CN114370796B - Small-caliber rotary bullet mechanical trigger fuze with safe explosive treatment after misfire - Google Patents

Small-caliber rotary bullet mechanical trigger fuze with safe explosive treatment after misfire Download PDF

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CN114370796B
CN114370796B CN202210084491.7A CN202210084491A CN114370796B CN 114370796 B CN114370796 B CN 114370796B CN 202210084491 A CN202210084491 A CN 202210084491A CN 114370796 B CN114370796 B CN 114370796B
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safety
ball
pin
centrifugal
explosion
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CN114370796A (en
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王雨时
李俊鸿
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Nanjing University of Science and Technology
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/20Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin
    • F42C15/21Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin using spring action
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/20Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin
    • F42C15/22Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin using centrifugal force

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Abstract

The invention discloses a small-caliber rotary bullet mechanical trigger fuse which is safe in explosive treatment after blind fire, and adopts a collision type trigger mechanism, a centrifugal self-destruction and inertia trigger mechanism, a centrifugal safety mechanism of the centrifugal self-destruction and inertia trigger mechanism, an explosion-proof and delay release safety mechanism, a recoil safety mechanism of the explosion-proof and delay release safety mechanism and a centrifugal safety mechanism. The impact type trigger mechanism comprises a bidirectional trigger fire cap, a moistureproof sheet and an upper body. The centrifugal self-destruction and inertia trigger mechanism is a centrifugal ball-spring-firing pin mechanism. The explosion-proof and delay releasing safety mechanism is a ball rotor mechanism. The recoil safety mechanism and the centrifugal safety mechanism of the explosion-proof and delay releasing safety mechanism are respectively a safety pin-shearing pin mechanism and a split ring. The fuze has a simple structure, fully utilizes the fuze space, has the functions of explosion suppression, redundant insurance, delay relief insurance, self-destruction, collision triggering, standby inertial triggering, floor cleaning and explosion and fire insulation, and is safe in explosive treatment after fire extinction.

Description

瞎火后爆炸物处理安全的小口径旋转弹弹头机械触发引信Blind-Fire Post-Explosive Ordnance Disposal Safe Small Caliber Rotary Projectile Warhead Mechanical Trigger Fuze

技术领域technical field

本发明属于小口径炮弹引信技术,具体涉及一种瞎火后爆炸物处理特性优异的小口径旋转弹弹头触发引信。The invention belongs to the fuze technology of small-caliber artillery shells, and in particular relates to a small-caliber rotary projectile warhead trigger fuze with excellent characteristics of handling explosives after misfire.

背景技术Background technique

小口径炮弹一般是指口径为20毫米到40毫米,利用火炮进行发射并完成杀伤、爆破、侵彻或其他战术目的的弹药,由于其机动性强,发射速率高而被广泛运用于陆海空三军。Small-caliber artillery shells generally refer to ammunition with a caliber of 20 mm to 40 mm, which are fired by artillery and complete killing, blasting, penetration, or other tactical purposes. Due to their strong mobility and high firing rate, they are widely used in the army, sea, and air forces.

用于20~30 mm口径的炮弹引信,由于外形尺寸受限,全面满足《引信安全性设计准则》且同时具有擦地炸、大着角发火和自毁性能,难度较大。并且在瞎火后其敏感爆炸元件仍然存在,甚至往往处于危险的待发状态,使未爆弹药的爆炸物处理安全性无法得到保证。Due to the limited size, it is difficult for the fuze of shells with a caliber of 20 to 30 mm to fully meet the "Design Criteria for Safety of Fuze" and have the performance of wiping the ground, igniting at a large angle, and self-destructing at the same time. And its sensitive explosive elements still exist after misfiring, and are often even in a dangerous ready state, so that the explosive ordnance disposal safety of unexploded ammunition cannot be guaranteed.

发明内容Contents of the invention

本发明的目的在于提供一种瞎火后爆炸物处理安全的小口径旋转弹弹头机械触发引信,改善小口径旋转炮弹引信瞎火后形成的未爆弹药的爆炸物处理安全性,并全面满足《引信安全性设计准则》的相关要求,同时具有擦地炸、大着角发火和自毁性能。The purpose of the present invention is to provide a small-caliber rotary projectile warhead mechanical trigger fuze that is safe to dispose of explosives after misfire, improve the safety of explosive disposal of unexploded ammunition formed after the small-caliber rotary projectile fuze is misfired, and fully meet the " According to the relevant requirements of the Fuze Safety Design Criteria, it also has the performance of wiping the ground, igniting at a large angle and self-destructing.

实现本发明目的的技术解决方案:一种瞎火后爆炸物处理安全的小口径旋转弹弹头机械触发引信,包括本体、上体、碰击式触发机构、离心自毁兼惯性触发机构、离心自毁兼惯性触发机构的离心保险机构即保险环、隔爆兼延期解除保险机构、隔爆兼延期解除保险机构的后坐保险机构即保险销-剪切销机构、隔爆兼延期解除保险机构的离心保险机构即开口环、传爆管;上体与本体同轴设置,且本体的上部伸入上体的下部后两者固连构成引信外壳,碰击式触发机构、离心自毁兼惯性触发机构、隔爆兼延期解除保险机构自上而下依次设置于引信外壳内;保险销-剪切销机构将隔爆兼延期解除保险机构约束在本体上;保险环套在离心自毁兼惯性触发机构的顶面;开口环设置在隔爆兼延期解除保险机构上,传爆管位于引信外壳底部,并贴近隔爆兼延期解除保险机构。The technical solution to realize the object of the present invention: a small-caliber rotating warhead mechanical trigger fuze that is safe to dispose of explosives after blind fire, including a main body, an upper body, an impact trigger mechanism, a centrifugal self-destruction and inertial trigger mechanism, a centrifugal self-destruction The centrifugal insurance mechanism of the destruction and inertia trigger mechanism is the safety ring, the explosion-proof and delayed release insurance mechanism, the recoil insurance mechanism of the explosion-proof and delayed release insurance mechanism is the safety pin-shear pin mechanism, the centrifugal of the explosion-proof and delayed release insurance mechanism The safety mechanism is the split ring and the detonator tube; the upper body and the main body are coaxially arranged, and the upper part of the main body extends into the lower part of the upper body, and then the two are fixedly connected to form the fuze shell, the impact trigger mechanism, the centrifugal self-destruction and inertial trigger mechanism The explosion-proof and delayed release insurance mechanism is arranged in the fuze casing from top to bottom in sequence; the safety pin-shear pin mechanism constrains the explosion-proof and delayed release insurance mechanism on the body; the safety ring is set on the centrifugal self-destruct and inertial trigger mechanism The top surface of the fuse; the split ring is set on the flameproof and delayed release safety mechanism, and the detonator is located at the bottom of the fuze shell, and is close to the flameproof and delayed release safety mechanism.

碰击式触发机构主要包括设置在上体内的防潮片和双向触发火帽;离心自毁兼惯性触发机构主要包括击针架、击针、弹簧和若干离心球;击针向上指向双向触发火帽,保险环套在击针上,击针架和保险环和上体共同实现了对离心自毁兼惯性触发机构的离心保险,隔爆兼延期解除保险机构主要包括隔离球、球座和两个双向输入火焰雷管;保险销-剪切销机构主要包括保险销、剪切销和封塞;封塞为圆柱形,与剪切销同轴设置,缩短了剪切销孔,改善了加工工艺性能;所述隔离球上设置有一个通过球心的横向通孔,该横向通孔内对称设置有两个双向输入火焰雷管;所述隔离球顶端设置有与引信同轴的第一盲孔;本体、保险销、剪切销、封塞共同实现了对隔爆兼延期解除保险机构的后坐保险;保险销设置于隔离球上的第一盲孔内;剪切销垂直穿过保险销伸入隔离球,将保险销固定在隔离球上的第一盲孔内,同时保险销的向上伸出部分伸入本体的中心孔,约束了隔离球的转动;封塞通过点铆固定在隔离球上,封堵住剪切销;所述开口环卡于隔离球下端月牙形缺口外侧,限制了隔离球即球转子的转动,实现了对隔离球的另一道保险,即离心保险,球座和开口环构成了隔爆兼延期解除保险机构即球转子部件的离心保险机构;传爆管设置于隔爆兼延期解除保险机构后端,且传爆管上部伸入本体与球座固连。碰击式触发机构的双向触发火帽位于碰击式触发机构顶端,其直径为上体头部孔(第二阶孔)直径的60%-90%,可提高碰击触发灵敏度、大着角发火和擦地炸作用正确性。离心自毁兼惯性触发机构采用离心球-弹簧-击针机构,可实现离心自毁和惯性触发,其中的击针为中空结构,可在引信自毁和触发时不影响传火。隔爆兼延期解除保险机构为球转子机构,使双向输入火焰雷管平时处于隔爆状态,并在其保险机构均解除保险后实现延期解除保险功能,保证引信在弹丸飞出炮口安全距离以外才解除保险,确保发射安全。保险销-剪切销和开口环实现球转子机构的冗余保险。隔离球内双向输入火焰雷管以及隔离球上的多条传火通道确保引信头部双向触发火帽输出能够可靠引燃已对正或未对正的双向输入火焰雷管。如果该双向输入火焰雷管处于对正状态,引信就是正常发火;如果该双向输入火焰雷管处于未对正状态,引信就实现绝火,确保引信瞎火所形成的未爆弹药的爆炸物处理安全。The percussion trigger mechanism mainly includes a moisture-proof sheet and a two-way trigger cap set in the upper body; the centrifugal self-destruct and inertial trigger mechanism mainly includes a firing pin frame, firing pin, spring and several centrifugal balls; the firing pin points upward to the two-way trigger cap , the insurance ring is set on the firing pin, the firing pin holder, the insurance ring and the upper body together realize the centrifugal insurance of the centrifugal self-destruction and inertial trigger mechanism. The explosion-proof and delayed release insurance mechanism mainly includes an isolation ball, a ball seat and two Two-way input flame detonator; safety pin-shear pin mechanism mainly includes safety pin, shear pin and plug; the plug is cylindrical and coaxial with the shear pin, which shortens the shear pin hole and improves the processing performance ; The isolation ball is provided with a transverse through hole passing through the center of the ball, and two bidirectional input flame detonators are symmetrically arranged in the transverse through hole; the top of the isolation ball is provided with a first blind hole coaxial with the fuze; the body , safety pin, shear pin, and plug jointly realize the recoil insurance of the explosion-proof and delayed release safety mechanism; the safety pin is set in the first blind hole on the isolation ball; the shear pin vertically passes through the safety pin and extends into the isolation Ball, fix the safety pin in the first blind hole on the isolation ball, and at the same time, the upward protruding part of the safety pin extends into the center hole of the body, constraining the rotation of the isolation ball; the plug is fixed on the isolation ball by point riveting, Block the shear pin; the split ring is stuck outside the crescent-shaped notch at the lower end of the spacer ball, limiting the rotation of the spacer ball, that is, the ball rotor, and realizing another insurance for the spacer ball, that is, centrifugal safety, ball seat and split ring The explosion-proof and delayed release safety mechanism is constituted, that is, the centrifugal safety mechanism of the ball rotor part; the explosion-proof tube is arranged at the rear end of the flame-proof and delayed release safety mechanism, and the upper part of the explosion-proof tube extends into the body and is fixedly connected with the ball seat. The two-way trigger cap of the impact trigger mechanism is located at the top of the impact trigger mechanism, and its diameter is 60%-90% of the diameter of the upper body head hole (second-order hole), which can improve the impact trigger sensitivity and increase the angle of attack. Fire and ground blasting effects are correct. The centrifugal self-destruction and inertial trigger mechanism adopts the centrifugal ball-spring-firing pin mechanism, which can realize centrifugal self-destructing and inertial triggering. The firing pin is a hollow structure, which does not affect the fire transmission when the fuze is self-destructing and triggering. The explosion-proof and delayed release safety mechanism is a ball rotor mechanism, which keeps the two-way input flame detonator in the explosion-proof state at ordinary times, and realizes the delayed release safety function after the safety mechanisms are released, so as to ensure that the fuze is released when the projectile flies out of the muzzle. Release the insurance to ensure safe launch. Safety Pin - Shear pin and split ring for redundant safety of the ball rotor mechanism. The two-way input flame detonator in the isolation ball and the multiple fire transmission channels on the isolation ball ensure that the output of the two-way trigger cap of the fuze head can reliably ignite the aligned or unaligned two-way input flame detonator. If the two-way input flame detonator is in the alignment state, the fuze is normally ignited; if the two-way input flame detonator is in the non-alignment state, the fuze will achieve flameout, ensuring the safety of explosive disposal of unexploded ammunition formed by fuze misfiring.

本发明与现有技术相比,其显著优点是:Compared with the prior art, the present invention has the remarkable advantages of:

(1)总体结构沿轴向布局紧凑,合理利用内部空间,全面满足《引信安全性设计准则》的相关设计要求。(1) The overall structure has a compact layout along the axial direction, rational use of internal space, and fully meets the relevant design requirements of the "Fuze Safety Design Guidelines".

(2)一件多能,一件多用,简化了结构,降低了成本,有助于提高可靠性。(2) One piece is multi-functional, and one piece is multi-purpose, which simplifies the structure, reduces the cost, and helps to improve reliability.

(3)功能分区,结构分立,易于研制过程中的试验验证,从而缩短研制周期,降低研制成本。(3) Functional partitions and separate structures are easy to test and verify during the development process, thereby shortening the development cycle and reducing development costs.

(4)双向触发火帽直径为引信上体头部孔直径的60%-90%,提高了碰击触发、大着角发火暨擦地炸作用正确性。(4) The diameter of the two-way trigger cap is 60%-90% of the diameter of the hole in the upper body of the fuze, which improves the accuracy of impact triggering, large-angle ignition and ground-grazing action.

(5)采用空心击针,相比传统击针,该击针在发火后其针尖部易被双向触发火帽装药炸碎从而形成传火通道,使火焰或爆轰可靠下传。(5) The hollow firing pin is adopted. Compared with the traditional firing pin, the tip of the firing pin is easily broken by the two-way trigger cap charge after firing, thus forming a fire transmission channel, so that the flame or detonation can be transmitted reliably.

(6)在隔离球上设置有多个传火通道通向双向输入火焰雷管内侧端,有利于双向触发火帽火焰传播,可靠实现未解除保险状态下的绝火作用。(6) There are multiple fire transmission channels on the isolation ball leading to the inner side of the two-way input flame detonator, which is conducive to the two-way triggering of the fire cap flame propagation, and reliably realizes the fire-proof function in the unreleased state.

附图说明Description of drawings

图1为本发明瞎火后爆炸物处理安全的小口径旋转弹弹头机械触发引信的结构主剖视图。Fig. 1 is the main cross-sectional view of the structure of the mechanical trigger fuze of the small-caliber rotary projectile warhead safe for explosive ordnance disposal after blind fire of the present invention.

具体实施方式Detailed ways

下面结合附图对本发明作进一步的详细描述。The present invention will be described in further detail below in conjunction with the accompanying drawings.

结合图1,一种瞎火后爆炸物处理安全的小口径旋转弹弹头机械触发引信,包括本体1、上体2、碰击式触发机构3、离心自毁兼惯性触发机构4、离心自毁兼惯性触发机构4的离心保险机构即保险环5、隔爆兼延期解除保险机构6、隔爆兼延期解除保险机构6的后坐保险机构即保险销-剪切销机构7、隔爆兼延期解除保险机构6的离心保险机构即开口环8、传爆管9;上体2与本体1同轴设置,且本体1的上部伸入上体2的下部后两者固连构成引信外壳,碰击式触发机构3、离心自毁兼惯性触发机构4、隔爆兼延期解除保险机构6自上而下依次设置于引信外壳内;保险销--剪切销机构7将隔爆兼延期解除保险机构6约束在本体1上;保险环5套在离心自毁兼惯性触发机构4的顶面;开口环8设置在隔爆兼延期解除保险机构6上,传爆管9位于引信外壳底部,并贴近隔爆兼延期解除保险机构6。Combining with Figure 1, a small-caliber rotating warhead mechanical trigger fuze with safe explosive disposal after blind fire, including body 1, upper body 2, impact trigger mechanism 3, centrifugal self-destruct and inertial trigger mechanism 4, centrifugal self-destruct The centrifugal insurance mechanism of the inertial trigger mechanism 4 is the safety ring 5, the explosion-proof and delayed release insurance mechanism 6, the explosion-proof and delayed release insurance mechanism 6 The recoil insurance mechanism is the safety pin-shear pin mechanism 7, the explosion-proof and delayed release The centrifugal safety mechanism of safety mechanism 6 is split ring 8, detonator tube 9; upper body 2 and body 1 are coaxially arranged, and the top of body 1 stretches into the bottom of upper body 2, and the two are fixedly connected to form the fuze shell after impacting. Type trigger mechanism 3, centrifugal self-destruction and inertial trigger mechanism 4, explosion-proof and delayed release safety mechanism 6 are arranged in the fuze shell from top to bottom in sequence; 6 is constrained on the body 1; the safety ring 5 is set on the top surface of the centrifugal self-destruct and inertial trigger mechanism 4; the split ring 8 is set on the flameproof and delayed release safety mechanism 6, and the detonator tube 9 is located at the bottom of the fuze shell and is close to Explosion-proof and delayed release insurance mechanism 6.

进一步地,上体2自顶面沿其中心轴线向下开有内径不同的七阶阶梯通孔,自上向下依次为第一阶孔、第二阶孔、第三阶孔、第四阶孔、第五阶孔、第六阶孔和第七阶孔,第四阶孔的孔径小于第三阶孔的孔径,且小于第五阶孔的孔径。Further, the upper body 2 is provided with seven-step through holes with different inner diameters from the top surface along its central axis. From top to bottom, there are first step holes, second step holes, third step holes, and fourth step holes. Holes, fifth-order holes, sixth-order holes and seventh-order holes, the diameter of the fourth-order holes is smaller than the diameter of the third-order holes, and smaller than the diameter of the fifth-order holes.

碰击式触发机构3主要包括设置在上体2内的防潮片31和双向触发火帽32,防潮片31设置在上体2的第一阶孔内,通过上体2顶面收口固定,双向触发火帽32固定在上体2的第三阶孔内。离心自毁兼惯性触发机构4包括击针架41、击针42、弹簧44和若干离心球43。击针42向上指向双向触发火帽32,保险环5套在击针42上,保险环5位于第五阶孔内,击针架41位于第六阶孔内且与第七阶孔内壁上端固连,击针42向上穿过击针架41、由保险环5实施轴向约束,上体2通过其第七阶孔与本体1螺纹固连,使得本体1抵住击针架41。击针架41、保险环5和上体2共同实现了对离心自毁兼惯性触发机构4的离心保险。隔爆兼延期解除保险机构6(即球转子机构)主要包括隔离球61、球座63和两个双向输入火焰雷管62。保险销-剪切销机构7主要包括保险销71、剪切销72和封塞73。封塞73为圆柱形,与剪切销72同轴设置。所述隔离球61上设置有一个通过球心的横向通孔,该横向通孔内对称设置有两个双向输入火焰雷管62。所述隔离球61顶端设置有与引信同轴的第一盲孔。本体1、保险销71、剪切销72、封塞73共同实现了对隔爆兼延期解除保险机构6的后坐保险。保险销71设置于该第一盲孔内。剪切销72垂直穿过保险销71伸入隔离球61,将保险销71固定在隔离球61上的第一盲孔内,同时保险销71的向上伸出部分伸入本体1的中心孔,约束了隔离球61的转动。封塞73通过点铆固定在隔离球61上,封堵住剪切销72。所述开口环8卡于隔离球61下端月牙形缺口外侧,限制了隔离球61即球转子的转动,实现了对隔离球61的另一道保险,即离心保险。球座63和开口环8构成了隔爆兼延期解除保险机构6的离心保险机构。传爆管9设置于隔爆兼延期解除保险机构6后端,且传爆管9上部伸入本体1与球座63固连。The impact trigger mechanism 3 mainly includes a moisture-proof sheet 31 arranged in the upper body 2 and a two-way trigger fire cap 32. The moisture-proof sheet 31 is arranged in the first-stage hole of the upper body 2, and is fixed through the top surface of the upper body 2. Two-way The trigger cap 32 is fixed in the third-order hole of the upper body 2 . The centrifugal self-destruction and inertia trigger mechanism 4 includes a firing pin frame 41 , a firing pin 42 , a spring 44 and several centrifugal balls 43 . The firing pin 42 points upward to the two-way firing cap 32, the safety ring 5 is set on the firing pin 42, the safety ring 5 is located in the fifth-order hole, and the firing pin frame 41 is located in the sixth-order hole and fixed to the upper end of the seventh-order hole inner wall. Even, the firing pin 42 passes through the firing pin frame 41 upwards, and is axially restrained by the safety ring 5 , and the upper body 2 is screwed to the body 1 through its seventh-order hole, so that the body 1 is against the firing pin frame 41 . The firing pin holder 41, the insurance ring 5 and the upper body 2 jointly realize the centrifugal insurance of the centrifugal self-destruction and inertial trigger mechanism 4. The explosion-proof and delayed release safety mechanism 6 (ie, the ball rotor mechanism) mainly includes an isolation ball 61 , a ball seat 63 and two bidirectional input flame detonators 62 . The safety pin-shear pin mechanism 7 mainly includes a safety pin 71 , a shear pin 72 and a plug 73 . The plug 73 is cylindrical and coaxial with the shear pin 72 . The isolation ball 61 is provided with a transverse through hole passing through the center of the sphere, and two bidirectional input flame detonators 62 are symmetrically arranged in the transverse through hole. The top of the isolation ball 61 is provided with a first blind hole coaxial with the fuze. Body 1, safety pin 71, shear pin 72, and plug 73 jointly realize the recoil insurance to explosion-proof and delay release insurance mechanism 6. The safety pin 71 is disposed in the first blind hole. The shear pin 72 vertically passes through the safety pin 71 and extends into the spacer ball 61, and the safety pin 71 is fixed in the first blind hole on the spacer ball 61, while the upward protruding part of the safety pin 71 extends into the central hole of the body 1, The rotation of the spacer ball 61 is constrained. The plug 73 is fixed on the spacer ball 61 by spot riveting to block the shear pin 72 . The split ring 8 is stuck outside the crescent-shaped notch at the lower end of the isolation ball 61, limiting the rotation of the isolation ball 61, that is, the ball rotor, and realizing another insurance for the isolation ball 61, that is, centrifugal insurance. Ball seat 63 and split ring 8 have constituted the centrifugal insurance mechanism of explosion-proof holding concurrently to postpone to release insurance mechanism 6. The detonator tube 9 is arranged on the explosion-proof and delayed release safety mechanism 6 rear end, and the detonator tube 9 top stretches into the body 1 and is fixedly connected with the ball seat 63 .

所述碰击式触发机构3的双向触发火帽32的直径为上体2中第二阶孔直径的60%-90%,引信以大着角或小落角命中目标时,能提高大着角发火和擦地炸作用可靠性,还有助于提高触发灵敏度。The diameter of the two-way trigger cap 32 of the percussion trigger mechanism 3 is 60%-90% of the diameter of the second-order hole in the upper body 2, and when the fuze hits the target with a large or small drop angle, it can improve the large impact. The reliability of the horn firing and ground blasting effects also helps to improve the trigger sensitivity.

进一步地,保险环5与击针架41自上而下同轴设置,保险环5在击针架41与上体2的第五阶孔底面之间形成间隙配合,保险环5能在离心力作用下甩开从而释放击针42。击针42为中空结构,因而在引信自毁和触发时不影响传火。Further, the safety ring 5 and the firing pin frame 41 are arranged coaxially from top to bottom, and the safety ring 5 forms a clearance fit between the firing pin frame 41 and the bottom surface of the fifth-order hole of the upper body 2, and the safety ring 5 can be used under centrifugal force. Swing it down to release the firing pin 42. The firing pin 42 is a hollow structure, so it does not affect the fire transmission when the fuze is self-destructed and triggered.

进一步地,所述保险销71设置有一个轴向阶梯盲孔和两个横向通孔,轴向阶梯盲孔沿保险销71的顶端向下设置,轴向阶梯盲孔沿保险销71上方的孔径大于下方的孔径,两个横向通孔沿轴向排布,分别贯穿直径小的下方阶梯孔,形成传火通道,利于双向触发火帽火焰输入并传播给隔离球61内的双向输入火焰雷管62,使引信实现未解除保险状态下的绝火,从而保证引信瞎火后形成的未爆弹药的爆炸物处理安全。Further, the safety pin 71 is provided with an axial stepped blind hole and two transverse through holes, the axial stepped blind hole is arranged downward along the top end of the safety pin 71, and the axial stepped blind hole is arranged along the aperture above the safety pin 71. Larger than the lower aperture, two transverse through holes are arranged in the axial direction, and respectively pass through the lower stepped holes with small diameters to form a fire transmission channel, which is beneficial to the bidirectional trigger fire cap flame input and spread to the bidirectional input flame detonator 62 in the isolation ball 61 , so that the fuze can realize the flameout in the state of not releasing the insurance, so as to ensure the safety of the explosive disposal of the unexploded ammunition formed after the fuze is misfired.

进一步地,所述隔离球61在其过球心且垂直于双向输入火焰雷管轴线的平面内还对称设有2个通向中心的传火孔,借助于本体1多个轴向偏心传火孔以及球转子部件与其腔室间的间隙,将双向触发火帽火焰传递给隔离球61内的双向输入火焰雷管62的内侧端和外侧端,引信实现未解除保险状态下的绝火,从而保证引信瞎火后形成的未爆弹药的爆炸物处理安全。Further, the isolation ball 61 is also symmetrically provided with two fire transmission holes leading to the center in a plane passing through the center of the ball and perpendicular to the axis of the two-way input flame detonator. And the gap between the ball rotor part and its chamber, the two-way trigger fire cap flame is transmitted to the inner side and the outer side of the two-way input flame detonator 62 in the isolation ball 61, and the fuze realizes the flame-out in the unsafe state, thereby ensuring the fuze Explosive ordnance disposal safety of unexploded ordnance formed after misfire.

进一步地,所述离心球43是陶瓷球,如用作轴承滚动体的氧化锆陶瓷球,其密度在6 g/cm3左右,略低于不锈钢,但其摩擦系数较低,有利于提高自毁、惯性触发、擦地炸作用和大着角发火时的作用可靠性。Further, the centrifugal ball 43 is a ceramic ball, such as a zirconia ceramic ball used as a bearing rolling body, its density is about 6 g/cm 3 , which is slightly lower than that of stainless steel, but its friction coefficient is low, which is beneficial to improve the self-improvement. The reliability of the action when destroying, inertial triggering, ground-grazing action, and high-angle fire.

进一步地,所述球座63下部外壁设有一圈凸缘,所述本体1底端向里对该凸缘收口以固定球座63,从而提高球座63与本体1之间的连接强度,确保发射冲击过载与隔爆内部压力叠加作用下的结构完整性和安全性。Further, the outer wall of the lower part of the ball seat 63 is provided with a ring of flanges, and the bottom end of the body 1 closes inwards to the flange to fix the ball seat 63, thereby improving the connection strength between the ball seat 63 and the body 1, ensuring Structural integrity and safety under the superposition of launch shock overload and flameproof internal pressure.

实施例Example

结合图1,本发明所述的一种瞎火后爆炸物处理安全的小口径旋转弹弹头机械触发引信,包括本体1、上体2、碰击式触发机构3、离心自毁兼惯性触发机构4、离心自毁兼惯性触发机构4的离心保险机构即保险环5、隔爆兼延期解除保险机构6、隔爆兼延期解除保险机构6的后坐保险机构即保险销-剪切销机构7、隔爆兼延期解除保险机构6的离心保险机构即开口环8、传爆管9;上体2与本体1同轴设置,且本体1的上部伸入上体2的下部后两者固连构成引信外壳,碰击式触发机构3、离心自毁兼惯性触发机构4、隔爆兼延期解除保险机构6自上而下依次设置于引信外壳内;保险销-剪切销机构7将隔爆兼延期解除保险机构6约束在本体1上;保险环5套在离心自毁兼惯性触发机构4的顶面;开口环8设置在隔爆兼延期解除保险机构6上,传爆管9位于引信外壳底部,并贴近隔爆兼延期解除保险机构6。With reference to Fig. 1, a mechanical trigger fuze of a small-caliber rotary projectile warhead safe for disposal of explosives after blind fire according to the present invention includes a main body 1, an upper body 2, an impact trigger mechanism 3, and a centrifugal self-destruction and inertial trigger mechanism 4. The centrifugal safety mechanism of the centrifugal self-destruction and inertial trigger mechanism 4 is the safety ring 5, the explosion-proof and delayed release safety mechanism 6, the recoil safety mechanism of the explosion-proof and delayed release safety mechanism 6 is the insurance pin-shear pin mechanism 7, The centrifugal safety mechanism of the explosion-proof and delayed release safety mechanism 6 is the split ring 8 and the blast tube 9; the upper body 2 and the main body 1 are coaxially arranged, and the upper part of the main body 1 extends into the lower part of the upper body 2, and then the two are fixedly connected to form Fuze casing, impact trigger mechanism 3, centrifugal self-destruct and inertia trigger mechanism 4, explosion-proof and delayed release safety mechanism 6 are arranged in the fuze casing in sequence from top to bottom; safety pin-shear pin mechanism 7 combines explosion-proof and The delayed release safety mechanism 6 is bound on the body 1; the insurance ring 5 is set on the top surface of the centrifugal self-destruct and inertial trigger mechanism 4; the split ring 8 is set on the flameproof and delayed release safety mechanism 6, and the detonator tube 9 is located in the fuze shell Bottom, and close to the explosion-proof and delay release insurance mechanism 6.

进一步地,碰击式触发机构3主要包括设置在上体2内的防潮片31和双向触发火帽32,防潮片31设置在上体2的第一阶孔内,通过上体2顶面收口固定,双向触发火帽32固定在上体2的第三阶孔内。离心自毁兼惯性触发机构4包括击针架41、击针42、弹簧44和若干离心球43。击针42向上指向双向触发火帽32,保险环5套在击针42上,保险环5位于第五阶孔内,击针架41位于第六阶孔内且与第七阶孔内壁上端固连,击针42向上穿过击针架41、由保险环5实现轴向约束,上体2通过其第七阶孔与本体1螺纹固连,使得本体1抵住击针架41。击针架41、保险环5和上体2共同实现了对离心自毁兼惯性触发机构的离心保险。隔爆兼延期解除保险机构6(即球转子机构)主要包括隔离球61、球座63和两个双向输入火焰雷管62。保险销-剪切销机构7主要包括保险销71、剪切销72和封塞73。封塞73为圆柱形,与剪切销72同轴设置。所述隔离球61上设置有一个通过球心的横向通孔,该横向通孔内对称设置有两个双向输入火焰雷管62。所述隔离球61顶端设置有与引信同轴的第一盲孔。本体1、保险销71、剪切销72、封塞73共同实现了对隔爆兼延期解除保险机构的后坐保险。保险销71设置于该第一盲孔内。剪切销72垂直穿过保险销71伸入隔离球61,将保险销71固定在隔离球61上的第一盲孔内,同时保险销71的向上伸出部分伸入本体1的中心孔,约束了隔离球61的转动。封塞73通过点铆固定在隔离球61上,封堵住剪切销72。所述开口环8卡于隔离球61下端月牙形缺口外侧,限制了隔离球61即球转子的转动,实现了对隔离球61的另一道保险,即离心保险,球座63和开口环8构成了隔爆兼延期解除保险机构的离心保险机构。传爆管9设置于隔爆兼延期解除保险机构6后端,且传爆管9上部伸入本体1与球座63固连。Furthermore, the impact trigger mechanism 3 mainly includes a moisture-proof sheet 31 and a two-way trigger cap 32 arranged in the upper body 2. The moisture-proof sheet 31 is arranged in the first-stage hole of the upper body 2 and closes through the top surface of the upper body 2. Fixed, the two-way trigger fire cap 32 is fixed in the third-order hole of the upper body 2. The centrifugal self-destruction and inertia trigger mechanism 4 includes a firing pin frame 41 , a firing pin 42 , a spring 44 and several centrifugal balls 43 . The firing pin 42 points upward to the two-way firing cap 32, the safety ring 5 is set on the firing pin 42, the safety ring 5 is located in the fifth-order hole, and the firing pin frame 41 is located in the sixth-order hole and fixed to the upper end of the seventh-order hole inner wall. Even, the firing pin 42 passes through the firing pin frame 41 upwards, and is axially constrained by the safety ring 5 , and the upper body 2 is screwed to the body 1 through its seventh-order hole, so that the body 1 is against the firing pin frame 41 . The firing pin holder 41, the insurance ring 5 and the upper body 2 jointly realize the centrifugal insurance of the centrifugal self-destruction and inertial trigger mechanism. The explosion-proof and delayed release safety mechanism 6 (ie, the ball rotor mechanism) mainly includes an isolation ball 61 , a ball seat 63 and two bidirectional input flame detonators 62 . The safety pin-shear pin mechanism 7 mainly includes a safety pin 71 , a shear pin 72 and a plug 73 . The plug 73 is cylindrical and coaxial with the shear pin 72 . The isolation ball 61 is provided with a transverse through hole passing through the center of the sphere, and two bidirectional input flame detonators 62 are symmetrically arranged in the transverse through hole. The top of the isolation ball 61 is provided with a first blind hole coaxial with the fuze. Body 1, safety pin 71, shear pin 72, and plug 73 have jointly realized the recoil insurance of the explosion-proof and delayed release insurance mechanism. The safety pin 71 is disposed in the first blind hole. The shear pin 72 vertically passes through the safety pin 71 and extends into the spacer ball 61, and the safety pin 71 is fixed in the first blind hole on the spacer ball 61, while the upward protruding part of the safety pin 71 extends into the central hole of the body 1, The rotation of the spacer ball 61 is constrained. The plug 73 is fixed on the spacer ball 61 by spot riveting to block the shear pin 72 . The split ring 8 is stuck on the outer side of the crescent-shaped notch at the lower end of the spacer ball 61, which limits the rotation of the spacer ball 61, that is, the ball rotor, and realizes another insurance for the spacer ball 61, that is, centrifugal safety. The ball seat 63 and the split ring 8 constitute Centrifugal insurance mechanism with explosion-proof and delayed release insurance mechanism. The detonator tube 9 is arranged on the explosion-proof and delayed release safety mechanism 6 rear end, and the detonator tube 9 top stretches into the body 1 and is fixedly connected with the ball seat 63 .

所述上体2为圆台形,自上体2顶面沿其中心轴线向下开有内径不同的七阶阶梯通孔,自上向下依次为第一阶孔、第二阶孔、第三阶孔、第四阶孔、第五阶孔、第六阶孔和第七阶孔。所述上体2第一阶孔到第四阶孔直径自上向下依次减小,第五阶孔至第七阶孔直径依次增大,第七阶孔底端位置设有内螺纹。所述本体1外轮廓包括自上而下的第一圆柱、第一圆台和第二圆柱,其中第一圆柱和第二圆柱上设有外螺纹,分别用于与上体2第七阶孔和弹体口部内螺纹相连接。第一圆台与上体2的外轮廓(锥面)锥角相等,结合部直径相同,系平滑过渡。所述本体1内腔是沿中心轴线自上而下同轴设置的五阶阶梯通孔,分别为第八阶孔、第九阶孔、第十阶孔、第十一阶孔、第十二阶孔和第十三阶孔。本体1的第八阶孔用于卡住击针架41,第九阶孔内设置击针42,第十阶孔用于收纳弹簧44,第十一阶孔用来卡住保险销71,第十二阶孔为半球形腔室是球转子腔室的一部分,第十三阶孔口部设置有一段内螺纹用于与球座63外螺纹连接。The upper body 2 is in the shape of a conical cone. From the top surface of the upper body 2 along its central axis, there are seven stepped through holes with different inner diameters. From top to bottom, there are first hole, second hole, third hole Holes of first order, fourth order, fifth order, sixth order and seventh order. The diameters of the first to fourth holes of the upper body 2 decrease sequentially from top to bottom, the diameters of the fifth to seventh holes increase sequentially, and internal threads are provided at the bottom of the seventh holes. The outer contour of the body 1 includes a top-down first cylinder, a first circular platform and a second cylinder, wherein the first cylinder and the second cylinder are provided with external threads for connecting with the seventh-order hole and the upper body 2 respectively. The inner thread of the body mouth is connected. The cone angles of the outer contour (conical surface) of the first circular platform and the upper body 2 are equal, and the diameter of the joint is the same, which is a smooth transition. The inner cavity of the body 1 is a five-step stepped through hole coaxially arranged from top to bottom along the central axis, which are respectively the eighth step hole, the ninth step hole, the tenth step hole, the eleventh step hole, the twelfth step hole and thirteenth-order holes. The eighth-order hole of the body 1 is used to block the firing pin frame 41, the ninth-order hole is provided with the firing pin 42, the tenth-order hole is used to accommodate the spring 44, the eleventh-order hole is used to block the safety pin 71, and the tenth-order hole is used to hold the safety pin 71. The twelfth-stage hole is a hemispherical chamber, which is a part of the ball rotor chamber, and the thirteenth-stage orifice is provided with a section of internal thread for connecting with the external thread of the ball seat 63 .

所述隔离球61为圆球,其上设置有一个通过球心的横向通孔,该横向通孔内设置有两个双向输入火焰雷管62。这两个双向输入火焰雷管62的朝里端是输入端,而朝外端既是输入端也是输出端。所述开口环8卡于隔离球61下端月牙形缺口外侧,限制了隔离球61即球转子的转动,实现了对隔离球61的一道保险,即离心保险。The isolation ball 61 is a sphere, on which a transverse through hole passing through the center of the sphere is arranged, and two bidirectional input flame detonators 62 are arranged in the transverse through hole. The inward ends of these two bidirectional input flame detonators 62 are input ends, and the outward ends are both input ends and output ends. The split ring 8 is stuck outside the crescent-shaped notch at the lower end of the isolation ball 61, limiting the rotation of the isolation ball 61, that is, the ball rotor, and realizing an insurance for the isolation ball 61, that is, centrifugal insurance.

所述隔离球61上端设有一个横向盲孔,为第一横向盲孔。The upper end of the spacer ball 61 is provided with a transverse blind hole, which is the first transverse blind hole.

所述隔离球61顶端设置有与引信同轴的第一盲孔,本体1、保险销71、剪切销72和封塞73构成隔爆兼延期解除保险机构的后坐保险机构,隔爆兼延期解除保险机构的后坐保险机构主要是保险销71设置于该第一盲孔内。所述保险销71为圆柱销结构,下端靠近底端设有一横向通孔,为第一通孔。在保险销71中心部位设置有另一横向通孔,为第二通孔。在第二通孔上还设置有另一横向阶梯通孔,为第三通孔。从第一盲孔底部中心,穿过第一通孔、第二通孔设置有与引信同轴的第二盲孔,第二盲孔的直径小于第一盲孔的直径。所述剪切销72设置于隔离球61上第一横向盲孔内,同时穿过所述保险销71上的第三通孔,将所述保险销71固定于所述隔离球61上。所述封塞73位于隔离球61上的第三通孔口部外侧,用以固定剪切销72。The top of the isolation ball 61 is provided with a first blind hole coaxial with the fuze, and the main body 1, safety pin 71, shear pin 72 and plug 73 constitute a recoil safety mechanism of the explosion-proof and delay release safety mechanism, and the explosion-proof and delay The recoil safety mechanism of the release safety mechanism is mainly that the safety pin 71 is arranged in the first blind hole. The safety pin 71 is a cylindrical pin structure, and a transverse through hole is provided at the lower end near the bottom end, which is the first through hole. Another transverse through hole, which is the second through hole, is provided at the center of the safety pin 71 . Another transverse stepped through hole is also provided on the second through hole, which is the third through hole. From the center of the bottom of the first blind hole, a second blind hole coaxial with the fuze is provided through the first through hole and the second through hole, and the diameter of the second blind hole is smaller than that of the first blind hole. The shear pin 72 is disposed in the first transverse blind hole on the isolation ball 61 and passes through the third through hole on the safety pin 71 to fix the safety pin 71 on the isolation ball 61 . The plug 73 is located outside the opening of the third through hole on the isolation ball 61 to fix the shear pin 72 .

以上所述即为引信的装配状态。The above is the assembly state of the fuze.

在勤务处理阶段,可信的冲击、振动,包括跌落、磕碰和运输震动等,都不会使引信改变装配状态。引信头向下跌落时,上体2和防潮片31可能会有变形,会有压缩,但不会触发双向触发火帽32,另外由于保险环5的保险作用,击针42也不会刺发双向触发火帽32。引信中的隔爆兼延期解除保险机构的后坐保险机构(保险销71和剪切销72)和开口环8均处于保险位置,保证隔爆兼延期解除保险机构6处于隔爆状态,此时即使引信中双向输入火焰雷管62中的一个或全部意外发火爆炸,不会对外产生危险破片,也不会引爆传爆管9,更不会有高温高压气态产物窜出引信进入弹丸炸药室,引信和弹丸均不会意外发火,能保证勤务处理阶段安全。During the service processing stage, credible shocks and vibrations, including dropping, knocking and transport shocks, etc., will not cause the fuze to change its assembly state. When the fuze head falls downward, the upper body 2 and the moisture-proof sheet 31 may be deformed and compressed, but the two-way firing cap 32 will not be triggered. In addition, due to the insurance effect of the safety ring 5, the firing pin 42 will not trigger the fire. Two-way trigger flash hider 32. The flameproof and delayed release safety mechanism in the fuze has a recoil safety mechanism (safety pin 71 and shear pin 72) and split ring 8 all in the safety position, ensuring that the flameproof and delay release safety mechanism 6 is in the flameproof state. One or all of the two-way input flame detonators 62 in the fuze are accidentally ignited and exploded, will not produce dangerous fragments externally, will not detonate the detonator tube 9, and will not have high-temperature and high-pressure gaseous products to escape from the fuze and enter the projectile explosive chamber. Fuze and The projectiles will not be accidentally fired, which can ensure the safety of the service processing stage.

在弹丸发射时,在后坐力作用下,保险销71将剪断剪切销72而向下运动,直到保险销71不再凸出于隔离球61的外轮廓,从本体1的中心孔中缩回,解除对隔离球61的一道保险。之后保险销71继续向下运动直到其底端面抵靠在隔离球61轴向盲孔孔底,此时保险销71的质心低于隔离球61的球心位置,确保在隔离球61后续运动过程中保险销71始终会因其离心力及其约束反力产生的摩擦力的作用而处于隔离球61的第一盲孔孔底部位而不会再恢复保险,保证隔离球61正确解除保险。When the projectile is launched, under the recoil force, the safety pin 71 will cut off the shear pin 72 and move downward until the safety pin 71 no longer protrudes from the outer contour of the isolation ball 61 and retracts from the center hole of the body 1, Remove one insurance to isolation ball 61. Afterwards, the safety pin 71 continues to move downward until its bottom surface abuts against the bottom of the blind hole in the axial direction of the isolation ball 61. At this time, the center of mass of the safety pin 71 is lower than the position of the center of the isolation ball 61, ensuring that the subsequent movement of the isolation ball 61 The middle safety pin 71 will always be in the bottom position of the first blind hole of the isolation ball 61 due to the centrifugal force and the frictional force produced by its restraint reaction force and will not restore the safety again, so as to ensure that the isolation ball 61 is correctly released.

在弹丸发射的同时,在弹丸运动至最大膛压点之前,击针42、离心球43以及弹簧44的后坐力使击针42、离心球43和弹簧44向下运动,压缩弹簧44,使击针42底部环面抵靠在本体1头部中心孔孔底平面上。离心球43在离心力作用下沿径向孔甩出,在弹丸运动接近炮口时,弹丸转速逐渐趋于最大值,离心球43以其离心力通过击针架41底部的自毁斜面将击针42卡持在接近后坐到底的待发位置上,此时击针尖远离双向触发火帽32,弹簧44处于压缩状态。While the projectile is fired, before the projectile moves to the maximum bore pressure point, the recoil force of the firing pin 42, the centrifugal ball 43 and the spring 44 moves the firing pin 42, the centrifugal ball 43 and the spring 44 downward, compresses the spring 44, and makes the firing pin 42 The bottom ring surface abuts against the bottom plane of the central hole of the head of the body 1 . The centrifugal ball 43 is thrown out along the radial hole under the action of centrifugal force. When the projectile moves close to the muzzle, the rotational speed of the projectile gradually tends to the maximum value. Clamped on the ready-to-fire position close to the recoil, at this moment, the striker tip is away from the two-way trigger cap 32, and the spring 44 is in a compressed state.

弹丸运动接近炮口,转速接近最大,开口环半环在离心力的作用下,以离心力矩的形式使开口环8张开,进而解除对隔离球61的另一道保险。此后,隔离球61在离心力矩的作用下转动,并在弹丸飞出炮口安全距离(小口径炮弹通常取为20 m)以外转动至对正位置,即隔离球61一端的双向输入火焰雷管62正对所述击针架41和击针42,另一端的双向输入火焰雷管62正对传爆管9,双向输入火焰雷管62的轴线与弹轴重合或接近重合,引信处于解除保险状态。The projectile moves close to the muzzle, and the rotational speed is close to the maximum. Under the action of centrifugal force, the split ring half ring makes the split ring 8 open in the form of centrifugal torque, and then removes another insurance for the isolation ball 61. Thereafter, the isolation ball 61 rotates under the action of centrifugal torque, and rotates to the alignment position beyond the safe distance of the projectile flying out of the muzzle (usually 20 m for small-caliber projectiles), that is, the two-way input flame detonator 62 at one end of the isolation ball 61 Facing said firing pin frame 41 and firing pin 42, the two-way input flame detonator 62 at the other end faces the detonator 9, the axis of the two-way input flame detonator 62 coincides or nearly coincides with the bomb shaft, and the fuze is in the disarmed state.

在弹丸运动接近炮口开口环8张开的同时,保险环5也依与开口环相同的原理在离心力矩的作用下张开,不再限制击针42的轴向运动,引信碰击触发机构3的惯性发火通道和自毁发火通道打开,引信碰击触发机构3处于待发状态。When the projectile moves close to the opening of the muzzle opening ring 8, the safety ring 5 also opens under the action of the centrifugal force according to the same principle as the opening ring, which no longer restricts the axial movement of the firing pin 42, and the fuze hits the trigger mechanism. The inertia firing channel of 3 and the self-destruction firing channel are opened, and the fuze impact trigger mechanism 3 is in a ready state.

弹丸以正向碰击目标或以擦地炸姿态或以大着角姿态碰击目标时,防潮片31连同目标靶片共同作用打击双向触发火帽32顶端而发火,或稍后击针42也会在前冲力的作用下向前运动针刺碰击触发机构3的双向触发火帽32底端而发火,炸碎击针42尖部,其爆轰产物特别是高温高压气体与固态微粒沿击针42中心通道下传,沿弹簧轴线经其中心孔道,直接引发处于对正状态的隔离球61上端的双向输入火焰雷管62,隔离球61上端的双向输入火焰雷管62再引爆隔离球61下端双向输入火焰雷管62,继而引爆传爆管9,引信完成正常发火起爆过程。双向触发火帽32直径较大,因而引信擦地炸和大着角发火可靠性得以实现。而离心球-弹簧-击针机构具有的惯性触发作用,与碰击触发作用冗余,在头部碰击发火失效时起后备作用,也提高了发火可靠性。When the projectile hits the target in the forward direction or with the posture of wiping the ground or with the posture of a large angle of attack, the moisture-proof sheet 31 and the target sheet work together to hit the top of the two-way trigger cap 32 and fire, or the firing pin 42 will also fire after a while. Under the action of the forward momentum, the needle will move forward and hit the bottom of the two-way trigger cap 32 of the trigger mechanism 3 to ignite, and the tip of the firing pin 42 will be smashed, and the detonation products, especially high-temperature and high-pressure gas and solid particles, will be fired along the strike. The needle 42 passes down through the central channel, passes through its central channel along the axis of the spring, and directly triggers the two-way input flame detonator 62 at the upper end of the isolation ball 61 in the alignment state, and the two-way input flame detonator 62 at the upper end of the isolation ball 61 detonates the two-way input flame detonator at the lower end of the isolation ball 61. Input the flame detonator 62, then detonate the detonator 9, and the fuze completes the normal detonation process of firing. The diameter of the two-way trigger cap 32 is relatively large, so that the fuze wipes the ground and explodes and the reliability of firing at a large angle of attack can be realized. The inertial triggering effect of the centrifugal ball-spring-firing pin mechanism is redundant with the impact triggering action, and it plays a backup role when the head impact ignition fails, which also improves the firing reliability.

弹丸在空中飞行时若未命中目标,当弹丸转速衰减到一定程度时(落地前),弹簧44的抗力会大于离心球43通过击针架41底部自毁斜面所产生的轴向反作用力,离心球43会收回到击针径向孔内,弹簧44推动击针42向前运动戳击双向触发火帽32,实现预定的空中自毁功能,确保地面安全。If the projectile misses the target while flying in the air, when the rotational speed of the projectile decays to a certain degree (before landing), the resistance force of the spring 44 will be greater than the axial reaction force generated by the centrifugal ball 43 passing through the self-destructing slope at the bottom of the firing pin frame 41. The ball 43 can be withdrawn in the radial hole of the firing pin, and the spring 44 promotes the firing pin 42 to move forward and poke the two-way firing cap 32, so as to realize the predetermined self-destruct function in the air and ensure the safety on the ground.

如果球转子保险意外未能对正,则在预定的触发作用或自毁时,双向触发火帽32的爆轰产物会通过隔离球61与其腔室间的间隙以及隔离球61上预设的径向传火孔,可靠引燃未对正的隔离球61中的双向输入火焰雷管62,隔离球61中的两个双向输入火焰雷管62也会相互殉爆,但不会引爆传爆管,此时引信丧失正常起爆功能,进入绝火状态,从而保证由于引信瞎火所形成的未爆弹药的爆炸物处理安全性。If the ball rotor safety fails to align accidentally, then during predetermined trigger action or self-destruction, the detonation product of the two-way trigger cap 32 will pass through the gap between the isolation ball 61 and its chamber and the preset diameter on the isolation ball 61. To the fire transmission hole, reliably ignite the two-way input flame detonator 62 in the isolation ball 61 that is not aligned, and the two two-way input flame detonators 62 in the isolation ball 61 will also be killed each other, but the detonator can not be detonated. When the fuze loses its normal detonation function, it enters the flameout state, thereby ensuring the safety of explosive disposal of unexploded ammunition formed by fuze misfiring.

如果保险环5因意外未能张开,则引信会丧失自毁性能。但由于双向触发火帽仍能炸碎击针尖部向下可靠传火,所以引信的碰击触发功能和绝火功能仍然存在,不受影响。If the safety ring 5 fails to open due to an accident, the fuze will lose its self-destruct performance. However, since the two-way trigger cap can still smash the tip of the firing needle and transmit the fire reliably downward, the impact trigger function and fire-stop function of the fuze still exist and are not affected.

Claims (4)

1. The utility model provides a safe rotatory bullet warhead machinery of small-bore bullet trigger fuse of explosive treatment after blind fire which characterized in that: the explosion-proof and delay-relieving safety mechanism comprises a body (1), an upper body (2), a collision type triggering mechanism (3), a centrifugal self-destruction and inertia triggering mechanism (4), a centrifugal safety mechanism of the centrifugal self-destruction and inertia triggering mechanism (4), namely a safety ring (5), an explosion-proof and delay-relieving safety mechanism (6), a recoil safety mechanism of the explosion-proof and delay-relieving safety mechanism (6), namely a safety pin-shearing pin mechanism (7), a centrifugal safety mechanism of the explosion-proof and delay-relieving safety mechanism (6), namely a split ring (8) and a booster tube (9); the upper body (2) and the body (1) are coaxially arranged, the upper part of the body (1) stretches into the lower part of the upper body (2) and is fixedly connected with the lower part of the upper body to form a fuse shell, and the impact type triggering mechanism (3), the centrifugal self-destruction and inertial triggering mechanism (4) and the flameproof and delay releasing safety mechanism (6) are sequentially arranged in the fuse shell from top to bottom; the explosion-proof and delay releasing safety mechanism (6) is restrained on the body (1) by the safety pin-shearing pin mechanism (7); the safety ring (5) is sleeved on the top surface of the centrifugal self-destruction and inertia trigger mechanism (4); the opening ring (8) is arranged on the flameproof and delay relief mechanism (6), and the detonating tube (9) is positioned at the bottom of the fuze shell and is close to the flameproof and delay relief mechanism (6); the method is characterized in that:
the impact type trigger mechanism (3) mainly comprises a moistureproof sheet (31) and a bidirectional trigger fire cap (32) which are arranged in the upper body (2); the centrifugal self-destruction and inertia trigger mechanism (4) mainly comprises a needle striking frame (41), a needle striking (42), a spring (44) and a plurality of centrifugal balls (43); the firing pin (42) points upwards to the bidirectional trigger fire cap (32), the safety ring (5) is sleeved on the firing pin (42), the firing pin frame (41), the safety ring (5) and the upper body (2) jointly realize centrifugal safety of the centrifugal self-destruction and inertia trigger mechanism (4), and the flameproof and delay release safety mechanism (6) mainly comprises a separation ball (61), a ball seat (63) and two bidirectional input flame detonators (62); the safety pin-shear pin mechanism (7) mainly comprises a safety pin (71), a shear pin (72) and a seal plug (73); the sealing plug (73) is cylindrical and is coaxially arranged with the shearing pin (72); the isolating ball (61) is provided with a transverse through hole passing through the center of the ball, and two bidirectional input flame detonators (62) are symmetrically arranged in the transverse through hole; the top end of the isolation ball (61) is provided with a first blind hole coaxial with the fuze; a safety pin (71) is arranged in the first blind hole; the shear pin (72) vertically penetrates through the safety pin (71) to extend into the isolation ball (61), the safety pin (71) is fixed in a first blind hole on the isolation ball (61), and meanwhile, the upward extending part of the safety pin (71) extends into the central hole of the body (1), so that the rotation of the isolation ball (61) is restrained; the sealing plug (73) is fixed on the isolation ball (61) through point riveting, and seals the shearing pin (72); the isolation ball (61), the safety pin (71), the shearing pin (72) and the sealing plug (73) jointly realize the squat safety of the explosion-proof and delay relief mechanism (6); the split ring (8) is clamped at the outer side of the crescent notch at the lower end of the isolation ball (61), so that the rotation of the isolation ball (61), namely a ball rotor, is limited, and the other safety of the isolation ball (61), namely centrifugal safety, is realized; the ball seat (63) and the opening ring (8) jointly realize centrifugal insurance of the explosion-proof and delay releasing insurance mechanism (6); the explosion-proof and delay releasing safety mechanism (6) is arranged at the rear end of the explosion-proof and delay releasing safety mechanism, and the upper part of the explosion-proof and delay releasing safety mechanism (9) extends into the body (1) and is fixedly connected with the ball seat (63);
seven step through holes with different inner diameters are formed downwards along the central axis of the upper body (2), and a first step hole, a second step hole, a third step hole, a fourth step hole, a fifth step hole, a sixth step hole and a seventh step hole are sequentially formed from top to bottom; the diameter of the bidirectional trigger fire cap (32) of the impact type trigger mechanism (3) is 60-90% of the diameter of the second step hole in the upper body (2), when the fuze hits a target with a large or small landing angle, the reliability of the firing and floor scrubbing actions with the large landing angle can be improved, and the trigger sensitivity can be improved;
the safety pin (71) is provided with an axial stepped blind hole and two transverse through holes, the axial stepped blind hole is downwards and coaxially arranged along the top end of the safety pin (71), the aperture of the axial stepped blind hole along the upper part of the safety pin (71) is larger than that of the lower part, the two transverse through holes are axially distributed and respectively penetrate through the lower stepped holes with small diameters to form a fire transmission channel, so that bidirectional triggering of the flame of the fire cap is facilitated to be input from the top end of the safety pin (71) and transmitted to the inner side end of a bidirectional input flame detonator (62) in the isolation ball (61), and the fuse achieves fire insulation under the state of not releasing the fuse, thereby ensuring the explosive treatment safety after the fuse is in a fire failure;
the isolating ball (61) is symmetrically provided with 2 fire transmission holes leading to the center in a plane which passes through the center of the isolating ball and is perpendicular to the axis of the bidirectional input flame detonator, and the bidirectional trigger flame cap flame is transmitted to the outer side end of the bidirectional input flame detonator (62) in the isolating ball (61) by means of a plurality of axial eccentric fire transmission holes on the body (1) and gaps between the ball rotor component and the cavity of the ball rotor component, so that the fuse realizes fire insulation under the state of not releasing the fuse, and the explosive treatment safety after the fuse is out of fire is ensured.
2. A post-blind explosive handling safe small caliber rotary bullet mechanical triggering fuse according to claim 1, wherein: the safety ring (5) and the firing pin frame (41) are coaxially arranged from top to bottom, the safety ring (5) forms clearance fit between the firing pin frame (41) and the bottom surface of the fifth-order hole of the upper body (2), and the safety ring (5) can be thrown away under the action of centrifugal force so as to release the firing pin (42).
3. A post-blind explosive handling safe small caliber rotary bullet mechanical triggering fuse according to claim 1, wherein: the centrifugal ball (43) is a ceramic ball.
4. A post-blind explosive handling safe small bore rotary warhead mechanical triggering fuse according to claim 3, wherein: the outer wall of the lower part of the ball seat (63) is provided with a circle of flange, the bottom end of the body (1) is inwardly closed to the flange to fix the ball seat (63), so that the connection strength between the ball seat (63) and the body (1) is improved, and the structural integrity and the safety under the superposition effect of the emission impact overload and the explosion-proof internal pressure are ensured.
CN202210084491.7A 2022-01-25 2022-01-25 Small-caliber rotary bullet mechanical trigger fuze with safe explosive treatment after misfire Active CN114370796B (en)

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CN118758120B (en) * 2024-06-07 2025-10-21 南京理工大学 A self-destructive high-reliability warhead mechanical trigger fuze for a grenade launcher

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