IN-SITU FREEZING MACHINING METHOD FOR INTEGRATED THIN-WALLED ARRAY STRUCTURE

    公开(公告)号:US20240075568A1

    公开(公告)日:2024-03-07

    申请号:US17785657

    申请日:2021-11-17

    CPC classification number: B23Q3/086 B23Q3/065 B23Q2703/10

    Abstract: The present invention proposes an in-situ freezing machining method for an integrated thin-walled array structure. In the method, the area among cups is cut off first; then, the outer walls of a cup array are machined; and finally, water filling and freezing are carried out, and in-situ freezing machining of the inner walls of the cup array is carried out. Then, hoisting and turning over are carried out, and the area among cavities is cut off; then, the outer walls of a cavity array are machined; and finally, water filling and freezing are carried out, and in-situ freezing machining of the inner walls of the cavity array is carried out. The method realizes in-situ freezing clamping of workpieces, avoids error accumulation caused by repeated installation of a fixture, and can refrigerate efficiently, suppress ambient and cutting thermal interference, and ensure the stability of freezing fixture.

    Structure multi-dimensional loading test system considering real complex boundary conditions

    公开(公告)号:US11913913B2

    公开(公告)日:2024-02-27

    申请号:US17617867

    申请日:2021-06-30

    CPC classification number: G01N3/10 G01M7/02 G01N3/04

    Abstract: A structure multi-dimensional loading test system considering real complex boundary conditions considering real complex boundary conditions comprises a main part of machine, a base part, a hydraulic power supply and a control system. The system can simulate the load borne by a structure in a real working environment better and more accurately, realize multi-dimensional loading of the structure with six degrees of freedom in space and provide more real and valuable experimental data for the research on damage of reinforced concrete materials, components and structures under the action of an earthquake, and the research results will help researchers further reveal the damage mechanism of reinforced concrete structures, put forward the corresponding damage criteria and develop the corresponding seismic design methods.

    A METHOD FOR PREPARING A SUBMICRO/NANO-POROUS NIO/APATITE-TYPE LANTHANUM SILICATE ANODE FUNCTIONAL LAYER

    公开(公告)号:US20240039003A1

    公开(公告)日:2024-02-01

    申请号:US18268495

    申请日:2022-01-11

    Inventor: Li XIANG Yuhang WEI

    CPC classification number: H01M4/8657 H01M4/8835 H01M2008/1293

    Abstract: This invention relates to a method for preparing of a submicro/nano-porous NiO/apatite-type lanthanum silicate anode functional layer. In the method a functional layer nanopowder, ethyl cellulose and terpineol are added into a rotary evaporation bottle containing anhydrous ethanol, and a suspension obtained after mixing is dispersed ultrasonically. The anhydrous ethanol in the suspension is removed by a rotary evaporator. When the suspension becomes a viscous paste, the paste is taken out and ground to complete the preparation of a functional layer paste. The functional layer paste is applied onto an anode substrate by screen printing, and 3 sublayers are screen printed. After dried, the sublayers are heat treated and sintered. The heating rate, the cooling rate and the holding time are controlled in the heating and cooling processes to complete the preparation of the anode functional layer.

    HOLE MAKING TOOL FOR ARAMID FIBER-REINFORCED PLASTIC AND DESIGN METHOD THEREOF

    公开(公告)号:US20240024993A1

    公开(公告)日:2024-01-25

    申请号:US18350921

    申请日:2023-07-12

    CPC classification number: B23P15/32 B23P15/46

    Abstract: The present invention belongs to the technical field of composite material processing, and relates to a hole making tool for aramid fiber-reinforced plastic and a design method thereof. The drill bit has a step reversed point angle structure, which can reduce a trust force during drilling and effectively cut off a high toughness aramid fiber, thus to improve the hole making quality of an AFRP-related component. It is proved that the new tool can significantly improve the hole making quality of an AFRP component, improve the service life and safety degree, and greatly reduce the processing cost. Therefore, the present invention has a broad application prospect in the fields of aerospace, military industries and civil application.

    STEADY FLOW PREDICTION METHOD IN PLANE CASCADE BASED ON GENERATIVE ADVERSARIAL NETWORK

    公开(公告)号:US20240012965A1

    公开(公告)日:2024-01-11

    申请号:US17920167

    申请日:2021-12-27

    CPC classification number: G06F30/27 G06F30/28

    Abstract: A steady flow prediction method in a plane cascade based on a generative adversarial network is provided. Firstly, CFD simulation experimental data in the plane cascade are preprocessed, and a test dataset and a training dataset are divided from the simulation experimental data. Then, an Encoding-Forecasting network module, a deep convolutional network module and a generative adversarial network prediction model are constructed successively. Finally, prediction is conducted on test set data: the test set data is preprocessed in the same manner, and data dimensions are adjusted according to input requirements of a saved optimal prediction model; and flow field images in the plane cascade at an inlet attack angle of 10° are obtained through the prediction model. The present invention can effectively avoid the problem of limited measurement range of sensors in an axial flow compressor, and the prediction result is highly consistent with the calculation result of CFD.

    Method of high energy efficiency unmanned aerial vehicle (UAV) green data acquisition system

    公开(公告)号:US11858627B2

    公开(公告)日:2024-01-02

    申请号:US17619487

    申请日:2021-06-10

    CPC classification number: B64C39/024 G05B17/02 B64U2201/10

    Abstract: A design method of a high energy efficiency unmanned aerial vehicle (UAV) green data acquisition system belongs to the technical field of data acquisition and optimization for UAV uplink communication. Firstly, a system optimization objective is constructed; and in a uplink communication network of a single UAV and ground sensors, the UAV receives data periodically. Secondly, according to a constructed optimization problem, the optimization objective is maximization of EE({W},{t},{S}). Finally, an original problem is decomposed into two approximate concave-convex fractional sub-problem based on a block coordinate descent method and a successive convex approximation technique to obtain a suboptimal solution; an overall iterative algorithm is proposed: in each iteration, by solving the sub-problems, wake-up scheduling S, time slot t and UAV trajectory W are alternately optimized. The solution obtained in each iteration is used as the input of next iteration. The present invention can jointly optimize the UAV flight trajectory, the sensor wake-up scheduling and the flight time slot to ensure that the transmission information amount and energy consumption of the sensors satisfy system requirements, while maximizing the energy efficiency of the system.

    AERO-ENGINE SURGE ACTIVE CONTROL SYSTEM BASED ON FUZZY CONTROLLER SWITCHING

    公开(公告)号:US20230392556A1

    公开(公告)日:2023-12-07

    申请号:US18032898

    申请日:2021-06-04

    CPC classification number: F02C9/16 F04D27/02 G06N7/02 F05D2270/707

    Abstract: An aero-engine surge active control system based on fuzzy controller switching is provided. The present invention selects a basic controller with the most appropriate current state for switching control according to the operating state of a compressor based on the principle of fuzzy switching, and can realize large-range, adaptive and performance-optimized surge active control. Controllers designed by the present invention realize large-range surge active control through fuzzy switching, so that the effective operating ranges of the controllers are expanded and the reliability of the controllers is improved. The designed controllers can be applied to the active control of surge caused by various causes, so that the adaptability of the controllers is improved and is closer to the actual operating condition of the engine. Some optimization indexes are added in the design process of the controllers, which can realize optimal control under corresponding optimization objectives.

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