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66 results about "Elastic analysis" patented technology

Geometric nonlinear static aeroelasticity analysis method based on structure reduced-order model

The invention provides a geometric nonlinear static aeroelasticity analysis method based on a structure reduced-order model. The method includes: building an aircraft wing or full-aircraft finite element model, presetting follow-up test load, and using finite element software to solve corresponding test deformation; under a given nonlinear rigidity coefficient form, performing regression analysison the follow-up test load and the test deformation to solve a nonlinear rigidity coefficient and built the structure reduced-order model; applying the structure reduced-order model to aircraft geometric nonlinear static aeroelasticity analysis, and building aircraft wing geometric nonlinear static aeroelasticity deformation calculation flow and full-aircraft geometric nonlinear static aeroelasticity trim analysis flow. The method has the advantages that the cubic polynomial nonlinear rigidity coefficient is given, an aerodynamic force follow-up effect and extension-direction deformation underaircraft wing geometric nonlinear large deformation are considered, the reasonability and accuracy of geometric nonlinear static aeroelasticity analysis are increased, and efficient analysis and calculation of geometric nonlinear static aeroelasticity deformation and trim are benefited.
Owner:BEIHANG UNIV

Hypersonic speed guided missile multi-field coupling dynamics integrated simulation analysis method

The invention provides a hypersonic speed guided missile multi-field coupling dynamics integrated simulation analysis method, which comprises the following steps of: establishing a coupled structural motion equation; improving an aerodynamic heating calculation method; improving an unsteady aerodynamics calculation method; establishing an integrated simulation analysis technique process; designing a relationship between an integrated simulation analysis operation model and data; and realizing an integrated simulation analysis system. Compared with the prior art, the aerodynamic heating calculation method and the unsteady aerodynamics calculation method are improved; various techniques of flutter analysis, thermal flutter analysis, pneumatic servo elastic analysis and thermal pneumatic servo elastic analysis are integrated; and an effective integration method for integrally solving and optimally designing a high-speed winged missile all-missile combination body coupling dynamics problem is provided.
Owner:SHANGHAI INST OF ELECTROMECHANICAL ENG

Coaxial rigid rotor pneumatic elastic response method

The invention provides a coaxial rigid rotor coupling pneumatic elastic response analysis method, and belongs to a helicopter kinetic analysis technology. The method is characterized in that according to the operation and control characteristics of a coaxial rigid rotor helicopter, a balance equation optimization solution method is built, and an optimization solution is found according to the given target and constraint conditions. According to the characteristic of complicated coaxial rigid rotor flow field environment, a rotor flow field is calculated by using a computational fluid dynamic method based on an Euler / N-S equation; and then, the coupling pneumatic elastic response is calculated by using a computational fluid dynamic / computational structural dynamic loose coupling analysis method. The coaxial rigid rotor coupling pneumatic elastic analysis method has the advantage that when the analysis method is used, balance operation and control parameters, blade response, rotor loads and the like of the coaxial rigid rotor helicopter can be calculated. The method has good analysis precision and engineering applicability; the relying of the development process on the test can be reduced; and the design period and the development cost can be greatly reduced.
Owner:CHINA HELICOPTER RES & DEV INST

Method for extracting two-dimensional dynamic blood vessel information based on ultrasonic echo in real time

The invention relates to a method for extracting two-dimensional dynamic blood vessel information based on ultrasonic echo in real time, which comprises the following steps: forming and displaying a blood vessel indication cursor on an ultrasonic two-dimensional image; conducting extraction on the information about the blood vessel diameter for the original blood vessel digital radio frequency echo data to obtain the blood vessel diameter data and the blood vessel diameter variation data, wherein the representation unit of the diameter information is the number of sampling points; determining the actual diameter and fluctuations of the blood vessel according to the blood vessel indication cursor and the information about the blood vessel diameter; and further calculating blood flow volume, the fluctuation range and characteristic points of the blood vessel as well as blood flow diameter arc graphs according to the blood vessel diameter information of the blood vessel diameter variation information by combining other existing information, namely electrocardiogram information and blood flow frequency spectrogram, thus obtaining real-time two-dimensional dynamic blood vessel information. According to the invention, an analysis tool is provided for dynamic assessment of blood flow / blood vessel and compliance / elastic analysis of the blood vessel, pressure signals in the axial and radial directions of the blood vessel are provided for pulse condition analysis and research, and the extraction method has the characteristics of practical applicability and clinical practice.
Owner:PHILIPS & NEUSOFT MEDICAL SYST

Elastic analysis method of vascular wall based on finite element deformation theory

InactiveCN101474082AAccurately characterize the lesionCharacterize the lesionSurgeryCatheterSonificationCardiac cycle
A method for analyzing the elasticity of vessel walls based on finite element deformation theory belongs to the medical image analysis field. The elasticity of the vessel wall is analyzed by calculating strain characteristic values of the vessel wall in an IVUS image under pressure. An ultrasound transducer hovers in a certain position of a blood vessel lumen for acquiring images of a plurality of cardiac cycles; and the images are input into a computer for processing. The method comprises that: a template matching method is used for searching out matching points of marking points in an original image in a template image; the vessel wall is divided into a plurality of layers according to the organization characters of the vessel wall; a method for calculating the elasticity of the vessel walls based on finite element partition is provided; the vessel walls are divided into a plurality of conjoined triangles according to the characteristics of triangle infinite element strain; with a view to the interaction of the triangles in deformation, factors of influence are also added into the calculation of the strain value. The limitations existing in the existing method for analyzing the elasticity of the vessel walls are changed. The characteristics of pathological changes of the vessel walls are exactly portrayed, thus creating conditions for the analyzing of pathological changes.
Owner:BEIJING UNIV OF TECH

Structure reduced-order model-based geometric nonlinear static aeroelastic full-aircraft trim method

The invention provides a structure reduced-order model-based geometric nonlinear static aeroelastic full-aircraft trim method. The method comprises the steps of firstly building a full-aircraft finiteelement model of an aircraft, giving a follow-up test load and solving corresponding test deformation through finite element software; secondly solving a nonlinear stiffness coefficient by performingregression analysis on the follow-up test load and the test deformation in a given nonlinear stiffness coefficient form to build a structure reduced-order model; and finally applying the model to thegeometric nonlinear static aeroelastic full-aircraft trim analysis of the aircraft, and establishing wing geometric nonlinear static aeroelastic deformation calculation and full-aircraft geometric nonlinear static aeroelastic trim analysis processes. The nonlinear stiffness coefficient in a cubic polynomial form is given, and the aerodynamic follow-up effect and the spanwise deformation under thewing geometric nonlinear large deformation are considered, so that the reasonability and accuracy of geometric nonlinear static aeroelastic analysis are improved and the efficient analysis calculation of geometric nonlinear aeroelastic deformation and trim is facilitated.
Owner:BEIHANG UNIV

Main shock-aftershock sequence-based method for estimating damage index

The invention relates to a main shock-aftershock sequence-based method for estimating a damage index, and aims at solving the problem that influence of an aftershock to a structure is ignored due to the fact that only single action of a main shock is considered in an existing method for estimating an earthquake damage index. The main shock-aftershock sequence-based method disclosed by the invention comprises the following steps: I: selecting a structural hysteresis model according to an actual earthquake motion type; II: selecting a period, mass and damping of a single-degree-of-freedom structure, and calculating a structural dynamic characteristic; III: performing elastic analysis on selected earthquake motion and the structural characteristic to obtain an elastic strength demand Fe; IV: selecting a strength reduction factor value R, and working out yield strength Fy of an inelastic structure; V: working out a reaction of the structure under action of an earthquake according to a structural dynamic method, and working out the damage index DI according to a damage calculation formula; VI: presenting a damage spectrum prediction model of a main shock-aftershock sequence according to a statistical result of the structural damage index DI. The main shock-aftershock sequence-based method for estimating the damage index disclosed by the invention can be applied to the field of earthquake engineering.
Owner:HARBIN INST OF TECH

Neural network for aeroelastic analysis

A system and method of performing aeroelastic analysis using a neural network. Input parameters, such as mass and location, contributing to aeroelastic characterization are determined and constrained. A model of a structure to be analyzed can be constructed. The model can include a number of locations where the input parameters can be varied. The aeroelastic characteristic of the structure can be analyzed using a finite element model to determine a number of output characteristics, each of which can correspond to at least one of a plurality of input samples. A neural network can be generated for determining the aeroelastic characteristic based on input parameters. The input sample / output characteristic pairs can be used to train the neural network. The weights and bias values from the trained neural network can be used to generate a non-linear transfer function that generates the aeroelastic characteristic in response to input parameters.
Owner:THE BOEING CO

Elasticity analysis process oriented cloud resource allocation optimization method

The invention provides an elasticity analysis process oriented cloud resource allocation optimization method. The method comprises the steps of S1, carrying out performance modeling on an elasticity analysis process through adoption of an open queuing network theory, namely modeling the whole analysis process to form an open queuing network, wherein each component in the process corresponds to sub-queues in a queuing network system, and the output of one component is the input of another component; and S2, estimating average response time of the whole open queuing network through a queuing theory, carrying out cloud resource allocation on each component according to the estimated average response time, thereby enabling the total number of resources to be the least on the premise of satisfying the average response time required by a user. According to the method, the resource allocation can be carried out on the analysis process with requests arriving continuously, the average response time of the system is estimated by employing a queuing theory; the response time is estimated relatively accurately, an allocable server solution set of each component is estimated according to the queuing theory, and a quasi-optimal solution is obtained by employing a heuristic algorithm.
Owner:SHANGHAI JIAO TONG UNIV

Method of Performing Computational Aeroelastic Analyses

Computational aeroelastic analyses typically use a mathematical model for the structural modes of a flexible structure and a nonlinear aerodynamic model that can generate a plurality of unsteady aerodynamic responses based on the structural modes for conditions defining an aerodynamic condition of the flexible structure. In the present invention, a linear state-space model is generated using a single execution of the nonlinear aerodynamic model for all of the structural modes where a family of orthogonal functions is used as the inputs. Then, static and dynamic aeroelastic solutions are generated using computational interaction between the mathematical model and the linear state-space model for a plurality of periodic points in time.
Owner:NASA

Elastic-plastic buckling bearing capacity calculation method

The invention discloses an elastic-plastic buckling bearing capacity calculation method which comprises the following steps: S1, carrying out linear elasticity analysis on a truss structure under a stress load condition, and determining the most unfavorable rod piece of the truss structure under the load condition; S2, calculating and acquiring the linear elastic buckling bearing capacity and the elastic-plastic buckling bearing capacity of the most unfavorable rod piece of the truss structure; S3, calculating the elastic-plastic buckling bearing capacity of the truss structure according to the elastic-plastic buckling bearing capacity of the most unfavorable rod piece of the truss structure; S4, respectively calculating the elastic-plastic buckling bearing capacity of the truss structure by adopting a characteristic value buckling analysis method and a riks analysis method in finite element software Abaqus, comparing and analyzing the obtained elastic-plastic buckling bearing capacity result of the truss structure and the calculated elastic-plastic buckling bearing capacity result of the truss structure so as to verify the correctness and feasibility of the elastic-plastic buckling bearing capacity of the truss structure.
Owner:SOUTHWEST JIAOTONG UNIV

Thermoset coupling structure dynamics order reduction model method suitable for thermodynamic elasticity analysis

The invention discloses a thermoset coupling structure dynamics order reduction model method suitable for thermodynamic elasticity analysis and belongs to the technical field of aerodynamics. The method comprises the steps of S1, performing order reduction on a structure temperature field, constructing a structure temperature field order reduction model, and obtaining a structure temperature fieldlow-order vector after order reduction of the structure temperature field at any moment; S2, selecting a modal shape of a reference structure as a reference modal shape phi ref, and performing orderreduction on a deformation field to obtain a low-dimensional vector q based on phi ref; s3, establishing a kinetic equation of the heated structure; s4, establishing a thermosetting coupling kinetic model of the heated structure; sampling is carried out in the q and the formed L + N-dimensional space; a series of sample working conditions with different deformation field and temperature field loads are obtained, M, D and K (1) in a formula (7) are identified through a system, and nonlinear structure dynamics analysis under a time-varying temperature load is carried out after training is completed, so that a thermosetting coupling dynamics model based on a neural network is a nonlinear model and has generality.
Owner:AERODYNAMICS NAT KEY LAB +1

First linear elastic estimation method for analyzing ultimate bearing capacity of planar circular tube structure

A first linear elastic estimation method for analyzing ultimate bearing capacity of a planar circular tube structure comprises the steps of (1) establishing a planar circular tube structure analyzing model; (2) determining a failure unit; (3) calculating ultimate bearing capacity of the planar circular tube structure by means of first linear elastic estimation; the method allows the ultimate bearing capacity of the planar circular tube structure to be solved accurately and quickly through first linear elastic analysis; the defect is overcome that a universal elastoplasticity incremental analysis method for analyzing structural ultimate bearing capacity is insufficient due to the need for setting a complex loading process and carrying out multiple incremental iterative analysis; the efficient method for estimating the overall safety of the planar circular tube structure is provided.
Owner:GUANGXI UNIV

Three-dimensional acousto-elastic analysis method of ship for arbitrary damping processing of structure

The invention discloses a three-dimensional acousto-elastic analysis method of a ship for arbitrary damping processing of a structure and relates to the technical field of acoustics. The method comprises the steps of performing modal analysis on a finite element model of a ship structure with an initial damping laying layer to obtain a modal damping ratio of modalities at various orders of the ship structure; substituting the modal damping ratio of the modalities at various orders of the ship structure into an acousto-elastic coupling dynamic equation of the ship structure to obtain a composite structure dynamic equation of the ship structure; and performing vibration noise analysis on the coupling dynamic equations by use of a three-dimensional acousto-elastic theory of the ship. A damping laying optimization design scheme for the ship structure with structural acoustic radiation as an optimization objective is provided. According to the three-dimensional acousto-elastic analysis method of the ship for arbitrary damping processing of the structure, the direct vibration noise analysis for the laying-damped ship structure is implemented, and the method can be widely used for processing of the damping structure when the vibration noise of the ship is calculated and can provide a technical support for the damping laying design of the ship.
Owner:CHINA SHIP SCIENTIFIC RESEARCH CENTER (THE 702 INSTITUTE OF CHINA SHIPBUILDING INDUSTRY CORPORATION)

Combination method for demand response based time-of-use power price strategy suitable for smart grid development

The present invention discloses a combination method for a demand response based time-of-use power price strategy suitable for smart grid development. The combination method comprises the following steps: estimating electricity price affordability of enterprises with changes in multiple factors; according to a system load situation in conjunction with user demand-side analysis with seasonal attributes, carrying out period optimization that takes the seasonal attributes into account; and based on analysis of demand price elasticity in industries, differentiating application of the time-of-use power price in different situations, thereby forming a demand response based time-of-use power price strategy. According to the combination method for the time-of-use power price strategy, for different seasons, valley and peak power prices suitable for the seasons are set according to differences in demand price elasticity, so as to finally form a time-of-use power price strategy that combines peak and valley power prices, time-of-use power prices, and season-differentiated power prices.
Owner:STATE GRID CORP OF CHINA +2

Elastic analysis method of vascular wall based on finite element deformation theory

InactiveCN101474082BAccurately characterize the lesionCharacterize the lesionSurgeryCatheterSonificationCardiac cycle
A method for analyzing the elasticity of vessel walls based on finite element deformation theory belongs to the medical image analysis field. The elasticity of the vessel wall is analyzed by calculating strain characteristic values of the vessel wall in an IVUS image under pressure. An ultrasound transducer hovers in a certain position of a blood vessel lumen for acquiring images of a plurality of cardiac cycles; and the images are input into a computer for processing. The method comprises that: a template matching method is used for searching out matching points of marking points in an original image in a template image; the vessel wall is divided into a plurality of layers according to the organization characters of the vessel wall; a method for calculating the elasticity of the vessel walls based on finite element partition is provided; the vessel walls are divided into a plurality of conjoined triangles according to the characteristics of triangle infinite element strain; with a view to the interaction of the triangles in deformation, factors of influence are also added into the calculation of the strain value. The limitations existing in the existing method for analyzing the elasticity of the vessel walls are changed. The characteristics of pathological changes of the vessel walls are exactly portrayed, thus creating conditions for the analyzing of pathological changes.
Owner:BEIJING UNIV OF TECH

Estimation method for analyzing ultimate bearing capacity of bends

The invention relates to a numerical method for analyzing ultimate bearing capacity of bends and in particular relates to an estimation method for analyzing ultimate bearing capacity of bends. The method comprises the following steps: (1) establishing a bend structure analysis model; (2) performing primary linear elastic analysis; (3) performing secondary linear elastic analysis; and (4) calculating the ultimate bearing capacity of the bends according to the estimation method. According to the method disclosed by the invention, only the linear elastic analysis twice is needed, and rapid estimation of the ultimate bearing capacity of the bends is realized. The defects that a complicated loading process needs to be set in an elastic-plastic incremental method for analyzing the ultimate bearing capacity of the bends, repeated incremental iterative analysis is performed and the like are overcome, and a high-efficiency pathway is provided for rapidly and reasonably determining the ultimatebearing capacity of the bends at a primary design stage of the bends.
Owner:NANCHANG INST OF TECH

Low-impact development multi-objective interval optimal configuration method based on SWMM model

The invention discloses a low-impact development multi-objective interval optimal configuration method based on an SWMM model, and the method comprises the steps: building a current situation model ofan urban research region based on the SWMM model, and carrying out the current situation simulation and elastic analysis of a drainage pipe network system in the urban research region; establishing amulti-objective optimization system, and determining an optimization variable and an objective function of the optimization system; and enabling the objective function to take the minimum LID facility cost and the minimum drainage pipe network system elastic index as optimization objectives, and optimizing by combining a multi-objective interval optimization algorithm. A formula for calculating the elasticity index U-Res of the drainage pipe network system is provided to comprehensively evaluate the elasticity of the drainage pipe network system, and water quantity and water environment indexes are comprehensively considered; the minimum LID facility cost and the minimum pipe network system elasticity index U-Res are used as optimization objectives for solving by adopting an intelligent algorithm; the optimization model taking the runoff reduction rate as the constraint condition effectively overcomes the subjectivity of the traditional weight method and reduces the artificial noise influence.
Owner:GUANGDONG UNIV OF TECH

Static aeroelasticity analysis method, device and apparatus for aircraft and storage medium

The invention relates to a static aeroelasticity analysis method, device and apparatus of an aircraft and a storage medium. The static aeroelasticity analysis method, device and apparatus are appliedto high-lift aircraft configuration in a climbing or landing scene. The method comprises the following steps: generating a three-dimensional skin grid of each component in a target component; carryingout steady flow field analysis on each component to obtain an aerodynamic load generated on each component; determining the structural deformation of each component according to the aerodynamic loadon each component; and according to the structural deformation amount of each component, deforming the aerodynamic surface grid and the aerodynamic space grid of each component, and outputting an analysis result of each component when it is determined that static aerodynamic elasticity analysis of each component reaches a preset convergence condition. According to the method, the static aeroelasticity analysis of the low-speed high-lift aircraft configuration can be automatically realized in the whole process, the complexity of the static aeroelasticity analysis of the low-speed high-lift aircraft configuration is simplified, and the analysis efficiency is improved. Meanwhile, the accuracy of an analysis result is also improved.
Owner:BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1

Machine learning systems and methods for elasticity analysis

InactiveUS20210312560A1Minimize reduce impactReduce the impactFinanceMachine learningElastic analysisEngineering
A machine learning system determines an estimate of elasticity of an insurance policy. The system includes one or more processors in communication with at least one memory device, the one or more processors programmed to store an insurance policy model including a plurality of characteristics for the insurance policy and historical insurance policy data including a plurality of individual insurance policies. The one or more processors are further programmed to execute the insurance policy model to calculate an estimate of elasticity of the insurance policy based upon analyzing the historical data to detect a change to a characteristic of the insurance policy. The one or more processors are further programmed to modify a characteristic based upon the calculated elasticity. The processors are further programmed to receive a user insurance application, generate an individualized insurance policy based upon the application and the modified characteristic, and transmit the individualized insurance policy.
Owner:STATE FARM MUTUAL AUTOMOBILE INSURANCE

One click job placement

ActiveUS20210312401A1Broad and analysisDigital data information retrievalOffice automationJob placementElastic analysis
A job matching algorithm improves matching a job opening profile to a job-seeker with accuracy and efficiency by breaking down the job opening profile into a data model of standard codes. Job criteria are abstracted as attributes into at least categories of qualifications and characteristics, having an associated assigned weight. Job-seeker profile's corresponding attributes in qualifications and characteristics are multi-dimensionally mapped to those in the job opening profile to calculate an overall score against a threshold score for successful matching. The job-seeker's profile and the job opening's profile may also be re-matched using an elastic analysis to model job seeker's strengths and growth potential for a same or a different job, through adjusting individual weights of each attribute of the qualifications and characteristics of one or both of the job-seeker's profile and the job opening profile to predict risks or successes for the job-seeker in taking the job opening.
Owner:THE UNIFY PROJECT D B A UNIFY LABS

Atrium cross-floor frame column design method based on rigidity equivalence

The invention provides an atrium cross-floor frame column design method based on rigidity equivalence. The method includes respectively establishing a floor slab non-holing model (a first model) and afloor slab holing model (a second model), and carrying out the static and seismic response spectrum analysis; based on a first model meeting specification requirements and an elastic analysis resultof the first model, respectively extracting the floor lateral stiffness of the two models, according to the principle that the floor lateral stiffness of the first model is equivalent to the floor lateral stiffness of the second model, amplifying the earthquake action of a cross-floor frame column (namely a frame column within a floor holing range) in the second model, and carrying out component reinforcement design to achieve the effect that the earthquake resistance indexes of the first model and the second model are similar. According to the method, aiming at the problem that earthquake shearing force distributed to the cross-floor frame column is small due to the fact that a large hole is formed in a floor slab, the amplification coefficient based on floor lateral stiffness equivalenceis provided, the anti-seismic contribution of the cross-floor frame column is improved, the anti-seismic performance of the whole structure is improved, and reference is provided for similar engineering projects.
Owner:CHINA IPPR INT ENG

Efficient parallel algorithm for three-dimensional acoustic elastic generalized hydrodynamic coefficient

The invention relates to an efficient parallel algorithm for a three-dimensional acoustic elastic generalized hydrodynamic coefficient. The efficient parallel algorithm comprises the following steps:obtaining a vibration mode displacement matrix of a ship dry mode based on finite element software; respectively distributing the total frequency number and the total process number into each frequency group; obtaining a Green function matrix and a partial derivative matrix of the Green function matrix for each frequency in each frequency group; constructing a wet surface element source intensitymatrix equation for a single frequency, performing two-dimensional parallel division on a Green function partial derivative matrix and a vibration mode displacement normal component matrix in the equation, and performing calculation to obtain a wet surface element source intensity matrix; and calculating the dry-mode attached water mass and the attached water damping in the generalized hydrodynamic coefficient. Aiming at a ship three-dimensional acoustic elasticity analysis method, the efficient parallel algorithm distributes the total frequency number to the frequency groups for parallel calculation, and performs two-dimensional parallel division on the Green function partial derivative matrix and the vibration mode displacement normal component matrix, so that the bottleneck problem of large calculation amount is effectively solved, and the large-scale engineering calculation applicability of the ship three-dimensional acoustic elasticity analysis method is greatly improved.
Owner:CHINA SHIP SCIENTIFIC RESEARCH CENTER (THE 702 INSTITUTE OF CHINA SHIPBUILDING INDUSTRY CORPORATION)

Aeroelastic structure coupling optimization method based on self-adaptive point adding proxy model

The invention discloses an aeroelastic structure coupling optimization method based on a self-adaptive point adding proxy model, and the method comprises the steps: firstly considering the parameter uncertainty and the model uncertainty, carrying out the quantification of the uncertainty, and providing a self-adaptive intelligent point adding criterion based on a Kriging proxy model, the maximum stress of the aircraft structure and the upper and lower boundaries of the flutter speed are obtained, and then the aircraft structure is optimally designed by considering the structural strength constraint condition and the aeroelasticity constraint condition based on the self-adaptive point adding agent model. According to the method, the number of times of finite element analysis and aeroelasticity analysis in the aircraft structure optimization process is reduced, the calculation amount is reduced, the optimization efficiency is improved, and a new thought is provided for aircraft structure optimization design.
Owner:BEIHANG UNIV

An aeroelasticity analysis method considering internal fluid dynamic characteristics

The invention belongs to an aircraft aeroelasticity analysis technology, and particularly relates to an aeroelasticity analysis method considering internal fluid dynamic characteristics. According tothe method, firstly, an additional mass matrix considering internal fluid is generated, then a motion equation considering the additional mass matrix is assembled, and then aeroelasticity analysis considering the influence of the internal fluid is carried out. According to the method provided by the invention, the influence of internal fluid dynamic characteristics can be considered in the dynamicsimulation model of the aircraft with a large number of internal fluid, so that the aeroelasticity analysis precision of the whole aircraft can be improved, and the aeroelasticity design can be better guided. And the provided analysis method is simple and convenient to operate and has a relatively high engineering application value.
Owner:XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA

Transient shearlet excitation system and transient shearlet excitation method based on ring external vibration

The invention provides a transient shearlet excitation system and a transient shearlet excitation method based on ring external vibration. The transient shearlet excitation system comprises a transient shearlet excitation device driving module, a shearlet excitation device, an ultrasonic testing device and an elastic analysis module, wherein the transient shearlet excitation device driving module is used for generating transient low-frequency signals which are used for driving an electromagnetic vibrator after being amplified, and the electromagnetic vibrator drives the shearlet excitation device to vibrate; the shearlet excitation device is used for subjecting the medium surface to be tested to transient vibration under drive of vibration of the electromagnetic vibrator, and shearlet is generated in a medium; the ultrasonic testing device comprises an ultrasonic transducer arranged on a central axis of the shearlet excitation device, and is used for giving out ultrasonic waves to test sidelobe-focused shearlet components in the shearlet. The transient shearlet excitation system and the transient shearlet excitation method based on ring external vibration have the advantages that since the shearlet excitation device subjects the medium surface to be tested to transient vibration and superimposed shearlet components are generated in the central axis of the medium, energy and depth of the shearlet in the ring central axis direction of the medium to be tested are increased, and transient elastography test penetration depth is increased.
Owner:SHENZHEN UNIV

Nonlinear gasket-based flange bolt pre-tightening load design method

InactiveCN106971033ASimple and effective quantitative evaluation methodGeometric CADSpecial data processing applicationsAxial displacementElastic analysis
The invention relates to a nonlinear gasket-based flange bolt pre-tightening load design method. The compression resilience performance of a gasket is analyzed; a relationship between unloading performance and bolt pre-tightening force of the gasket is discussed; a flange connection system is subjected to elastic analysis, and the nonlinear performance of a gasket material can enable the bolt pre-tightening force to be nonlinearly changed; a flange connection is subjected to coordination analysis of axial displacement; a law of change of gasket pressing force along with a working pressure and the bolt pre-tightening force is solved; a law of change of a flange deflection angle along with the working pressure and the bolt pre-tightening force is solved; the tightness of the bolt flange connection system is subjected to safety assessment; and a safety region of the nonlinear bolt pre-tightening force of a flange under the condition of a certain nominal pressure is given by integrating two aspects of the gasket pressing force and the flange deflection angle, so that the tightness of the bolt flange system reaches the best. According to the method, a simple and effective quantitative assessment method is given for the tightness of the normal-temperature flange connection system; a basis is provided for design and tightness assessment of the bolt flange connection system; and the safety is improved.
Owner:WUHAN INSTITUTE OF TECHNOLOGY

CFD (computational fluid dynamics)/CSD (circuit switch data) coupled solving nonlinear aeroelasticity simulation method

InactiveCN102012953BCapable of nonlinear couplingSpecial data processing applicationsAviationElastic analysis
The invention discloses a CFD (computational fluid dynamics) / CSD (circuit switch data) coupled solving nonlinear aeroelasticity simulation method, comprising: firstly, carrying out calculation initialization; then solving the CFD of unsteady aerodynamic force; converting boundary load information; solving the CSD of nonlinear structure dynamic response; judging whether to exist computation or notby taking the response of structural finite-element mesh point displacement as a convergence criteria; if not exiting, carrying out the dynamic mesh deformation of a flow field after the surface displacement information of a computation model is converted; and then, continuing to compute until the convergence criteria is satisfied, thus finishing computation. By means of the simulation method disclosed by the invention, the problem of pneumatic nonlinearity and structural nonlinearity coupling and the problem of geometric large deformation dynamic mesh can be solved; and the simulation methoddisclosed by the invention can be applied on the nonlinear aeroelasticity analysis of aerospace aircrafts and the nonlinear aeroelasticity analysis of civil high-rise buildings and bridges.
Owner:NORTHWESTERN POLYTECHNICAL UNIV
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