17results about "Nitrocellulose explosive compositions" patented technology

The invention belongs to the technical field of plant fiber recycling, and particularly relates to corncob nitrocellulose as well as a preparation method and application thereof. The preparation method comprises the following steps: performing alkalization treatment on corncob powder to form corncob powder easy to hydrolyze, and removing hemicellulose and lignin; neutralizing and acidizing to remove impurities such as grease and the like; carrying out nitration treatment on the acidified corncob powder to form a corncob fiber rubber powder semi-finished product; reacting potassium nitrate, diphenylamine and the preheated corncob fiber rubber powder semi-finished product under a heating condition, and adding a stabilizer to form corncob fiber rubber powder, namely the corncob nitrocellulose. The corncob fiber rubber powder is excellent in combustion performance, free of smoke and peculiar smell, only has trace residues after combustion, can be used as various safe and environment-friendly firework products, and can also be used as an environment-friendly coating additive material.

The invention relates to a combustible propellant charge case for ammunition dischargeable from a gun barrel, comprising cellulose, nitrocellulose, MO3 particles, wherein M = Mo and / or W, and cationic surfactant, wherein the average particle size d50 of the MO3 particles is 0.5–2.0 µm, the maximum particle size d100 of the MO3 particles is ≤ 20 µm, and the quotient of the average MO3 concentration in wt.% in a volume element of approximately 0.05 to 1.0 cm3 (cVE) at any desired point in the propellant charge case and the total MO3 concentration in wt.% (ctot) in the propellant charge case is cVE:ctot = 0.80–0 1.20.

The invention relates to a combustible propellant charge case for ammunition dischargeable from a gun barrel, comprising cellulose, nitrocellulose, MO3 particles, wherein M = Mo and / or W, and cationic surfactant, wherein the average particle size d50 of the MO3 particles is 0.5–2.0 µm, the maximum particle size d100 of the MO3 particles is ≤ 20 µm, and the quotient of the average MO3 concentration in wt.% in a volume element of approximately 0.05 to 1.0 cm3 (cVE) at any desired point in the propellant charge case and the total MO3 concentration in wt.% (ctot) in the propellant charge case is cVE:ctot = 0.80–0 1.20.

The invention discloses a smokeless and odorless firework oxidant which is prepared from the following components: zirconium dioxide, hafnium dioxide, silicon dioxide, manganese dioxide, iron oxide, arsenic trioxide and calcium oxide. Wherein the weight ratio of zirconium dioxide is not less than 90%; all the components are mixed, calcined and then subjected to wet ball milling, and a powdery material is obtained. The firework oxidizing agent is suitable for firework firework compositions, can be widely applied to firework spraying compositions and launching compositions, and is smokeless and odorless during combustion; the firework oxidant is not easy to decompose, good in stability, zero in friction sensitivity and impact sensitivity and suitable for high-automation-degree production, and the safety risk of production and transportation is greatly reduced.

A Combustion igniter cord with enhanced power. Combustion igniter cord for a propellant charge contained in the case of a cartridge, said igniter cord consisting of a core comprising a pyrotechnic material and surrounded by a sheath. The sheath consists of two concentric cylindrical tubes between which is arranged a free powder energetic material. Both tubes are made of an inert polymer material or contain an extruded energetic propellant powder material or one tube may be made of an inert polymer material and the other may contain an extruded energetic propellant powder material.

To provide a propellant composition that does not use nitroglycerin, which is difficult to handle safely, and that has a combustion temperature and low pressure index suitable for the application. [Solution] A propellant composition characterized by containing the following components: (a) nitrocellulose (NC): 15% by mass or more; (b) cyclotrimethylenetrinitramine (RDX): 1% by mass or more and 45% by mass or less; (c) nitroguanidine (NQ): 15% by mass or more and 60% by mass or less; (d) energy plasticizer other than nitroglycerin: 5% by mass or more and less than 15% by mass; and (e) additive as an optional component: 5% by mass or less; and having Q = {mass% of component (b) + mass% of component (d)} ÷ {mass% of component (c)} of 0.1 or more and 3.0 or less, and satisfying the following conditions: (i) component (b) is 24% by mass or less, or (ii) component (b) is greater than 24% by mass and the sum of component (b) and component (c) is greater than 58% by mass.

Increased power combustion ignition cord Combustion ignition cord of a propellant charge contained in the case of a cartridge, said cord being constituted by a core comprising a pyrotechnic material and surrounded by a sheath, characterized in that the sheath is constituted by two concentric cylindrical tubes between which is arranged a loose powder energetic material. The two tubes are made of an inert polymer material or be based on an extruded propellant powder energetic material or one of the tubes may be made of an inert polymer material and the other be based on an extruded propellant powder energetic material.

Ignition cord for combustion of a propellant charge contained in the case of a cartridge, said cord being constituted by a core comprising a pyrotechnic material and surrounded by a sheath, in which the sheath is constituted by two concentric cylindrical tubes between which is arranged an energetic material in loose powder, characterized in that one of the two tubes is based on an energetic material in propellant powder extruded in a block and that the other of the two tubes is based on an energetic material in propellant powder extruded in a block or made of an inert polymer material.

A combustible propellant charge sleeve for ammunition which can be fired from an armor barrel includes pulp, nitrocellulose, MO3 particles, wherein M=Mo and / or W, and cationic surfactant, wherein the average particle size d50 of the MO3 particles is 0.5-2.0 μm, the maximum particle size d100 of the MO3 particles is ≤20 μm, and the quotient of the average MO3 concentration in % by weight in a volume element of about 0.05 to 1.0 cm3 (CVE) at any point in the propellant charge sleeve and the total MO3 concentration in % by weight (Ctotal) in the propellant charge sleeve is CVE:Ctotal =0.80-1.20.

The present invention relates to a method for obtaining a highly flammable combustible textile structure which comprises: a) producing a nitrocellulose collodion, b) manufacturing at least one nitrocellulose filament by extrusion by spinning the collodion produced in step a), with passage of the at least one nitrocellulose filament in and through at least one nitrocellulose coagulation bath, c) sizing the at least one nitrocellulose filament obtained in step b) by passage in and through an aqueous solution containing a sizing agent, d) spinning and drying the at least sized nitrocellulose filament obtained in step c), and winding it, e) manufacturing a textile forming a textile structure by knitting, weaving or braiding with at least one sized nitrocellulose filament obtained in step d),f) the chemical treatment of the textile structure obtained in step e) for the desizing of at least one sized nitrocellulose filament composing it, then its drying. Figure 1.,

Enhanced combustion ignition cord: An ignition cord for the combustion of a propellant charge contained within a cartridge case, said cord consisting of a core comprising a pyrotechnical material and surrounded by a sheath, characterized in that the sheath consists of two concentric cylindrical tubes between which is arranged a free-flowing powdered energy material. The two tubes are made of an inert polymer material or are based on an extruded powdered energy material, or alternatively, one of the tubes may be made of an inert polymer material and the other of an extruded powdered energy material.

An ignition propellant loading cylinder for ammunition that can be fired from an armored gun barrel, comprising pulp, nitrocellulose, MO3 particles (where M = Mo and / or W), and a cationic surfactant, where the average particle size d 50 of the MO3 particles is 0.5 to 2.0 μm, and the maximum particle size d 100 of the MO3 particles is ≦ 20 μm, and the average MO3 concentration (c 3 )(wt%) in a volume element of about 0.05 to 1.0 cm VE at any location in the propellant loading cylinder and the total MO3 concentration (c total )(wt%) in the propellant loading cylinder, the quotient c VE :c total is 0.80 to 1.20, an ignition propellant loading cylinder is provided.

The invention belongs to the technical field of nitrocotton preparation, and particularly relates to ultrahigh-nitrogen nitrocotton and a preparation method thereof. In order to further improve the nitration degree of B-grade nitrocotton, the invention provides a preparation method of nitrocotton with ultrahigh nitrogen content, which comprises the following steps: carrying out esterification reaction on defibered flocculent cotton and mixed acid in a mass ratio of 1: (40-60) at 15-19 DEG C for 36-45 minutes, wherein the mixed acid contains 26-35 wt% of nitric acid, 5.0-8.0 wt% of water, 0.5-0.8 wt% of nitric oxide and the balance of sulfuric acid. According to the method, the mixed acid formula in the esterification reaction is improved, and the liquid-solid ratio, the reaction temperature and the reaction time are improved, so that the nitrification degree of the B-grade nitrocotton is obviously improved, and the nitrification degree is 216.5-218 mL / g. The improvement of the nitration degree of the B-grade nitrocotton is a favorable support for improving the product energy and further improving the capacities of propellant powder, propellants and the like.

Combustible propellant case for ammunition fired from a gun barrel, comprising - pulp, - Nitrocellulose, - 5 - 10 wt.% MO3 particles, based on the total weight of the propellant case, where M = Mo and / or W, and - 0.01 - 2 wt.% cationic surfactant, based on the total weight of the propellant case, wherein the average particle size d 50 the MO3 particles are 0.5 - 2.0 µm, the maximum particle size d 100 the MO3 particles are ≤ 15 µm, and the quotient of the average MO3 concentration in wt.% in a volume element of about 0.05 to 1.0 cm 3 (c VE ) at any point in the propellant case and the total MO3 concentration in wt.% (c] ges ) in the propellant case c VE : c ges = 0.80 - 1.20.