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Method for designing gaps of end straight sections of diagonal few-leaf main springs and auxiliary springs

ActiveCN105526290AExact design valueReliable design valueGeometric CADLeaf springsEngineeringDesign values
The invention relates to a method for designing gaps of end straight sections of diagonal few-leaf main springs and auxiliary springs, and belongs to the technical field of suspension steel plate springs. The method includes determining endpoint deformation coefficients of the various main springs and deformation coefficients G<x-CD> of contact points of the end straight sections of the N main springs and the auxiliary springs according to structure sizes and elastic modulus of the various diagonal variable-section main springs; acquiring endpoint force F<N> of the N main springs according to acting load of the auxiliary springs and the endpoint deformation coefficients of the various main springs; designing the main and auxiliary spring gaps between contact points of the end straight sections of the main springs and the auxiliary springs according to the thicknesses h<2> of roots of the N main springs, the endpoint force F<N> and the deformation coefficients G<x-CD>. The method has the advantages that as known from simulation verification, design values of the gaps of the end straight sections of the diagonal few-leaf variable-section main springs and the auxiliary springs can be accurately and reliably obtained by the aid of the method, and accordingly the product design level and performance and the vehicle ride comfort can be improved; the design and experiment costs can be reduced, and the product development speeds can be increased.
Owner:山东恒日悬架弹簧股份有限公司

Direct3D 11-based 3D graphics rendering engine

The invention discloses a Direct3D 11-based 3D graphics rendering engine, which comprises a master control module and a plurality of functional sub modules, wherein the functional sub modules comprise a matrix module, a view point module, a head-up display module, a multi-character set word module, a 3D primitive base class module, a poster board module, a mesh model module, a smoke and rain and snow particle system module, a halo special effect calculation module, and a soft shadow calculation module. According to the default rendering process for each frame, the soft shadow module is firstly called, and with the illumination direction as the view point, the depth information of each primitive in the rendering scene is calculated; then, with the sight line of eyes of an observer as the angle, each primitive in the scene is rendered to the surface, an original scene view is obtained, highlight information is obtained at the same time, and the actual lighting effects of each pixel point is obtained according to the depth information and the illumination calculation result; and finally, in combination with the first sum depth information and the highlight information, highlight aura special effect post-processing on the illumination is carried out on the original scene view, and the final single-frame rendering graph is obtained.
Owner:钱进 +3

Software-as-a-service (SaaS) application generation and deployment supporting method and device

ActiveCN102135883AStrong development independenceSupport personalized customizationTransmissionSpecific program execution arrangementsPortletSoftware engineering
The invention relates to a software-as-a-service (SaaS) application generation and deployment supporting method and an SaaS application generation and deployment supporting device, which aim to solve the problems of the conventional SaaS software generation and release. The method comprises the following steps that: A, an independent software vendor obtains a development license of an SaaS application generation and deployment device by registration to become an official development user; B, the independent software vendor downloads a generation and testing tool kit by an independent software vendor (ISV) portlet, and integrates the tool kit into a local generation environment to make the local generation environment become an SaaS application description generation device for rapidly generating SaaS application; C, the independent software vendor performs application generation by utilizing the SaaS application description generation device, and uploads the description of the application into an SaaS application deployment device; D, the SaaS application deployment device adds bottom-layer realization to the application generated by the ISV to deploy the application into the SaaS application supporting multiple tenants and personalized customization; and E, the tenants try on, rent and customize the SaaS application.
Owner:SHANDONG UNIV

Auxiliary spring work load checking method of non end part contact type end part strengthened few-leaf main and auxiliary springs

The invention relates to an auxiliary spring work load checking method of a non end part contact type end part strengthened few-leaf main and auxiliary springs belonging to the suspension steel plate spring technical field. According to the method of the invention, firstly, according to the structure size and the elastic modulus of each end part strengthened few-leaf cross-section variable main spring, the end point deformation coefficient Gx-Ei and the half rigidity KMi of each main spring, and the deformation coefficient Gx-BC at the contact point of the Nth main spring and an auxiliary spring on a parabolic segment can be determined; then, according to the half rigidity KMi of each main spring, the thickness h2 of a root straight section, the Gx-BC of the Nth main spring and a main and auxiliary spring interval Delta design value, the auxiliary spring work load of the non end part contact type end part strengthened few-leaf cross-section variable main and auxiliary springs is checked. Through the emulation proof, in adoption of the method of the invention, the accurate and reliable auxiliary spring work load checking value can be obtained; therefore, the design levels and performances of the few-leaf cross-section variable main and auxiliary springs and the smoothness of a vehicle are improved; moreover, the design and test cost is saved; and the product development speed is accelerated.
Owner:SHANDONG AUTOMOBILE SPRING FACTORY ZIBO CO LTD

Testing system and method for electric part of power system for weak hybrid electric vehicle

The invention discloses a testing system and a method for electric part of power system for weak hybrid electric vehicle, and the system comprises a BSG motor module provided with a BSG motor and a BSG motor controller; a dynamometer module provided with a dynamometer, a measuring and control instrument and a torque and speed sensor, and a transducer or an inverter; a power module provided with a power storage battery, a battery management system, a program control power supply and a program control power supply controller; an auxiliary electric system load simulation module provided with a DC / DC convertor and an auxiliary electric system load; an upper computer module. The method adopts the half object simulation principle, the dynamometer simulates the engine for doing test to the BSG motor module and does the service life test for the electric part of weak hybrid power system at different working conditions that the BSG motor starts the engine, the engine drives the BSG motor for generating, regenerative braking, idle parking while the battery drives the load, the system and method can reduce the test cost, shorten the test period for vehicle performance and raise the developing speed for product.
Owner:GUANGDONG MECHANICAL & ELECTRICAL COLLEGE

Method for designing few-leaf oblique line type variable-section main springs in gaps between oblique line segments and auxiliary spring

The invention relates to a method for designing few-leaf oblique line type variable-section main springs in the gaps between oblique line segments and an auxiliary spring, and belongs to the technical field of suspension steel plate springs. According to the structural sizes and the elasticity moduli of the oblique line type variable-section main springs, the endpoint deformation coefficient Gx-Di of each main spring and the deformation coefficient Gx-BC of the Nth main spring at the contact point of the corresponding oblique line segment and the auxiliary spring are determined first; then, according to the required auxiliary spring acting load design value and the endpoint deformation coefficient Gx-Di of each main spring, endpoint force FN of the Nth main spring is obtained; then, according to the thickness h of the root straight section of the Nth main spring, the Gx-BC and the FN, main spring and auxiliary spring gaps between the oblique line segment of the main springs and the contact point of the auxiliary spring are designed. Through simulation verification, it can be known that the main and auxiliary spring gap design value meeting the auxiliary spring acting load requirement can be obtained by means of the method, and the product design level, product performance and vehicle smoothness are improved. Meanwhile, design and testing cost is reduced, and product development speed is increased.
Owner:JIANGSU HAIHONG MACHINERY MFG

Processing method and system for updating and changing interface theme of WinCE product

The invention discloses a processing method and system for updating and changing the interface theme of a WinCE product. The method comprises the following steps: when the WinCE application program is developed, separating an interface presentation layer from a business logic layer by adopting a design mode of separating interface layout from program codes, adopting segmented modular programming in the interface presentation layer, and adopting independent XML extensible markup language to describe the elements of the interface theme for each module; when a user interface is required to be amended, writing and amending xml (extensible markup language) interface configuration files relevant to the modules, controlling and realizing the loading engine of the interface element according to the amended contents, mapping the label elements in the amended xml (extensible markup language) interface configuration files into internal storage objects, and automatically generating the user interface layout of the corresponding amended modules. The interface layout and the program codes are separated, so that the problem that the application program interface cannot be freely customized by a client is solved, and simultaneously, the development efficiency of the application program is improved.
Owner:SHENZHEN APICAL TECH CO LTD

Development, testing, operation and maintenance integration system, deployment and full-quantity and incremental updating method

The invention discloses a development, testing, operation and maintenance integration system, deployment and a full-quantity and incremental updating method. The system comprises an automatic deployment module and an automatic updating module, wherein the automatic deployment module configures corresponding backup controller information and load balancer information according to mirror images in a mirror image warehouse at a developer end, automatically generates an application deployment script, and automatically / manually spreads the application deployment script to a testing deployment end; the testing deployment end automatically deploys an application to the testing, operation and maintenance environment by executing an application deployment script file, the automatic updating module updates an application program according to the mirror images in the mirror image warehouse at the developer end, generates an update pack file in a full-quantity or incremental updating mode and automatically / manually spreads the update pack file to the testing deployment end; the testing deployment end automatically deploys the updated application to the testing, operation and maintenance environment by executing the update pack file. Cooperation obstacles among development, testing, operation and maintenance are reduced, the cooperation efficiency is improved, application deployment processes are simplified, a developer pays close attention to business flows, and the requirement for technological levels of operation and maintenance staffs is lowered.
Owner:SHANDONG UNIV

Design method for few parabolic type variable cross-section main spring end and auxiliary spring gaps

The invention relates to a design method for few parabolic type variable cross-section main spring end and auxiliary spring gaps, and belongs to the technical field of suspension steel plate springs. The method comprises the steps that according to the structural size and elastic modulus of each parabolic type variable cross-section main spring, an end point deformation coefficient of each main spring and a deformation coefficient Gx-CD of the Nth main spring on the contact point of an auxiliary spring and the end straight section; then, according to the auxiliary spring acting load design requirement value and the end point deformation coefficient of each main spring, the endpoint force FN of the Nth main spring is obtained; then, according to the thickness h2 of the straight section at the root of the Nth main spring, the FN and the Gx-CD, the main and auxiliary gaps between the contact points of the auxiliary springs and the end straight sections of the main springs are designed. According to simulation verification, the accurate and reliable main and auxiliary spring gap design values can be obtained by means of the method, the auxiliary spring acting load design requirement is met, and the product design level and performance and the vehicle ride comfort are improved; meanwhile, the product development speed is increased, and the design and testing expenses are lowered.
Owner:慕贝尔汽车部件(太仓)有限公司

Software development platform

The invention discloses a software development platform, which belongs to the technical field of software development. The platform is a PaaS platform of an enterprise level. Enterprises can be helpedto go to DevOps practice. A business capability supermarket is constructed, an enterprise is enabled to get rid of complex infrastructure management and more concentrate on business research and development and delivery, an internet distributed architecture is adopted for design and development, normalization, standardization and internet technicalization of development and operation and maintenance processes are realized through a PaaS platform, and the development efficiency and the operation and maintenance capability are improved; design is carried out based on a micro-service architecture, high reliability and high expansion capability are taken as basic attributes, and use scenes such as single-point faults and large concurrency are dealt with; pROVIDING AUTOMATED DEPLOYMENT OF STANDS, rapid iteration and automatic operation and maintenance are used as basic attributes; the software development platform supports scenes of rapid development, smooth upgrading and the like, so thatthe user experience of the software development platform can be improved, the software development speed and the software quality are improved, one-stop service is provided for the software development process, smooth and continuous development of software and dynamic analysis and positioning during operation are facilitated, and the customer satisfaction is improved.
Owner:青岛华正信息技术股份有限公司

Aeroplane buffet air tunnel model integration design and manufacturing method

The invention relates to an integrated design and manufacture method of a full resin airplane low-velocity flutter wind tunnel model based on photocuring rapid prototyping. The method first conducts the integrated design of the flutter model according to the actual structure of an airplane, the requirement of a wind tunnel experiment and the parameters of photocuring resin material and based on the photocuring resin material, and makes the full resin flutter model in an integrated way on the basis of the optimization of the photocuring rapid process. The method proposes a new design and manufacture concept of the flutter model of low modulus material, gets rid of unnecessary assembly links by the use of the advantages of accuracy, quickness and low cost of the photocuring rapid prototyping technology, the uniformity of the model material, the low modulus of the resin material and isotropy characteristic, and designs and manufactures the full resin flutter wind tunnel model meeting the full dynamic similarity. The method overcomes the defects of traditional technologies, improves the manufacture precision of the wind tunnel model, reduces cost, shortens the period and realizes structural similarity, thus boosting the development speed of an airplane.
Owner:XI AN JIAOTONG UNIV

Method for checking useful load of auxiliary springs of non-end contact diagonal main and auxiliary spring

The invention relates to a method for checking a useful load of auxiliary springs of a non-end contact diagonal primary and auxiliary spring, and belongs to the technical field of suspension steel plate springs. The method comprises the following steps: firstly, determining an endpoint deformation coefficient and the half rigidity of each main spring, as well as a deformation coefficient Gx-CB of the contact point between an Nth main spring and the auxiliary spring at an oblique line segment according to a structural dimension and an elastic modulus of the diagonal variable cross-section main spring with non-isostructural end parts; then, checking the useful load of the auxiliary springs of the non-end contact few-leaf diagonal variable cross-section main and auxiliary spring according to the thicknesses of root straight sections of the main springs, Gx-CB of the Nth main spring, the half rigidity of each main spring and a design value of the clearance Delta between the main springs and the auxiliary springs. The simulated verification shows that an accurate checking value of the useful load of the auxiliary springs of the non-end contact diagonal main and auxiliary spring can be obtained by using the method, the design level and performance of products are improved, the vehicle running smoothness is improved, meanwhile, the design, manufacturing and test costs are reduced, and the product development speed is increased.
Owner:平邑经济开发区投资发展有限公司

Method for realizing software phase-locked loop with unfixed sampling frequency

The invention discloses a method for realizing a software phase-locked loop with an unfixed sampling frequency. The method comprises the following steps: firstly adopting an analog phase-locked loop digital controlled oscillator of the DSP period counter to obtain digital controlled oscillator output signals; then working out the phase error between the mains voltage and a reference signals in the DQ-transformation phase demodulation mode by using the digital controlled oscillator output signals as the reference signals; and establishing a closed loop transfer function secular equation of a phase-locked loop system and determining the parameters of the designed loop filter based on the digital controlled oscillator output signals and the phase error between the mains voltage and the reference signals. The invention can maintain the fixed number of the sampling points in the primitive period, and is used for repeatedly controlling various grid-connected converting devices, such as active electric filters, new energy-powered grid-connected converters and the like. By adopting the DQ-transformation phase demodulation mode, the invention can well inhibit the harmonic and unbalanced mains, resist the fluctuation of the mains voltage, and ensure the reliable operation of the phase-locked loop under the conditions of multiple mains voltage zero passage, voltage harmonics, voltage fluctuation and mains voltage imbalance.
Owner:ZHEJIANG UNIV

Automatic test system and method of vehicle millimeter wave radar

The invention relates to an automatic test system and method of a vehicle millimeter wave radar simulation scene. The automatic test system of the vehicle millimeter wave radar simulation scene includes a test control computer, vehicles and scene simulation tools, a radar target simulator and radar to be tested; and a control system is arranged in the test control computer. The test method performed by using the automatic test system of the vehicle millimeter wave radar simulation scene comprises the following steps: combining the vehicles and scene simulation tools and the system, and using the vehicles and scene simulation tools to perform simulation and construction on vehicle types, road environments, weather conditions and the like; using the target simulator and the radar to be tested to perform transmission and reception on target information; and using the control system to perform real-time collection and saving on the target information, perform comparison, judgment, analysisand process with the working condition scene information constructed by the simulation tools, and automatically output a detection report. The invention integrates the vehicles and scene simulation tools and the system to form a complete, effective and integrated millimeter wave radar automatic test system.
Owner:HUIZHOU DESAY SV INTELLIGENT TRANSPORTATION TECH INST CO LTD

Intelligent sensor for measuring high current

ActiveCN102944737AReduce design difficultyOvercoming the technical shortcomings of measuring large currentsTemperature compensation modificationElectrical testingDigital signal processingArea network
Provided is an intelligent sensor for measuring high current. A large-power sampling resistor (R1) of the intelligent sensor converts current signals into voltage signals. Converted voltage signals are processed and filtered through a signal processing filter circuit and fed to an AD chip (U9). A negative temperature coefficient (NTC) thermal resistor (R23) is adopted by a temperature measurement module to measure the temperature of the large-power sampling resistor so as to be used for temperature compensation for the large-power sampling resistor. The AD chip converts output voltage of the measuring signal processing filter circuit and the temperature value of the NTC thermal resistor into digital signals, digital filtering processing is performed, and digital signals of voltage and the temperature are sent to an external main central processing unit (CPU) through a serial peripheral interface (SPI) communication interface isolated through an optocoupler. Isolation of the SPI communication digital signals is achieved through a digital isolation and direct current (DC) / DC conversion module, and the digital isolation and DC / DC conversion module supplies power to the signal processing filter circuit, the temperature measurement module and an analog to digital (A / D) conversion chip with a CPU processor. The main CPU and a controller area network (CAN) communication module receive external instructions and send digital signals of current measurement values.
Owner:INST OF ELECTRICAL ENG CHINESE ACAD OF SCI

Simulation and verification method of control method of near space aircraft

The invention relates to the simulation and the verification of a control method in the field of aerospace. In order to provide a simulation and verification platform capable of supporting a near space aircraft to real-time simulation tests and performance evaluation from the design of a flight control system, the technical scheme adopted by the invention is as follows: a simulation and verification method of the control method of the near space aircraft is realized by virtue of the following devices: a simulation master control machine and a dSPACE real-time simulation machine, wherein the simulation master control machine is provided with a DS817 high-speed serial communication interface plate; and the simulation master control machine is communicated with the DS814 high-speed serial communication interface plate of the dSPACE real-time simulation machine through an optical fiber. The method comprises the following steps of: operating master control software; dividing a whole evaluation process into two parts, namely a control system efficiency evaluation process and an evaluation confirmation process, by performance evaluation software; and obtaining data, which is needed by control system efficiency evaluation, by the control system efficiency evaluation process through three steps. The simulation and verification method of the control method of the near space aircraft is mainly applied to simulation and verification in the field of aerospace.
Owner:TIANJIN UNIV
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