Active body

Information

  • Patent Grant
  • 8763533
  • Patent Number
    8,763,533
  • Date Filed
    Tuesday, December 27, 2011
    12 years ago
  • Date Issued
    Tuesday, July 1, 2014
    10 years ago
Abstract
An active body (1) is proposed that has, as active mass (5), multiple flares (2, 3) arranged behind each other or stacked, in particular for the generation of decoys, wherein the flares (2, 3) are NC (nitrocellulose) and RP (red phosphorus) single flares. The single flares (2, 3) are evenly or unevenly stacked in succession such that one RP single flare (3) lies on an NC single flare (2), or multiple NC single flares (2) or multiple RP single flares (3) follow each other, so that it is possible to vary the percentage of NC and RP in the active body (1) from about 0% to about 100%. A container (4) houses the active mass (5), and can in turn have predetermined breaking points (7) to facilitate the break up of the active body (1).
Description
FIELD OF THE INVENTION

The invention relates to an active body, or active masses, consisting of a plurality of flares, which are arranged or stacked one behind the other, for producing decoy targets.


BACKGROUND OF THE INVENTION

By way of example, an active body such as is described briefly in DE 199 51 767 C2, and, in that case, carries out the task of a dual-mode decoy body. The active mass, which emits radiation in the IR band, ism in that case, formed from flares. A concealment and decoy munition of this type for protection of objects against guided missiles, which contains active substances that form smoke and/or decoy targets, is furthermore disclosed in DE 10 2005 020 159 B4.


Red phosphorus (RP) has already been used in military applications for many decades, for example, in smoke grenades for protection of infantry, artillery and watercraft, or for aircraft decoy targets with an infrared (IR) effect. The smoke or IR effect is produced by the RP by combustion after corresponding ignition by activation. The RP unit is traditionally itself ignited and distributed via an ignition or break-up charge, which ensures that the active body and the active mass are optimally ignited and distributed for the respective purpose, that is to say, that the IR decoy target blooms optimally to form a cloud or a decoy target over an area.


Particularly in conjunction with civil applications in aviation and for marine purposes, ignition and break-up charges, that is to say explosives, are, however, undesirable in bodies or masses such as these, and should not be used. However, dispensing with a break-up charge results in the problem that the IR decoy target cannot bloom in the ideal manner. Correspondingly, new concepts are and were required.


A novel ignition concept such as indicated above, in this direction, is described in more detail in DE 10 2006 004 912 A1. This document discloses a system for protection, in particular, of large flying platforms, such as aircraft, against an IR-guided or radar-guided threat. In this case, the active bodies are preferably activated and ignited without contact. The active bodies are then ejected pneumatically or mechanically. The active bodies themselves are packs without any munitions, which are ignited by means of hot air or a laser.


Building on this idea, the present invention is based on the object of developing an active body of the type described above so as to ensure that the active body and its active masses act reliably in order to form a decoy target.


SUMMARY OF THE INVENTION

The object of the present invention is achieved by the features of a first embodiment, which pertains to an active body (1) having a plurality of flares (2, 3), which are arranged or stacked one behind the other, as an active mass (5), in particular, for production of decoy targets, characterized in that the flares (2, 3) are NC (nitrocellulose) and RP (red phosphorus) individual flares that are stacked uniformly or non-uniformly in their sequence such that an RP individual flare (3) comes to rest on the NC individual flare (2), or a plurality of NC individual flares (2), or a plurality of RP individual flares (3) follow one another, thus making it possible to vary the proportions of NC and RP in the active body (1) from 0% to 100%. Advantageous refinements of the invention are specified in additional embodiments summarized below.


In accordance with a second embodiment of the present invention, the first embodiment is modified so that a container (4) holds the active mass (5). In accordance with a third embodiment of the present invention, the second embodiment is further modified so that the parameters of the container (4) can be adjusted by coloring and/or addition of additives in order to optimize the energy absorption. In accordance with a fourth embodiment of the present invention, the second embodiment or the third embodiment are further modified so that an intermediate layer (6) can be included in the container (4) and the active mass (5). In accordance with a fifth embodiment of the present invention, the fourth embodiment is further modified so that the intermediate layer (6) consists of NC and/or RP granulate. In accordance with a sixth embodiment of the present invention, the second embodiment, the third embodiment, the fourth embodiment and the fifth embodiment are further modified so that additional weak points (7) are provided in the container (4).


The invention is based on the idea of constructing the munitions-free IR decoy target concept based on NC (nitrocellulose) and/or RP (red phosphorus), and in this case varying the proportions of NC/RP (i.e., the NC/RP ratio), in which case the variation can be carried out between the extremes of 0% and 100%. The major configuration options that this approach offers are spontaneity and duration of the IR characteristic reflected in the rise flank and the jet duration, as a result of which the invention offers the capability for configuration of the jet characteristic of the IR decoy target by the variable proportions of NC and RP. A desired IR curve can be achieved for the decoy target between the two extremes (100% NC/0% RP and 100% RP/0% NC) even in a continuously variable manner by variation of the active mass proportions from in each case 0% to 100%, for the geometric and spatial distribution.


The NC active masses can themselves be caused to react at ambient pressure (normal atmosphere). Therefore, they do not require any additional activation energy.


As is known, the active masses are kept in shape by a film sheet, or the like. Better protection against environmental influences during storage, transportation and handling is now achieved by the use of an active body casing/active body container, which burns away without any residue. This combustible casing is preferably based on NC. The combustibility ensures that no casing residues are left. In a development of the inventive idea, a type of ignition transmission layer is included, which is used to optimize the ignition transmission between the active body casing and the active masses.


Thus, in accordance with the present invention, a munitions-free, non-pyrophoric IR decoy target is proposed, based on NC and/or RP, which can be activated by alternative ignition concepts, such as a laser, high temperature, induction, etc. The stacked individual flares automatically break up after activation.





BRIEF SUMMARY OF THE DRAWINGS

The invention will be explained in more detail using at least one exemplary embodiment and the following drawings, in which:



FIG. 1 schematically illustrates an active body composed of individual flares,



FIG. 2 shows an active body, consisting of NC/RP individual flares without a casing,



FIG. 3 shows the active body from FIG. 2 with a casing,



FIG. 4 shows the active body from FIG. 2 with an intermediate layer included and a casing,



FIG. 5 shows the active body from FIG. 3 with weak points formed in the casing.





DETAILED DESCRIPTION OF THE INVENTION


FIG. 1 shows a schematic illustration of an active body 1 consisting of so-called individual flares 10. FIG. 2 shows active masses 5 of an active body, which is annotated 1, and is formed from stacked flares 2, 3. In this case, by way of example and preferably, the flares 2, 3 are stamped NC and RP flare disks, respectively, although they do not necessarily need to be circular. Other surface geometries for the flares 2, 3 are likewise possible. The flares 2, 3 are combined in variable proportions. The respective proportions may be varied from about 0% to about 100%. This makes it possible to control the IR jet characteristic of the active body 1. The flares 2, 3 can be stacked alternately, but need not be. It would be possible to use a stacking sequence of a flare 2, always alternating with a flare 3, or else two flares 2 and only one flare 3 thereon, or else two flares 3 and only one flare 3 thereon, etc. (not illustrated in any more detail). In some embodiments of the present invention, the active body includes only nitrocellulose flares 2 or only red phosphorus flares 3. Because this may be the case, in some embodiments whereas other embodiments include combinations of nitrocellulose flares 2 and red phosphorus flares 3, the respective proportions of nitrocellulose flares 2 to red phosphorus flares 3 can be varied from 0% to 100%, and vice versa.


The individual flare disks 2, 3, which have been stacked in this way, are now incorporated in a container or a casing 4 (See FIG. 3). This container 4 is preferably composed of NC material, for example, NC paper, NC lacquer, and protects the actual active mass 5 (i.e., individual flares 2, 3), in particular against environmental influences. The choice of the material allows the container 4 to burn away completely, and this is likewise ignited when the active body 1 is activated.


By way of example, the active body 1 is activated on a laser basis, thermally etc., with the aid of a so-called ejection tube or the like, for example, as in an application submitted in parallel by the same applicant entitled “Activation unit for explosive masses and explosive bodies,” namely, U.S. patent application Ser. No. 13/291,281 to which reference is hereby made, and which is incorporated herein by reference for all that it discloses. Thus, in accordance with the present invention, the active body 1 is activated by a laser, or is thermally activated, etc., by an ejection tube, such as the one disclosed in the application entitled “Activation unit for explosive masses and explosive bodies” (U.S. patent application Ser. No. 13/291,281).


In order to optimize the ignition, the active mass 5 and/or the container 4 of the active body 1 of present invention can be blackened (i.e., colored, for example, to the color black), which ensures that more energy is introduced to the active mass by scattering of the absorption level (laser absorption, for example). It is likewise possible to add additives to the active mass 5 and/or the container 4 in order to optimize ignition of the active mass 5. Thus, in accordance with the present invention, ignition parameters of the container are adjusted by coloring the container, or by addition of additives to a material of the container, such as by including nitrocellulose paper or nitrocellulose lacquer, etc. as a component of the material of the container, or by both coloring the container and the addition of additives to the material of the container, in order to optimize energy absorption by the container. In this way, it is possible to optimize one or more ignition parameters of the container 4 and the active mass 5 held within the container 4. In accordance with the present invention, it is also possible to blacken the active mass 5 and/or to add additives to the active mass 5 in order to optimize one or more ignition parameters of the active mass 5.


If optimization of the firing chain is desirable, an intermediate layer 6 can be included between the container 4 and the active mass 5 (See FIG. 4). This structure then makes it possible to control the firing transmission, for example, to speed it up. The intermediate layer 6 should, in this case, consist of NC granulate and/or RP granulate.


Additional weak points 7 (See FIG. 5) in the container 4 are likewise used to break the active body 1 up optimally in order to form a decoy target after activation/deployment, and are used to optimize blooming behavior of the decoy target. Weak points such as these are already known from so-called explosive projectiles.

Claims
  • 1. An active body comprising: (a) an active mass comprising a plurality of flares that are arranged or stacked one behind the other and that are ignitable to produce decoy targets, wherein the plurality of flares include one or more nitrocellulose individual flares and one or more red phosphorus individual flares that are stacked in sequence so that at least one red phosphorus individual flare comes to rest on at least one nitrocellulose individual flare; and(b) a container that holds the active mass therein, andwherein the active body is munitions-free, non-pyrophoric, and produces an infrared jet when ignited.
  • 2. The active body as claimed in claim 1, wherein ignition parameters of the container are adjusted by coloring the container, or by addition of additives to a material of the container, or by both coloring the container and the addition of additives to the material of the container, in order to optimize energy absorption by the container.
  • 3. The active body as claimed in claim 2, wherein an intermediate layer is included in the container and is disposed between the active mass and the container.
  • 4. The active body as claimed in claim 3, wherein the intermediate layer comprises nitrocellulose granulate, or red phosphorus granulate, or a mixture of nitrocellulose granulate and red phosphorus granulate.
  • 5. The active body as claimed in claim 1, wherein an intermediate layer is included in the container and is disposed between the active mass and the container.
  • 6. The active body as claimed in claim 5, wherein the intermediate layer comprises nitrocellulose granulate, or red phosphorus granulate, or a mixture of nitrocellulose granulate and red phosphorus granulate.
  • 7. The active body as claimed in claim 1, wherein the container includes a plurality of additional weak points formed in the container.
  • 8. The active body as claimed in claim 1, wherein the one or more nitrocellulose individual flares and the one or more red phosphorus individual flares are stacked uniformly in sequence.
  • 9. The active body as claimed in claim 1, wherein the one or more nitrocellulose individual flares and the one or more red phosphorus individual flares are stacked non-uniformly in sequence.
  • 10. The active body as claimed in claim 1, wherein the proportions of nitrocellulose individual flares and red phosphorus individual flares in the stacked sequence of the active mass varies from about 0% to about 100%.
  • 11. The active body as claimed in claim 1, wherein the proportions of red phosphorus individual flares and nitrocellulose individual flares in the stacked sequence of the active mass varies from about 0% to about 100%.
  • 12. An active body comprising: (a) an active mass comprising a plurality of flares that are arranged or stacked one behind the other and that are ignitable to produce decoy targets, wherein the plurality of flares include one or more nitrocellulose individual flares and one or more red phosphorus individual flares that are stacked in sequence so that a plurality of nitrocellulose individual flares follow a plurality of red phosphorus individual flares, or vice versa; and(b) a container that holds the active mass therein, andwherein the active body is munitions-free, non-pyrophoric, and produces an infrared jet when ignited.
  • 13. The active body as claimed in claim 12, wherein ignition parameters of the container are adjusted by coloring the container, or by addition of additives to a material of the container, or by both coloring the container and the addition of additives to the material of the container, in order to optimize energy absorption by the container.
  • 14. The active body as claimed in claim 13, wherein an intermediate layer is included in the container and is disposed between the active mass and the container.
  • 15. The active body as claimed in claim 14, wherein the intermediate layer comprises nitrocellulose granulate, or red phosphorus granulate, or a mixture of nitrocellulose granulate and red phosphorus granulate.
  • 16. The active body as claimed in claim 12, wherein an intermediate layer is included in the container and is disposed between the active mass and the container.
  • 17. The active body as claimed in claim 16, wherein the intermediate layer comprises nitrocellulose granulate, or red phosphorus granulate, or a mixture of nitrocellulose granulate and red phosphorus granulate.
  • 18. The active body as claimed in claim 12, wherein the container includes a plurality of additional weak points formed in the container.
  • 19. The active body as claimed in claim 12, wherein the plurality of nitrocellulose individual flares and the plurality of red phosphorus individual flares are stacked uniformly in sequence.
  • 20. The active body as claimed in claim 12, wherein the plurality of nitrocellulose individual flares and the plurality of red phosphorus individual flares are stacked non-uniformly in sequence.
  • 21. The active body as claimed in claim 12, wherein the proportions of nitrocellulose individual flares and red phosphorus individual flares in the stacked sequence of the active mass varies from about 0% to about 100%.
  • 22. The active body as claimed in claim 12, wherein the proportions of red phosphorus individual flares and nitrocellulose individual flares in the stacked sequence of the active mass varies from about 0% to about 100%.
  • 23. An active body comprising: (a) an active mass comprising a plurality of flares that are arranged or stacked one behind the other and that are ignitable to produce decoy targets, wherein the plurality of flares are nitrocellulose and red phosphorus individual flares that are stacked uniformly or non-uniformly in sequence so that a red phosphorous individual flare comes to rest on a nitrocellulose individual flare, and a plurality of nitrocellulose individual flares follow one another or a plurality of red phosphorus individual flares follow one another, in order to vary a proportion of nitrocellulose and red phosphorous in the active body from about 0% to about 100%, or in order to vary a proportion of red phosphorous and nitrocellulose in the active body from about 0% to about 100%; and(b) a container that holds the active mass therein, andwherein the active body is munitions-free, non-pyrophoric, and produces an infrared jet when ignited.
Priority Claims (1)
Number Date Country Kind
10 2009 030 869 Jun 2009 DE national
Parent Case Info

This is a Continuation-in-Part Application in the United States of International Patent Application No. PCT/EP2010/003567 filed Jun. 15, 2010, which claims priority on German Patent Application No. DE 10 2009 030 869.5, filed Jun. 26, 2009. The entire disclosures of the above patent applications are hereby incorporated by reference.

US Referenced Citations (47)
Number Name Date Kind
2787217 Mahaffie Mar 1953 A
2678603 Prince, Jr. et al. May 1954 A
3216410 Trombatore et al. Nov 1965 A
3628416 Kernan Dec 1971 A
3760729 Freeman Sep 1973 A
4002122 Gould Jan 1977 A
4060435 Schroeder Nov 1977 A
4068591 Betts Jan 1978 A
4096804 Bilsbury Jun 1978 A
4374494 Maury Feb 1983 A
4409898 Blix et al. Oct 1983 A
4624186 Widera et al. Nov 1986 A
4838167 Prahauser et al. Jun 1989 A
H0000778 Carlton et al. May 1990 H
5074216 Dunne et al. Dec 1991 A
5635666 Bannasch et al. Jun 1997 A
5929369 Bissig et al. Jul 1999 A
5992327 Wardecki et al. Nov 1999 A
6055909 Sweeny May 2000 A
6427599 Posson et al. Aug 2002 B1
6513438 Fegg et al. Feb 2003 B1
6659012 Grassi et al. Dec 2003 B1
6666351 Hartz et al. Dec 2003 B1
7343861 Baker Mar 2008 B1
7363861 Brune et al. Apr 2008 B2
7421950 Dillard et al. Sep 2008 B2
7516700 Callaway Apr 2009 B1
7584702 Sutherland et al. Sep 2009 B1
7866265 Kravel et al. Jan 2011 B1
7992496 Dillard et al. Aug 2011 B2
8146504 Wallner et al. Apr 2012 B2
8276518 Dillard et al. Oct 2012 B2
20020011173 Schildknecht et al. Jan 2002 A1
20030116050 Brum et al. Jun 2003 A1
20040139876 Wilson et al. Jul 2004 A1
20040244626 Ehmig Dec 2004 A1
20060032391 Brune et al. Feb 2006 A1
20060201372 Nicolae Sep 2006 A1
20070039505 Dillard et al. Feb 2007 A1
20090007768 Wallner et al. Jan 2009 A1
20090095186 Dillard et al. Apr 2009 A1
20090301336 Wardercki et al. Dec 2009 A1
20100288111 Kunz Nov 2010 A1
20110146520 Guth Jun 2011 A1
20110174182 Guth et al. Jul 2011 A1
20120137913 Prelic et al. Jun 2012 A1
20120160121 Prelic et al. Jun 2012 A1
Foreign Referenced Citations (22)
Number Date Country
2146015 Feb 1995 CA
649 530 Aug 1937 DE
2359758 Jul 1988 DE
94 14 263 Oct 1994 DE
197 56 204 Mar 1999 DE
199 10 074 Sep 2000 DE
199 51 767 May 2001 DE
103 23 531 Feb 2005 DE
10 2005 020 159 Nov 2006 DE
10 2006 004 912 Jul 2007 DE
196 49 892 Jul 2008 DE
10 2007 032 112 Jan 2009 DE
10 2009 020 558 Nov 2010 DE
10 2009 030 868 Jan 2011 DE
0 204 115 Dec 1986 EP
715 614 Dec 1931 FR
250 271 Oct 1926 GB
11-173796 Jul 1999 JP
0019164 Apr 2000 WO
2007087948 Aug 2007 WO
20101003496 Jan 2010 WO
20101019291 Dec 2010 WO
Non-Patent Literature Citations (20)
Entry
International Search Report and IPRP issued in PCT/EP2010/003565, completed Aug. 31, 2010 and mailed Sep. 7, 2010.
International Search Report and IPRP issued in PCT/EP2010/003566, completed Aug. 27, 2010 and mailed Sep. 7, 2010.
International Search Report and IPRP issued in PCT/EP2010/003567, completed Sep. 16, 2010 and mailed Sep. 22, 2010.
International Search Report issued in co-pending related application PCT/EP2009/004113, completed Sep. 29, 2009 and mailed Oct. 6, 2009.
International Search Report issued in co-pending related application PCT/EP2009/004114, completed Oct. 1, 2009 and mailed Oct. 13, 2009.
International Search Report issued in co-pending related application PCT/EP2010/002332, completed Jun. 29, 2010 and mailed Jul. 6, 2010.
McGraw-Hill Dictionary of Scientific and Technical Terms (Sixth Ed.) 814 (2003).
“United States Naval Pyrotechnical Compositions,” at http://www.google.com/urlsa=t&rct=j&q=&esrc=s&source=web&cd=9&ved=0CGYQFjAI&url=http%3A%2F%2Fwww.ammunitionpages.com%2Fdownload%2F237%2FUS%2520navy%2520pyrotechnics pdf&ei=zjI6UsagMLXi4AOnw4Fw&usg=AFQjCNGhmQURaXkLjZAoI124I0jajOvmIg&sig2=vw04ff4-VMe—PYiiD8aZzw&bvm=bv.52434380,d.dmg (downloaded Sep. 18, 2013, five pages).
S.M. Danali et al., Developments in Pyrotechnics, 60 Defense Science Journal 152-158 (2010).
Clarence W. Gilliam et al., Flare, Igniter and Pyrotechnic Disposal: Red Phosphorous Smokes, Naval Ammunition Depot, AD-A013 182 (1975).
“Pyrotechnic Chemistry,” at http://www.islandgroup.com/military/pyrotechnic—chemistry.php (2013)(downloaded Sep. 18, 2013, two pages).
Charles A. Knapp, New Infrared Flare and High-altitude Igniter Compositions, Feltman Research and Engineering Laboratories, Picatany Arsenal (1959).
Rui Shu, Explosive Chemistry: The History and Chemistry of Explosives, Dartmouth Undergraduate Journal of Science 21-23 (2012).
Gao Guangyan, Nitrocellulose Synthesis Outline, at http://www.loneoceans.com/labs/nitrocellulose/ (2012).
Random House Webster's College Dictionary 506 (1991).
Office Action issed in co-pending related U.S. Appl. No. 13/291,281 on Sep. 5, 2013.
“Stainless Steels,” at http://www.dew-stahl.com/fileadmin/files/dew-stahl.com/documents/Publikationen/ Broschueren/015—DEW—RSH—GB.pdf (downloaded Dec. 2, 2013).
Notice of Allowance issued in co-pending related U.S. Appl. No. 13/380,959 on Nov. 26, 2013.
English translation (Jan. 2012) of the Written Opinion of the International Searching Authority in PCT/EP2010/003565.
Notice of Allowance issued in co-pending related U.S. Appl. No. 13/380,959 on Aug. 22, 2013.
Related Publications (1)
Number Date Country
20120174812 A1 Jul 2012 US
Continuation in Parts (1)
Number Date Country
Parent PCT/EP2010/003567 Jun 2010 US
Child 13337692 US