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41results about How to "Improve one-time assembly pass rate" patented technology

Method for calculating rotor assembly axis deflection based on end-skip measurement

ActiveCN109117460AReduce the number of repeated disassembly and assemblyImprove one-time assembly pass rateComplex mathematical operationsAviationTransformation algorithm
The invention relates to a method for calculating rotor assembly axis deflection based on end-skip measurement, which comprises three parts: calculation of three contact points, triangle judgment criterion and homogeneous coordinate transformation algorithm of deflection matrix. The three-point contact calculation mainly includes the characterization of initial measurement data, the determinationof contact point, the determination of deflection direction and the characterization method. The triangle criterion is used to judge whether the three points are in conformity with the reality, and the principle of determination, calculation method and the determination process of abandoned points are described in detail. The homogeneous coordinate transformation algorithm of deflection matrix includes the matrix representation of inclination direction and size, the calculation method and matrix representation of the overall axis deflection of the final assembly result, etc. Based on the measured end-skip data in production practice, the method realizes the prediction of axis deviation before assembly, improves the coaxiality of the assembled rotor, and greatly improves the pass rate of one-time assembly, which has important practical guiding significance for the axis prediction, assembly phase adjustment and optimization in the assembly process of aero-engine rotor parts.
Owner:DALIAN UNIV OF TECH

Method for calculating rotor assembly axis eccentricity based on radial skip measurement

ActiveCN109117461AReduce the number of repeated disassembly and assemblyImprove one-time assembly pass rateComplex mathematical operationsContact forceComputer science
The invention relates to a method for calculating the eccentricity of a rotor assembly axis based on radial skip measurement, which comprises the matrix representation of each point data and the calculation of relative skip value, the establishment of an equivalent spring model and the calculation of each point contact force under an ideal state, and the direction and magnitude of the eccentricity. The calculation of relative runout value of each point and the calculation of assembly interference of each point according to the diameter jump data of two stopper fitting surfaces; Based on the assumption of elastic deformation, the spring equivalent model is established to analyze the relationship between force and displacement in each stage of the contact process, and then the non-uniform contact force at each point is obtained by the non-uniform interference. The determination of eccentricity is based on the equivalent model of spring and the equilibrium equation of state to determine the size of the eccentricity. Based on the measured diameter skip data in production practice, the method realizes the prediction of axis eccentricity before assembly, improves the coaxiality of rotorafter assembly, and has important practical guiding significance for the axis prediction, assembly phase adjustment and optimization in the assembly process of aero-engine rotor parts.
Owner:DALIAN UNIV OF TECH

Elastic algorithm for calculating rotor assembly pose based on end jump measurement

The invention discloses an elastic algorithm for calculating a rotor assembly pose based on end jump measurement. A rotor matching surface is equivalent to a plurality of micro-convex body contact pairs; the contact elastic deformation is calculated by using a Hertz contact rule, contact pairs which actually contact with each other are separated; the final contact state is judged through the energy and torque balance equation, the normal vector of the contact plane is finally solved to represent the contact pose, the rotor assembly pose prediction accuracy is improved, the assembly coaxialitycan be well reflected, and rotor assembly phase prediction and optimization are better achieved. The method is based on actually measured end hop data in actual production; elastic deformation generated in the assembly process is considered; the method has the advantages that the defects of a rigid prediction algorithm are overcome, the accurate prediction of the assembly pose before assembly is realized, the rotor coaxiality after assembly is improved, meanwhile, the one-time assembly qualification rate is greatly improved, and the method has important practical guiding significance for axisprediction and assembly phase adjustment and optimization in the assembly process of the aero-engine rotor piece.
Owner:DALIAN UNIV OF TECH

End pressure type coaxial load

InactiveCN104409819AImprove power carrying capacityReduce reflectance valueWaveguide type devicesFrequency bandHeat sink
The invention discloses an end pressure type coaxial load. The end pressure type coaxial load comprises a cylindrical resistor, a compressed spring, an inner conductor, an insulating medium and an outer conductor which are coaxially arranged, as well as an end face shaft sleeve, wherein a compressed spring and a resistor hole are formed in the tail of the inner conductor; the cylindrical resistor is cylindrical; the two ends of the cylindrical resistor are sintered with silver resistors, and the other part of the cylindrical resistor is sintered with a thick-film resistor; the insulating medium is of a circle structure; the single side of the insulating medium is cut off through a seamless cutting technology, and impedance compensation rings are arranged on the both sides; the end face shaft sleeve is positioned at the top part of the outer conductor, used for positioning the insulating medium, the inner conductor and the cylindrical resistor, and meanwhile participates in transmission of electrical performance; cooling fins are arranged on the outer periphery of the outer conductor; a coaxial step type conical transmission cavity is defined inside the outer conductor. The end pressure type coaxial load disclosed by the invention is simple in structure, stable and reliable in properties, high in signal transmission efficiency, high in working frequency band, simple to assemble, easy to operate, and suitable for large batch production.
Owner:安徽蓝麦通信股份有限公司

Rotation axis determination method and system

The invention provides a rotation axis determination method, which is used for determining the rotation axis of an engine rotor, the engine rotor comprises two journals which are aligned and assembledon turntable equipment, and the method comprises the following steps of: establishing a cylindrical coordinate system and a Cartesian coordinate system on the turntable equipment; based on the cylindrical coordinate system, acquiring bounce data of a plurality of sections on the supporting cylindrical surface of each journal, wherein the bounce data comprises bounce values, angular phases and z-direction index values of the data acquisition points; converting the runout data of each journal into coordinate data relative to a Cartesian coordinate system in combination with the size of the engine rotor; obtaining a linear vector of each journal according to the coordinate data of each journal by utilizing a spiral theory and combining a cylindrical surface fitting method; and in combinationwith the gravity center distribution and the supporting range of the supporting cylindrical surface of each journal, coupling the linear vectors of the two journals, and obtaining the rotating axis of the engine rotor. The determination method can improve the determination precision of the rotation axis of the engine rotor.
Owner:AECC SHANGHAI COMML AIRCRAFT ENGINE MFG CO LTD +1

A Method for Calculating Eccentricity of Rotor Assembly Axis Based on Radial Runout Measurement

ActiveCN109117461BReduce the number of repeated disassembly and assemblyImprove one-time assembly pass rateComplex mathematical operationsContact forceMechanics
A method for calculating the eccentricity of the rotor assembly axis based on radial runout measurement, including the matrix representation of each point data and the calculation of the relative runout value, the establishment of the spring equivalent model and the calculation of the contact force of each point under the ideal state, the direction and size of the eccentricity; The calculation of the relative runout value of each point, and the process of calculating the assembly interference of each point according to the radial runout data of the two seam mating surfaces; the establishment of the spring equivalent model is based on the assumption of elastic deformation, and analyzes the force and contact at each stage during the contact process. Displacement relationship, the non-uniform contact force of each point is obtained by the non-uniform interference; the determination of the eccentricity is based on the spring equivalent model, and the final determination of the eccentricity is calculated according to the equilibrium state equation. This method is based on the measured radial runout data in actual production, realizes the prediction of the axis eccentricity before assembly, improves the rotor coaxiality after assembly, and predicts the axis, adjusts and optimizes the assembly phase during the assembly process of the aeroengine rotor parts It has important practical guiding significance.
Owner:DALIAN UNIV OF TECH

A radiation unit matching block assembly device and method

The invention relates to a radiation unit matching block assembly device and method. The assembly device includes a matching block clamp and a radiation unit clamp. An elastic pin is arranged in the radiation unit clamp, and a matching block limiter is provided on one side of the matching block clamp close to the end. slot, one end of the matching block fixture is provided with a limit opening connected with the limit groove of the matching block; wherein, when the matching block fixture drives the matching block to extend into the radiation unit, the elastic pin in the radiation unit fixture extends from the limit opening Matching block stop slot and abut one end of mating block. The invention sends the matching block into the radiation unit fixture through the matching block fixture, and uses the elastic pin to limit the matching block in the matching block limit groove, so that the fast installation of the matching block in the narrow space of the speaker cavity can be realized, and the traditional The problem of precise installation and positioning of the matching block improves the stability and consistency of assembly accuracy, ensures the distance dimension accuracy between the matching block inside the cavity of the antenna radiation unit and the positioning reference plane of the flange, and improves the first-time assembly qualification rate.
Owner:BEIJING INST OF RADIO MEASUREMENT

Low noise and high pressure differential regulating valve

The invention provides a low-noise high-pressure-difference adjusting valve which comprises a valve body, a valve cover, a sleeve, a valve element and a valve rod. The valve cover is connected to the top of the valve body through bolts, the sleeve is clamped between the valve cover and the valve body, a plurality of first-kind adjusting holes are formed in the upper portion of the side wall of the sleeve, a plurality of second-kind adjusting holes are formed in the lower portion of the side wall of the sleeve and the bottom face of the sleeve, the valve element is arranged in an inner cavity of the sleeve and can vertically move in the inner cavity of the sleeve, so that the low-noise high-pressure-difference adjusting valve is closed or opened, a plurality of pressure balance holes are formed in the valve element in the axial direction of the valve element, and the valve rod penetrates through a center through hole in the valve cover and is connected with the valve element. The low-noise high-pressure-difference adjusting valve is simple, compact and reasonable in structure, small in size and light, and has the advantage of being capable of bearing a high pressure difference and a high leakage level under the condition of the same drive source.
Owner:上海铂嘉阀门有限公司

Radiation unit matching block assembling device and method

ActiveCN112676807AQuick installationSolve the problem of precise installation and positioningRadiating elements structural formsMetal working apparatusControl theoryMechanical engineering
The invention relates to a radiation unit matching block assembling device and method. The assembling device comprises a matching block clamp and a radiation unit clamp, an elastic pin is disposed in the radiation unit clamp, a matching block limiting groove is disposed at the position, close to the end part, of one side of the matching block clamp, and a limiting port communicated with the matching block limiting groove is disposed on the end surface of one end of the matching block clamp; and when the matching block clamp drives a matching block to extend into a radiation unit, the elastic pin in the radiation unit clamp extends into the matching block limiting groove from the limiting port and abuts against one end of the matching block. The matching block is sent into the radiation unit clamp through the matching block clamp, the matching block in the matching block limiting groove is limited through the elastic pin, rapid installation of the matching block in a narrow space of a horn cavity can be achieved, the problem of accurate installation and positioning of a traditional matching block is solved, the stability and consistency of the assembly precision are improved, distance dimension precision between the matching block in an antenna radiation unit cavity and a flange plate positioning reference surface is guaranteed, and one-time assembling qualified rate is improved.
Owner:BEIJING INST OF RADIO MEASUREMENT

Pressure reduction type backflow preventing device

The invention provides a pressure reduction type backflow preventing device. According to an existing backflow preventing device, a pressure reduction portion adopts a membrane for transferring pressure and is sealed, however, due to the fact that a processing technique of the membrane is complex, the product quality is unstable, and the service life is influenced. The pressure reduction type backflow preventing device is composed of two check valves which work independently. A differential pressure relief valve is externally connected between the two check valves. The two ends of each check valve are further directly connected with two ball valves used for maintenance and four elastic sealed test ball valves, and therefore the complete pressure reduction type backflow preventing device is formed. Under the water supply condition, water in a main water delivery pipeline passes through a pressure reduction area from the check valve in the inlet position, reaches the outlet of the check valve in the outlet position, and is supplied to users. High-pressure water at the inlet of the check valve in the inlet position is directly led into an upper membrane cavity of a pressure reduction valve, and a lower membrane cavity communicates with the inlet of the check valve in the outlet position. Due to the fact that a certain pressure difference exists, a membrane is pushed to move rightwards, the pressure reduction valve is closed, and water supply is normal.
Owner:HARBIN REYAX TECH CO LTD

Coaxiality adjustment positioning device

ActiveCN104384917BEasy to liftSolve the problem of being stuck in the positioning toolMetal working apparatusEngineeringRelative motion
The invention discloses a coaxiality regulating and locating device. The coaxiality regulating and locating device comprises a bottom plate and a bearing seat, wherein the bearing seat is clamped in a through hole of the bottom plate through an upper flange, and the base is fixedly connected with the bearing seat through a screw; an air cylinder is fixedly connected with the base through a stud; an ejecting block in which an I-shaped hole is formed in the middle part is in clearance fit with a differential diameter hole, a piston rod of the air cylinder stretches into the I-shaped hole and is fixed with the I-shaped hole through a nut, a locating seat is arranged in a stepped hole of the bearing seat, and two bearings are arranged in a left gap and a right gap between the locating seat and the bearing seat. According to the coaxiality regulating and locating device disclosed by the invention, a workpiece and a locating tool can be rotated together by rotating the bearings, no relative motion is generated between the workpiece and the locating tool, friction is avoided, and thus the abrasion of a locating clamp is avoided; gaps between the locating tool and the workpiece are reduced, the regulating accuracy is increased, and the one-step assembling qualified rate is improved; a pneumatic lifting device is adopted, the problem that the workpiece is clamped in the locating tool due to high accuracy of the locating tool and small matching gaps between the locating tool and the workpiece is solved, and the workpiece can be conveniently lifted.
Owner:CHINA NTAIONAL NUCLEAR TIANJIN MACHINERY

A hydraulic shock absorber

The invention discloses an oil damper. The oil damper comprises an oil storage cylinder, a piston assembly, a work oil cylinder, a bottom valve assembly, a guide assembly and a gland. The oil storage cylinder comprises an outer cylinder body barrel and a base. An oil storage cavity is formed between the work oil cylinder and the outer cylinder body barrel. The guide assembly is arranged at the rear end of the work oil cylinder. The end, away from a piston, of a piston rod of the piston assembly penetrates out of the guide assembly and the gland outwards, and the piston divides the work oil cylinder into a first cavity and a second cavity. The base is provided with a compressing damping regulation valve, the inlet of the compressing damping regulation valve is communicated with the first cavity, and the outlet of the compressing damping regulation valve is communicated with the oil storage cavity. The guide assembly is provided with a stretching check valve and a stretching damping regulation valve, the inlet of the stretching check valve is communicated with the oil storage cavity, the outlet of the stretching check valve is communicated with the second cavity, the inlet of the stretching damping regulation valve is communicated with the second cavity, and the outlet of the stretching damping regulation valve is communicated with the oil storage cavity. The bottom valve assembly is provided with a one-way check valve. The oil damper has the advantages that the stretching and compressing damping force can be symmetric or asymmetric, can be independently adjusted and can be externally adjusted.
Owner:ZHUZHOU CSR TIMES ELECTRIC CO LTD

An Elastic Algorithm for Computing Rotor Assembly Pose Based on End Jump Measurement

An elastic algorithm for calculating the rotor assembly pose based on end-jump measurement. By equating the rotor mating surface into a plurality of asperity contact pairs, the Hertzian contact law is used to calculate the contact elastic deformation, and the actual contact contact pairs are separated. , use the energy and moment balance equation to judge the final contact state, and finally solve the normal vector of the contact plane to represent the contact pose, which improves the accuracy of the rotor assembly pose prediction, which can well reflect the assembly coaxiality, and better Realize the prediction and optimization of rotor assembly phase. This method is based on the measured end-jump data in actual production, and considers the elastic deformation generated during the assembly process, which makes up for the deficiency of the rigidity prediction algorithm, realizes the accurate prediction of the assembly pose before assembly, and improves the rotor synchronization after assembly. At the same time, the first-time assembly qualification rate is greatly improved, which has important practical guiding significance for axis prediction, assembly phase adjustment and optimization in the assembly process of aero-engine rotor parts.
Owner:DALIAN UNIV OF TECH

Pressure reduction piston type backflow preventer

The invention relates to the technical field of pressure reduction backflow preventers, in particular to a pressure reduction piston type backflow preventer which comprises a pressure reduction piston type backflow preventer body which is provided with a first test ball valve through a first test water nozzle. A first-stage check valve is arranged on the left side of the interior of the pressure reduction piston type backflow preventer body and corresponds to the water inlet, and a second-stage check valve is arranged on the right side of the interior of the pressure reduction piston type backflow preventer body and corresponds to the water outlet. A spring is arranged between the first-stage check valve and the second-stage check valve and located on the outer wall of the valve rod sleeve and the outer wall of the valve rod, a pressure reducing valve is installed at the end, away from the pressure reducing piston type backflow preventer body, of the pressure reducing pipe, and the valve rod sleeve and the valve rod are adopted between the first-stage check valve and the second-stage check valve to be used in cooperation with the spring through a piston connecting structure. The accuracy of spring force design of the pressure reduction part can be improved, and the one-time assembly yield of products is improved.
Owner:缪明镜

Solenoid valve and mass flow controller

The invention provides a solenoid valve and a mass flow controller. The solenoid valve includes a solenoid, a valve body assembly, a valve core assembly, a plug assembly, and a valve port component, wherein the valve core assembly, the plug assembly, and the valve port component are stacked in sequence. Placed in the accommodation chamber of the valve body assembly, the valve core assembly is movably arranged in the accommodation chamber, the plug assembly includes a magnetic seat and a plug, the magnetic seat is fixedly arranged in the accommodation chamber, and the plug is movably arranged In the mounting hole of the magnetic seat, the valve core assembly is in point contact with the plug, and the end face of the valve port part facing the plug assembly is provided with a valve port, and the plug is set opposite to the valve port; the electromagnetic part is used to magnetize the valve core assembly and the magnet. seat, so that the magnetic seat attracts the valve core assembly to move, and then drives the plug to move, and adjusts the distance between the plug and the valve port. The electromagnetic valve and the mass flow controller provided by the present invention can improve the working reliability and reduce the difficulty of assembly, so as to improve the first-time assembly pass rate, reduce the processing difficulty of parts and components, reduce the processing cost, and reduce their own volume.
Owner:BEIJING SEVENSTAR FLOW CO LTD
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