In order to meet the technical requirements for precise control of the arming time in high-dynamic environments and ammunition safety, this article proposes a silicon-based MEMS safety system force-electric fusion design scheme for small-caliber ammunition platforms. Modeling and computational analysis are conducted on the sensitive units in S&A. A mechanical equilibrium model is established to study the centrifugal overload and electromagnetic forces, followed by verification through dynamic simulation. The design aimed to achieve the safety and arming control of the MEMS security system using a plate-type electromagnetic driving scheme. A low driving energy electromagnetic coil model is designed, and the driving capability of the electromagnetic coil is analyzed. It is found that under the condition of a distance of 0.1mm and 8V, a driving force of 270mN could be achieved. Considering the complex operating conditions during the arming process, a low damping model is developed for the arming degree of the MEMS arming device. After the design is completed, the S&A and electromagnetic coils are processed and prepared using deep silicon etching and microcasting techniques. Finally, threshold verification is conducted for the recoil and centrifugal arming mechanisms of the S&A. The designed S&A ultimately achieved a size of less than or equal to circle divide 20mm.

针对现役小口径炮弹引信大着角碰靶发火率偏低、未爆弹存在隐患的可靠性与安全性问题,开展现役小口径炮弹引信大着角碰靶发火机构响应特性研究.建立了大着角碰靶发火机构的动力学模型,得到了发火机构作用的简易判据,基于有限元数值模拟方法,模拟了不同着速、着角、滚转角度及靶板厚度多工况下大着角碰靶发火机构的动态响应过程,数值模型有效性通过实弹试验对比验证.分析结果表明,着发球珠随机滚转角度为大着角碰靶时影响发火机构功能可靠的重要因素之一;随滚转角度增大,发火击针感受到轴向合力的幅值越小、时间越滞后,不利于大着角碰靶发火机构可靠作用;同时研究发现随着角、靶板厚度的增加,出现了导套"卡住"发火击针的故障模式.

The battlefield rapid pressure hemostatic microsystem maximizes hemostasis efficiency. Battlefield wound has the characteristics of rapid blood loss and irregular surface, which needs to be treated in a very short time. The existing rapid hemostasis method has poor efficiency and no sterilization and disinfection effect. Therefore, we reported a wound pressure hemostatic microsystem based on gas generated by rapid chemical reaction. Before the device is used, the two chemicals in the device are isolated. During hemostasis, the flexible device is applied to the wound surface, and the two chemicals in the device are mixed and chemically reacted. And the large amount of gas generated by the reaction causes the balloon in the device to expand and exert lateral and longitudinal pressure on the surface of the wound, so that the wound quickly closed. At the same time, the drug storage unit in the device is under pressure to release the drug to the wound surface. In addition, the chemical reaction of the device has an endothermic effect, which can rapidly cool the wound surface. The lateral and longitudinal pressures of the flexible microsystem in the process of hemostasis were analyzed by numerical simulation. In the experiment, the maximum longitudinal pressure reached 270mmHg, meeting the requirements of surface wound hemostasis.

A low-driving energy and bistable recoverable MEMS safety and arming device (S&A), based on microcasting technology and deep silicon etching technology, is proposed to meet safety system requirements. A force–electromagnetic combination solution is constructed for the Si MEMS S&A, with parameters and strength verified, ultimately achieving an S&A size of (13 × 13 × 0.4) mm. Additionally, a low-driving energy U-shaped electromagnetic coil (USEC) model is designed using microcasting technology, and an electrical–magnetic–mechanical coupling mathematical model is established to explore the relationship between design parameters and driving capacity and reliability. With a driving power of 8 V/0.5 A, the model achieves a stable electromagnetic driving force of 15 mN with a travel distance of 0.5 mm. Finally, the fabrication and testing of the USEC and S&A are carried out, with driving capability and S&A disarming ability tests conducted to verify the feasibility of the system design. Compared to the existing S&A, this scheme has the advantages of low-driving energy, recoverability, fast response speed, and strong adaptability.

The physical self-destruction of an information storage chip (ISC) driven by a detonation wave generated using energetic materials is an important method to ensure the security of key core information. To solve the related problems of high electrostatic sensitivity, poor overcurrent capability, and easy erroneous triggering, a bistable OFF- ON actuator (BO-OA)-based energetic material information self-destruction microsystem is proposed based on a fusible alloy. First, the BO-OA model based on the fusible alloy is constructed. By performing a finite element numerical analysis and experimenting, the response time of the Bi-Sn alloy with a continuous temperature rise from 22 °C to 138 °C is obtained. Second, a model of the energetic material dose and detonation wave transmission in an air domain is constructed. An analysis using LS-DYNA software indicates that copper azide can produce GPa-level stress waves in a millimeter-level air domain to realize ISC physical self-destruction. Finally, through bulk silicon processing and in situ reaction of the energetic materials, self-destruction module preparation and functional integration are realized. Experiments and simulations show that when driven by a 12 V electromotive force, the BO-OA reaches the fusible alloy melting point of 138 °C within $320 \mu \text{s}$ and can realize electrical conduction within $33 \mu \text{s}$ . 0.45 mg of copper azide can generate a 3.27 GPa detonation wave within $5.9 \mu \text{s}$ at 0.3 mm in the air domain to realize the physical self-destruction of the ISC. This scheme can greatly improve the safety of the energetic materials and provides strong practical value for information self-destruction.

Information self-destruction modules (ISDMs) play a vital role in the information security area. In this paper, an ISDM based on the integration of a micro-thermoelectric generation mechanism (M-TEGM) with energetic materials (EMs) is proposed. On the basis of energy conversion relationship, an open-loop electromotive force is induced, and this energy will drive the EMs to release the detonation wave and realize information storage module self-destruction. During the tests, under the temperature difference (100 K), the open-loop electromotive force (3.86 V) is induced by the M-TEGM and can drive the EMs (0.37 mg copper azide) to generate a detonation wave (GPa) in 3.4 μs, which can physically destroy the information storage modules. This ISDM has advantages that include rapid response times, low drive energy compared with traditional information security technology.

The lack of anti-strong electromagnetic interference ability of fuze has become an important aspect restricting the effectiveness of weapon system. Taking a certain type of fuze as an example, this paper analyzes the coupling mechanism of ultra-wide spectrum transient strong electromagnetic pulse to the fuze, analyzes the action mode of aperture coupling and field line coupling, establishes the mathematical model of space electromagnetic field, and then simulates the effect of aperture coupling and field line coupling of the fuze by using CST Microwave Studio software. It is concluded that the strongest coupling state is when the polarization direction of the electromagnetic field is parallel to the axis of the fuze. Combined with the theory and simulation, the ultra-wide spectrum transient strong electromagnetic pulse simulation system is used to conduct the strong electromagnetic pulse irradiation test, and the electromagnetic pulse effect threshold is obtained. It is concluded that the effect threshold leading to communication failure is about 27~40kV/m, which provides a certain theoretical and experimental basis for fuse strong electromagnetic protection.

A microelectromechanical systems (MEMS) solid-state logic control chip with three layers—diversion layer, control layer, and substrate layer—is designed to satisfy fuse miniaturization and integration requirements. A mathematical model is established according to the heat conduction equation, and the limit conditions of different structures are presented. The finite element multi-physical field simulation method is used to simulate the size and the action voltage of the diversion layer of the control chip. Based on the surface silicon process, fuse processing, and testing with the MEMS solid-state fuse-logic control chip, a diversion layer constant current, maximum current resistance test, and a control layer of different bridge area sizes, the bridge area size is 200 × 30 μm, and the minimum electrical explosion voltage is 23.6 V. The theoretical calculation results at 20 V and 100 μF demonstrate that the capacitor energy is insufficient to support the complete vaporization of the bridge area, but can be partially vaporized, consistent with the experimental results.

With the aim of achieving the combat technical requirements of super-quick (SQ) initiation and reliable self-destruction (SD) of a small-caliber projectile fuze, this paper describes a high-functional-density integrated (HFDI) inertial switch based on the “ON-OFF” state transition (i.e., almost no terminal ballistic motion). The reliable state switching of the HFDI inertial switch is studied via elastic–plastic mechanics and verified via both simulations and experiments. The theoretical and simulation results indicate that the designed switch can achieve the “OFF-ON” state transition in the internal ballistic system, and the switch can achieve the “ON-OFF” state transition in the simulated terminal ballistic system within 8 μs or complete the “ON-OFF” state transition as the rotary speed sharply decreases. The experimental results based on the anti-target method show the switch achieves the “ON-OFF” state transition on the μs scale, which is consistent with the simulation results. Compared with the switches currently used in small-caliber projectile fuzes, the HFDI inertial switch integrates more functions and reduces the height by about 44%.

目的 厘清某型引信在贮存14 a后的失效模式,研究温度周期性交变对引信及其薄弱零件的影响.方法 利用ANSYS workbench软件,建立基于时间硬化的蠕变仿真方法.以某型引信为研究对象,开展周期性温度交变的蠕变仿真,根据仿真计算结果和实物的对比分析,找出薄弱零件,分析其老化失效模式.结果 在每个周期内环境温度循环条件下,仿真时长设定为 14 a,结果显示,引信整体蠕变应变率超过1%,平均压紧应力下降 21%,松弛稳定性变弱,密封性在一定程度上变差.其中,引信电机外壳、电机扇叶、底部线路对接板为薄弱零件,容易发生失效行为.结论 引信贮存在典型西南湿热环境14 a后,周期性温度交变应力将导致引信出现缺陷,缺陷集中在电机外壳、电机扇叶、底部线路对接板处,应重点对这些部位进行防护.

Information self-destruction devices represent the last protective net available to realize information security. The self-destruction device proposed here can generate GPa-level detonation waves through the explosion of energetic materials and these waves can cause irreversible damage to information storage chips. A self-destruction model consisting of three types of nichrome (Ni-Cr) bridge initiators with copper azide explosive elements was first established. The output energy of the self-destruction device and the electrical explosion delay time were obtained using an electrical explosion test system. The relationships between the different copper azide dosages and the assembly gap between the explosive and the target chip with the detonation wave pressure were obtained using LS-DYNA software. The detonation wave pressure can reach 3.4 GPa when the dosage is 0.4 mg and the assembly gap is 0.1 mm, and this pressure can cause damage to the target chip. The response time of the energetic micro self-destruction device was subsequently measured to be 23.65 μs using an optical probe. In summary, the micro-self-destruction device proposed in this paper offers advantages that include low structural size, fast self-destruction response times, and high energy-conversion ability, and it has strong application prospects in the information security protection field.

Detonation waves released by energetic materials provide an important means of physical self-destruction (Psd) for information storage chips (ISCs) in the information insurance field and offer advantages that include a rapid response and low driving energy. The high electrical sensitivity of energetic materials means that they are easily triggered by leakage currents and electrostatic forces. Therefore, a Psd module based on a graphene-based insurance actuator heterogeneously integrated with energetic materials is proposed. First, the force–balance relation between the electrostatic van der Waals force and the elastic recovery force of the insurance actuator’s graphene electrode is established to realize physical isolation and an electrical interconnection between the energetic materials and the peripheral electrical systems. Second, a numerical analysis of the detonation wave stress of the energetic materials in the air domain is performed, and the copper azide dosage required to achieve reliable ISC Psd is obtained. Third, the insurance actuator is prepared via graphene thin film processing and copper azide is prepared via an in situ reaction. The experimental results show that the energetic materials proposed can release physical isolation within 14 μs and can achieve ISC Psd under the application of a voltage signal (4.4–4.65 V). Copper azide (0.45–0.52 mg) can achieve physical damage over an ISC area (23.37–35.84 mm2) within an assembly gap (0.05–0.25 mm) between copper azide and ISC. The proposed method has high applicability for information insurance.

A self-destruction module for information storage equipment (ISE) that releases a detonation wave via energetic materials (EMs) is discussed. The module uses an energy-grooming actuator (EGA) to isolate EMs from external electronic systems to improve security. The response time of removing electrical constraint for EMs, the stress transferring of detonation wave in air domain and the response time of ISE physical self-destruction are obtained via COMSOL, LS-DYNA, the module function integration is realized by stacked graphene and platinum films and in-situ copper azide synthesis. During tests, the response time of removing electrical constraint for EMs by EGA was 0.942 ms. When a voltage pulse (below 5.5 V) exploded the EMs, the detonation wave was generated under 61.8-63.2 mu s to destroy the ISE. Overall, ISE physical self-destruction was realized with a lower driving energy, a fast response time and security control for the EMs. The module has potential applications for information security.

Implantable drug-delivery microsystems have the capacity to locally meet therapeutic requirements by maximizing local drug efficacy and minimizing potential side effects. The internal organs of the human body including the esophagus, gastrointestinal tract, and respiratory tract, with anfractuos contours, all manifest with endoluminal lesions often located in a curved or zigzag area. The ability of localized drug delivery for these organs using existing therapeutic modalities is limited. Spraying a drug onto these areas and using the adhesion and water absorption properties of the drug powder to attach to lesion areas can provide effective treatment. This study aimed to report the development and application of microsystems based on microshockwave delivery of drugs. The devices comprised a warhead-like shell with a powder placed at the head of the device and a flexible rod that could be inserted at the tail. These devices had the capacity to deposit drugs on mucous membranes in curved or zigzag areas of organs in the body. The explosive impact characteristics of the device during drug delivery were analyzed by numerical simulation. In the experiment of drug delivery in pig intestines, we described the biosafety and drug delivery capacity of the system. We anticipate that such microsystems could be applied to a range of endoluminal diseases in curved or zigzag regions of the human body while maximizing the on-target effects of drugs.