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304 results about "Damage effects" patented technology

Effect damage. Edit. Share. Effect Damage is any damage that is not caused by battle (with the exception of "Gravekeeper's Vassal") or is a reduction. Examples of cards that cause effect damage are "Poison Mummy", "Ookazi", and "Ceasefire". Costs are not considered Effect Damage, such as with cards like "Injection Fairy Lily" and "Dimension Fusion".

Model and method for studying landslide surge propagation rules and predicting service life of dam

ActiveCN104699892AReal-time prediction of remaining lifeOvercome against natureSpecial data processing applicationsNavier stokesWave model
The invention belongs to the field of hydraulic engineering, and provides a model and a method for studying landslide surge propagation rules and predicting the service life of a dam, and aims to build a landslide surge model which can embody interaction of a landslide mass and a water body and can take features of the landslide surge in river channels into consideration on the premise that materials and movement states of the landslide mass are considered. According to the method, a reservoir landslide surge calculation model is built on the basis of a water wave model algorithm adopting an N-S (Navier-Stokes) equation, with combination of a numerical simulation and landslide surge model test and with use of source data acquired by relevant instruments, the rationality and universality of the built landslide surge calculation model are verified through multiple landslide surge model schemes, a lost boundary surface is introduced for consideration of a dam damage effect, not only are the landslide surge propagation rules disclosed, but also one method for predicting the residual life of the dam is worked out, and theoretical basis and scientific evidence are provided for further study of the landslide surge propagation rules and reasonable prediction of the service life of the dam.
Owner:CHINA THREE GORGES UNIV

Liquid crystal medium composite as well as liquid crystal display using same and manufacturing method of liquid crystal medium composite

The invention provides a liquid crystal medium composite as well as a liquid crystal display using the liquid crystal medium composite and a manufacturing method of the liquid crystal medium composite. The liquid crystal medium composite comprises the following components: a liquid crystal material, a polymerizable monomer, a stabilizing agent and a sensitizing agent, wherein the sensitizing agent has strong absorption on ultraviolet light with the wavelength in a range of 300-380 nm; and the structure is formed by connecting a polycyclic aromatic hydrocarbon formed by connecting a plurality of benzene rings, with an aromatic ring. The liquid crystal display comprises an upper substrate, a lower substrate and the liquid crystal medium composite, wherein the upper substrate and the lower substrate are arranged in parallel; and the liquid crystal medium composite is arranged between the upper substrate and the lower substrate. According to the invention, the stabilizing agent which has the strong absorption on the ultraviolet light with the wavelength in the range of 300-380 nm is used so that a reaction wavelength of the polymerizable monomer can be moved towards a long wavelength; the ultraviolet light with the wavelength in the range of 300-380 nm is used for irradiating to keep away from the absorption wave section of a liquid crystal material, so that the damage effect on the liquid crystal material and an alignment material PI (Polyimide) by the ultraviolet light is reduced, and the polymerization reaction efficiency and the uniformity of the polymerizable monomer can be improved.
Owner:TCL CHINA STAR OPTOELECTRONICS TECH CO LTD

High-temperature and high-pressure multi-phase flow dynamic visualization loop corrosion testing apparatus and method thereof

InactiveCN106248570ASatisfy the experimental conditions of high temperature and high pressureInvestigate the effect of scour damageWeather/light/corrosion resistanceInlet valveEngineering
The invention discloses a high-temperature and high-pressure multi-phase flow dynamic visualization loop corrosion testing apparatus and a method thereof. The high-temperature and high-pressure multi-phase flow dynamic visualization loop corrosion testing apparatus comprises a medium displacement unit, an experiment parameter measurement unit, a visualization unit, a corrosion testing unit, a gas inlet valve, a circulation loop, a driving pump, a 1# end cover, a 2# end cover, a gas discharge valve and an H2S absorption device, wherein the experiment parameter measurement unit, the corrosion testing unit, the 1# end cover, the 2# end cover, the gas discharge valve and the H2S absorption device are arranged on the circulation loop, and the medium displacement unit is connected to the circulation loop through the driving pump. According to the present invention, the subcritical and supercritical fluids under the high-temperature and high-pressure environment can be realistically simulated, the shearing force can be measured, the erosion damage effect of the multi-phase flow corrosion medium on the corrosion inhibitor film and the corrosion product film can be quantitatively analyzed, and the online testing of the pipeline corrosion effect can be completed and the results are recorded.
Owner:SOUTHWEST PETROLEUM UNIV

Displacement damage dosage detection method based on p-i-n structure

ActiveCN104459372AAvoid simulation technical bottlenecksEffective assessment of displacement damage effectsElectrical testingX/gamma/cosmic radiation measurmentSpace environmentRadioactive source
The invention relates to a displacement damage dosage detection method based on a p-i-n structure. The method comprises the steps that a probe of the p-i-n structure is screened, detector parameters are adjusted and determined, and the detector response is obtained and calibrated under different radioactive sources; according to non-ionizing energy loss (NIEL) of different radioactive sources for probe materials, the detector response and the fluence or dosage relation of different radioactive sources are unified into the relation between the detector response and displacement damage dosage; according to the actual detection result, a damage enhancement factor is determined. The displacement damage dosage detection method has the advantages that the detected physical quantity is displacement damage dosage and comprises any particle capable of causing the displacement damage effect; compared with detection particle species and energy spectra, the displacement damage degree of a semiconductor element can be directly reflected; a detector based on the structure is portable, flexible, easy to use and applicable to space environment monitoring, semiconductor element displacement damage effect estimation and service life prediction.
Owner:XINJIANG TECHN INST OF PHYSICS & CHEM CHINESE ACAD OF SCI

Shrink ratio equivalent test model for explosion effect in warship cabin

ActiveCN104568612AMeet the needs of damage effect assessmentReduce manufacturing costStrength propertiesVibration measurementAccelerometer
The invention discloses a shrink ratio equivalent test model for the explosion effect in a warship cabin. The shrink ratio equivalent test model comprises a cabin body, a pressure measurement mounting seat, a pressure measurement assembly, a vibration measurement mounting seat, an accelerometer, a support pillar, a powder charge hole and a locating block; the shrink ratio equivalent test model is mainly characterized in that the cabin body is an enclosed compartment provided with a cornice; the dimensions of all wall plates are determined according to the shrinkage scale of 1 to 4 with the prototype, and the thicknesses of the wall plates are determined according to the shrinkage scale of 1 to 4 and by the similarity criterion formed by material and the thickness of the wall plates; the restraint of an adjacent cabin for a compartment structure is simulated by the support pillar and the cornice of the compartment. The shrink ratio equivalent test model has the remarkable advantages the test model is the shrink ratio equivalent model for the warship cabin, so that the dimension is small, the manufacturing cost is low, and the destroy effect of the test model is basically equivalent to that of the actual ship; therefore, the shrink ratio equivalent test model is suitable for warship target damage effect test and evaluation research.
Owner:XIAN MODERN CHEM RES INST

An evaluation method of explosive internal explosion power based on a prefabricated bar-shaped hole cylinder device

The invention discloses an evaluation method of explosive internal explosion power based on a prefabricated bar-shaped hole cylinder device. According to the characteristics of explosion of anti-shipweapons and ammunition in cabin, based on a cylindrical test device as a carrier which simulates the explosion effect in ship cabin after the perforation of strip fragments, a data acquisition method,measuring point layout method and data processing method of characterization parameters of the power evaluation method are determined, and a power evaluation method of explosive internal explosion isestablished. At present, that evaluation method of the internal explosion power can only reflect the shock wave and the quasi-static pressure damage effect, and it is difficult to reflect the shock wave universally existing in the real scene. The invention can overcome the defect that the current evaluation method of the internal explosion power can only reflect the shock wave and the quasi-static pressure damage effect and the insufficiency of shock wave-fragmentation combined damage effect generally existing in a real scene cannot be reflected, the explosion effect of explosives in ship cabin structure is reflected comprehensively, which is helpful to evaluate the explosion power of anti-ship implosion weapon and ammunition more objectively and scientifically, and support explosives loading screening evaluation.
Owner:XIAN MODERN CHEM RES INST

Displacement damage dose detecting method for spacecraft device

ActiveCN101697000AOvercoming non-ideal monoenergeticOvercome the effects of secondary radiationContactless testingNuclear technologySecondary radiation
The invention discloses a displacement damage dose detecting method for a spacecraft device, which belongs to the technical field of radiation detection in nuclear technology. The method comprises the following steps: scaling a photoelectric coupler integrated with an LED and a PD by using a radiation source to acquire a response curve of the increment of current transmission rate reciprocal of the photoelectric coupler during normalization and the displacement damage dose; then radiating the photoelectric coupler by using a ground displacement damage effect testing and evaluating source to acquire the increment of the current transmission rate reciprocal of the photoelectric coupler; and according to the increment of the current transmission rate reciprocal of the photoelectric coupler during specific radiation, searching the displacement damage dose corresponding to the increment in the response curve so as to detect the displacement damage dose at the moment. The method overcomes the influence of non-ideal single energy and secondary radiation of a general testing simulation source; and compared with the conventional method which only uses the LED to perform displacement damage detection, the testing system is simple and practical, and the error of optical coupling introduction is eliminated.
Owner:NO 510 INST THE FIFTH RES INST OFCHINA AEROSPAE SCI & TECH

Tianhe supercomputer-based city explosion damage effect assessment method

The invention relates to the technical field of explosion damage assessment, in particular to a Tianhe supercomputer-based city explosion damage effect assessment method. The method comprises the steps of extracting typical analysis characteristics of city buildings through a BIM; establishing and solving a setting rule according to a simulation model; developing modeling and solving display programs on a simulation software platform and a Tianhe supercomputer platform; realizing automatic simulation model building, solving calculation and display function customization; and realizing city explosion damage effect assessment. According to the method, large-scale and high-precision multi-task parallel calculation of the complex simulation model can be performed based on a Tianhe-1 supercomputer, so that the calculation cycle is shortened; by virtue of the BIM, accurate city geometric information can be quickly extracted, and a corresponding geometric model is generated according to analysis needs; and based on this, a simulation solving model is automatically built according to the analysis needs, and corresponding software and hardware resources are matched, so that the time for adjusting the model by personnel is shortened and relatively good calculation configuration is achieved.
Owner:国家超级计算天津中心

Space radiation reliability evaluation method for an aerospace electronic product

The invention discloses a space radiation reliability evaluation method for an aerospace electronic product. The method comprises the steps of making fault physical analysis; establishing a space radiation related fault information matrix, and classifying and collecting parameters of the physical model; carrying out single event effect simulation, total dose effect simulation and displacement damage effect simulation, considering the mutual relation between spatial fault mechanisms, analyzing the simulation life of the tested device under the single event effect, the total dose effect and thedisplacement damage effect, and acquiring the failure life of the tested device under the combined action of the spatial radiation environment effect. According to the invention, from the perspectiveof a fault mechanism; Aimed at the reliability development research related to the space radiation of the spaceflight electronic product, the invention provides a method for evaluating the space radiation reliability of the spaceflight electronic product based on simulation analysis, so that a designer can intuitively understand the space radiation reliability level of the product in the design stage, thereby providing a reference basis for the design improvement of the product.
Owner:BEIHANG UNIV

Multifunctional high-speed impact experimental equipment

The invention discloses multifunctional high-speed impact experimental equipment. The multifunctional high-speed impact experimental equipment comprises a launching device, a barrel and a target chamber, wherein the launching device is connected with the barrel, and the barrel is connected with the target chamber through a projectile sabot separation device. A speed measuring device and a target plate loading device are arranged in the target chamber, the target plate loading device comprises a horizontal stretching servo actuator, a vertical stretching servo actuator, a frame, a horizontal adjusting mechanism, a vertical adjusting mechanism, a rotating mechanism, wheels and a hydraulic source, the periphery of the hydraulic source is arranged on the frame through the horizontal stretching servo actuator, the vertical stretching servo actuator, the horizontal adjusting mechanism and the vertical adjusting mechanism, the rotating mechanism is arranged at the lower end of the vertical adjusting mechanism, the wheels are arranged at two ends below the rotating mechanism, and the target plate loading device is mobile. The multifunctional high-speed impact experimental equipment can be used for plate impact experiments and high-speed impact damage effect experiments when a structure is in a loaded state.
Owner:AIR FORCE ENG UNIV OF PLA AIRCRAFT MAINTENACE MANAGEMENT SERGEANT SCHOOL

Missile control method based on to-ground perpendicular strike guidance law

The invention relates to a missile control method based on a to-ground perpendicular strike guidance law. The method comprises the steps that (1) a missile and target relative motion mathematical model is established, the aim of constraining the missile strike angle can be indirectly achieved by assigning the missile and target relative motion speed, and an optimum control model containing strikeangle constraining is established; (2) a Schwartz inequality method is used for deriving a solution of an optimal control problem, that is, a relation expression of a missile overload command, the estimated strike time and the missile and target relative speed is obtained; and (3) the missile and target relative speed and the missile and target relative distance are obtained through missile-bornedetection equipment, a missile-borne computer is used for calculating the missile and target remaining flight time, the missile overload command is formed by using the guidance law, and a missile is manipulated to strike the target with a vertical attack angle. The guidance law can make the missile strike the target vertically, the characteristics such as the simple structure, easy realization andthe optimal result are achieved, and the damage effect on the to-ground target can be improved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV
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