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126results about How to "Ensure high precision requirements" patented technology

Digital loudspeaker drive method and device based on quaternary code dynamic mismatch reshaping

The invention relates to a digital loudspeaker drive method and a device based on quaternary code dynamic mismatch reshaping. The method comprises the steps of (1) conducting input format conversion, (2) conducting multi-bit sigma to delta modulation, (3) conducting thermometer code conversion, (4) conducting dynamic mismatch reshaping processing, (5) conducting channel data combination and mapping coding, (6) controlling metal-oxide-semiconductor field effect transistor (MOSFET) pipe of a full-bridge power amplifier network to conduct opening and closing status switching, and driving a digitalized loudspeaker load to produce sound. The device comprises a sound source (1), a digital format converter (2), a multi-bit sigma to delta modulator (3), a thermometer coder (4), a dynamic mismatch reshaper (5), a channel data combiner (6), a mapping coder (7), a multi-channel digital amplifier (8) and the digitalized loudspeaker load (9). The units are sequentially connected in order. According to the digital loudspeaker drive method and the device based on quaternary code dynamic mismatch reshaping, use efficiency of an amplifier pipe and the load is improved, development periods and hardware implementation cost are saved, and good immunity is provided for frequency response deviation of digital channels.
Owner:INST OF ACOUSTICS CHINESE ACAD OF SCI

Hinged mounting base on 100% modern city tramcar

The invention discloses a hinged mounting base on a 100% modern city tramcar. The hinged mounting base comprises an upper panel, a lower panel, a connecting rib plate, a rear block plate and a base, wherein the connecting rib plate is respectively connected to the upper panel, the lower panel and the rear block plate in a welding manner; the upper panel and the lower panel are welded on the rear block plate; the rear block plate is welded on the base; a hole for riveting is formed in the base. The hinged mounting base can be applied to installation of an upper hinge device of a 100% low-floor tramcar. The connection mode of the hinged mounting base and a car body is a riveting manner, so that not only is the hinged mounting base not limited by a roof end part material, but also the hinged mounting base can be conveniently repaired and replaced after being damaged. The hinged mounting base is welded by a high-strength carbon steel material, so that the hinged mounting base has enough strength and rigidity, and is especially applicable to local reinforcement on the hinged part on an aluminum alloy car body, the strength index of the overall car body is met, the weight of the car body is reduced, and the hinged mounting base has significant advantages of simple structure, reliable performance, good repairability and the like, and is convenient to assemble.
Owner:CHENGDU XINZHU ROAD & BRIDGE MASCH CO LTD

A method for modeling and forecasting that motion trajectory of space cluster target

ActiveCN109242886AHigh precisionComprehensive portrayal of sports characteristicsImage analysisAviationMathematical model
A method for characterizing and forecasting that trajectory of space group target features is disclosed, relating to the field of aerospace. That the mathematical model of the trajectory of group target is used to characterize the trajectory of space group target, and the tracking and forecasting accuracy of such target is improved. This method decomposes the cluster target motion into two parts:the whole cluster motion event and the salient target motion event in the cluster. For the whole cluster, the movement rule is characterized and predicted from the movement trend of cluster center, the evolution of cluster spatial structure and the relative movement of subgroups. For the salient target, based on the target resolution, the hierarchical modeling idea, the application of dynamics, kinematics and compensation modeling techniques are combined to achieve the characterization and prediction of its motion characteristics. The method described in the patent adopts the idea of combiningthe whole tracking with the local resolution to realize the modeling and prediction of the motion trajectory of the space cluster targets, and can directly serve the design of the tracking methods inthe fields of the space debris environment monitoring, the on-orbit service, the anti-missile early warning, the situation sensing, and the like, so as to improve the tracking performance of the cluster targets.
Owner:NO 63921 UNIT OF PLA

Guidance method for endoatmospheric powered phase of RLV (reusable launch vehicle)

The invention provides a guidance method for the endoatmospheric powered phase of a RLV (reusable launch vehicle), which includes the following steps: (S1) according to flight altitude, the ascent phase of the flight track of the RLV is divided into a previous flight phase and a later flight phase; (S2) open-loop guidance is adopted at the previous flight phase, and closed-loop guidance is adopted at the later flight phase; (S3) in the process of closed-loop guidance at the later flight phase, a compensation scheme for altitude and / or trajectory inclination angle is adopted. Compared with the prior art, the guidance method has the following advantages: (1) according to flight altitude, the guidance method divides the ascent phase into the two phases, which respectively adopt open-loop guidance and closed-loop guidance, consequently, not only is the problem that the robustness of closed-loop guidance is decreased by strong interference factors within the dense atmosphere effectively prevented, but also the high precision requirement of the guidance is ensured, and thereby both the robustness of a guidance algorithm and the high precision are taken into consideration; (2) the requirement of the scheme on the memory space and on-line computation load of an onboard computer of launch vehicle is low, guidance commands can be obtained only by interpolation and simple calculation, the reliability is high, and engineering implementability is ensured.
Owner:CHINA ACAD OF LAUNCH VEHICLE TECH

Rotating type varying stiffness flexible joint

The invention relates to a rotating type varying stiffness flexible joint. The joint is characterized by comprising a driving disc, an end cover, a torsional spring, a special-shaped gear set, a standard gear set, a first shaft, a second shaft, an output shaft, a shaft end fixed frame, a worm, a worm gear, a direct-current speed reduction motor, a coupler, a connecting plate, a worm fixing block, a clamping spring, a motor mounting base, fixing blocks and a bearing pedestal; the driving disc is fixed to the end cover, the end of the driving disc is connected with an outer motor directly through a speed reducer to serve as input of the flexible joint, the bearing pedestal and the shaft end fixing frame are arranged in the driving disc, the bearing pedestal and the driving disc are of an integral structure, the driving disc and the end cover are connected through a bolt to serve as a shell of the joint, the two ends of the shaft end fixing frame are fixed to the driving disc through the fixing blocks, the output shaft is fixedly arranged between the end cover and the shaft end foxing frame through a deep groove ball bearing, and the output shaft is connected with an outer component; the first shaft and the second shaft are fixed to the driving disc and the end cover through the deep groove ball bearing and the bearing pedestal.
Owner:HEBEI UNIV OF TECH

Attitude Compensation Method for Agile Satellite Imaging with Pushbroom Velocity Mismatch in Any Direction

The invention relates to a posture compensation method for dealing with mismatching of a push-scanning speed for imaging along random direction of a quick satellite. For breaking through the limitation (only taking the deflecting effect caused by earth rotation into consideration) of the posture compensation method under a traditional imaging mode (fixed direction from satellite to earth), the reason why the deflecting effect is generated under the imaging mode with constantly changing posture-to-earth direction (namely, posture-to-earth direction constantly changes under the condition of mismatching between a satellite spot speed and a camera push-scanning speed) when the satellite is used for push-scanning along random direction is analyzed and the imaging deflecting effect is analyzed from three aspects of orbital motion, earth rotation and camera push-scanning speed, thereby acquiring a deflecting angle calculation formula under such a mode according to the track posture parameters and the basic definition of a deflecting angle. Based on the deflecting angle calculation formula and a basic principle of TDICCD (Time Delay Integral Charge-coupled Device) imaging as well as a yawcontrol principle, the posture compensation method, which can meet the imaging requirement for push-scanning along random direction of the quick satellite, is provided.
Owner:AEROSPACE DONGFANGHONG SATELLITE

Method for manufacturing buoyancy tanks of semi-submerged ship

The invention discloses a method for manufacturing buoyancy tanks of a semi-submerged ship, which comprises the following steps of: (1) marking the center line of a movable jig frame, an involution line, the lower bottom position line and the top position line of an upper buoyancy tank as well as the upper top position line and the lower bottom position line of the lower buoyancy tank by using a total station on a jig position, and controlling the position line distance between the lower bottom of the upper buoyancy tank and the upper top of the lower buoyancy tank to be between 1 mm and 4 mm; (2) respectively manufacturing six face sheets of the upper buoyancy tank and sixe face sheets of the lower buoyancy tank on a platform; (3) respectively suspending the respective six face sheets ofthe upper buoyancy tank and the lower buoyancy tank to build the buoyancy tanks; (4) completing the assembly and welding of limiting slide slots of the upper buoyancy tank and the lower buoyancy tank, and completing the matching and drilling of connecting bolt holes of the upper buoyancy tank and the lower buoyancy tank; and (5) respectively and vertically suspending the upper buoyancy tank and the lower buoyancy tank by using a crane to leave the movable jig frame after the upper buoyancy tank and the lower buoyancy tank are approved to be qualified, and completing the separation of the upper buoyancy tank and the lower buoyancy tank in the air. The invention not only ensures the high-precision building requirements of the upper buoyancy tank and the lower buoyancy tank, but also completes the matching and drilling works of the connecting bolts of the upper buoyancy tank and the lower buoyancy tank in a section in advance.
Owner:CSSC HUANGPU WENCHONG SHIPBUILDING COMPANY

Attitude Compensation Method for Agile Satellite Imaging Side Swing Pushbroom Velocity Mismatch

The invention discloses a posture compensation method in case of mismatched side-swing push-broom velocity in imaging of an agile satellite. For the limitation (only the drift action caused by auto-rotation of the earth is considered) of the posture compensation method in the traditional imaging mode (the pointing direction of the satellite to the ground is fixed), the drift angle calculation formula is obtained under the mode according to the track posture parameter by analyzing the reason for the generation of the drift angle under the imaging mode (namely the condition that the substellar point velocity is mismatched with the push-broom velocity of a camera, and the pointing direction of the posture at the moment to the earth changes continuously) that the pointing direction of the side-swing push-broom posture of the satellite to the earth changes continuously, considering the drift action of the imaging from the three aspects such as orbital motion, auto-rotation of the earth andthe push-broom velocity of a camera and combining the basic definition of the drift angle. On the basis, by combination of the basic principle of TDICCD (time delay integration charged coupling device) imaging and the yawing control principle, the satellite posture compensation method is given, so that the imaging requirement for side-swing push and broom of the agile satellite can be met.
Owner:AEROSPACE DONGFANGHONG SATELLITE

Workpiece micro shock excitation device and workpiece micro shock excitation method for vibration machining

The invention discloses a workpiece micro shock excitation device and a workpiece micro shock excitation method for vibration machining, in order to solve the problem that no simple and practical workpiece micro shock excitation device or workpiece micro shock excitation method for the vibration machining exists at present. The workpiece micro shock excitation device is characterized in that a servo motor drives an eccentric shaft; an eccentric groove at the bottom of a vibration table is tangent with an eccentric wheel of the eccentric shaft; n pin rollers are equally divided into two groups to be arranged on the two sides of the eccentric shaft; two sliding blocks are arranged on the two sides of the bottom of the vibration table; and the top and the bottom of each sliding block correspond to one group of pin rollers to form a rolling pair. The workpiece micro shock excitation method for the vibration machining comprises the steps as follows: a workpiece is arranged at the top of a three-directional force sensor and clamped by a fixture; the servo motor drives the eccentric shaft to excite the vibration table to vibrate; and a monitoring system monitors and optimizes workpiece vibration cutting, and controls the servo motor to adjust the vibration frequency of the workpiece. According to the workpiece micro shock excitation device and the workpiece micro shock excitation method for the vibration machining, workpiece micro shock excitation machining can be realized efficiently, and the micro displacement vibration frequency and the cutting carrying capacity of the workpiece are monitored, detected and diagnosed in real time.
Owner:长沙启铭机电设备有限公司

Turning fixture for once clamping processing of valve

InactiveCN102179713ASolving Machining ComplexitySolve the processing technologyPositioning apparatusMetal-working holdersEngineeringGasket
The invention discloses a turning fixture for once clamping processing of a valve, wherein bottom outer side walls of a support block (6) and an angle iron module (1) are horizontal; a bottom central hole of the angle iron module is tightly matched with the central hole of the support block; a T-shaped bolt (5) is placed in the support block (6) through an opening slot, passes through two throughholes on the bottom of the angle iron module (1) and then is fixed by a locking nut (2); a correcting block which is leveled is fixed on the support block (6) through a bolt (4); bottoms of two hanging bolts (10) are respectively arranged in the support block (6); top mounting pressing blocks (11) of the two hanging bolts (10) are fixed by hanging nuts (12); and a rotary spindle (8) is connected to the central hole of the support block (6) and the central hole of the angle iron module (1) through a gasket (7), thereby integrally forming the turning fixture. By using the turning fixture, the threads and openings at two ends of the valve can be once fixed and successfully processed by using a common lathe or a numeric control lathe, the cost is lowered, the processing efficiency is increased, and the problem of difficult processing of similar parts is thoroughly solved.
Owner:JIANGSU JINSHI VALVE

Assembly process of blind hole tool with high precision requirement

ActiveCN111168326AReduce dependency on skill levelGuaranteed accuracy requirementsStructural engineeringMachine
The invention belongs to the field of machining, and relates to an assembly process of a blind hole tool with a high precision requirement. The assembly process comprises the following steps of 1) processing a base, and ensuring the parallelism of two surfaces of the thickness of the base and the perpendicularity with an alignment reference surface; 2) processing a support plate, and ensuring theparallelism of the two surfaces of the thickness of the support plate and the perpendicularity with the bottom surface; 3) processing a support, and ensuring the parallelism of the two of the thickness of the support and the perpendicularity with the bottom surface; 4) processing a positioning plate; 5) processing a guide plate; 6) assembling the base, the support and the positioning plate into anintegral structure, fixing the integral structure on a workbench of the coordinate boring machine, machining a blind hole in the support by adopting a boring cutter, axially lifting the boring cutter, assembling the support plate on the base, replacing the boring cutter, and machining a through hole in the support plate on the support plate; and 7) assembling the guide plate on the support by anadjusting assembly method. According to the assembly process of the blind hole tool with the high precision requirement, the requirement for the assembly form and location tolerance is met, dependenceon the skill level of workers is reduced, and the assembly qualification rate can be greatly increased.
Owner:XIAN AERO ENGINE CONTROLS
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