CN110330398A - A kind of reducing agent of propellant powder - Google Patents

A kind of reducing agent of propellant powder Download PDF

Info

Publication number
CN110330398A
CN110330398A CN201910633331.1A CN201910633331A CN110330398A CN 110330398 A CN110330398 A CN 110330398A CN 201910633331 A CN201910633331 A CN 201910633331A CN 110330398 A CN110330398 A CN 110330398A
Authority
CN
China
Prior art keywords
reducing agent
parts
weight
propellant powder
powder
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201910633331.1A
Other languages
Chinese (zh)
Inventor
郭辉
宋牛
钟纯文
晏红亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Liuyang Kaida Industrial Co Ltd
Original Assignee
Liuyang Kaida Industrial Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Liuyang Kaida Industrial Co Ltd filed Critical Liuyang Kaida Industrial Co Ltd
Priority to CN201910633331.1A priority Critical patent/CN110330398A/en
Publication of CN110330398A publication Critical patent/CN110330398A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B43/00Compositions characterised by explosive or thermic constituents not provided for in groups C06B25/00 - C06B41/00
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A50/00TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE in human health protection, e.g. against extreme weather
    • Y02A50/20Air quality improvement or preservation, e.g. vehicle emission control or emission reduction by using catalytic converters

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Adhesives Or Adhesive Processes (AREA)

Abstract

The invention discloses a kind of reducing agents of propellant powder, including adhesive 8-12 parts by weight;Reducing agent 9.6-14.4 parts by weight;Conductive reducing agent 6.4-9.6 parts by weight;Bond reducing agent 2.4-3.6 parts by weight;Catalyst 2.4-3.6 parts by weight;Stabilizer 0.4-0.6 parts by weight.Sulphur or sulfide are not present in mixture of the invention, while not using nitrocotton, to greatly reduce cost while substantially reducing to air pollution.

Description

A kind of reducing agent of propellant powder
Technical field
The invention belongs to a kind of fireworks powder field more particularly to a kind of reducing agents of propellant powder.
Background technique
Existing propellant powder usually contains the substances such as sulphur, the pollutants such as sulfur dioxide can be generated after burning, thus people The reducing agent in addition to a kind of propellant powder is developed, if patent 201810922401.0 has disclosed a kind of propellant powder and preparation method, The propellant powder is composed of the following components: 30-50 parts of potassium permanganate, 8-20 parts of adhesive, 10-20 parts of Potassium Hydrogen Phthalate and can Agent 20-40 parts of combustion;Wherein, the fuel agent is the mixture of nitrocotton and charcoal powder.The propellant powder, friction sensitivity and shock sense Spend that low, hydroscopicity is small, thrust by force while reducing pollution to environment.But it wherein must often mix nitrocotton or inflammable Height fires warm metal (aluminium, magnesium) and rare earth powder, to guarantee in formula, the temperature of powder burning and fires what reaction under environment was filled Adequacy.Since the requirement of propellant powder is high, nitrocotton must be the nitrocotton of technical grade, and price is higher, therefore propellant powder Prime cost concentrates on nitrocotton, and furthermore nitrocotton, which also has, easily decomposes naturally, than relatively hazardous.
The oxidant of propellant powder is frequent species, such as potassium permanganate, potassium hyperchlorate at present, therefore people's replacement The predominantly reducing agent of propellant powder, reducing agent also determine the quality of propellant powder.
Summary of the invention
The object of the present invention is to design a kind of reducing agent of novel propellant powder, sulphur is not present in mixture of the invention Or sulfide, and propellant powder can be made not use nitrocotton or the warm metal (aluminium, magnesium) of inflammable high combustion and rare earth metal powder End, to greatly reduce cost while substantially reducing to air pollution.
In order to achieve the above object, technical scheme is as follows:
A kind of reducing agent of propellant powder, including adhesive 8-12 parts by weight;Reducing agent 9.6-14.4 parts by weight;Conduction reduction Agent 6.4-9.6 parts by weight;Bond reducing agent 2.4-3.6 parts by weight;Catalyst 2.4-3.6 parts by weight;Stabilizer 0.4-0.6 weight Part.
It is further to improve, including 10 parts by weight of adhesive;12 parts by weight of reducing agent;Conductive 8 parts by weight of reducing agent;Bonding 3 parts by weight of reducing agent;3 parts by weight of catalyst;0.5 parts by weight of stabilizer.
Further to improve, described adhesive is phenolic resin.
Further to improve, the reducing agent is carbon dust.
Further to improve, the conduction reducing agent is graphite powder.
Further to improve, the bonding reducing agent is starch.
Further to improve, the catalyst is ferrocene.
Further to improve, the stabilizer is calcium stearate.
Detailed description of the invention
Fig. 1 is the examining report figure one at national fireworks and firecrackers product quality supervision and inspection center;
The examining report figure two at Fig. 2 country fireworks and firecrackers product quality supervision and inspection center.
Specific embodiment
Embodiment 1
A kind of reducing agent of propellant powder, including 10g phenolic resin;12g carbon dust;8g graphite powder;3g starch;3g ferrocene; 0.5g calcium stearate is mixed to prepare propellant powder.Hair is mixed to prepare with the oxidant (potassium hyperchlorate) of 70g after above-mentioned material mixing Penetrate medicine.
Wherein graphite powder is used as conductive agent and hydrophobing agent when not emitting, and the electrostatic in propellant powder is exported, is prevented Danger is used as reducing agent in transmitting, accelerates chemical reaction.Ferrocene is used as catalyst, is catalyzed after propellant powder is lighted Reaction, thus in the propellant powder for being compound reaction more rapidly and completely so that launching effect is more preferable, cigarette (carbon and the gold of generation Belong to oxide) it is less.Ferrocene is stable in the air, to heat it is quite stable, relative to metal powder material have it is easy to maintain, no Oxidizable advantage.The effect of propellant powder can be achieved in above-mentioned each material in ± 20% ratio of said ratio.
Examining report data of the above-mentioned propellant powder at national fireworks and firecrackers product quality supervision and inspection center are as follows:
Wherein oxidant may be replaced by potassium permanganate.
Above-described embodiment is only the specific embodiment of the present invention, not as a limitation of the invention.

Claims (8)

1. a kind of reducing agent of propellant powder, which is characterized in that including adhesive 8-12 parts by weight;Reducing agent 9.6-14.4 weight Part;Conductive reducing agent 6.4-9.6 parts by weight;Bond reducing agent 2.4-3.6 parts by weight;Catalyst 2.4-3.6 parts by weight;Stabilizer 0.4-0.6 parts by weight.
2. the reducing agent of propellant powder as described in claim 1, which is characterized in that including 10 parts by weight of adhesive;Reducing agent 12 Parts by weight;Conductive 8 parts by weight of reducing agent;Bond 3 parts by weight of reducing agent;3 parts by weight of catalyst;0.5 parts by weight of stabilizer.
3. the reducing agent of propellant powder as claimed in claim 1 or 2, which is characterized in that described adhesive is phenolic resin.
4. the reducing agent of propellant powder as claimed in claim 1 or 2, which is characterized in that the reducing agent is carbon dust.
5. the reducing agent of propellant powder as claimed in claim 1 or 2, which is characterized in that the conduction reducing agent is graphite powder.
6. the reducing agent of propellant powder as claimed in claim 1 or 2, which is characterized in that the bonding reducing agent is starch.
7. the reducing agent of propellant powder as claimed in claim 1 or 2, which is characterized in that the catalyst is ferrocene.
8. the reducing agent of propellant powder as claimed in claim 1 or 2, which is characterized in that the stabilizer is calcium stearate.
CN201910633331.1A 2019-07-15 2019-07-15 A kind of reducing agent of propellant powder Pending CN110330398A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910633331.1A CN110330398A (en) 2019-07-15 2019-07-15 A kind of reducing agent of propellant powder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910633331.1A CN110330398A (en) 2019-07-15 2019-07-15 A kind of reducing agent of propellant powder

Publications (1)

Publication Number Publication Date
CN110330398A true CN110330398A (en) 2019-10-15

Family

ID=68145062

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910633331.1A Pending CN110330398A (en) 2019-07-15 2019-07-15 A kind of reducing agent of propellant powder

Country Status (1)

Country Link
CN (1) CN110330398A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2031898C1 (en) * 1992-06-22 1995-03-27 Товарищество с ограниченной ответственностью "Абрис" Pyrotechnical composition for bengal candle
CN102531811A (en) * 2012-01-18 2012-07-04 肖永富 Cast charge and application thereof to production of firework propellant
CN102924193A (en) * 2012-10-15 2013-02-13 周健 Smokeless propellant powder with safe, environmental-friendly and porous structure for fireworks
CN104557352A (en) * 2015-01-05 2015-04-29 浏阳市诚发科技有限公司 Sulfur-free environment-friendly gun propellant
CN105016933A (en) * 2015-07-15 2015-11-04 江西省东安新材料有限公司 Sulfur-free propellant powder

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2031898C1 (en) * 1992-06-22 1995-03-27 Товарищество с ограниченной ответственностью "Абрис" Pyrotechnical composition for bengal candle
CN102531811A (en) * 2012-01-18 2012-07-04 肖永富 Cast charge and application thereof to production of firework propellant
CN102924193A (en) * 2012-10-15 2013-02-13 周健 Smokeless propellant powder with safe, environmental-friendly and porous structure for fireworks
CN104557352A (en) * 2015-01-05 2015-04-29 浏阳市诚发科技有限公司 Sulfur-free environment-friendly gun propellant
CN105016933A (en) * 2015-07-15 2015-11-04 江西省东安新材料有限公司 Sulfur-free propellant powder

Similar Documents

Publication Publication Date Title
CN106397075A (en) Safe blasting-fuse composition for firecracker
CN102219622A (en) Smokeless propellant for fireworks
CN103626612A (en) Environment-friendly sulfur-free propellant formula
CN110734353A (en) gas generating agent for gas type superfine dry powder fire extinguishing system and preparation method thereof
US3293187A (en) Oxygen-generating product
US20070068610A1 (en) Microcrystalline Nitrocellulose Pyrotechnic Compositions
CN110330398A (en) A kind of reducing agent of propellant powder
CN110330397A (en) A kind of propellant powder
CN104591933B (en) Modified carbon powder for preparing sulfur-free micro-smoke environment-friendly propellant
CN101265146B (en) Environment-friendly type safety fireworks firecracker gun powder oxidant
US4417900A (en) High temperature solid fire starter
CN106316724A (en) Safe and environmentally-friendly firework propellant powder
US2530491A (en) Incendiary composition
JP4719528B2 (en) Ignition agent, ignition device, and signal illumination bullet firing device
US907007A (en) Safety-explosive.
KR860001093B1 (en) Solid fuel
RO123536B1 (en) Pyrotechnic composition
RU2541025C2 (en) Pyrotechnic composition of black smoke
CN109206289A (en) Application of the bamboo charcoal fiber cotton in firework launching medicine
CN109721446A (en) A kind of micro- pyrotechnic composition complex composition and its application
CN108947750A (en) A kind of micro-smoke firework medicament composition
RU2571753C1 (en) Ice-forming propellant
Jackson et al. Substitution of Aluminum for Magnesium as a Fuel in Flares
SU1445739A1 (en) Gas-generating composition for pushing out the fire-extinguishing means
RU2722031C1 (en) Red fire pyrotechnic composition

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20191015

RJ01 Rejection of invention patent application after publication