices, and/or multiple bypass connections, results in greater system safety as well as the ability to design for any desired type of triggering condition. For example, if two MEMS devices are employed, each coupled to a separate bypass connection implemented as respective springs, the high impedance trigger mechanism will not be activated unless both springs are broken. For a redundancy application, the MEMS devices can be arranged such that both must move in the same direction in order to break both springs and activate the high impedance trigger mechanism. For control of the triggering condition, it may be that the MEMS devices must each move in opposite directions to cause their respective springs to break and thereby activate the high impedance trigger mechanism. Of course, various combinations can be implemented at the discretion of the implementer. Alternatively, a single MEMS device can be arranged to disrupt the bypass circuit by more than one motion, or two require at least two motions of the MEMS device.
The high impedance trigger mechanism may be a so-called “slapper”, which is at least one high-impedance filament in contact with a dielectric membrane and which operates to generate a shock wave that triggers the explosion of a an explosive pellet when sufficient current is supplied to the high-impedance filament, which in turn causes the main charge of the armament to explode.
In accordance with another aspect of the invention, the fuse may be arranged so as various ones of its parts may be tested and an indication of the results that is perceivable by a human being provided. Furthermore, the fuse may be arranged to be tested both electrically as well as mechanically. For example, a test voltage may be applied, and the voltage at a point along the high-impedance filament is measured to verify the integrity of the high-impedance filament. Similarly, the impedance of the entire assembly may be tested by supplying a test voltage and measuring the resulting current. A high current indicates that the bypass circuit is intact. Electrodes may be positioned with respect to the MEMS device, and various voltages supplied to move the MEMS device. The change in capacitance, if any, that results from such movement may be measured, and from the measurement information about the mechanical condition of the MEMS device may be determined.
In the drawing:
The following merely illustrates the principles of the invention. It will thus be appreciated that those skilled in the art will be able to devise various arrangements that, although not explicitly described or shown herein, embody the principles of the invention and are included within its spirit and scope. Furthermore, all examples and conditional language recited herein are principally intended expressly to be only for pedagogical purposes to aid the reader in understanding the principles of the invention and the concepts contributed by the inventor(s) to furthering the art, and are to be construed as being without limitation to such specifically recited examples and conditions. Moreover, all statements herein reciting principles, aspects, and embodiments of the invention, as well as specific examples thereof, are intended to encompass both structural and functional equivalents thereof. Additionally, it is intended that such equivalents include both currently known equivalents as well as equivalents developed in the future, i.e., any elements developed that perform the same function, regardless of structure.
Thus, for example, it will be appreciated by those skilled in the art that any block diagrams herein represent conceptual views of illustrative circuitry embodying the principles of the invention.
In the claims hereof any element expressed as a means for performing a specified function is intended to encompass any way of performing that function. This may include, for example, a) a combination of electrical or mechanical elements which performs that function or b) software in any form, including, therefore, firmware, microcode or the like, combined with appropriate circuitry for executing that software to perform the function, as well as mechanical elements coupled to software controlled circuitry, if any. The invention as defined by such claims resides in the fact that the functionalities provided by the various recited means are combined and brought together in the manner which the claims call for. Applicant thus regards any means which can provide those functionalities as equivalent as those shown herein.
Unless otherwise explicitly specified herein, the drawings are not drawn to scale.
The term micro-electromechanical systems (MEMS) device as used herein is intended to mean an entire MEMS device or any portion thereof. Thus, if a portion of a MEMS device is inoperative, or if a portion of a MEMS device is occluded, such a MEMS device is nonetheless considered to be a MEMS device for purposes of the present disclosure.
In the description, identically numbered components within different ones of the FIGs. refer to the same components.
A highly reliable fuse for explosives and armaments can be achieved, in accordance with the principles of the invention, by employing a micro mechanical device that operates to disrupt a relatively low impedance bypass circuit coupled in parallel with a relatively high impedance trigger mechanism. The removal of the electrical bypassing is performed as a result of the movement of the micro mechanical device to enable detonation under prescribed conditions. In accordance with an aspect of the invention, the electrical bypassing is removed by having at least one low impedance electrical bridge that is part of the bypass circuit break when the micro mechanical device is subjected to prescribed trigger activation forces, which are typically large forces, such as are generated during launch or impact.
Relatively high impedance trigger 101 triggers an explosion when supplied with a sufficiently high current. The explosion is stimulated by the heating, due to the supplied current, of relatively high impedance wires 113 within the trigger. For example, trigger 101 may be a so-called “slapper” which includes relatively high impedance wires 113. Application of a sufficiently high current to relatively high impedance wires 113 causes wires 113 to heat up, causing material 115 to expand violently. This may in turn set a larger explosion, possibly as a result of a shockwave produced by the violent expansion of material 115. Such slappers and similar devices are known to those of ordinary skill in the art.
Mass 103 is coupled to bridges 105. MEMS device operates by the movement of mass 103 under prescribed conditions so as to exert sufficient force on bridges 105 so that at least one of them breaks. In one embodiment of the invention, bridges 105 support mass 103. In another embodiment of the invention mass 103 may be supported at least in part independently of bridges 105.
In accordance with an aspect of the invention, bridges 105 are part of a relatively low impedance bypass circuit leg which is electrically connected in parallel with, and which bypasses, trigger 101. Thus, so long as bridges 105 remain intact, a current of sufficiently high magnitude to cause detonation of explosive 115 cannot be applied across trigger 101. Therefore, trigger 101 cannot be operated and the armament does not explode.
Electrical connection and test ports 109-1 and 109-2 are used to supply the current which may be used to cause the explosion of trigger 101. However, so long as bridges 105 are intact, trigger 101 is effectively short circuited, and the current is simply shunted from one of electrical connection and test ports 109, through a first of bridges 105, through mass 103, through the other of bridges 105 and then out the other of electrical connection and test ports 109.
Optional electrodes 107 may employed to test the ability of mass 103 to move. By applying a test signal between one of electrical connection and test ports 109 and one of optional electrical connections 111, mass 103 may be caused to move. The motion of mass 103 may be detected by changes in the capacitance measured between the other of test ports 109 and the other of optional electrical connections 111. If the capacitance does not change, this indicates that mass 103 has not moved, and the trigger is defective.
In order to test that relatively high impedance wires 113 are intact and are connected to electrical connection and test ports 109, a small test voltage may be applied between electrical connection and test ports 109. A measurement of the voltage between test port 117 and one of electrical connection and test ports 109 provides information about the electrical integrity of relatively high impedance wires 113. More specifically, if test port 117 is located substantially at the midpoint of relatively high impedance wires 113, the voltage measured at test port 117 should be about one half of the small test voltage that was applied between electrical connection and test ports 109. Furthermore, by measuring the resulting test current should be relatively large if the bypass circuit made up of bridges 105 and mass 103 is intact.
In accordance with an aspect of the invention, relatively high impedance trigger 101 and connections thereto may be outside of sealed package 131, which includes the remainder of the fuse.
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5131328 | Chan | Jul 1992 | A |
6314887 | Robinson | Nov 2001 | B1 |
6622629 | Hodge et al. | Sep 2003 | B2 |
20030070571 | Hodge et al. | Apr 2003 | A1 |
Number | Date | Country |
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1 189 012 | Mar 1992 | EP |
Number | Date | Country | |
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20050217467 A1 | Oct 2005 | US |