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250 results about "Large deflection" patented technology

Method for configuring shape of supporting roll of four-high mill and shape of working roll thereof

ActiveCN101554635ASolve peelingSolve the large amount of wear and tearCounter-pressure devicesRollsProduction lineStress concentration
The invention relates to a method for configuring the shape of a supporting roll of a four-high mill and the shape of a working roll thereof, belonging to the technical field of steel rolling. According to three types of width specifications of band steel which are most rolled by hot-rolling band steel production line, sixth-power polynomial supporting roll shape technology and second-power working roll shape curve are used for configuration so as to lead the contact length of the supporting roll and the working roll and the width of the rolled band steel to be fit. The method has the advantages of eliminating hazardous contact areas in which the parts of the two ends of the supporting roll with the flat roll shape and the working roll expand out of the edge of the band steel to generate large deflection and deformation, solving the problems that the stress concentration of the edges of the supporting roll and the working roll in a hot continuous mill for wide band steel causes stripping and the mill roll with the flat roll shape has large wearing capacity and is not even, reducing the consumption of the mill rill, saving energy, reducing consumption and reducing cost for rolling steel; and by the technical configuration of R2 working roll shape and the supporting roll shape, the invention solves the plate-shape problems that the middle blank generates negative convexity and the wedge shape is large, and improves the control precision of the shape of hot-rolled band steel.
Owner:SHOUGANG CORPORATION

Puncture enhancing method and system

The invention discloses a puncture enhancing method. The method comprises the steps that when an ultrasonic probe transmits ultrasonic waves with a large deflection angle for scanning in this cycle so as to display a puncture needle image in an enhanced mode, ultrasonic waves with different transmitting angles and a specific waveform are transmitted for scanning; the insertion orientation of a puncture needle is identified according to scanned image frame data corresponding to the ultrasonic waves with the specific waveform at different transmitting angles; a corresponding large deflection angle when the ultrasonic probe transmits ultrasonic waves with the large deflection angle in a next cycle is adjusted according to the identified insertion orientation of the puncture needle, and the transmitting direction of the ultrasonic waves is perpendicular to or approximately perpendicular to the identified insertion orientation of the puncture needle under the large deflection angle. The invention further discloses a puncture enhancing system. By means of the puncture enhancing method and system, the insertion orientation of the puncture needle can be rapidly detected, and therefore the insertion direction of the puncture needle does not need to be fixed. Meanwhile, the complexity of puncture enhancing manipulation is reduced by automatically adjusting the large deflection angle of the ultrasonic probe, and the optimal display effect of the puncture enhancing image is always maintained.
Owner:SHENZHEN WISONIC MEDICAL TECH CO LTD

Prejudging method for static-test load carrying capacity of wing structure

The invention belongs to the technology of airplane structural strength and relates to a prejudging method for the static-test load carrying capacity of a wing structure. The prejudging method of the invention comprises the steps as follows: establishing a finite element model according to a wing structure before carrying out an actual test, and performing elastoplasticity and large deflection nonlinear finite element analysis to the model to obtain a wingtip deflection-load curve; determining maximum load carrying capacity of the wing structure according to the variation characteristic of the wingtip deflection-load curve and giving out the breaking load of the wing structure; obtaining a dangerous portion of the wing structure and the process form the unstable condition to the destructive condition and pre-judging the static-test load carrying capacity of the wing structure. According to the invention, the error between the calculated breaking load and the tested breaking load is 6.25 percent. The calculated dangerous part and the tested breaking portion are consistent. The calculated process form the unstable condition to the destructive condition is consistent with the tested unstable process. The method of the invention provides a guarantee for the one-time success of the static test of the structure and provides reference for evaluating the structural strength of the wing.
Owner:上海秦耀航空试验技术有限公司

Fast reflection mirror

The invention discloses a fast reflection mirror, comprising a base, a working mirror body, cross spring bearings and a driver; the working mirror body is assembled on a reflection mirror seat; two cross spring bearings constitute one group, there are totally two groups, wherein the axes of the two cross spring bearings in the first group of cross spring bearings coincide with a first straight line, and the axes of the two cross spring bearings in the second group of cross spring bearings coincide with a second straight line; the first straight line and the second straight line are perpendicular to each other and intersected at an origin; each cross spring bearing is connected to the reflection mirror seat and the base respectively; and the driver is used for driving the reflection mirrorseat to rotate within a preset angle range around the first straight line and/or the second straight line. According to the fast reflection mirror, the cross spring bearings support the reflection mirror seat, the cross spring bearings have the advantages of large deflection range and high rotating precision, and when the cross spring bearings are used with the driver, the deflection angle and therotating precision of the working mirror body can be improved, so that the fast reflection mirror is applicable in the fields of precision machinery, precision measuring instruments, medical equipment and the like.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Control mechanism for rapid deflection reflection mirror with rotation center arranged at reflection surface and method thereof

The invention provides a control mechanism for a rapid deflection reflection mirror with the rotation center arranged at the reflection surface and a method thereof. The control mechanism comprises a first driving mechanism and a third driving mechanism which are arranged at the two ends of an X-axis of deflection and symmetrical about a Y-axis of deflection, and a second driving mechanism and a fourth driving mechanism which are arranged at the two ends of the Y-axis of deflection and symmetrical about the X-axis of deflection. The first driving mechanism is connected with a mirror supporting structure via a first flexible hinge perpendicular to the first driving mechanism. The structure and the size of the second driving mechanism, the third driving mechanism and the fourth driving mechanism are identical to those of the first driving mechanism, and the second driving mechanism, the third driving mechanism and the fourth driving mechanism are connected with the mirror supporting structure via a second flexible hinge, a third flexible hinge and a fourth flexible hinge respectively. The side surface of the reflection mirror is fixed on the mirror supporting structure. The mirror surface of the reflection mirror and the X-axis of deflection and the Y-axis of deflection are arranged in the same plane. The invention also provides a control method of the control mechanism. The control mechanism has relatively large deflection range and also has the characteristics of high response speed, small size and low weight.
Owner:XI AN JIAOTONG UNIV

Method for butting and synchronously unloading segments of steel truss structure in air

ActiveCN107143145ASolve problems that are difficult to control qualityRelease local internal forceBuilding material handlingShoresEngineeringStructure Collapse
The invention discloses a method for butting and synchronously unloading segments of a steel truss structure in the air. The method comprises the following steps: (1) manufacturing and mounting a temporary supporting frame; (2) manufacturing and mounting an operating platform; (3) manufacturing and mounting a scaffold; (4) hoisting a truss in position; (5) butting truss segments in the air and permanently fixing; (6) enabling a jack to be in position; (7) mounting a first U-shaped sleeve groove; (8) removing the scaffold, and mounting a lower bearing beam; (9) mounting a second U-shaped sleeve groove; (10) mounting a limiting steel pin rod and a limiting plate; and (11) unloading step by step. The method disclosed by the invention has the advantages that the problem that the quality is difficult to control when a long-span plane truss adopts a segmental mounting method is effectively solved, an unloading process is steady and controllable, the phenomena that the original structure produces larger deflection, local rod pieces are over-stressed, node connection is destroyed and even structure collapse is caused due to an improper unloading scheme can be avoided, and synchronous unloading of the truss structure is realized.
Owner:浙江中南绿建科技集团有限公司

Large-deflection self-adaptive seal for low-speed equipment

ActiveCN105465372AFit closelyEnlarging the sealing surfaceEngine sealsLow speedEngineering
The invention discloses a large-deflection self-adaptive seal for low-speed equipment. The large-deflection self-adaption seal for the low-speed equipment comprises a shaft sleeve, a seal cavity, a connecting plate and a static ring and a moving ring which are arranged in a cavity body of the seal cavity; the shaft sleeve penetrates through the seal cavity, the static ring and the moving ring are arranged on the shaft sleeve in a sleeving mode, the connecting plate is fixedly connected with the shaft sleeve, and the moving ring is fixedly installed on the connecting plate; the static ring comprises a connecting end and a seal end which are connected by adopting a flexible structure, the static ring is fixedly connected with the seal cavity through the connecting end, a static ring seal ring is arranged between the seal end and the shaft sleeve, and the seal end is provided with an arc-shaped seal end face; the moving ring is provided with an arc-shaped seal end face matched with the seal end of the static ring, the static ring and the moving ring are cooperatively connected through the seal end faces, the seal end of the static ring is provided with a jacking mechanism, and the jacking mechanism applies jacking force to the seal end to enable the seal end face of the static ring and the seal end face of the moving ring to be closely matched. The seal adopts arrangement of the arc-shaped seal end faces and the flexible connecting structure and solves the leakage problem caused by rotating shaft eccentricity.
Owner:CHENGDU YITONG SEAL

Two-dimensional large-angle fast deflection reflector

The invention relates to a two-dimensional large-angle rapid deflection reflector. The reflector comprises a reflecting mirror assembly, a supporting assembly, a driving assembly, a sensor assembly and a base. The supporting assembly is a self-made ball bearing and can freely rotate around the sphere center of the supporting assembly; and the supporting assembly is pre-tightened through a conical spiral spring, so that the supporting assembly can be kept at an initial zero angle position without the driving of an external force. According to the driving assembly, four voice coil motors are adopted as driving components; the sphere centers of the voice coil motors are overlapped with the sphere center of the supporting assembly; the voice coil motors push the supporting assembly to perform two-dimensional rotation; and gaps between the magnetic steel and coils of the voice coil motors are always constant, and therefore, the magnetic steel will not collide with the coils, and relatively large deflection angles can be generated. The sphere centers of the supporting assembly and the driving assembly are located on the reflection surface of a plane reflecting mirror, so that the two mutually perpendicular deflection axes of the reflecting mirror are located on the surface of the reflecting mirror. In the fast deflecting process of the reflecting mirror, the translational movement of a reflection light beam caused by a condition that the deflection axes of a reflecting mirror are not overlapped with the surface of the reflecting mirror can be eliminated, and the control precision of the light beam is improved.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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