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232results about How to "Strong engineering application value" patented technology

Dispatching end grid fault diagnosis method based on wide-area fault recording information

ActiveCN103837795AResolution frequencySolve key problems such as difficult data synchronizationFault locationInformation technology support systemDiagnosis methodsCondition monitoring
The invention discloses a dispatching end grid fault diagnosis method based on wide-area fault recording information. The method comprises the following steps that when a grid breaks down, fault data of a primary system of the grid are recorded according to a certain sampling frequency mode and are sent to a dispatching main station end through a fault recording networking system; the mapping relation between a basic data platform of grid equipment and a fault recording system is established through CT identification; different sampling frequencies of a fault recorder are unified to be the same sampling frequency according to an interpolation method; a differential-current out-of-limit value is set and independent grid equipment serves as a calculation unit to carry out differential-current calculation; whether the differential-current value is out of limit is confirmed to position fault places and confirm protection actions. The dispatching end grid fault diagnosis method has the advantages of solving the key problems that sampling frequency of the fault recorder is different and data are hard to synchronize, and achieves fault diagnosis application functions such as system operation state monitoring, protection behavior analyzing and accurate fault positioning through the fault recording information only.
Owner:STATE GRID SHANDONG ELECTRIC POWER +2

Inertia/astronomy/satellite high-precision integrated navigation system and navigation method thereof

The invention provides an inertia/astronomy/satellite high-precision integrated navigation system and a navigation method thereof. The inertia/astronomy/satellite high-precision integrated navigation system comprises a sensor module, an integrated navigation resolving module and a real-time display module, wherein the sensor module is sequentially connected in series with the integrated navigation resolving module and the real-time display module and comprises an inertia sensor, a star sensor and a satellite receiver; the integrated navigation resolving module comprises a four-step Runge-Kutta strapdown navigation resolving module, an astronomy attitude determination resolving module, an unequal-interval Kalman filtering module and a position and speed compensation algorithm module; and the real-time display module comprises a three-dimensional real-time display module. The navigation method realizes the real-time acquisition of sensor data, utilizes the inertia sensor data to carry out strapdown navigation resolving based on a four-step Runge-Kutta algorithm and can carry out the integrated navigation resolving on the inertia sensor data, star sensor data and satellite receiver data and carry out the real-time three-dimensional display on an integrated navigation result by utilizing a projection algorithm.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Time-frequency transform based method for identifying parameters of synchronous generator

The invention provides a time-frequency transform based method for identifying parameters of a synchronous generator. The method includes steps of S1. carrying out Laplace transform on a differential equation of a d axle and a q axle of a generator in time domain in a generator model to obtain an equation of the d axle and the q axle of the generator in frequency domain, and carrying out inverse Laplace transform to obtain an integral equation of the d axle and the q axle of the generator in the time domain; S. replacing state variable of the integral equation of the d axle and the q axle of the generator in the time domain; S3. dispersing the integral equation of the d axle and the q axle of the generator in the time domain into that measurable column vectors or integration of the measurable column vectors are equal to a matrix multiplying by column vectors of coefficients of the integration equation, and solving to obtain the column vectors of the coefficients of the integration equation; and S4. solving to obtain parameters of the generator model according to the relation between the column vectors of the coefficients of the integration equation and parameters of the generator. A differential equation of a generator is converted to an integration equation according to the time-frequency transform based method for identifying the parameters of the synchronous generator, stability of calculating a value is facilitated, and the problem of an unstable identification result is solved.
Owner:STATE GRID CORP OF CHINA +2

Method for automatically recognizing target at medium and low altitudes and positioning carrier with high accuracy

The invention discloses a method for automatically recognizing a target at medium and low altitudes and positioning a carrier with high accuracy and belongs to the field of scene matching guidance. The method comprises the following steps of: extracting a constant algorithm and establishing an H model based on an image scale characteristic to match and recognize targets and provide a high-accuracy navigation information source; coordinating and planning relative parameters according to a matching result which is fed back in a self-adaptive mode to further control matching performance; researching integral image-based average filtering which generates an image multi-scale space instead of Gauss convolutional filtering so as to increase a matching speed; establishing an image space transformation model which adapts to the strong matching capability of the algorithm based on the thought of random sampling consistency according to an image matching result; and eliminating accurate positioning pixels of wrongly matched points based on the model to recognize the target and provide the high-accuracy navigation information source through model mapping, and simultaneously, selecting a digraph of known transformation parameters to verify the performance and the result of an image matching algorithm according to the transformation model.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Preparation method of magnetic wave absorption patch shrinkage simulation composite material

The invention discloses a preparation method of a magnetic wave absorption patch shrinkage simulation composite material. The method comprises the following steps: step 1, in a given thickness range, calculating a bevel reflectivity of the simulation composite material of different formulas at a shrinkage frequency, finding out the simulation composite material with the bevel reflectivity most approximate to that of a magnetic wave absorption patch prototype material under a prototype frequency, and determining the formula of the simulation composite material; step 2, weighing electromagnetic particles and binders; step 3, charging, and mixing; step 4, vulcanizing to obtain a vulcanized sheet; and step 5, thermally treating the vulcanized sheet to obtain a magnetic wave absorption patch for shrinkage simulation. By adopting the preparation method, the problems that the electromagnetic parameters of electromagnetic particles are difficult to test, the influence of the shape and distribution form of the electromagnetic particles to the equivalent parameters of the material is difficult to calculate and the like can be avoided, the accurate calculation of the equivalent electromagnetic parameters of the composite material is realized, the formula is obtained by virtue of the optimized design of the bevel reflectivity, the engineering application value is high, and the method can be widely used for preparing the shrinkage simulation composite material.
Owner:SHANGHAI RADIO EQUIP RES INST

Data-based aero-engine complete machine performance decline assessment and prediction method

InactiveCN110276125ASolve the imprecise problemOptimal Monitoring MethodGeometric CADDesign optimisation/simulationAviationComputer science
The invention provides a data-based aero-engine complete machine performance decline assessment and prediction method. The method comprises the following steps: S1, selecting a measurement parameter related to engine complete machine performance decline as an evaluation parameter, establishing an engine complete machine performance decline monitoring index tree based on the evaluation parameter, and setting a weight index according to the influence degree of the evaluation parameter on the engine performance decline; S2, selecting evaluation parameters of different flight frames under the same working condition from the flight data of the same aircraft in one washing period to construct an evaluation sample; S3, taking the first data of the evaluation sample data as a reference, solving the distance between other data and the reference, and normalizing the distance data to define an engine complete machine performance decline index; and S4, using an algorithm based on an artificial neural network, and using the evaluation sample constructed in the step S2 and the recession index defined in the step S3 to construct an engine complete machine performance recession prediction model for engine complete machine performance recession prediction.
Owner:AERO ENGINE ACAD OF CHINA

Satellite amplitude-phase signal identification and demodulation method and device based on a recurrent neural network

The invention belongs to the technical field of satellite communication signal processing. The invention particularly relates to a satellite amplitude-phase signal identification and demodulation method and device based on a recurrent neural network. The method comprises the following steps of: constructing a modulation recognition and demodulation network model for a training sample set and a test sample set, training the network model by utilizing the training sample set, checking the convergence degree of the trained network model by utilizing the test sample set, and storing the modulationrecognition and demodulation network model meeting a preset convergence requirement; Receiving a target signal, and preprocessing the target signal to obtain to-be-identified data consistent with theinput signal of the network model; And performing modulation identification on the to-be-identified data by using the stored modulation identification and demodulation network model, and performing signal demodulation by using a modulation identification result to obtain signal bit stream data. The method does not need to estimate the carrier-to-noise ratio of the target signal, overcomes the defects of manual determination of a threshold value and the like in a traditional method, is high in tolerance to signal frequency offset errors and timing errors, and has a very good engineering application prospect.
Owner:PLA STRATEGIC SUPPORT FORCE INFORMATION ENG UNIV PLA SSF IEU

Cantilever beam type vibration absorber with adjustable frequency

The invention provides a cantilever beam type vibration absorber with adjustable frequency. The cantilever beam type vibration absorber comprises a base, a cantilever beam and a mass disc, the lower end of the base is fixed to vibration equipment, through holes are formed in the upper end of the base and the mass disc, internal threads are arranged in the through holes, external threads matched with the through holes are arranged on the cantilever beam, the cantilever beam is arranged in the through hole of the base and the through hole of the mass disc through the external threads, fixed nuts are arranged at the two ends of the through hole of the base and fix the position of the cantilever beam and the base, adjusting nuts are arranged at the two ends of the through hole of the mass disc and limit the relative position of the cantilever beam and the mass disc, the adjusting nuts are adjustable, that is, the relative position of the mass disc and the cantilever beam is adjustable. The vibration absorption frequency of the vibration absorber can be flexibly adjusted, and the adjustable scope is wide. Parts are easy to machine and replace. Compared with an electromagnetic type unable vibration absorber and an electrodynamic type tunable vibration absorber, the electromagnetic leakage phenomenon is avoided. The cantilever beam type vibration absorber is simple in structure, stable in work and easy to mount.
Owner:HARBIN ENG UNIV

Wheel-rail vertical force continuous measurement method and device based on rail strain

The invention relates to a wheel-rail vertical force continuous measurement method based on rail strain, comprising the following steps: a. one section of rail above a single sleeper is taken as an elastomer for measuring wheel-rail vertical force; b. two groups of appropriate strain outputs on a neutral axis of the elastomer are selected, slopes of all straight lines which are corresponding to different longitudinal action point positions of a sensing region of the elastomer and determined by the strain outputs under two sleeper support reference states are obtained on the same vertical force strain output plane; c. the strain output of passing through the sensing region of the elastomer of wheels is measured, the longitudinal positions of the action points of the vertical force are identified, negative values which are corresponding to the slopes obtained in the step b are taken as combination factors, the combined strain output is obtained by combining the selected two groups of strain outputs in the step b, and the combined strain output is unrelated with the sleeper support state; and d. the vertical force is obtained by the combined strain output of the effective measurement region. A measurement device comprises an elastomer selection unit, a strain selection and parameter obtainment unit, a longitudinal position identification and strain combination unit and an output unit which are connected.
Owner:CHINA ACADEMY OF RAILWAY SCI CORP LTD +2

Integrated navigation information fusion method

The invention discloses an integrated navigation information fusion method. The method is mainly divided into a GNSS satellite signal processing module, a SINS attitude, velocity and position updatingmodule, a SINS error compensation module, a SINS/GNSS information fusion module, a SINS error correction module and a result output module. According to the method, by means of high-frequency SINS attitude, velocity and position updating and low-frequency GNSS information measurement, the elevation angle and navigation information carrier-to-noise ratio of all visible satellites tracked by an integrated navigation receiver are combined, a SINS/GNSS integrated navigation Kalman filter observation noise matrix is adaptively adjusted in real time, by means of GNSS and SINS pseudorange and a pseudorange rate measuring value, an integrated navigation Kalman filter state equation and an error covariance matrix are updated, and finally by means of SINS and GNSS information infusion feedback, aninertial device measuring error is corrected. According to the integrated navigation information fusion method, the purpose that under the complex electromagnetic environment, the integrated navigation receiver completes robust information fusion resolving can be achieved, and the method has high integrated navigation receiver design theory value and engineering application value.
Owner:PEKING UNIV

Method for determining pile spacing of anti-liquefying vibrating-impacting crushed-stone piles

InactiveCN103870643AImproved anti-liquefaction effectIncrease amplitudeSpecial data processing applicationsEngineeringLiquefaction
The invention discloses a method for determining the pile spacing of anti-liquefying vibrating-impacting crushed-stone piles. The method comprises the following steps of 1, judging the liquefied degree of foundation soil according to an in-situ test, wherein one or several methods in a, a critical standard penetration number method, b, a static sounding judging method and c, a shear-wave velocity method is or are adopted by the liquefaction judging method of the foundation soil; 2, determining the dry density needing to be reached by the foundation soil among the piles for eliminating liquefaction; 3, determining the pile spacing of the crushed-stone piles. According to the contrastive analysis of the on-site in-situ testing, the indoor test and the finite-element numerical-value analyzing results of the foundation soil before and after driving the crushed-stone piles, the anti-liquefying efficacy of the vibrating-impacting crushed-stone piles is comprehensive studied, and the method for determining the pile spacing of the crushed-stone piles is provided on the basis and on the basis of a compaction effect, so that pile-testing projects are omitted, the construction period is shortened, and the construction cost of the projects is lowered.
Owner:STATE GRID CORP OF CHINA +4
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