The invention relates generally to explosive fuzes, and more particularly to an explosive fuze booster incorporating detonation-wave shaping features.
Many aircraft-delivered bombs have what is known as a fuze well centrally positioned in either the bomb's nose or the bomb's tail. An electronic fuze is seated in one of these fuze wells. Electric and communications lines are led to the electronic fuze through a conduit extending through the bomb to the fuze well. The electronic fuze includes a fuze booster that is generally an annularly-shaped element to accommodate the passage of the aforementioned electric and communications lines on their way to the fuze's safe-and-arming mechanism. The annular shape of the fuze booster necessitates that its initiation is off-center in what is known as a side-light initiation. While such side-light initiation is satisfactory for conventional-explosive bomb fills, side-light initiation has been less effective at fully initiating highly-insensitive-explosive bomb fills.
Accordingly, it is an object of the present invention to provide an annularly-shaped fuze booster configured for side-light initiation to achieve an effective initiation of highly insensitive explosives.
Other objects and advantages of the present invention will become more obvious hereinafter in the specification and drawings.
In accordance with the present invention, a fuze booster includes a first explosive charge having a cavity extending there through. The first explosive charge has an annular portion encircling a first axial portion of the cavity and has a semi-annular portion partially encircling a second axial portion of the cavity. The annular portion abuts the semi-annular portion. An explosively-inert material abuts the semi-annular portion, abuts the annular portion, and partially encircles the second axial portion of the cavity. A second explosive charge abuts the explosively-inert material, abuts the semi-annular portion, and partially encircles the second axial portion of the cavity. As a result, the second axial portion of the cavity is completely encircled by a combination of the semi-annular portion, the explosively-inert material, and the second explosive charge.
Other objects, features and advantages of the present invention will become apparent upon reference to the following description of the exemplary embodiments and to the drawings, wherein corresponding reference characters indicate corresponding parts throughout the several views of the drawings and wherein:
Referring now to the drawings, simultaneous reference will be made to
Fuze booster 10 includes an explosive main booster charge 12, a detonation-wave-shaping element 14, and an explosive transfer charge 16. These three elements are assembled in an abutting relationship illustrated in
Main booster charge 12 is a solid high-explosive material (e.g., PBXN-7, PBXN-5, PBXN-9 or PBXN-12) that can be molded, printed, injection-loaded or cast to have a cavity 120 extending axially through a central portion thereof. Cavity 120 provides a “conduit” through fuze booster 10 for electric and communication lines (not shown). Main booster charge 12 has an annular portion 121 that completely encircles cavity 120 and has a semi-annular portion 122 that partially encircles cavity 120, e.g., encircling approximately one-half of cavity 120 in the illustrated embodiment. Portions 121 and 122 abut one another along cavity 120 as indicated by dashed line 121A. That is, in terms of a solid molded, pressed, printed, injection-loaded or cast high-explosive main booster charge 12, portions 121 and 122 are integrated with one another. The resulting ledge 123 defined in main booster charge 12 is filled with the combination of detonation-wave-shaping element 14 and transfer charge 16.
Detonation-wave-shaping element 14 (or “wave-shaping element 14” as it will be referred to hereinafter) is made from an explosively-inert material such as plastic, felt, rubber or wood. Wave-shaping element 14 may be a solid, hollow, porous or foamed material without departing from the scope of the present invention. In general and as will be explained further below, wave-shaping element 14 shapes the detonation wave associated with a side-lit initiated transfer charge 16 to provide an effective initiation of main booster charge 12.
Wave-shaping element 14 fits on/in ledge 123 and axially abuts annular portion 121 and the internally-facing diametrical edge 122A of semi-annular portion 122 of main booster charge 12, while also partially encircling cavity 120. In the illustrated embodiment, wave-shaping element 14 includes backstop region 140 against which transfer charge 16 rests. Backstop region 140 holds transfer charge 16 in place and directs the detonation wave of an initiated transfer charge 16 towards semi-annular portion 122.
Transfer charge 16 is a solid, molded, pressed, printed, injection-loaded or cast piece of high-explosive material (e.g., PBXN-7, PBXN-5, PBXN-9 or PBXN-12) abutting wave-shaping element 14 and the internally-facing diametrical edge 122A of semi-annular portion 122 such that transfer charge 16 partially encircles a portion of cavity 120 passing through semi-annular portion 122. In this way, cavity 120 is completely encircled in-part by annular portion 120 and in-part by the combination of semi-annular portion 122, wave-shaping element 14, and transfer charge 16.
When transfer charge 16 undergoes a side-lit initiation at point 100, wave-shaping element 14 directs the resulting detonation wave towards radial edge 122A of semi-annular portion 122. As shown in
Another embodiment of a fuze booster in accordance with the present invention is illustrated in
Main booster charge 22 is analogous to the previously-described main booster charge 12 such that the analogous features of a cavity 220, an annular portion 221 abutting (at 221A) a semi-annular portion 222 defining a diametrical edge 222A, and a ledge 223 need not be described further herein. Main booster charge 22 further includes an axially-extending socket 224 formed in an axial end of annular portion 221 that is aligned with side-lit initiation point 100. Socket 224 provides for the indexing of wave-shaping element 24 to main booster charge 22. In addition, by aligning socket 224 with initiation point 100, a larger wave-shaping gap is provided between transfer charge 26 and main booster charge 22 to prevent shock transfer through wave-shaping element 24 caused by detonation of transfer charge 26 at initiation point 100. Additional sockets can be provided in annular portion 221 for indexing purposes without departing from the scope of the present invention.
Wave-shaping element 24 is a hollow structure (e.g., made from an explosively-inert material such as plastic, felt, rubber, or wood) that fits into/on ledge 223 and functions similarly to wave-shaping element 14 described above. However, rather than having a simple backstop region, wave-shaping element 24 defines a wedge-shaped nest region 240 for receiving transfer charge 26. Transfer charge 26 is correspondingly wedge-shaped to nest in region 240. In addition, wave-shaping element 24 includes a hollow pin 241 (only visible in
The advantages of the present invention are numerous. The fuze booster provides a new arrangement of explosive charges and a detonation-wave-shaping element to generate diametrically-opposed jet initiations that provide for more efficient detonation of even insensitive explosive fills.
Although the invention has been described relative to a specific embodiment thereof, there are numerous variations and modifications that will be readily apparent to those skilled in the art in light of the above teachings. For example, various adhesives and/or mechanical fasteners, springs, etc., could be included in the fuze booster to facilitate its assembly and/or parts retention without departing from the scope of the present invention. It is therefore to be understood that, within the scope of the appended claims, the invention may be practiced other than as specifically described.
Finally, any numerical parameters set forth in the specification and attached claims are approximations (for example, by using the term “about”) that may vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should be at least construed in light of the number of significant digits and by applying ordinary rounding.
The invention described herein was made in the performance of official duties by employees of the Department of the Navy and may be manufactured, used, licensed by or for the Government for any governmental purpose without payment of any royalties thereon.
Number | Name | Date | Kind |
---|---|---|---|
4050381 | Heinemann | Sep 1977 | A |
4425850 | Grossler | Jan 1984 | A |
4665826 | Marer | May 1987 | A |
4672896 | Precoul et al. | Jun 1987 | A |
4711181 | Ringel et al. | Dec 1987 | A |
4875414 | Stadler et al. | Oct 1989 | A |
4982662 | Beck | Jan 1991 | A |
5204493 | Christmann | Apr 1993 | A |
5221810 | Spahn | Jun 1993 | A |
5259317 | Lips | Nov 1993 | A |
7752972 | Baker et al. | Jul 2010 | B1 |
8037822 | Althof | Oct 2011 | B2 |
8056478 | Berlin | Nov 2011 | B2 |
8272326 | Berlin et al. | Sep 2012 | B2 |
9291435 | Scheid | Mar 2016 | B2 |
9903692 | Arnold | Feb 2018 | B2 |
10048047 | Van Niekerk | Aug 2018 | B2 |
20130061771 | Betancourt | Mar 2013 | A1 |
20160216085 | Scheid | Jul 2016 | A1 |
20190107371 | Grace | Apr 2019 | A1 |