CN206330494U - Electrical fuze firing energy test device - Google Patents
Electrical fuze firing energy test device Download PDFInfo
- Publication number
- CN206330494U CN206330494U CN201621274100.4U CN201621274100U CN206330494U CN 206330494 U CN206330494 U CN 206330494U CN 201621274100 U CN201621274100 U CN 201621274100U CN 206330494 U CN206330494 U CN 206330494U
- Authority
- CN
- China
- Prior art keywords
- ignition
- energy
- flyer
- powder
- electric
- 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.)
- Expired - Fee Related
Links
- 238000012360 testing method Methods 0.000 title claims abstract description 75
- 238000010304 firing Methods 0.000 title claims description 6
- 239000011521 glass Substances 0.000 claims 1
- 239000000843 powder Substances 0.000 abstract description 63
- 238000000034 method Methods 0.000 abstract description 21
- 230000008569 process Effects 0.000 abstract description 18
- 230000008859 change Effects 0.000 abstract description 12
- 238000012545 processing Methods 0.000 abstract description 7
- 238000005259 measurement Methods 0.000 abstract description 6
- 238000006243 chemical reaction Methods 0.000 abstract description 4
- 238000009529 body temperature measurement Methods 0.000 abstract 1
- 230000009466 transformation Effects 0.000 abstract 1
- 239000003292 glue Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- NAWXUBYGYWOOIX-SFHVURJKSA-N (2s)-2-[[4-[2-(2,4-diaminoquinazolin-6-yl)ethyl]benzoyl]amino]-4-methylidenepentanedioic acid Chemical compound C1=CC2=NC(N)=NC(N)=C2C=C1CCC1=CC=C(C(=O)N[C@@H](CC(=C)C(O)=O)C(O)=O)C=C1 NAWXUBYGYWOOIX-SFHVURJKSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000009795 derivation Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000605 extraction Methods 0.000 description 2
- 238000013100 final test Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 239000010453 quartz Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000010998 test method Methods 0.000 description 2
- 238000005314 correlation function Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
Landscapes
- Investigating Or Analyzing Materials Using Thermal Means (AREA)
Abstract
本实用新型提供的电引火药头发火能量测试装置,包括:测试管、飞片、固定塞、真空箱、高速摄像机、记录装置、真空泵、数据处理系统和测温装置。利用转化思想将电引火药头发火能量转化为飞片所受能量,真空条件下拍摄电引火药头发火过程中飞片在测试管中的运动轨迹,简化成物理模型,利用数学手段处理飞片运动模型的相关数据,求解飞片的动能,即电引火药头发火能量转化为动能的部分;测温装置测量测试管在电引火药头发火时的温度变化,求解电引火药头发火能量转化为热能的部分;动能与热能之和即为所测电引火药头发火能量。本实用新型解决了电引火药头发火能量动态测量的难题,有可靠的理论依据,操作方便,测量结果精确。
The utility model provides an ignition energy testing device for electric igniting powder, comprising: a test tube, a flying piece, a fixed plug, a vacuum box, a high-speed camera, a recording device, a vacuum pump, a data processing system and a temperature measuring device. Using transformation ideas to convert the ignition energy of the electric igniter powder into the energy received by the flyer, photograph the trajectory of the flyer in the test tube during the ignition of the electric igniter powder under vacuum conditions, simplify it into a physical model, and use mathematical means to process the flyer The relevant data of the motion model is used to solve the kinetic energy of the flying piece, that is, the part where the ignition energy of the electric ignition powder is converted into kinetic energy; the temperature measurement device measures the temperature change of the test tube when the electric ignition powder is fired, and the conversion of the ignition energy of the electric ignition powder is solved The part of thermal energy; the sum of kinetic energy and thermal energy is the ignition energy of the measured electric ignition powder. The utility model solves the difficult problem of dynamic measurement of the ignition energy of the electric ignition powder, has a reliable theoretical basis, is convenient to operate, and has accurate measurement results.
Description
技术领域technical field
本实用新型涉及火工品测试技术,特别涉及电引火药头发火能量的测试。The utility model relates to the testing technology of pyrotechnics, in particular to the testing of the ignition energy of electric ignition powder.
背景技术Background technique
常用的延期电雷管,其延期药的点火方式为电引火药头受热燃烧点火。目前,我国常用的电引火药头多为桥丝式、钢片式,在其上涂有一定量的点火药,通电后桥丝或钢片升温引燃点火药,为延期药提供起始能量。电引火药头产生的发火能量会使延期药的点火时间和燃烧速度不同,从而影响延期电雷管的延期精度。所以对电引火药头发火能量的测试还是尤为重要的。Commonly used delay electric detonators, the ignition mode of its delay charge is that the electric ignition charge head is heated and burned to ignite. At present, most of the electric ignition powder heads commonly used in my country are bridge wire type and steel sheet type, and a certain amount of ignition powder is coated on it. After the electricity is turned on, the bridge wire or steel sheet heats up to ignite the ignition powder, providing initial energy for the delay charge. The ignition energy produced by the electric ignition charge will make the ignition time and burning speed of the delay charge different, thereby affecting the delay accuracy of the delay electric detonator. So it is still particularly important to test the ignition energy of the electric ignition powder.
实用新型内容Utility model content
本实用新型提供的电引火药头发火能量测试装置,能够精确测量出电引火药头发火能量及其动态变化,可作为评估电引火药头性能和测量电引火药头发火能量对延期药延期精度影响的一种测试手段,为提高延期电雷管精度提供理论指导。The ignition energy testing device of the electric ignition powder provided by the utility model can accurately measure the ignition energy of the electric ignition powder and its dynamic change, and can be used as an evaluation of the performance of the electric ignition powder and a measurement of the impact of the ignition energy of the electric ignition powder on the delay accuracy of the delay medicine. It is a test method of the impact, and provides theoretical guidance for improving the accuracy of the delay electric detonator.
本实用新型采用的技术方案是:电引火药头发火能量一部分转化为周围物体的动能,一部分转化为热能,使与之接触的物体升温;则在真空条件下,设计一个与电引火药头接触的飞片,利用高速摄像机拍摄电引火药头发火过程中飞片在测试管中的运动轨迹,简化成物理模型,利用数学手段处理飞片运动模型的相关数据,求解飞片的动能,即电引火药头发火能量转化为动能的部分;测温装置测量测试管在电引火药头发火过程的温度变化,求解电引火药头发火能量转化为热能的部分;动能与热能之和即为所测电引火药头发火能量。The technical scheme adopted in the utility model is: a part of the ignition energy of the electric ignition powder is converted into the kinetic energy of the surrounding objects, and a part is converted into heat energy, so that the objects in contact with it are heated up; Using a high-speed camera to capture the trajectory of the flyer in the test tube during the ignition of the electric igniter, simplify it into a physical model, use mathematical means to process the relevant data of the flyer motion model, and solve the kinetic energy of the flyer, that is, the electric The part where the ignition energy of the ignition powder is converted into kinetic energy; the temperature measuring device measures the temperature change of the test tube during the ignition process of the electric ignition powder, and calculates the part where the ignition energy of the electric ignition powder is converted into heat energy; the sum of kinetic energy and heat energy is the measured Electric pyrotechnic powder emits ignition energy.
其理论推导为:Its theoretical derivation is:
电引火药头发火能量转化为动能的部分,包括转动动能和平动动能:飞片为质量m,半径R、厚h的均质刚性圆片,测试过程中受到冲击,飞片在测试管中一边以飞片中心旋转,一边向前运动。将该过程分解成定轴旋转运动和沿测试管平动两个过程,求解飞片的动能,即电引火药头发火能量转化为动能的部分。The part where the ignition energy of the electric ignition powder is converted into kinetic energy, including rotational kinetic energy and translational kinetic energy: the flyer is a homogeneous rigid disc with mass m, radius R, and thickness h. It is impacted during the test, and the flyer is on one side of the test tube. Rotate around the center of the fly piece while moving forward. The process is decomposed into two processes of fixed-axis rotation and translation along the test tube, and the kinetic energy of the flyer is solved, that is, the part where the ignition energy of the electric ignition powder is converted into kinetic energy.
对飞片定轴旋转过程:The process of rotating the flyer with fixed axis:
将飞片看成由若干薄圆环组成,取任一半径r、宽度dr、质量为dm的薄圆环,此薄圆环的转动惯量dJ为:Consider the flyer as composed of several thin rings, take any thin ring with radius r, width dr, and mass dm, the moment of inertia dJ of this thin ring is:
dJ=r2dm (1)dJ=r 2 dm (1)
其中in
dm=ρdV=ρ·2πrhdr (2)dm=ρdV=ρ·2πrhdr (2)
ρ为飞片密度,dV为薄圆环的体积;将式(2)代入式(1),整理得:ρ is the flyer density, and dV is the volume of the thin ring; substituting formula (2) into formula (1), we can get:
dJ=2πr3hρdr (3)dJ=2πr 3 hρdr (3)
将式(3)在飞片半径范围内进行积分,求解飞片绕中心轴转动惯量J:Integrate formula (3) within the radius of the flyer to solve the moment of inertia J of the flyer around the central axis:
将式(5)代入式(4)得:Substitute formula (5) into formula (4):
由式(6)可知:J与h无关,即飞片绕中心轴线旋转的转动惯量与其厚度无关;It can be known from formula (6): J has nothing to do with h, that is, the moment of inertia of the flyer rotating around the central axis has nothing to do with its thickness;
飞片转动动能:Flyer rotational kinetic energy:
式中,ER为飞片转动动能,ω为飞片转动角速度;In the formula, E R is the rotational kinetic energy of the flyer, ω is the rotational angular velocity of the flyer;
ω的求解方法:高速摄像机拍摄侧面设有刻线的飞片在测试管内的转动轨迹,采集飞片转动角度与所对应的时间,利用数据处理系统拟合飞片转动角度α与时间T的函数关系,其多项式方程:The solution method of ω: the high-speed camera shoots the rotation trajectory of the flyer with the engraved line on the side in the test tube, collects the rotation angle of the flyer and the corresponding time, and uses the data processing system to fit the function of the flyer rotation angle α and time T relation, its polynomial equation:
α=A0+A1T1+A2T2+A3T3+A4T4+…AnTn (8)α=A 0 +A 1 T 1 +A 2 T 2 +A 3 T 3 +A 4 T 4 +...A n T n (8)
式(8)中,A0…An为待定系数;式(8)对时间T求导,得飞片绕中心轴线转动角速度ω与时间T的函数关系:In the formula (8), A 0 ... A n are undetermined coefficients; the formula (8) is derived from the time T, and the functional relationship between the rotational angular velocity ω of the flying piece around the central axis and the time T is obtained:
通过式(9),求解任意时刻飞片绕中心轴线旋转的瞬时角速度ω;Through formula (9), the instantaneous angular velocity ω of the flyer rotating around the central axis at any time is solved;
将式(6)、(9)代入式(7)得:Substituting equations (6) and (9) into equation (7), we get:
通过式(10),求解出飞片绕圆心轴线旋转的转动动能及其动态变化。Through formula (10), the rotational kinetic energy and dynamic change of the flyer rotating around the center axis of the circle are solved.
对飞片沿测试管平动过程:The translational process of the flyer along the test tube:
高速摄像机拍摄测试管内飞片平动轨迹,采集飞片平动距离与所对应的时刻,利用数据处理系统拟合飞片平动距离D与时间T的关系,其多项式方程:The high-speed camera shoots the translational trajectory of the flyer in the test tube, collects the translational distance of the flyer and the corresponding moment, and uses the data processing system to fit the relationship between the translational distance D and the time T of the flyer. The polynomial equation:
D=B0+B1T1+B2T2+B3T3+B4T4+…BnTn (11)D=B 0 +B 1 T 1 +B 2 T 2 +B 3 T 3 +B 4 T 4 +...B n T n (11)
式(11)中:B0…Bn为待定系数,式(11)对时间T求导,得飞片平动速度v与时间T的多项式方程:In the formula (11): B 0 ... B n are undetermined coefficients, and the formula (11) is derived from the time T, and the polynomial equation of the flying piece translational velocity v and time T is obtained:
由动能定理:By the kinetic energy theorem:
将式(12)带入式(13):Bring formula (12) into formula (13):
由式(14)求解飞片平动动能EL及其动态变化;Solve the translational kinetic energy E L of the flying piece and its dynamic change by formula (14);
电引火药头发火能量转化为热能的部分,使测试管升温:设测试管比热容为C、质量为M,室温为t0,用测温装置测量测试管在电引火药头发火过程温度值t的动态变化:The part where the ignition energy of the electric ignition powder is converted into heat energy makes the test tube heat up: assuming that the specific heat capacity of the test tube is C, the mass is M, and the room temperature is t 0 , use a temperature measuring device to measure the temperature value t of the test tube during the ignition process of the electric ignition powder The dynamic changes of:
t=C0+C1T1+C2T2+C3T3+C4T4+…CnTn (15)t=C 0 +C 1 T 1 +C 2 T 2 +C 3 T 3 +C 4 T 4 +...C n T n (15)
测试过程,测试管温度t与室温之间的温度差Δt随时间的变化为:During the test, the temperature difference Δt between the test tube temperature t and the room temperature varies with time as:
Δt=t-t0=C0+C1T1+C2T2+C3T3+C4T4+…CnTn-t0 (16)Δt=tt 0 =C 0 +C 1 T 1 +C 2 T 2 +C 3 T 3 +C 4 T 4 +...C n T n -t 0 (16)
则转化为热能的能量Q为:Then the energy Q converted into heat energy is:
Q=C·M·Δt=C·M·(C0+C1T1+C2T2+C3T3+C4T4+…CnTn-t0) (17)Q=C·M·Δt=C·M·(C 0 +C 1 T 1 +C 2 T 2 +C 3 T 3 +C 4 T 4 +...C n T n -t 0 ) (17)
电引火药头发火能量E为:The ignition energy E of the electric ignition powder is:
E=ER+EL+Q (18)E=E R +E L +Q (18)
根据式(8)先拟合出飞片绕圆心轴线旋转的角度α与时间T的函数关系,式(9)求解飞片转动角速度ω与时间T的函数关系,结合式(9)、(10)及飞片质量m、飞片半径R,求解飞片转动动能ER及其动态变化。再由式(11)拟合出飞片平动距离D与时间T的函数关系,由式(12)求解飞片平动速度v与时间T的函数关系,结合式(12)、(14)及飞片质量m,求解飞片平动动能EL及其动态变化。式(15)、(16)、(17)结合测试管比热容C、测试管质量M、室温t0,求解电引火药头发火能量转化为热能的部分及其动态变化;根据式(10)、(14)、(17)及(18),求解电引火药头发火能量E及其动态变化。According to the formula (8), first fit the functional relationship between the angle α of the rotation of the flying piece around the axis of the circle and the time T, and the formula (9) solves the functional relationship between the rotational angular velocity ω of the flying piece and the time T, and combines the formulas (9), (10 ) and flyer mass m, flyer radius R, to solve flyer rotational kinetic energy E R and its dynamic changes. Then fit the functional relationship between the translational distance D and time T of the flying piece by formula (11), solve the functional relationship between the translational velocity v and time T of the flying piece by formula (12), combine formulas (12), (14) and the flying piece The mass m of the flying piece is used to solve the translational kinetic energy E L of the flying piece and its dynamic change. Formulas (15), (16), and (17) combine the specific heat capacity C of the test tube, the mass M of the test tube, and the room temperature t 0 to solve the part of the conversion of the ignition energy of the electric ignition powder into heat energy and its dynamic change; according to the formula (10), (14), (17) and (18), solve the ignition energy E and its dynamic change of the electric ignition powder.
为了实现上述过程,本实用新型的装置设计包括:测试管、飞片、固定塞、真空箱、高速摄像机、记录装置、真空泵、数据处理系统和测温装置;所述测试管为一根设有刻度线的中空透明刚性管体;所述飞片为一轻质刚性圆片结构,其直径略小于测试管内径,飞片侧面设刻线;所述固定塞为圆柱体结构,外径与测试管内径契合,其中轴设孔,孔径与电引火药头上塑料塞的外径一致;所述真空箱为一长方体透明箱,其上设抽气孔、发爆器。In order to realize the above-mentioned process, the device design of the present utility model includes: test tube, flyer, fixed plug, vacuum box, high-speed camera, recording device, vacuum pump, data processing system and temperature measuring device; The hollow transparent rigid tube body of the scale line; the fly piece is a light rigid disc structure, its diameter is slightly smaller than the inner diameter of the test tube, and the side of the fly piece is provided with a score line; the fixed plug is a cylindrical structure, and the outer diameter is the same as the test tube. The inner diameter of the tube fits, and the shaft is provided with a hole, and the aperture is consistent with the outer diameter of the plastic plug on the electric ignition powder head; the vacuum box is a rectangular parallelepiped transparent box, and an air extraction hole and a detonator are arranged on it.
常用电引火药头发火时间为毫秒级,则高速摄像机拍摄频率至少为1000帧/秒。The ignition time of commonly used electric igniter powder is on the order of milliseconds, so the shooting frequency of the high-speed camera is at least 1000 frames per second.
测量所需为普通真空条件,普通实验用真空泵即可。The measurement requires ordinary vacuum conditions, and ordinary experimental vacuum pumps are sufficient.
测试时,先将电引火药头的脚线穿过固定塞的孔中,至电引火药头上塑料塞与固定塞的孔相契合,用胶水固定、密封;将固定有电引火药头的固定塞插入测试管一端,由固定塞固定、胶水密封。飞片由测试管另一端置入,将飞片推至与电引火药头相接触;将电引火药头的脚线密封连接至真空箱上的发爆器,将连接后的测试管水平置于真空箱内,密封真空箱;用真空泵经抽气孔将真空箱内抽至真空状态,密封抽气孔;高速摄像机、测温装置垂直于测试管轴线放置,高速摄像机、测温装置与记录装置连接。启动高速摄像机、测温装置和记录装置;发爆器充电后引燃电引火药头,飞片在测试管内旋转沿轴线向前运动,飞片停止后关闭高速摄像机,飞片运动过程和测试管温度值由记录装置记录。数据处理系统根据记录装置记录的飞片不同时刻所对应的测试管上刻度线的位置,以及不同时刻所对应的飞片侧面刻线,拟合出电引火药头发火过程飞片的运动状态函数,求解飞片的动能,即电引火药头发火能量转化为动能的部分;结合测温装置测得的测试管温度值,求解电引火药头发火能量转化为热能的部分;动能与热能之和,即为电引火药头发火能量。When testing, first pass the foot wire of the electric ignition powder through the hole of the fixing plug until the plastic plug on the electric ignition powder matches the hole of the fixing plug, fix and seal with glue; The fixing plug is inserted into one end of the test tube, fixed by the fixing plug and sealed with glue. Insert the fly piece from the other end of the test tube, push the fly piece to contact with the electric igniter head; connect the foot wire of the electric igniter head to the detonator on the vacuum box, and place the connected test tube horizontally In the vacuum box, seal the vacuum box; use a vacuum pump to pump the vacuum box to a vacuum state through the pumping hole, and seal the pumping hole; place the high-speed camera and the temperature measuring device perpendicular to the axis of the test tube, and connect the high-speed camera and the temperature measuring device to the recording device . Start the high-speed camera, temperature measuring device and recording device; the detonator ignites the electric ignition charge after charging, the flyer rotates in the test tube and moves forward along the axis, and the high-speed camera is turned off after the flyer stops, the movement process of the flyer and the test tube The temperature value is recorded by a recording device. The data processing system fits the motion state function of the flyer during the firing process of the electric ignition powder according to the position of the scale line on the test tube corresponding to the flyer recorded by the recording device at different times, and the corresponding score line on the side of the flyer at different times , to solve the kinetic energy of the flying piece, that is, the part where the ignition energy of the electric ignition powder is converted into kinetic energy; combined with the temperature value of the test tube measured by the temperature measuring device, to solve the part where the ignition energy of the electric ignition powder is converted into heat energy; the sum of kinetic energy and heat energy , which is the ignition energy of the electric igniter.
本实用新型提供的电引火药头发火能量测试装置,涉及的测试管为一根中空的刚性透明管,便于高速摄像机拍摄飞片的运动轨迹,测试管上刻度线是为了准确定位飞片的平动距离,拟合飞片平动的相关函数。飞片整体为轻质刚性圆片结构,其直径略小于测试管内径,便于飞片在测试管内的运动,又使在抽真空过程中,飞片两侧的气压与真空箱内的气压保持一致,从而保证抽真空过程中不会因为内外气压差导致的飞片移动;由于该缝隙很小,电引火药头发火过程为毫秒级,点火药化学反应快、产气速率快,气体快速向抵抗力小的飞片端膨胀,极少量的气体从飞片与测试管之间的狭小缝隙流向真空箱,其对飞片运动状态和最终测试结果的影响很小,可忽略不计;飞片具有一定的厚度,能很好的固定飞片运动过程中在测试管内的角度;飞片侧面设刻线,便于高速摄像机拍摄飞片的旋转运动轨迹,拟合飞片转动的相关运动函数;圆片型结构减轻了飞片的质量,减少飞片与测试管的摩擦,质量轻、摩擦小,利于飞片的运动,飞片平动距离变长,相当于扩大实验现象,拟合的飞片平动函数更为精确,使得测试结果更为准确。固定塞中轴设孔,可将电引火药头固定于测试管一端。所述真空箱透明,便于高速摄像机拍摄;抽气孔的设置,便于真空泵将真空箱内抽真空,防止大气压对飞片运动产生影响,导致测试结果误差过大。The utility model provides an ignition energy testing device for electric igniting powder. The test tube involved is a hollow rigid transparent tube, which is convenient for a high-speed camera to take pictures of the trajectory of the flying piece. The moving distance is used to fit the correlation function of the translational motion of the flyer. The flyer as a whole is a lightweight rigid disc structure, its diameter is slightly smaller than the inner diameter of the test tube, which facilitates the movement of the flyer in the test tube, and makes the air pressure on both sides of the flyer consistent with the air pressure in the vacuum box during the vacuuming process , so as to ensure that the flying piece will not move due to the difference in internal and external air pressure during the vacuuming process; because the gap is small, the ignition process of the electric ignition powder is milliseconds, the chemical reaction of the ignition powder is fast, the gas production rate is fast, and the gas quickly moves to the resistance The end of the flyer with small force expands, and a very small amount of gas flows from the narrow gap between the flyer and the test tube to the vacuum box, which has little influence on the motion state of the flyer and the final test result, which can be ignored; the flyer has a certain Thickness, which can well fix the angle of the flyer in the test tube during the movement process; the side of the flyer is provided with a scribe line, which is convenient for the high-speed camera to capture the rotation trajectory of the flyer, and fit the related motion function of the flyer rotation; the disc structure The weight of the flyer is reduced, and the friction between the flyer and the test tube is reduced. The weight is light and the friction is small, which is beneficial to the movement of the flyer. The translational distance of the flyer becomes longer, which is equivalent to expanding the experimental phenomenon. The fitted translational function of the flyer is more accurate. Accurate, making the test results more accurate. A hole is arranged on the central axis of the fixing plug, and the electric ignition charge head can be fixed on one end of the test tube. The vacuum box is transparent, which is convenient for high-speed camera shooting; the setting of the air extraction hole is convenient for the vacuum pump to evacuate the vacuum box, and prevents atmospheric pressure from affecting the movement of the flyer, resulting in excessive error in test results.
本实用新型提供的电引火药头发火能量测试装置的优点和积极效果在于:该测试方法及装置可通过测量飞片的运动状态,间接测量出电引火药头发火能量转化为动能的部分;通过测温装置测量的测试管温度变化,求解电引火药头发火能量转化为热能的部分;动能和热能总和即为所测电引火药头发火能量;可以此来评估电引火药头的性能和探究电引火药头发火能量对延期药延期精度的影响。本实用新型有可靠的理论依据,操作方便,测量结果精确,为实际生产提供一定的理论依据。The advantages and positive effects of the ignition energy testing device of the electric ignition powder provided by the utility model are: the test method and the device can indirectly measure the part where the ignition energy of the electric ignition powder is converted into kinetic energy by measuring the motion state of the flying piece; The temperature change of the test tube measured by the temperature measuring device is used to solve the part of the ignition energy of the electric ignition powder that is converted into heat energy; the sum of kinetic energy and thermal energy is the ignition energy of the measured electric ignition powder; this can be used to evaluate the performance of the electric ignition powder and explore Influence of the ignition energy of the electric ignition charge on the delay accuracy of the delay charge. The utility model has reliable theoretical basis, convenient operation and accurate measurement result, which provides certain theoretical basis for actual production.
下面结合实施例详细描述本实用新型提供的电引火药头发火能量测试装置的技术方案。The technical scheme of the ignition energy testing device for electric ignition powder provided by the utility model will be described in detail below in conjunction with the embodiments.
附图说明Description of drawings
图1是本实用新型电引火药头发火能量测试装置的测试管结构示意图;Fig. 1 is the test tube structure schematic diagram of the utility model electric ignition charge firing energy test device;
图2是本实用新型电引火药头发火能量测试装置的飞片结构示意图;Fig. 2 is the schematic diagram of the flyer structure of the utility model electric ignition charge firing energy testing device;
图3是本实用新型电引火药头发火能量测试装置飞片与测试管组合示意图;Fig. 3 is a schematic diagram of the combination of the flying piece and the test tube of the electric ignition charge ignition energy testing device of the utility model;
图4是本实用新型电引火药头发火能量测试装置部分结构示意图;Fig. 4 is a schematic diagram of the partial structure of the ignition energy testing device of the electric ignition charge of the utility model;
图5是本实用新型电引火药头发火能量测试装置原理图。Fig. 5 is a schematic diagram of the ignition energy testing device of the electric ignition powder of the utility model.
具体实施方式detailed description
高速摄像机选用NAC Memr ecam HX-3型彩色高速摄像机,拍摄频率为130万fps。The high-speed camera is NAC Memr ecam HX-3 color high-speed camera with a shooting frequency of 1.3 million fps.
真空泵选用藤原FUJIWARA型二级真空泵,真空度可达-98kpa。The vacuum pump adopts the Fujiwara FUJIWARA type two-stage vacuum pump, and the vacuum degree can reach -98kpa.
测试时,将电引火药头的脚线3穿过固定塞4的孔,至电引火药头上塑料塞与固定塞4的孔相契合,用胶水固定、密封;将固定有电引火药头的固定塞4插入测试管1一端,由固定塞4固定,胶水密封。飞片2由测试管1另一端置入,将飞片2推至与电引火药头相接触,将电引火药头的脚线3密封连接至真空箱6上的发爆器8;将连接后的测试管1水平置于真空箱6内,密封真空箱6;用真空泵经抽气孔7将真空箱6内部抽至真空状态,密封抽气孔7;将高速摄像机9、测温装置5垂直于测试管1轴线放置,记录装置10与高速摄像机9和测温装置5连接。启动高速摄像机9、测温装置5和记录装置10;发爆器8充电后引燃电引火药头,飞片2沿着测试管1轴线旋转向前运动;飞片2停止后关闭高速摄像机9,飞片2运动过程和测试管1的温度变化由记录装置10记录。During the test, pass the foot line 3 of the electric ignition powder through the hole of the fixed plug 4, until the plastic plug on the electric ignition powder matches the hole of the fixed plug 4, fix and seal with glue; The fixed plug 4 is inserted into one end of the test tube 1, fixed by the fixed plug 4, and sealed with glue. The flying piece 2 is inserted from the other end of the test tube 1, and the flying piece 2 is pushed to contact with the electric ignition powder, and the foot line 3 of the electric ignition powder is sealed and connected to the detonator 8 on the vacuum box 6; The final test tube 1 is horizontally placed in the vacuum box 6, and the vacuum box 6 is sealed; the inside of the vacuum box 6 is evacuated to a vacuum state through the air hole 7 with a vacuum pump, and the air hole 7 is sealed; the high-speed camera 9 and the temperature measuring device 5 are perpendicular to the The test tube 1 is placed on the axis, and the recording device 10 is connected with the high-speed camera 9 and the temperature measuring device 5 . Start the high-speed camera 9, the temperature measuring device 5 and the recording device 10; the detonator 8 ignites the electric ignition charge after charging, and the flyer 2 rotates forward along the axis of the test tube 1; the flyer 2 stops and then closes the high-speed camera 9 , the movement process of the flyer 2 and the temperature change of the test tube 1 are recorded by the recording device 10 .
数据处理系统根据记录装置10记录的飞片2不同时刻所对应的测试管1上刻度线的位置,以及不同时刻所对应的飞片2侧面刻线,拟合出电引火药头发火过程飞片2的运动状态函数,间接测量出电引火药头发火能量转化为动能的部分,通过测温装置5测量的测试管1的温度变化,求解电引火药头发火能量转化为热能的部分;动能和热能总和即为电引火药头发火能量。According to the position of the scale line on the test tube 1 corresponding to the different moments of the flyer 2 recorded by the recording device 10, and the corresponding marking lines on the side of the flyer 2 at different times, the data processing system fits the flyer during the firing process of the electric ignition powder. 2, the motion state function of 2 indirectly measures the part where the ignition energy of the electric ignition powder is converted into kinetic energy, and the temperature change of the test tube 1 measured by the temperature measuring device 5 solves the part where the ignition energy of the electric ignition powder is converted into heat energy; kinetic energy and The sum of the heat energy is the ignition energy of the electric ignition powder.
实施例一Embodiment one
参照图1,测试管1为一根长550mm,内径10mm,壁厚1.50mm的中空透明石英管,其上设有量程为550mm的刻度线,相邻刻度值为1mm。Referring to Figure 1, the test tube 1 is a hollow transparent quartz tube with a length of 550 mm, an inner diameter of 10 mm, and a wall thickness of 1.50 mm. There are scale lines with a measuring range of 550 mm on it, and adjacent scale values are 1 mm.
参照图2,飞片2为圆片结构,材质为彩色轻质高强度石英,直径9.96mm,厚1mm,其侧面等间距设360条刻线,相邻两条刻线对应圆心角为1°。彩色飞片使高速摄像机拍摄飞片运动状态更为清晰,利于测量精度的提高。Referring to Figure 2, the flyer 2 is a disc structure, made of colored lightweight high-strength quartz, with a diameter of 9.96mm and a thickness of 1mm. There are 360 engraved lines at equal intervals on its side, and the corresponding central angle of two adjacent engraved lines is 1°. . The color flyer makes the motion state of the flyer captured by the high-speed camera clearer, which is beneficial to the improvement of measurement accuracy.
参照图3,将飞片2置入测试管1。Referring to FIG. 3 , put the fly piece 2 into the test tube 1 .
参照图4,固定塞4外径10mm,其中轴设孔径8mm的孔,将桥丝式电引火药头的脚线3穿过固定塞4的孔,至电引火药头上塑料塞与固定塞4的孔相契合,用胶水固定、密封;将固定有电引火药头的固定塞4从测试管1一端置入,胶水固定、密封;飞片2由测试管1另一端置入,推至与电引火药头相接触。Referring to Figure 4, the outer diameter of the fixed plug 4 is 10 mm, and the shaft is provided with a hole with an aperture of 8 mm, and the foot line 3 of the bridge wire type electric ignition powder head is passed through the hole of the fixed plug 4 to the plastic plug on the electric ignition powder head and the fixed plug. The holes of 4 are matched with each other, fixed and sealed with glue; the fixed plug 4 with the electric ignition powder tip is inserted from one end of the test tube 1, and the glue is fixed and sealed; the flying piece 2 is inserted from the other end of the test tube 1 and pushed to the In contact with the electric ignition powder tip.
参照图5,将电引火药头的脚线3与发爆器8密封连接,将连接后的测试管1水平放于真空箱6内,密封真空箱6,用真空泵经抽气孔7将真空箱6抽真空,密封抽气孔7,高速摄像机9、测温装置5垂直于测试管1轴线放置,高速摄像机9、测温装置5与记录装置10连接。Referring to Fig. 5, connect the pin line 3 of the electric ignition powder head to the detonator 8 in a sealed manner, place the connected test tube 1 horizontally in the vacuum box 6, seal the vacuum box 6, and use a vacuum pump to pump the vacuum box through the air hole 7. 6. Vacuumize and seal the air hole 7. The high-speed camera 9 and the temperature measuring device 5 are placed perpendicular to the axis of the test tube 1. The high-speed camera 9 and the temperature measuring device 5 are connected to the recording device 10.
结合上述理论推导,数据处理系统根据记录装置10记录的飞片2不同时刻所对应的测试管1上刻度线的位置,以及不同时刻所对应的飞片2侧面刻线,拟合出电引火药头发火过程飞片2的运动状态函数,间接测量出电引火药头发火能量转化为动能的部分;通过测温装置5测得的测试管1的温度变化,求解电引火药头发火能量转化为热能的部分;动能和热能总和即为电引火药头发火能量。Combined with the above theoretical derivation, the data processing system fits the electric ignition powder according to the position of the scale line on the test tube 1 corresponding to the different moments of the flyer 2 recorded by the recording device 10, and the corresponding marking lines on the side of the flyer 2 at different times. The motion state function of the flying piece 2 in the ignition process indirectly measures the part where the ignition energy of the electric ignition powder is converted into kinetic energy; the temperature change of the test tube 1 measured by the temperature measuring device 5 solves the conversion of the ignition energy of the electric ignition powder into The part of thermal energy; the sum of kinetic energy and thermal energy is the ignition energy of the electric ignition powder.
实施例二Embodiment two
本实用新型的方法及装置也可用于导爆管发火能量的测量,与实施例一类似,在此不再赘述。The method and device of the present invention can also be used to measure the ignition energy of the detonator, which is similar to the first embodiment and will not be repeated here.
上面所述的实施例仅仅是对本实用新型优选实施方式进行描述,并非对本实用新型的构思和范围进行限定。在不脱离本实用新型设计构思的前提下,本领域普通人员对本实用新型的技术方案做出的各种变型和改进,均应落入到本实用新型的保护范围,本实用新型请求保护的技术内容,已经全部记载在权利要求书中。The above-mentioned embodiments are only descriptions of preferred implementations of the present utility model, and are not intended to limit the concept and scope of the present utility model. Under the premise of not departing from the design concept of the present utility model, various modifications and improvements made by ordinary persons in the art to the technical solution of the present utility model should fall into the protection scope of the present utility model, and the technology claimed by the utility model The contents are all described in the claims.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621274100.4U CN206330494U (en) | 2016-11-24 | 2016-11-24 | Electrical fuze firing energy test device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621274100.4U CN206330494U (en) | 2016-11-24 | 2016-11-24 | Electrical fuze firing energy test device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206330494U true CN206330494U (en) | 2017-07-14 |
Family
ID=59287957
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201621274100.4U Expired - Fee Related CN206330494U (en) | 2016-11-24 | 2016-11-24 | Electrical fuze firing energy test device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206330494U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110926283A (en) * | 2019-09-10 | 2020-03-27 | 贵州全安密灵科技有限公司 | Ignition head bridgewire brightness testing device |
-
2016
- 2016-11-24 CN CN201621274100.4U patent/CN206330494U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110926283A (en) * | 2019-09-10 | 2020-03-27 | 贵州全安密灵科技有限公司 | Ignition head bridgewire brightness testing device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106198849A (en) | A kind of test device for solid propellant combustion rate/combustion temperature and method of testing thereof | |
CN105974049B (en) | A kind of device and measuring method for measuring the instantaneous burn rate of solid propellant | |
CN206330494U (en) | Electrical fuze firing energy test device | |
CN106352747A (en) | Electric firing explosive head ignition pressure test method | |
CN106679516B (en) | Electrical fuze firing energy method of testing | |
CN102156198A (en) | Method for testing projectile muzzle speed by means of rotation speed | |
CN110823020B (en) | A missile-borne integrated explosive power field can measure the warhead in real time and control method | |
CN111366263B (en) | A high temperature calibration device and method for TDLAS temperature measurement based on shock tube | |
CN106556292B (en) | Electrical fuze gas production and gas production rate method of testing | |
CN209148459U (en) | A dynamic experimental system for testing the impact resistance of two-dimensional structural materials | |
CN206096055U (en) | A testing arrangement that is used for solid propellant to fire invite / firing temperature | |
CN204389169U (en) | The device of test solid fuel micro-thruster ignition characteristic and propulsive performance | |
CN104457457A (en) | Novel method for delay test of delay element of detonator | |
CN206223591U (en) | Electrical fuze gas production and gas production rate test device | |
CN106440979B (en) | Electrical fuze firing pressure method of testing and device | |
CN206330495U (en) | Electrical fuze firing pressure test device | |
CN106370068A (en) | Electrical ignition charge head igniting energy testing method and device | |
CN106500553A (en) | Electrical fuze gas production and gas production rate method of testing and device | |
CN106950396A (en) | A kind of speed-measuring method of Exploding foil initiator driven flyer plates | |
CN110758780B (en) | Device and method for observing combustion of aerospace equipment in weightless state | |
CN108801846B (en) | A two-chamber quasi-airtight container experimental device | |
CN103149327B (en) | High altitude environment gas automatic collection method and device | |
CN105258581A (en) | Low-air-pressure delay time test system for infantry grenade | |
CN106370234A (en) | Testing method and testing apparatus for temperature and suction resistance of electronic cigarette | |
CN206146459U (en) | Electron gas temperature degree and suction resistance testing arrangement |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170714 Termination date: 20171124 |