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    30 July 2023, Volume 44 Issue 7
    Electronic edition of this issue
    Electronic edition of this issue
    2023, 44(7):  0. 
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    Contents
    Contents
    2023, 44(7):  1. 
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    Accurate Internal Ballistics Modeling and Testing of Rodless High Pressure Pneumatic Catapult Considering Leakage
    WANG Xueqin, MA Wuning, MA Dawei, WANG Shanglong, ZHANG Zhendong
    2023, 44(7):  1867-1880.  doi:10.12382/bgxb.2022.0172
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    The rodless high-pressure pneumatic catapult experiences a certain amount of leakage due to the inherent structure of the opening. In this study, a prototype leakage test is designed and conducted. Based on the standard dry air thermodynamic equation of state fitted by the experimental data, the leakage rate is calculated and compared under the hypothesis of ideal gas and real gas. The empirical formula of leakage rate varying with pressure and stroke is fitted. An accurate interior ballistic model considering dynamic leakage, real gas effects, and the real valve opening law is established. The two working conditions with and without leakage are solved numerically and compared. Then, the variation laws of thermodynamic parameters and load motion parameters in the ejection process with leakage are analyzed in detail and compared with the ejection test data and fluid simulation results. The results show that the leakage rate calculated under ideal gas assumption is about 4% lower than that under real gas assumption. Moreover, the calculated leakage rate shall not exceed 4%/s. The calculation results of the accurate interior ballistic model considering leakage are basically consistent with the ejection test data and the fluid simulation results, indicating high calculation accuracy.

    Unmanned Aerial Vehicle Cluster Cooperative Guidance Technology Based on Conflict Trigger Mechanism
    HAN Yu, SONG Tao, ZHENG Duo, LIU Xin
    2023, 44(7):  1881-1895.  doi:10.12382/bgxb.2022.0152
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    Cooperative strike is an important mode to improve the overall combat effectiveness of aircraft clusters. To address the problem of mutual collision or interference in the process of cooperative attack on targets by dense aircraft clusters, a typical mission scenario model of multi-target cooperative attack is established, and the maneuver law in the process of cooperative movement of aircraft cluster is revealed. Then, based on the optimal theory of utility function, the coordinated optimal maneuver strategy of aircraft cluster to avoid collision is studied, ensuring collision avoidance between aircrafts. Considering the time/space synchronous arrival constraint in aircraft cluster cooperative guidance, a multi-constraint cooperative guidance strategy based on time control is adopted, which meets the requirements of arrival time and miss distance at the same time. On this basis, a cooperative collision avoidance mechanism based on conflict triggering is introduced, and a cooperative adjustment strategy that considers collision avoidance and cooperative attack is proposed. And a cooperative guidance method satisfying collision avoidance and spatio-temporal synchronization is obtained. The simulation results show that the proposed aircraft cluster cooperative guidance method considering collision avoidance constraints ensures safe distance constraints between aircrafts and has strong aircraft cluster cooperative time control ability and high guidance accuracy. It requires less iterative calculation, reduces the requirements for airborne processors, and provides a solution to the collision avoidance problem in aircraft cluster cooperative attack. This method has strong engineering application value.

    Analysis of Interior Ballistic Characteristics of Conical Three-Dimensional Charge Column Under Lateral Overload
    TIAN Zhongliang, LI Junwei, HE Ye, XU Tuanwei, DING Miao, WANG Ningfei
    2023, 44(7):  1896-1907.  doi:10.12382/bgxb.2022.0162
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    The occurrence of internal ballistic anomalies during high-altitude missile maneuvering can result in flight mission failures. To analyze the abnormal mechanism of internal ballistics, the internal ballistics characteristics of motor under lateral overload were studied. Experimental measurements of the burning rate of HTPB ternary propellant under overload conditions were conducted, and a burning rate model of the propellant under overload was established. Based on this model, the non-uniform combustion surface retreat of cone-hole grain was simulated. The interior ballistic characteristics of cone-hole grain under three overload modes, namely, full lateral overload, short-time constant lateral overload, and short-time oscillation lateral overload, were studied. The results show that lateral overload increases the pressure in the combustion chamber and accelerates the exposure time of the insulation layer. The pressure oscillation frequency produced by oscillating overload is consistent with that of overload oscillation. Instantaneous lateral overload leads to a transitional increase in combustion chamber pressure. Under 100g overload, the pressure increases by about 8%, the overload disappears, and the pressure plummets. When the lateral overload time interval is constant, stable pressure conditions are advantageous for missile maneuvering under overload conditions.

    Research Status of Surface Damage in Rails for Electromagnetic Launchers
    ZHANG Jiawei, LU Junyong, TAN Sai, LI Bai, ZHANG Yongsheng
    2023, 44(7):  1908-1919.  doi:10.12382/bgxb.2022.0128
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    Rails and armatures are critical components in electromagnetic rail launchers that convert electrical energy into kinetic energy. Due to high current, powerful magnetic fields, high relative speeds, intense heat, and immense pressure, these components inevitably experience material loss. This article provides a comprehensive review of domestic and international research conducted over the past few decades on surface damage to rails in electromagnetic rail launchers. The surface damage is mainly categorized into four types: grooving, gouging, transition ablation, and erosion wear. Each type exhibits distinct characteristics and occurs at different locations, resulting in varying degrees of material loss. Based on this, scientists put forward theories and models to explain and confirm the observed damage through experiments. To mitigate rail damage, structure, material and drive current waveform are modified. However, due to the deeply coupled system, extreme working conditions, limited measurements and the lack of valid experiments, few research about wear erosion has been reported. To understand the damage mechanism better, develop effective optimization strategies and unravel the process of damage evolution, the measurement and modeling methods should be improved.

    Novel Adaptive Robust Roll Control Method Based on LESO
    WANG Zhilin, WANG Jiang, QI Qi, FAN Shipeng
    2023, 44(7):  1920-1929.  doi:10.12382/bgxb.2022.0106
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    The roll channel mathematical model of missiles flying at large angles of attack is characterized by severe nonlinearity, instability, multivariable coupling, and uncertainty. An adaptive robust control method is designed to solve the issues. A linear extended state observer (LESO) is used to estimate aerodynamic nonlinear perturbations based on finite information of the missile. A novel adaptive sliding mode control law is employed together with a LESO to estimate and compensate disturbance online. The rapid adjustment of adaptive parameters can ensure the stability of the system and shorten the response time, thereby allowing for rapid convergence of the roll angle and roll angle rate, weakening chattering, and enhancing disturbance rejection ability. The simulation results show that the proposed control method has significant improvements in rapidity and robustness compared to traditional linear methods and also exhibits fault-tolerant control ability in typical fault handling scenarios.

    Modeling and Simulation of Pulsed Laser Ignition Based on Thermal Ignition Mechanism
    CHEN Huimin, GUO Pengyu, LIU Chengyi, YANG Xu
    2023, 44(7):  1930-1937.  doi:10.12382/bgxb.2022.0125
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    To study the influence of electrical parameters on the ignition delay time in the pulsed laser ignition system, a pulsed laser ignition simulation model is designed, and especially, the modeling and simulation of the pulsed laser excitation stage and the laser ignition stage are performed. Taking BNCP detonating agent as an example, an electrical simulation software is used to simulate the laser emission process of the semiconductor laser excited by the laser driver circuit in the simulation of the pulsed laser excitation stage. By changing the values of the energy storage capacitor and the resistance of the laser discharge circuit, the corresponding laser output power at different times is obtained. In the the laser ignition stage, the laser output power corresponding to different simulation steps obtained in the pulsed laser excitation stage is imported into the finite element simulation software, and the laser ignition delay time law corresponding to different electrical parameters is solved. The simulation results show that: the average output power of the laser increases and the ignition delay time is shortened by increasing the energy storage capacitance in the driver circuit; increasing circuit resistance leads to the reduction of the peak output power of the laser and the increase of the ignition delay time. The experiments has verified the simulation model. The established pulsed laser ignition model can provide theoretical reference for the hardware design of the pulsed laser ignition system.

    Dynamic Response of Honeycomb Sandwich Plate with Negative Poisson’s Ratio under Penetration
    LIU Yan, WANG Baichuan, YAN Junbo, YAN Zichen, SHI Zhenqing, HUANG Fenglei
    2023, 44(7):  1938-1953.  doi:10.12382/bgxb.2022.0208
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    With the intensification of war, projectiles pose a serious threat to high-value facilities, and improving the anti penetration performance of various facilities is particularly crucial. Study the anti penetration performance of 3D printed honeycomb sandwich structure through ballistic gun experiments and numerical simulation methods. Compare and analyze the dynamic response of 7 specimens through ballistic impact experiments. The sandwich structure consists of a Q345 steel top plate, a carbon fiber reinforced composite (CFRP) back plate, and an aluminum alloy honeycomb core layer. Three honeycomb core configurations are compared experimentally: foam aluminum, positive hexagon and concave hexagon with Negative Poisson’s ratio effect. The results show that compared with the honeycomb sandwich structure with foam aluminum core and positive Poisson’s ratio, the honeycomb sandwich structure with Negative Poisson’s ratio has lower residual velocity and stronger penetration resistance. The dynamic response process of honeycomb sandwich structure with Negative Poisson’s ratio is obtained through numerical simulation. Through parameter analysis, the influence of cell inflection angle, back plate thickness and back plate type on the anti penetration performance of honeycomb sandwich structures with Negative Poisson’s ratio is further obtained. The numerical research results indicate that all three factors have a certain impact on the anti penetration performance of honeycomb sandwich structures. The non dominated genetic algorithm is used to optimize the honeycomb sandwich structure with initial Negative Poisson’s ratio, and its mass is reduced by 21.1% under the premise of ensuring the same ballistic limit speed.

    Research on Impact Resistance and Failure Modes of Pyramid Sandwich Panel Subjected to Underwater Explosion
    LI Furong, RONG Jili, WANG Xi, CHEN Zichao, WEI Zhenqian, ZHAO Zitong
    2023, 44(7):  1954-1965.  doi:10.12382/bgxb.2022.0147
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    Studying the dynamic response and impact resistance of metal sandwich panels subjected to underwater explosion is of great significance for improving the protection capability of ships. An equivalent loading device for underwater explosion impact experiment is used for the pyramid lattice sandwich panel, and the dynamic response law of the panel is obtained. The Abaqus coupled Eulerian-Lagrangian method is adopted to calculate the impact process, and the error between the calculated results and the experimental data is small. The validity of the simulation is verified. The three-stage characteristics of the dynamic response of the pyramid sandwich panel is acquired. The impact resistance of the sandwich panel is evaluated through the deformation of the back plate and the plastic energy absorption of the core layer. The different failure modes of the sandwich panels with different parameters are analyzed by simulations. The results show that: when the total thickness of the sandwich panel is constant, the impact resistance of the sandwich panel with a thinner front panel and a thicker back panel is stronger; the failure modes of the core layer composed of pyramid rods with different thicknesses vary, but the deformations of the back panels are similar; the plastic energy absorption ratio of the core layer decreases with the increase of impact load; the multi-objective optimization method is used to optimize the parameters of the core layer. The conclusion is that the impact resistance of the optimized sandwich panel is significantly improved, and the optimization results have guiding significance for the design of pyramid sandwich panels.

    Numerical Simulation of the Effect of Curved Surface Reflectors on the External Flow Field of Pulse Detonation Engine
    KANG Yang, LI Ning, HUANG Xiaolong, ZHANG Junshan, WENG Chunsheng
    2023, 44(7):  1966-1977.  doi:10.12382/bgxb.2022.0261
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    To explore a technical way to effectively suppress the propagation of high-power detonation noise generated by a pulse detonation engine to the key parts of the engine head, the external flow field of pulse detonation engine equipped with three kinds of reflectors,which are ellipsoidal reflector,parabolic reflector and conical reflector,are numerically simulated by using the space-time conservation element and solution element method.The results show that the three types of reflectors have varying effects on the detonation noise due to their distinct reflection characteristics onthe rotating surface.The ellipsoidal reflector converges the reflected wave towards the axis of the reflector.The parabolic reflector approximately parallelizes the reflected waves downstream, whilethe conical reflector does not produce the reflected wave lagging behind the direct wave,which strengthens the direct wave and propagates downstream together.

    A Pulse Shaper Model for Hopkinson Pressure Bars
    MIAO Feichao, ZHANG Xiangrong, LI Dongwei, JIANG Tao, ZHOU Lin
    2023, 44(7):  1978-1984.  doi:10.12382/bgxb.2022.0517
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    Adding a pulse shaper for Hopkinson bars is an important method to adjust the profile of incident pulses and accurately measure the dynamic mechanical properties of explosives. To predict the complete profile of incident pulses after incorporating the pulse shaper, the wave propagation process in the striker-pulse shaper-incident bar system is analyzed based on the stress wave theory. A unified governing equation predicting the loading-unloading process of pulse shapers is obtained using the superposition principle of waves. Consequently, a general pulse shaper model is developed. The one-dimensional stress-strain relationship of T2 pure copper is obtained by using Hopkinson pressure bar and pulse shaper experiments. The model predicts the profile of incident pulses of single pulse shaper and dual pulse shaper experiments, and analyzes the deformation characteristics of the pulse shaper under various conditions. The results show that the pulse shaper model is able to predict the complete profile of incident pulses, including the unloading range. The profile of incident pulses predicted by the model is in good agreement with the experimental results, indicating the validity of the model and the high accuracy of the calibrated parameters.

    Electrostatic Spraying Preparation and Performance of Nanocomposite Energetic Material RDX@NGEC
    LI Qiang, CHEN Ling, GAN Huaiyin, ZHU Yongchen, HE Weidong
    2023, 44(7):  1985-1992.  doi:10.12382/bgxb.2022.0228
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    In this study, RDX and nitrate glycerol ether cellulose (NGEC) were selected as the raw materials, and acetone as the solvent to prepare precursor solution. A novel RDX@NGEC core-shell structured nanocomposite energetic material was prepared using the electrostatic spray drying technology. The structure and composition of the composite were characterized by scanning electron microscopy (SEM), Fourier transform infrared spectroscopy (FTIR), X-ray diffraction (XRD), and Raman spectroscopy (Raman). Differential scanning calorimetry (DSC) was carried out to analyzed the thermal decomposition reaction kinetics and thermodynamics of the composites using the Kissinger and the Ozawa methods. In addition, impact and friction sensitivity experiments were carried out to study the mechanical properties of the composite. The results showed that the particle size of the composite RDX@NGEC prepared by electrostatic spray drying technology exhibited uniform distribution and an even spherical morphology, forming a typical core-shell structure. Besides, compared with the raw material RDX, the activation energy (Ea) of the composite increased from 122.05kJ/mol to 131.70kJ /mol, with Ea gradually increasing as the NGEC content increased. The addition of an appropriate amount of NGEC significantly increased the critical temperature of thermal explosion for the composite from 513.696K to 524.989K, thereby enhancing the safety performance.

    Synthesis of Polycrystalline Diamond from Carbon Nanotubes Using Direct Detonation Method
    SHANG Shiyuan, TONG Yi, WANG Zhichao, HUANG Fenglei
    2023, 44(7):  1993-2001.  doi:10.12382/bgxb.2022.0268
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    To study the phase transformation mechanism of carbon nanotubes during detonation, synthesis experiments were carried out using direct detonation method with carbon nanotubes as the additional carbon source. The detonation product was chemically purified. X-ray diffraction (XRD) was used to characterize the purified product, and it was found that the product consisted of diamond. The purified product was characterized by transmission electron microscopy (TEM) and scanning electron microscopy (SEM), and after in-depth analysis, it was found that the carbon nanotubes transformed into diamond through solid in situ phase change during the detonation process. Multiple cores were observed on a carbon nanotube to form crystals at the same time. When adjacent crystals came into contact, crystal boundaries were formed, limiting growth in specific directions to form polycrystals. Depending on the circumferential, radial and axial dimensions of the formed diamond crystals, as well as the number and position of the crystals in the formed polycrystals, polycrystalline diamond particles of different shapes such as tubes, flakes, and blocks were obtained.

    Quantitative Characterization of Thermal Damage Evolution of RDX-Based PBX Explosives
    XU Liji, DUAN Zhuoping, BAI Zhiling, WU Yanqing, HUANG Fenglei
    2023, 44(7):  2002-2013.  doi:10.12382/bgxb.2022.0296
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    The thermal damaged features and evolutionbehaviors of high explosives (HEs) play a crucial roleintheir safety. In this study, micro-scale computerized tomography (Micro-CT)technology and quantitative image analysis were used to systematicallyinvestigatethe mesostructural defects in RDX-based PBXs after thermal damage, including defect geometrical features,quantitative statistics, and formation mechanism. The samples were heated untilreaching the critical ignition temperature. Significant changes in mesostructural morphology of the thermal damaged samples were observed,resulting in typical damage characteristics such asmechanical debonding of RDX particle-binder interfaces,meso-pores formed by thermal decomposition of RDX particles,and channels through interconnection of interfacial debonding. The variation of several key parameters with temperature used to characterize thermal damages were quantitatively analyzed,including porosity,pore size distribution,specific surface area,sphericity, and ubiquitiformal complexity.Through qualitative and quantitative observation of the mesostucture, the thermal damage mode and evolution of RDX-based PBXs with increasing temperature were obtained. This study provides physical basisfor investigating the sensitization mechanism of thermal damage on explosive ignition response and establishing a ubiquitiformal model for the ignition reaction evolution of damaged explosives.

    Structure and Properties of Four-hole Polydopamine-coated Gun Propellant
    CUI Libao, YANG Zhao, DING Yajun, ZHOU Jie, XIAO Zhongliang
    2023, 44(7):  2014-2022.  doi:10.12382/bgxb.2022.0283
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    To address issues such as regressive burning and deterrent migration in oblate spherical propellants, we developed a novel four-hole gun propellant coated with polydopamine (PDA) through self-polymerization of dopamine (DA) on the propellant’s surface. The microstructure, thermodynamics, and combustion performance of the propellant were analyzed using scanning electron microscope, Raman spectrometer, thermogravimetric analyzer, and closed bomb vessel. The results show that PDA can be well coated on the propellant’s surface, and the particle size of PDA can reach 5μm. The surface coating effect of PDA on the propellant can significantly improve the incremental combustion of propellant, resulting in a 42.05% decrease in initial burning activity (Li), a 60.25% decrease in maximum burning activity (Lm), and a 53.90% increase in burning progressivity index. After accelerated aging, the combustion performance of the PDA-coated four-hole gun propellant changed slightly. After accelerated aging at 55℃ for 30 days, the Li and Lm only increased by 1.69% and 0.59%, respectively, indicating high long-storage stability for the PDA-coated four-hole gun propellant.

    Design and Synthesis of Light-Curable Energetic Binders
    YUAN Jing, LIN Xiangyang, PENG Yang, TAN Cheng
    2023, 44(7):  2023-2032.  doi:10.12382/bgxb.2022.0315
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    To meet the demand of solid propellants with complex structuresin additive manufacturing and energy, epichlorohydrin was used as the raw material for cationic ring opening polymerization by boron trifluoride ethyl ether initiator system, azide reaction by sodium azide, isocyanate compound, and hydroxyethyl acrylate nucleophilic addition reaction.Three kinds of energetic binderprepolymers with light-curing properties were synthesized.The structures of the products were characterized by Fourier infrared spectroscopy, nuclear magnetic resonance hydrogen spectroscopy, and gel permeation chromatography. The thermal stability and glass transition temperature of the prepolymers were tested by high and low temperature differential scanning calorimetry analysis.The thermal polymerization onset temperature of the prepolymers was 140℃, the thermal decomposition onset temperature was 220℃, and the glass transition temperatures were -43.8℃, -52.7℃ and -55.8℃, respectively. The three prepolymers were compounded with diluent and photoinitiator to obtain a liquid photosensitive resin, and the cured film was further prepared and tested for mechanical properties, in which the tensile strength of GAP/IPDI/HEA-PUA cured film was 0.38MPa and the elongation at break was 470%, meeting the basic mechanical property requirements of adhesives for propellants, which is a new type of UV-curable energetic binders with practical applications.

    Study of Screw Drive Failure Mechanisms in a Flight Aid Carrier
    DU Yonggang, WANG Xuesong, WAN Zhihua
    2023, 44(7):  2033-2040.  doi:10.12382/bgxb.2022.0242
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    The friction and temperature-rise mechanisms in the screw transmission of a flight aid carrier have received limited research attention, focusing primarily on structural strength rather than thermal-mechanical coupling. This study aims to address this gap by developing a thermal-mechanical coupling model to simulate the thermal and mechanical characteristics of the contact surface using accurate parameters. By analyzing stress, temperature rise, and the law between temperature and the friction coefficient, this study reveals the failure mechanism of the transmission. The numerical simulation results show that the temperature of the contact surface can quickly rise to 454.3℃, and the contact stress can reach 699.4MPa during high-speed friction. The elevated temperature weakens the material strength of the contact surface, while the high-speed sliding fiction causes continuous damage to the contact surface. The calculation results align with observed fault phenomena and provide a theoretical basis for the engineering application of this transmission technology.

    Impact of Molecular Viscosity Variation on the Analytical Wall Function
    WANG Xinguang, CHEN Qi, WAN Zhao, GAO Xiaocheng, YAN Zhenguo
    2023, 44(7):  2041-2052.  doi:10.12382/bgxb.2022.0370
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    Based on the characteristics of hypersonic turbulent boundary layers, such as temperature, density, and laminar viscosity, the modified analytical wall function is improved to include the alternative definition of the dimensionless wall distance using variables at the edge of the viscous sublayer and the parabolic and hyperbolic variations of viscosity coefficients in the sublayer, named as para-MAWF and hyper-MAWF, respectively. Hypersonic shock boundary layer interactions are used to verify these two wall functions, which are compared with the Lauder-Sharma k-ε using fine meshes and the modified analytical wall function (MAWF). The results show that the proposed wall functions will increase the accuracy of temperature and molecular viscosity variation in the viscous sublayer compared to results by the original MAWF. As a result, the predicted wall heat-flux aligns more closely with experimental measurements, especially in the separation region. The heat flux predicted by hyperbolic analytical wall function agrees better with the experimental value. Considering that the difference of the numerical results predicted by the two wall functions is less than 5%, the hyperbolic wall function is recommended for hypersonic flows due to its simpler formulation.

    Effects of Injection Mass Flow Rate and Position on the Performance of Partial Admission Axial Impulse Turbines with Jet Impingement Cooling
    ZHI Ruoyang, LUO Kai, WANG Hanwei, QIN Kan
    2023, 44(7):  2053-2065.  doi:10.12382/bgxb.2022.0305
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    High turbine inlet temperatures can enhance turbine performance, but they often require additional cooling methods due to limitations in disk materials.However, the compact size and short blades of turbines used in underwater vehicles can hardly accommodate complex cooling channels.To address this issue, partial admission axial impulse turbines can utilize seawater as the cooling medium.An alternative way is jet impingement cooling. In this study, a three-dimensional computational fluid dynamics method is proposed to investigate the performance of partial admission axial impulse turbines with different injection mass flow rates and positions.The results show that the maximum temperature of the front and back disks decreases by 40.1% and 28.6%, respectively, and the maximum thermal stress of the disk decreases by 33.8% when the axial injection mass flow is 0.2kg/s.When 0.2kg/s axial water is injected with 0.1kg/s radial water, the maximum temperature of the front and back disks decreases by 46.2% and 33.8%, respectively, and the maximum thermal stress of the disk decreases by 36.7%.The efficiency of turbine and the temperature and thermal stress of the front and back disks are negatively correlated with the cooling water mass flow rate in the axial direction under the same radial water flow. These findings can provide insights into the jet impingement cooling strategy for partial admission axial impulse turbines.

    Numerical Simulation of Ditching of a Twin-Fuselage Aircraft
    SUN Xiaoyuan, DENG Feng, LIU Xueqiang
    2023, 44(7):  2066-2079.  doi:10.12382/bgxb.2022.0111
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    Aircraft ditching is a trans-media process, namely the process of the aircraft going from air to water. The exploration of the physical phenomena and dynamic characteristics of trans-media objects can provide insights into the research on airplane ditching and water entry of trans-media vehicles. The ditching process of a twin-fuselage aircraft is studied. The unsteady Reynolds-averaged Navier-Stokes (URANS) method, VOF method, dynamic grid technique and 6DOF model are used to numerically simulate the ditching process. Based on the numerical validation of the 3D plate water-skipping experiment, the effect of pitch angle on the ditching process of the twin-fuselage aircraft is analyzed. The numerical results show that: the larger the pitch angle, the greater the peak vertical velocity of the aircraft, the greater the vertical displacement and the smaller the change in pitch deflection angle during the ditching process; the horizontal velocity of the airplane decreases faster and the horizontal displacement of the aircraft is smaller as the pitch angle decreases; when the aircraft ditches with a 6° pitch angle, it is subjected to the largest horizontal force, and therefore stops in the shortest time; when the aircraft ditches with a 14° pitch angle, the vertical force is the largest, and meanwhile the submerged displacement is the largest.

    Numerical Study of Condensation Heat Transfer of Steam with Non-condensable Gas
    GUO Qing, LUO Kai, GENG Shaohang, QIN Kan
    2023, 44(7):  2080-2091.  doi:10.12382/bgxb.2022.0225
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    In order to study the performance of a high-pressure heat exchanger in an underwater semi-closed cycle power system, we establish a numerical model to analyze the condensation process of steam containing a significant proportion of non-condensable gas under high pressure. The model is verified through a specific experiment, and we conduct simulations of the gas flow channel in the heat exchanger under different working conditions, taking gravity into consideration. The results show that due to the gravity, the liquid film thicknesses at the top and bottom of the pipe are not uniform, resulting in swirling flow within the gas phase. These two effects lead to uneven heat transfer characteristics in the pipe. Additionally, the flow velocity increases with the decreasing pipe diameter, causing a rise in the Reynolds number and a thinning of the bottom liquid film. This contributes to heat transfer. The increased flow velocity also reduces the effect of gravity, reducing the disparity in heat transfer intensity between the top and bottom sections of the pipe. Under the working conditions in this paper, even with a reduced total heat transfer area, reducing the pipe diameter remains conducive to the improvement of the total heat transfer power. The maximum temperature error between the experimental and simulated results is 19.5%. The conclusions contribute to the design of high-pressure heat exchangers in underwater semi-closed cycle power systems.

    Robust Event-triggered Adaptive Pitch Attitude Control for Underwater Gliders with Actuator Faults
    MIN Boxu, GAO Jian, JING Anyan, CHEN Yimin, WANG Jiarun, PAN Guang
    2023, 44(7):  2092-2100.  doi:10.12382/bgxb.2022.0234
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    To ensure robustness against model uncertainties and actuator faults while reducing control energy consumption, this paper proposes a robust adaptive fault-tolerant scheme using the event-triggered input technique for the pitch attitude control of underwater gliders. Based on the backstepping method, the dynamic surface control technique is employed to avoid calulating the derivation of the virtual control law. Model uncertainties, external disturbances, and actuator faults are compensated as a whole using a RBF-NN that takes advantage of historical input and output data. A relative-threshold event-triggered condition is designed to avoid continuous updating of the control law. Finally, the Lyapunov stability theory is used to ensure the SGUUB of the closed-loop signals. The simulation results confirm that the proposed scheme has robust control performance and can better reduce control energy consumption and communication resource occupation.

    Simulation Analysis and Experimental Verification of the Electrical Energy Power System for Underwater Vehicles
    ZHANG Jian, SHEN Lin
    2023, 44(7):  2101-2113.  doi:10.12382/bgxb.2022.0198
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    The complexity of the electromagnetic and electromechanical coupling relationships in the Electrical Energy Power System (EEPS) poses challenges for analytical studies. To address the challenges, this paper focuses on the EEPS of future generation vessels with a cascade AC-DC-AC topology. A mathematical model for the EEPS is derived, and a parameter extraction method is provided. The complexity-accuracy relationship of each component model has been fully considered to meet the needs of real-time simulation. An electromechanical integration simulation model is constructed with a set of diesel engine and a controller, PMSM, converter, propeller, and vessel as a whole. Simulation studies of typical working conditions are carried out respectively, and the simulation results are compared with the results of ground experiment and real cruising test of the EEPS with an underwater vehicle. A good agreement between simulation model and the real EEPS has been verified by the test results. Based on the simulation platform built in this paper, the time of bench test and real cruising verification can be shortened, and the R&D costs of the EEPS can be reduced significantly.

    Underwater Multi-target Detection Method Based on Hough Transform Track-before-detect Technique
    WANG Xuemin, YU Hongbo, ZHANG Xiangyu, AN Shu, LI Wenhai
    2023, 44(7):  2114-2121.  doi:10.12382/bgxb.2022.0290
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    The development of unmanned underwater vehicle cluster poses a great challenge to underwater target detection. Aiming at the detection problem of underwater multiple low detectable targets and the need for concealment detection, an underwater multi-target passive detection method based on Hough transform tracking before detection technique was proposed. Firstly, a passive detection model of unmanned underwater vehicle was constructed by using aviation passive sonar buoy array. Secondly, the adaptive correlation cross location technology of multiple passive sonar buoys was used to realize data preprocessing before concealment detection. Finally, the two-threshold randomized Hough transform track-before-detect algorithm was adopted to achieve effective detection of multi-targets with low detectability in high noise density conditions. Simulation results show that this method has good detection performance under the conditions of low signal-to-noise ratio with intersecting point traces of multiple targets.

    Underwater Polarization Image Restoration Method Using Optimal Multi-Parameters Reconstruction
    CHEN Xiongfeng, RUAN Chi
    2023, 44(7):  2122-2131.  doi:10.12382/bgxb.2022.0343
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    Underwater imaging in high turbidity conditions often suffers from issues such as low resolution, reduced contrast, and overall poor image quality. Classical methods for underwater image polarization restoration require the selection of a background point without any target, making them inapplicable in certain scenarios. In order to solve this problem, the method of underwater polarization image restoration based on optimal multi-parameter reconstruction is proposed. Based on the classical underwater imaging physical model, the transmittance is divided into absorption and backscattering coefficients. By calculating the polarization degree of the underwater image using the Stokes vector, two target points are selected. The optimal reconstruction values of reflectivity, absorption coefficient and backscattering coefficient of two target points are obtained by optimizing the restored image. By using the optimized parameters to remove the backscattered light and recover the signal light lost due to absorption from the underwater image, the polarization restoration of the underwater image is realized. Two no-reference image quality assessment indexes are employed as quantitative indexes. Compared with other methods, experiments based on different turbidity and different targets show that this method can effectively restore the degraded underwater image, especially in the case of high turbidity. This method is expected to be applied to enhance optical imaging clarity of underwater vehicles and facilitate subsequent target detection.

    Analysis and Prediction of Surface Topographyin Peripheral Milling Based on Workpiece Vibration and Milling-Tool Structure
    LIU Yang, QIN Guohua, WU Zhuxi, LOU Weida, LAI Xiaochun
    2023, 44(7):  2132-2146.  doi:10.12382/bgxb.2022.0289
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    In the milling process, vibrations can lead to variations in the structure of machined parts, significantly influencing the machining quality of the finished surface. Therefore, investigating the milling formation method of the machined surface morphology is of great significance for predicting surface roughness and selecting reasonable machining parameters. First, by equivalently transforming the contact mode between workpiece and fixture into a linear spring damping system, the vibration differential equation of the workpiece is derived for the milling process by using the energy method. By using the coordinate transformation method, the modal analysis solution method is proposed for the vibration differential equations with constraint conditions to obtain the workpiece position deviation. Secondly, a method for determining the tool contact point and establishing the motion trajectory equation for the cutting edge in peripheral milling is presented. This enables the development of a discrete algorithm for surface topography by incorporating the workpiece position deviation. Experimental validations are conducted to verify the proposed algorithm for peripheral milling topography simulation. The results show that the maximum surface roughness error is 7.56% without considering the fixturing layout vibration, whereas the maximum contact force error is no more than 12% with fixturing layout vibration. Compared with calculations without clamping vibration considered, the calculation accuracy of contact force and surface roughness considering clamping vibration are improved by 3% and 4.72% (up milling)/3.00% (down milling), respectively.

    Data-Driven Online Monitoring and System Development of Multi-scale Targets in the Grinding Process
    LÜ Lishu, DENG Zhaohui, LIU Tao, TENG Hongzhao, ZHUO Rongjin
    2023, 44(7):  2147-2161.  doi:10.12382/bgxb.2022.0187
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    Grinding is a key process in high value-added industries, such as national defense and military,aerospace,and automobiles.The realization of intelligent acquisition and monitoring of the grinding process is essentialto improve product quality and ensure safe production.Aiming at the problems in the data collection of the existing grinding process,such as the single target of the monitoring plan,insufficient integration,and difficulty in obtaining complete grinding information,a multi-scale target integrated monitoring system framework is established for the grinding process.A multi-scale target correlation monitoring model including quality,efficiency,status, and a green multi-scale is constructed,which maps monitoring variables and monitoring targets. The multi-sensor acquisition fusion and grinding result monitoring feature mapping method is proposed,and an intelligent acquisition and monitoring system for the grinding process is developed.The system is used for real-time data acquisition and monitoring of a high-speed electric spindle bearing grinding process.The measurement results show that the developed monitoring system can effectively and accurately predict the grinding time,grinding energy consumption,grinding state, and surface roughness during the grinding process.

    Vehicle Trajectory Prediction Method Based on Graph Models and Attention Mechanism
    LIAN Jing, DING Rongqi, LI Linhui, WANG Xuecheng, ZHOU Yafu
    2023, 44(7):  2162-2170.  doi:10.12382/bgxb.2022.0117
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    In order to improve the accuracy of vehicle trajectory prediction in structured road scenes, a multimodal trajectory prediction method based on graph models and attention mechanism is proposed. For the purpose of modeling road environment characteristics, vehicle motion characteristics and characteristics of interaction between vehicles, the lane graph and vehicle interaction graph are constructed. Environment-vehicle feature fusion is completed by stacked attention modules, so as to realize the unification of static and dynamic features of traffic scenes. The final predicted trajectories and corresponding probabilities are obtained through a two-branch decoding module. The Argoverse dataset is used to train and validate the proposed method. The experimental results show that the proposed method achieves excellent performance of motion prediction in structured road scenes. The prediction accuracy is better than the current mainstream methods.

    A Ground Combat Weapon Target Assignment Model Based on Shooting Effectiveness and Improved Artificial Bee Colony Algorithm
    CHU Kaixuan, CHANG Tianqing, ZHANG Lei
    2023, 44(7):  2171-2183.  doi:10.12382/bgxb.2022.0294
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    This paper presents a ground combat Weapon Target Assignment (WTA) model that enhances the validity of firepower allocation for ground units. The model incorporates shooting effectiveness as a key factor and formulates an optimization function considering the benefits and costs of attack decisions on the battlefield. By assessing the threat level of targets, the model determines the urgency and necessity of an attack. By evaluating the battlefield value of targets, it calculates the threat reduction value. The model predicts enemy attack plans and estimates weapon losses based on the probability of damage inflicted by targets. It quantifies the value of ammunition by comparing forces with ammunition reserves. By analyzing the tactical intentions of both sides, the necessity of a strike is weighed against the cost of tactical intent exposure. To solve that WTA model, an improved artificial bee colony algorithm is proposed. This algorithm improves the search directionality of the algorithm and the ability to escape local optimum at the end of each iteration. At the same time, a population initialization strategy based on the Weapon Target Combination Library is adopted to improve the initial population quality of the algorithm. Simulation examples show the soundness of the proposed model and the advantages of the improved algorithm in terms of convergence speed, convergence accuracy, and robustness.

    Output Feedback Control for Launch Platform Using Neural Network Observer and Output Constraint
    SONG Qiuyu, HU Jian, YAO Jianyong, BAI Yanchun, YANG Zhengyin
    2023, 44(7):  2184-2196.  doi:10.12382/bgxb.2022.0229
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    A launch platform, driven by two permanent magnet synchronous motors, is used to launch kinetic energy loads. However, the platform often faces strong parameter uncertainties and unknown external disturbances, such as air impact, during practical operation. These factors can greatly reduce the platform’s tracking accuracy. To solve this problem, an output feedback controller based on adaptive neural network observer with output constraints is proposed for high-precision motion control of the launch platform. The controller uses ESO to estimate system parameter uncertainties in the system, and uses the velocity value of the system to design relevant control parameters to achieve the purpose of output feedback control. An improved Spline CMAC neural network is designed to estimate the unknown disturbances in the system. Feedforward compensation technique is used to compensate parameter uncertainty and time-varying disturbance. Considering the output constraints of the launch platform in practice, the control rate is designed by using the obstacle Lyapunov function analysis method. The stability of the system is also proved. The simulation and experimental results demonstrate that the proposed composite controller can achieve uniform final bounded stability of the system with good tracking performance and strong anti-interference capability while considering the output constraints. The proposed approach represents a great improvement over traditional control methods.

    Language Identification in Battlefield Environments
    HUA Yingjie, LIU Jing, SHAO Yubin, DUO Lin
    2023, 44(7):  2197-2206.  doi:10.12382/bgxb.2022.0367
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    To achieve accurate language identification in battlefield environments, a language identification method based on spectrogram gray transformation is proposed. Bandpass filtering is introduced based on the distribution characteristics of speech information and noise information in the spectrogram under battlefield noise conditions. Logarithmic gray spectrogram is extracted in line with human auditory characteristics. An automatic color adjustment algorithm is used to suppress noise information and enhance language information on the spectrogram, and a residual neural network model is used for training and identification. Experimental results show that compared with linear gray spectrogram features, the recognition accuracy is improved by 46% in the -10dB Predator fighter cockpit noise environment. In other noise environments, the recognition performance is also greatly improved.