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    • 专利摘要:
    The present invention relates to a composite pyrotechnic product containing DNA and RDX fillers in a plasticized binder, comprising an energy polymer, of the PAG type, crosslinked and at least one energetic plasticizer, and its preparation. Typically: said crosslinked energy polymer consists of a glycidyl polyazide (PAG) having a number-average molecular weight (Mn) of between 700 and 3000 g / mol, crosslinked, via its hydroxyl terminal functions, with at least one polyisocyanate crosslinking agent; and said energetic charges, present at a mass ratio of 50 to 70%, consist, for at least 95% of their mass, of large ammonium dinitroamide crystals (ADN) and small hexogen crystals (RDX) + said large crystals of DNA being present at a mass ratio of 8 to 65%, advantageously from 10 to 60%, and + said small hexogen crystals (RDX) being present at a mass ratio of 5 to 55%, advantageously from 8 to 50%.
    公开号:FR3027598A1
    申请号:FR1402432
    申请日:2014-10-28
    公开日:2016-04-29
    发明作者:Yves Longevialle；Martine Golfier；Fabienne Morin
    申请人:Herakles SA；
    IPC主号:
    专利说明:

    [0001] The present invention relates to composite pyrotechnic products, particularly suitable as solid propellants for rocket engine propellant loadings, particularly as solid propellants for propellant loading of tactical missile engines. These are composite pyrotechnic products containing a high level of energy charges in an energy binder. These products, especially dedicated to tactical missile engines, are efficient: in terms of the speed of combustion, in terms of specific impulse, and in terms of discretion, that is to say that they do not contain, or only in very small quantities, in their composition, constituents whose combustion generates halogenated products or products, liquid or solid, which give a visible "signature" or significant infrared. In the field of tactical missiles, we search for propellants (called "clean", ie very discrete) having a high rate of combustion, very advantageously greater than or equal to 20 mm / s at a pressure of 10 MPa, and a strong specific impulse very advantageously greater than 245 s (when calculated at 7 MPa for a 70/1 expansion). In any case, it is desired to generate, for a short period of time, a flow of gas ensuring a strong thrust. At present, so-called "clean" propellants contain as their energetic charge ammonium nitrate. The specific impulse and burning rates of such propellants remain low. The publication of Anders Larsson and Niklas Wingborg (2011), entitled "Green Propellants Based on Ammonium Dinitramide (DNA)", in "Advances in Spacecraft Technologies, Dr. Jason Hall (Ed.), ISBN 978-953-307-8" , evaluated propellants containing energetic charges of dinitroamidium ammonium ("ammonium dinitramide" = DNA; charges introduced in the form of "prills" (spherical granules (beads) prepared from crystals), typically at mass ratios (high) of 70 to 80%, in an energetic binder of the glycidyl polyazide type (PAG). Such propellants have high combustion rates, from about 30 mm / s to 10 MPa. They also have a high specific pulse, of about 300 s (value calculated under vacuum, corresponding to a value (calculated) of about 256 s to 7 MPa for a 70/1 expansion). They therefore theoretically meet the need. However, those skilled in the art are aware that the use of DNA in the form of "prills" increases the production of any material containing said DNA. He wishes to use the DNA crystals, directly obtained by crystallization of DNA in solution, at the end of one of his syntheses or simply crushed crystals. Said skilled man is also aware of the difficulties that exist to: manipulate the DNA crystals: the absorption of water by said crystals (which increases when the size of said crystals decreases) poses serious problems; and conditioning the DNA crystals in a polymer (here PAG) to cross-link with polyisocyanates (to obtain the binder): the DNA, by its intrinsic acidity, consumes a part of the crosslinking agent ( polyisocyanate (s)) and makes it necessary to use a rate of said agent all the more consequent that it is itself present in large quantities. This inevitably degrades the performance level of the final product (propellant). In addition, the skilled person is aware that, in general, to obtain a binder heavily loaded with crystals, it is not only necessary that the crystals in question have a low aspect ratio, ideally they are spherical, but also that crystals of different sizes are present, typically small and large crystals (the notions of "small" and "fat") are obviously relative), for example micron crystals, even submicron crystals, and crystals a dozen or even a hundred microns. Now, to date, it is difficult to obtain small crystals of DNA (even by grinding) in view of the hydroscopy of said small crystals. The easily accessible DNA crystals generally have a size greater than or equal to 10 μm and are therefore not suitable for obtaining propellants, and more generally for high-charge composite pyrotechnic products. Propellants heavily loaded with DNA crystals have so far still not experienced industrial development.
    [0002] The person skilled in the art, in view of the difficulties mentioned above, has therefore still not developed industrially propellants with high levels of DNA (crystals) in a binder of the PAG type (ie PAG / DNA type propellants). (crystals)), despite the good performance expected of such propellants (see above).
    [0003] Energy charges, other than DNA, exist elsewhere, in particular hexogen (RDX), octogen (H MX) and hexanitrohexaazaisowurtzitane (CL20), for which the production of crystals (small and large crystals), with a view to obtaining high-load propellants, is perfectly controlled.
    [0004] The patent applications FR 2 954 309 and FR 2 997 695 thus describe explosives heavily loaded with RDX, said RDX being present in the form of small and large crystals. U.S. Patent Applications Nos. 4,938,813, 5,061,330 and 5,507,891 disclose solid propellants containing energetic, octogen (HMX) or hexogen (RDX) charges in energetic binders plasticized with plasticizers. energy. The specific impulse of these propellants is much lower than that of propellants of PAG / DNA type. Their burning rate is less than 15 mm / s at a pressure of 10 MPa, even though their composition contains a ballistic catalyst. The addition of a ballistic catalyst generates, during the combustion of these propellants, particles, which affects their discretion. US Pat. No. 5,690,868 describes two formulations for obtaining oxetane energy-binding multilayer propellants, containing, for one, hexanitrohexaazaisowurtzitane (CL20) and, for the other, hexogen (RDX). or octogen (HMX). The burning rate of the layer containing RDX or HMX is lower than that of the layer containing CL20. However, although the CL20 is therefore a potentially interesting candidate (more interesting, in any case, than RDX or HMX) in substitution for DNA, its pyrotechnic sensitivity makes it difficult to use, especially at a high rate. charge (> 30 ° h in mass). It can not be used as an alternative to DNA.
    [0005] Those skilled in the art, in fact, ignore neither the sensitivity of CL20 per se, nor the very high sensitivity of a DNA / CL20 complex likely to form when both types of charge (in the form of crystals) are in Presence (see May 11, 2011, RTO MP-23, 41-1-41-8 by L. Chan and Alan D. Turner, entitled "Minimum-signature propellant with mixed-oxidizer concept" (corresponding to the document presented at the RTO AVT Symposium). on "Small Rocket Motors and Gas Generators for Land, Sea and Air Launched Weapon Systems", held in Corfu (Greece) from 19 to 23 April 1999)).
    [0006] US Patent Application 2003/0047260 discloses propellants, containing DNA crystals, DNA "prills" and / or CL20 crystals, in a plasticized energetic binder with energetic plasticizer (s). Said propellants have a minimal signature and a strong specific pulse (a calculated value of 265 s to 7 MPa is indicated for a 70/1 expansion), for such propellants with DNA charges or DNA charges and charges of CL20). A combustion catalyst (ballistic catalyst) of the carbon black type is conveniently present in the composition of said propellants. It is particularly described in this document propellants with DNA crystals, propellants with crystals and "prills" of DNA, and propellants with DNA "prills" and crystals of CL20. In the presence of carbon black (ballistic catalyst), the burning rate of these propellants is about 25 mm / s to 10 MPa (see Figures 2 to 6 of said application).
    [0007] The prior art thus teaches, on the one hand, that propellants of the PAG / DNA type, with high energetic charge rates (DNA introduced in the form of "prills"), have a high rate of combustion and a specific impulse, but that the properties (particularly of particle size) of the DNA crystals are incompatible with the feasibility of PAG / crystal crystals of high crystalline type propellants, and, secondly, that, if we consider only performance, the CL20 is a substitute (at least partial) interesting potential of DNA. Since composite pyrotechnic products containing RDX charges are known to exhibit a lower combustion rate than those containing charges of CL20, the RDX thus did not appear, in any way, according to the teaching of the prior art, a candidate interesting to associate with the DNA, in order to achieve the desired performance in the context of the invention (combustion rate, specific pulse and high discretion).
    [0008] In such a context, the plaintiff is currently proposing a new high-performance composite pyrotechnic product. It is the merit of the applicant to have identified, contrary to the teaching of the prior art (see above), the interest of co-formulating DNA (crystal) charges and charges. RDX (crystals) in a binder of the PAG type, particularly with reference to the objectives of high combustion rates and specific desired pulse; said objectives can be achieved without resorting to components that are deleterious in terms of signature (discretion) (the co-formulation in question proving particularly interesting according to a variant A = "strong" DNA level and "weak" RDX rate, but also interesting according to a variant B = "strong" rate of RDX and "low" DNA level, and therefore, interesting, in general, the mass levels of DNA and RDX specified below. It is already indicated here that the notions of "strong" rate and "low" rate are relative notions, identical or not depending on the context). According to its first object, the present invention thus relates to new composite pyrotechnic products. They are of the crosslinked energy binder type containing energy charges. They contain, more specifically, in a plasticized binder comprising a crosslinked energy polymer and at least one energetic plasticizer, energetic charges. Typically: said crosslinked energy polymer consists of a glycidyl polyazide (PAG) having a number-average molecular weight (Mn) of between 700 and 3000 g / mol, crosslinked, via its hydroxyl terminal functions, with at least one polyisocyanate crosslinking agent; and - said energy charges, present at a mass ratio (high) of 50 to 70% (in the composition of said product), consist, for at least 95 ° h of their mass, in large ammonium dinitroamidide crystals (DNA ) and small hexogen crystals (RDX): + said large ammonium dinitroamidide crystals (DNA), being present (in the composition of said product) at a mass ratio of 8 to 65 ° / 0, advantageously 10 at 60 ° A), and + said small hexogen crystals (RDX) being present (in the composition of said product) at a mass ratio of 5 to 55 ° h, preferably 8 to 50 ° h. The structure of the composite pyrotechnic products of the invention therefore typically associates: a specific energetic binder comprising a crosslinked PAG (hydroxytelechelic) type energy polymer and at least one energetic plasticizer, and a high level (50 to 70%) (H mass) energy charges, in the form of crystals, of which at least 95 ° h by mass, generally at least 97 ° A) by mass, or even 100 ° h by mass, are energy charges (crystals) of specific nature: DNA (highly energetic) + RDX (which unexpectedly proved to be a partner (of this DNA) much more interesting than CL20). One can speak of the presence of a "cocktail" of specific energy charges (crystals): DNA + RDX. The desired result, as for the high level of charges, is obtained ("in a known manner per se") by the co-presence of large crystals (of DNA easy to obtain) and small crystals (of RDX also easy to obtain) . These notions of "big" and "small" are obviously relative. It can be pointed out that the DNA crystals in question are generally at least 5 times larger than the RDX crystals in question, more generally at least 10 times larger, or even at least 25 times larger. The RDX crystals present are advantageously micron: they thus advantageously have a size of 1 to 10 μm (including extreme values), very advantageously from 2.5 to 5 μm (including extreme values). It is of course understood that said crystals advantageously have sizes from 1 to 10 μm (each crystal having a size), very advantageously from 2.5 to 5 μm. The DNA crystals advantageously have a size of 50 to 250 μm (including extreme values); it is understood that said crystals have sizes of 50 to 250 pm (each crystal having a size)). This association of small and large crystals (easy to obtain) is particularly appropriate in that, first of all, it does not require small DNA crystals (see the difficulty mentioned above to obtain such small crystals and the "acute" problem of the absorption of water by said small crystals) and in that it thus allows to obtain a product with a high level of charges. In addition, the density of RDX (1.82 g / cm3) being close to that of DNA (1.81 g / cm3), a homogeneous distribution of the two fillers (of the two types of crystals) in the product is ensured during the process of obtaining the product, without particular difficulty. This association has proved particularly advantageous in reference to the targeted performances. The nature of the binder (that of its precursor polymer) is therefore one of the key elements (of the composition) of the composite pyrotechnic products of the invention. Incidentally note here that the "a" glycidyl polyazide (= binder precursor polymer) should read "at least one" glycidyl polyazide throughout the present text. Indeed, it is in no way excluded from the scope of the invention to use a mixture of at least two glycidyl polyazides (having molecular weights (between 700 and 3000 g / mol) and / or different branching ratios). as precursor polymer of the binder of the products of the invention.
    [0009] The energetic polymer selected as precursor of the binder of the products of the invention is therefore a polyazide, a glycidyl polyazide (PAG) which has terminal hydroxy functions (a hydroxytelechelic PAG); hence 1) its energetic properties and 2) its ability to be crosslinked with polyisocyanate crosslinking agents. Said polymer has an adequate molecular weight (in particular, with reference to its consistency (liquid) and the consistency of its mixture with essentially the fillers and with reference to the relative content of crosslinked binder (s) crosslinking), number average molecular weight (Mn) between 700 and 3000 g / mol, preferably between 1700 and 2300 g / mol. It is the merit of the inventors to have selected this type (precursor polymer) of binder, (precursor polymer) of energy binder, perfectly suitable for use with the selected energy charges (the "cocktail" of energy charges, present at the same time). crystal state, recommended). Crosslinking agents, of the polyisocyanate type (at least bifunctional), which are suitable for the crosslinking of such a hydroxytelechelic glycidyl polyazide (PAG), are known per se. It may especially be di- or triisocyanates. Advantageously, these are liquid polyisocyanates chosen from toluene diisocyanate (TDI), isophorone diisocyanate (IPDI), dicyclohexylmethylene diisocyanate (MDCI), hexamethylene diisocyanate (HDI), trimer of said hexamethylene diisocyanate (especially commercialized by Bayer under the trade name Desmodur® N 3300), biuret trihexane isocyanate (BTHI), 3,5,5-trimethyl-1,6-hexamethylene diisocyanate and mixtures thereof. In a particularly preferred manner, the trimer of hexamethylene diisocyanate is used.
    [0010] Said crosslinking agents are conventionally used in an amount necessary and sufficient to ensure the crosslinking of the polymer (not excessive so as not to pollute the crosslinked product obtained). They are conventionally used in an amount such that the bridging ratio (NCO (of the crosslinking agent) / OH (of the polymer)) is between 0.8 and 1.4, or advantageously of 1. The crosslinked energy polymer is generally from 10 to 14% by weight of the total composition of the composite pyrotechnic products of the invention. The energy polymer per is generally involved for 8 to 12% by weight, the at least one crosslinking agent for about 2% by weight. It is understood that the nature of the binder (that of its precursor polymer) is not per se original but that the interest of the invention lies in the combination of such a (precursor polymer) binder with charges specific energy. Conventionally, the energy binder is associated with at least one energetic plasticizer. The energy plasticizer (s) in question is (are) advantageously of the nitrate and / or nitramine type. The energy plasticizer (s) in question is (are) very advantageously selected from diethylene glycol dinitrate (DEGDN), triethylene glycol dinitrate (TEGDN), butanetriol trinitrate (BTTN) , trimethylolethane trinitrate (TMETN), a mixture of 2,4-dinitro-2,4-diazapentane, 2,4-dinitro-2,4-diaza-hexane and 3,5-dinitro-3,5- diazaheptane (and especially DNDA 5.7), and nitrato ethyl nitramines (especially methyl-2-nitratoethyl nitramine (methylNENA) and ethyl-2-nitratoethyl nitramine (ethylNENA)) and mixtures thereof. The plasticizer (s) of the pyrotechnic products of the invention generally represent from 10 to 30% by weight, more generally from 15 to 25% by weight, of the total composition of said products.
    [0011] The specificity of the energy charges present (in the form of crystals) (of the "cocktail" of such energy charges present) is therefore the other of the key elements (of the composition) of the composite pyrotechnic products of the invention.
    [0012] Said specificity resides, partly, in the nature of said charges ((crystals of) DNA + (crystals of) RDX) and, on the other hand, in the relative size of said charges (large crystals of DNA and small crystals of RDX); this relative size of said charges ((crystals of) DNA + (crystals of) RDX) allowing the high overall rate of charge: from 50 to 70 ° h by mass, preferably from 55 to 65 ° h by mass. It has been noted that the presence of energetic charges, other than DNA fillers (crystals) and RDX fillers (crystals), is not totally excluded. In any case, energy charges, other than said DNA and RDX charges, are possibly present only at a mass ratio of not more than 5% by mass. The charges of the composite pyrotechnic products of the invention consist essentially, if not exclusively, of said DNA and RDX crystals. As indicated above: the DNA crystals are present in a proportion of 8 to 65%, advantageously 10 to 60%, very advantageously in a proportion of 40 to 60%, by weight in the composition of the products of the invention; and the RDX crystals are present at 5 to 55.degree., advantageously 8 to 50.degree., very advantageously at 8 to 20%, by weight in the composition of the products of the invention. invention. According to a particularly preferred variant, said DNA crystals are present at a mass content of 40 to 60% and said RDX crystals at a mass ratio of 8 to 20 ° h. As regards the size of said charges (crystals), reference is made to what has been developed earlier in the present text.
    [0013] As regards the morphology of said charges, it is obviously desirable that the crystals have a low aspect ratio 2, advantageously 1.5), ideally they are spherical. According to one variant of the invention (variant A above), in particular the particularly preferred one above, RDX is present, as a partial substitute for DNA, at a "low" level (typically 20%), in the form of small crystals therefore, resulting in a high content of fillers (small RDX crystals and large DNA crystals) possible, with a decrease in the intensity of the problems inherent in the DNA (to the extent that less DNA, in the form of large crystals, is present) and, quite unexpectedly, the presence of said RDX, however, allows the obtaining of specific values of combustion rate and pulse very interesting (see the results of the Example 1 of Table 1 below). According to another variant of the invention (variant B above), the RDX is present at a "high" level (typically 40 to 60% by mass) and the DNA at a "low" level ( typically 8 to 20 ° h by mass), which obviously allows high levels of charges (small crystals of RDX and large crystals of DNA), with a consequent decrease in the intensity of the problems inherent in the DNA, and Unexpectedly, in the context of this variant too, specific values of combustion rate and impulse value (albeit less interesting than in the context of the first variant above) have been obtained (see the results below). of Example 2 of Table 1 below and Example 2 'of Figure 1). It is recalled here, for all intents and purposes, that the notions of "strong" rate and "low" rate are relative notions, identical or not depending on the context. Moreover, it is understood that the two above variants of the invention are not exhaustive (the co-formulation of "equivalent" DNA and RDX levels obviously forming part of the invention (see above )). The absence (or the presence, in any case, in a minimal amount (<3% by mass)) of inorganic fillers (crystals), other than DNA, within the (composition) pyrotechnic products composites of the invention is interesting with reference to the technical problem of the signature of said products in combustion (the generation of combustion fumes). Thus, the composition of the composite pyrotechnic products of the invention is advantageously free of inorganic fillers other than DNA. The composition of the composite pyrotechnic products of the invention is also free of metal charges (capable of generating particles during their combustion). The composite pyrotechnic products of the invention are also likely to contain, and generally contain, in their binder, in addition to the fillers and plasticizer (s), at least one additive. Among the additives that are suitably present, the following conventional additives are preferred: the crosslinking catalysts and the stabilizing agents of the plasticizer (s) energy (s) present (s). Thus, according to an advantageous variant, the composite pyrotechnic products of the invention therefore contain in their composition, in addition to the crosslinked polymer (PAG), the plasticizers (s) and fillers, at least one additive; said at least one additive comprising at least one crosslinking catalyst and / or at least one stabilizing agent of the plasticizer (s) present. Said at least one polymerization catalyst may especially be chosen from triphenylbismuth and tin dibutyldilaurate (DBTL). Present, it is usually at a content not exceeding a few hundred ppm. Said at least one stabilizing agent for the plasticizer (s) present may, in particular, consist of at least one aromatic amine, such as 2-nitrodiphenylamine (2-NDPA) and N-methylparanitroaniline (MNA). Present, it is generally at a content of about 1% by weight. Other additives that may be present in the composition of the composite pyrotechnic products of the invention may especially consist of one or more processing agents (manufacturing aid). The said agent (s) are generally present at a content of 1 to 2% by weight. It is also not excluded that said composition contains (at least) a combustion catalyst (with reference to the optimization of its combustion rate). It is understood that the presence of (at least) such a combustion catalyst may be totally superfluous in a composition containing a high content of DNA, but that it may be appropriate within a composition containing a low content in DNA. Such at least one combustion catalyst (preferably consisting of bismuth citrate) is thus not present or, in any case, only present in a small amount 4 ° A) by mass). This is obviously advantageous with reference to the third stipulation of the specifications (discretion).
    [0014] The additives which may be present (in view of the above remarks, it has been understood that generally several types of additive are present) generally represent a maximum of 6% by weight of the composition of the composite pyrotechnic products of the invention. They generally represent from 0.1 to 6% by weight of the composition of said composite pyrotechnic products of the invention. In view of the above remarks, it is understood that the composite pyrotechnic products of the invention are not of a new type but that they are new by the combination, in their composition, of a specific binder (PAG (Hydroxytelechelic) (crosslinked with at least one polyisocyanate and plasticized with at least one energetic plasticizer) and with a "cocktail" of specific energetic charges (DNA crystals + RDX crystals). the composition of the composite pyrotechnic products of the invention, expressed in percentages by weight, thus contains: from 50 to 70.degree., advantageously from 55 to 65.degree., energy charges, consisting, for at least 95% of their mass, in DNA crystals and RDX crystals (see above), 10 - 14 ° h of the cross-linked energy polymer (of the hydroxytelechelic PAG type) (via its terminal hydroxy functions by at least one polyisocyanate), - from 10 to 30 ° h, advantageous 15 to 25.degree., from at least one energetic plasticizer, and from 0 to 6.degree., advantageously from 0.1 to 4%, of at least one additive. In the context of this advantageous variant, said composition is generally free from any other ingredient and therefore consists of the ingredients listed above, present in the amounts indicated above. Incidentally, it is recalled here that said composition is advantageously free of any inorganic energy charge other than DNA and any metal charge, or even any inorganic energy charge other than DNA, any metal charge and any combustion catalyst. The products of the invention are therefore interesting in terms of the combustion rate, specific impulse, and the weak signature (discretion) of the plume generated during their combustion, especially in propellant (their composition does not contain any charges. metal generating particles, no or very few inorganic energy charges other than DNA) and also by their feasibility. The coformulation of large crystals of DNA and small RDX crystals in a PAG-type energy binder made it possible to obtain products with high levels of charge, particularly efficient in reference to the specifications set out in the introduction to this text. . The DNA + RDX combination has surprisingly been particularly interesting. The above remarks are confirmed by the results of Table 1 below and those shown in FIG. 1. According to its second object, the present invention relates to a process for the preparation of a composite pyrotechnic product, as described above. above. This process comprises: - the constitution of a homogeneous paste by a) addition, with stirring, in a suitable glycidyl polyazide (hydroxytelechelic PAG having a number-specific molecular mass as specified above), of at least one plasticizer energy, energy charges and other constitutive ingredients of the desired composite pyrotechnic product, with the exception of any crosslinking agent and any crosslinking catalyst, and b) stirring the resulting mixture under partial vacuum; under partial vacuum, adding, to said homogeneous paste constituted by said at least one crosslinking agent and optionally at least one crosslinking catalyst, followed by stirring of the mixture constituted; Pouring said stirred mixture into at least one structure; and - the heat treatment of said stirred mixture formed in said at least one structure.
    [0015] The first steps of this process (constitution of the homogeneous paste and then mixing said paste with crosslinking agent (s) and optionally crosslinking catalyst (s)) are carried out at a suitable temperature (s) (s). ), with reference to the viscosity of the mixture concerned, to the problem of the reaction of the DNA present with the at least one crosslinking agent present (see the introduction to this text) (and of course to the stability of the energy charges present ). They are generally carried out at 20 to 40 ° C (20-40 ° C).
    [0016] The heat treatment (crosslinking) is generally carried out at atmospheric pressure at a temperature between 30 and 50 ° C (301550 ° C) for several days. In any event, it is expedient, throughout the process, to operate at a non-excessive temperature of 50.degree. C. in order to minimize any reaction of the DNA with the at least one crosslinking agent. The partial vacuum mentioned is intended for degassing of the medium above which it is applied. It is usually 10 mm Hg. Incidentally, it is not necessarily constant intensity.
    [0017] This method can be considered as a method by analogy, but, typically, it is carried out with the specific precursor polymer (binder precursor) and the "cocktail" of specific energetic fillers (crystals). It is now proposed to illustrate the invention by the examples below and the appended FIG. Said appended FIG. 1 shows the combustion rates (as a function of pressure) of a propellant of the invention and three reference propellants.
    [0018] A. The following comparative examples Ref. 1 to Ref. And Examples 1 and 2 illustrating the invention. For all the examples, the same energy polymer of the hydroxytelechelic PAG type (marketed by the company EURENCO 5 (Mn (number-average molecular weight) = 1900 g / mol) was used, the same crosslinking agent (Desmodur® N 3300 marketed by Bayer), the same plasticizers (BTTN / TMETN: 30/70 (mass%)), the same plasticizer stabilizers (MNA / 2-NDPA: 75/25 (mass%)) were used and also The same types of fillers (crystals) were used, DNA: 50 to 250 μm, RDX: 2.5 to 10 μm, and CL20: 20 to 50 μm.The same process for obtaining propellant from mixtures of The constituent ingredients of said propellant were used: first mixing steps at 40 ° C., casting and then crosslinking, in an oven, at atmospheric pressure, at 45 ° C. for 14 days, in the first part of Table 1 below. -after, the mass composition of the propellants is indicated and in the second part of said tab water 1 indicates properties of said propellants (combustion rates and specific impulse). The burning rates are measured, the specific pulses calculated at 7 MPa for a 70/1 expansion. The results obtained with the products of Réfs. 1 (without combustion catalyst) and 2 (with combustion catalyst: CiPb) confirm that RDX does not perform well. The product according to Ref. 3 (containing 62.5 ° H by mass of large DNA crystals) could not be tested since it was not healthy (the cross-linked block contained too many bubbles, witnesses of a DNA + reaction) trimer of hexamethylene diisocyanate (Desmodur® N 3300)). The calculation confirms a high value of the specific pulse (thus theoretical value).
    [0019] The product according to Ref. 4 is efficient but its obtaining involves the manipulation of CL20 crystals and the co-conditioning of crystals of CL20 and DNA. The product according to Ref. 5 (whose obtaining involves the manipulation of crystals of CL20) confirms that the performance of a mixture RDX (50%) + CL20 (10 ° / 0) + combustion catalyst (4 ° h) is greater than the performance of the RDX (65 ° h) only (see product results according to Ref.1). Said performance of said mixture RDX (50 ° h) + CL20 (10 ° h) + combustion catalyst (4%) corresponds, particularly as regards the rate of combustion, to that of RDX (62.5 ° h) with combustion catalyst (3.5 ° h) (see product results as per Ref 2). This performance remains inferior, especially with regard to the rate of combustion, to those of a "equivalent" ADN (10 ° h) + RDX (50 ° h) + combustion catalyst (4 ° h) (according to the The invention (see the results of the product according to Example 2) Example 1 illustrates the particularly preferred variant of the invention according to which the DNA is present between 40% and 60% by mass (at exactly 52% by weight). mass) and the RDX between 8 ° h and 20 ° h by mass (exactly 9.82% by mass) .This RDX is here present as a partial substitution of said DNA.The propellant obtained is very efficient. of this invention, according to this particularly preferred variant, have high combustion rates of greater than 20 mm / s at 10 MPa and 40 mm / s at 18 MPa, and this, in the absence of a ballistic catalyst, as well as high specific pulses, greater than 245 s (calculated at 7 MPa for one die) Example 2 illustrates the variant of the invention according to which the RDX is present at a high level (> 20% by weight, more precisely 50% by mass), which is much higher than the DNA (10% by weight). The copresence of DNA crystals, RDX crystals (DNA + RDX = 60 ° h by mass) and the combustion catalyst (CiBi) is very interesting. The performances obtained are superior to those of RDX alone (Ref.1: 65 ° h in RDX mass) and that of RDX (62.5 (Yo in mass) with combustion catalyst (Ref.2).
    [0020] 21 Table 1 Ref.1 Ref.2 Ref.3 Ref.4 Ref.5 Ex.1 Ex.2 Binder / charge PAG / RDX PAG / RDX PAG / DNA PAG / PAG / PAG / PAG / ADN / CL20 RDX / CL20 DNA / RDX DNA / RDX Energy charges RDX 65 62.5 / / 50 9.82 50 CL20 / / / 25 10 / / DNA / / 62.5 40/52 10 Polymer crosslinked PAG 10.63 9.63 9.63 10.63 10.63 9.82 10.63 Desmodur® N 3300 2.14 2.01 2.01 2.14 2.14 2.1 2.14 BTTN / TMETN Plasticizer 20.57 19.7 19.7 20.57 21.37 23.70 20.57 Stabilizers (MNA / 2-NDPA) 0.8 0.8 0.8 0.8 0.8 0.8 0.8 Catalyst for Combustion Lead Citrate (CiPb) / 3.5 / / / / Bismuth citrate (CiBi) 3.5 4 4 Processing aids 0.86 1.86 1.86 0.86 1.06 1.76 1.86 Properties Vc (mm / s) at 10 MPa 8.8 16.4 / -25 16.0 29.1 18.1 Vc (mm / s) at 18 MPa 15.3 20.4 / - 33 20.4 42 25.2 Isp (7 Mpa) ) (b) 236 236 251 258 247 250 239 B. Burning rates (as a function of pressure) were measured for products similar to those in Table 1: - a product of the invention according to Example 2 ( whose composition contained 10% by mass of DNA crystals (50-250 μm) and 50 ° AD by mass of RDX crystals (2.5-10 μm) (i.e. 60% by weight of energetic crystals) in a binder (obtained from a premix (34.5% by weight of PAG (see A above) + triisocyanate (HDI trimer, Desmodur® N3300 from Bayer) + BTTN / TMETM (30/70) + stabilizers of said BTTN and TMETM) + 4% by weight of bismuth citrate (combustion catalyst) + 1.5 ° h by weight of manufacturing auxiliaries); and - three reference products: + one product Ref. 1 '(the composition of which contained 60% by mass of RDX crystals (2.5-10 μm) in a binder (obtained from a premix (38.5% by weight of PAG (see A above ) + triisocyanate (HDI trimer, Desmodur® N3300 from Bayer) + BTTN / TMETM (30/70) + stabilizers of said BTTN and TMETM} + 1.5 ° h by weight of manufacturing auxiliaries) + a product Ref. 2 '(the composition of which contained 60 ° h by mass of RDX crystals (2.5-10 μm) in a binder (obtained from a premix (35 ° h by weight of {PAG (see A above ) + triisocyanate (HDI trimer, Desmodur® N3300 from Bayer) + BTTN / TMETM (30/70) + stabilizers of said BTTN and TMETM} + 3.5 ° h by mass of lead citrate (combustion catalyst) +1, 5% by weight of manufacturing aids) and + a product Ref 5 '(the composition of which contained 50 ° A) by mass of RDX crystals (2.5-10 μm) and 10 ° by mass of crystals of CL20 (20-50 μm) in a binder (obtained from a premix (34.5 ° h by weight of PAG (v ir A above) + diisocyanate (HDI trimer, Desmodur® N3300 from Bayer) + BTTN / TMETM (30/70) + stabilizers of said BTTN and TMETM} + 4% by mass of bismuth citrate (combustion catalyst) + 1.5 ° h by weight of manufacturing auxiliaries). The consideration of the curves of Figure 1 highlights the interest of the composite pyrotechnic products of the invention, more particularly that of said products according to the variant of the invention at "low" DNA level (variant B above).
    权利要求:
    Claims (9)
    [0001]
    REVENDICATIONS1. Composite pyrotechnic product comprising, in a plasticized binder, comprising a crosslinked energy polymer and at least one energetic plasticizer, energetic charges, characterized in that: said crosslinked energy polymer consists of a glycidyl polyazide (PAG) having a molecular weight number average (Mn) between 700 and 3000 g / mol, crosslinked, via its terminal hydroxyl functions, with at least one crosslinking agent of polyisocyanate type; and - said energy charges, present at a mass ratio of 50 to 70 ° h, consist, for at least 95% of their mass, in large ammonium dinitroamidide crystals (DNA) and small hexogen crystals (RDX ) + said large ammonium dinitroamidide crystals (DNA) being present at a mass ratio of 8 to 65 ° h, preferably 10 to 60 ° / 0, and + said small hexogen crystals (RDX) being present at a mass ratio of 5 to 55%, advantageously 8 to 50%.
    [0002]
    2. Composite pyrotechnic product according to claim 1, characterized in that said glycidyl polyazide (PAG) has a number-average molecular weight (Mn) of between 1700 and 2300 g / mol.
    [0003]
    3. composite pyrotechnic product according to claim 1 or 2, characterized in that said at least one energetic plasticizer is of the nitrate and / or nitramine type.
    [0004]
    4. Composite pyrotechnic product according to any one of claims 1 to 3, characterized in that said energy charges are present at a mass ratio of 55 to 65%.
    [0005]
    5. composite pyrotechnic product according to any one of claims 1 to 4, characterized in that said ammonium dinitroamidide crystals (DNA) are present at a mass content of 40 to 60% and said hexogen crystals (RDX) at a mass ratio of 8 to 20%.
    [0006]
    6. composite pyrotechnic product according to any one of claims 1 to 5, characterized in that it further contains at least one additive.
    [0007]
    7. Composite pyrotechnic product according to claim 6, characterized in that said at least one additive comprises at least one crosslinking catalyst and / or at least one stabilizing agent of the at least one energetic plasticizer.
    [0008]
    8. composite pyrotechnic product according to any one of claims 1 to 7, characterized in that its composition, expressed in percentages by weight, contains: - from 50 to 70 ° / 0, preferably from 55 to 65 ° A), said charges comprising at least 95% of their mass, said DNA crystals and said RDX crystals, from 10 to 14% of said crosslinked energy polymer, from 10 to 30 ° C., advantageously from 15 to 25 ° C. of said at least one energetic plasticizer, and 0 to 6 ° AD, preferably 0.1 to 4%, of at least one additive.
    [0009]
    9. Process for preparing a composite pyrotechnic product according to any one of claims 1 to 8, characterized in that it comprises: - the constitution of a homogeneous paste by a) addition, in said glycidyl polyazide, said at least one energetic plasticizer, energetic fillers and other constitutive ingredients of the desired composite pyrotechnic product except for any crosslinking agent and any crosslinking catalyst, and b) stirring the resulting mixture under partial vacuum ; under partial vacuum, adding, to said homogeneous paste constituted by said at least one crosslinking agent and optionally at least one crosslinking catalyst, followed by stirring of the mixture constituted; then pouring said stirred mixture into at least one structure; and - the heat treatment of said stirred mixture formed in said at least one structure.
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    同族专利:
    公开号 | 公开日
    IL251767A|2020-04-30|
    IL251767D0|2017-06-29|
    WO2016066946A1|2016-05-06|
    PL3212593T3|2018-11-30|
    US20170320787A1|2017-11-09|
    KR20170101898A|2017-09-06|
    JP6510641B2|2019-05-08|
    FR3027598B1|2018-05-04|
    JP2018500260A|2018-01-11|
    EP3212593B1|2018-08-01|
    EP3212593A1|2017-09-06|
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    法律状态:
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    2018-08-24| TP| Transmission of property|Owner name: ARIANEGROUP SAS, FR Effective date: 20180724 |
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    优先权:
    申请号 | 申请日 | 专利标题
    FR1402432A|FR3027598B1|2014-10-28|2014-10-28|COMPOSITE PYROTECHNIC PRODUCT WITH DNA AND RDX LOADS IN PAG TYPE BINDER AND PREPARATION THEREOF|
    FR1402432|2014-10-28|FR1402432A| FR3027598B1|2014-10-28|2014-10-28|COMPOSITE PYROTECHNIC PRODUCT WITH DNA AND RDX LOADS IN PAG TYPE BINDER AND PREPARATION THEREOF|
    EP15798505.2A| EP3212593B1|2014-10-28|2015-10-27|Composite pyrotechnic product with adn and rdx charges in a gpa binder and preparation of same|
    PL15798505T| PL3212593T3|2014-10-28|2015-10-27|Composite pyrotechnic product with adn and rdx charges in a gpa binder and preparation of same|
    JP2017522950A| JP6510641B2|2014-10-28|2015-10-27|Composite pyrotechnic product having ADN charge and RDX charge in GAP type binder and method for producing the same|
    PCT/FR2015/052889| WO2016066946A1|2014-10-28|2015-10-27|Composite pyrotechnic product with adn and rdx charges in a gpa binder and preparation of same|
    US15/522,650| US10040731B2|2014-10-28|2015-10-27|Composite pyrotechnic product with ADN and RDX charges in a gap type binder, and preparation thereof|
    KR1020177014381A| KR20170101898A|2014-10-28|2015-10-27|Composite pyrotechnic product with adn and rdx charges in a gap binder and preparation of same|
    IL251767A| IL251767A|2014-10-28|2017-04-18|Composite pyrotechnic product with adn and rdx charges in a gpa binder and preparation of same|
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