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602 results about "Torsional deformation" patented technology

High-frequency vibration motor for electric toothbrush

The invention relates to the technical field of electric toothbrushes, in particular to a high-frequency vibration motor for an electric toothbrush. The high-frequency vibration motor for the electric toothbrush comprises a shell and a rear cover, wherein a stator, a rotating shaft and an adjusting pad are arranged in the shell; the output end of the rotating shaft is connected with the rear cover through a spring piece; the spring piece comprises a spring piece main body and an elastic arm; the motor generates power to drive the rotating shaft to rotate reciprocally so as to drive the springpiece connected with the rotating shaft to twist to generate torsional deformation; when the frequency of the motor generating reciprocating movement is close to or reaches the torsional resonant frequency of the spring piece, the torsional vibration amplitude of the spring piece reaches the maximum so that the swinging amplitude of the motor reaches the maximum; because of the influence of the reluctance force of the motor per se, the vibration amplitude of an overall system reaches a balanced state, and the spring piece and the motor generate movement under the balanced condition. The high-frequency vibration motor for the electric toothbrush is easy to manufacture and position, along with reasonable structure, less elements, simple machining process, low cost and long service life.
Owner:DONGGUAN LEBOND ELECTRONICS TECH CO LTD

Precise milling processing method with variable inter-row allowance for thin walled blade of difficult-to-process material

ActiveCN102873384AThe direct effect is obviousImprove section positionMilling equipment detailsSpecial data processing applicationsNumerical controlTorsional deformation
The invention provides a precise milling processing method with a variable inter-row allowance for thin walled blades of difficult-to-process materials; four driving curved surfaces are obtained by cutting a blade root boundary surface and a blade tip boundary surface into a blade back curved surface and a blade basin curved surface; parameter lines with equal u on the driving curved surfaces are used as processing paths; a cutting row allowance for each processing path is set respectively; and finally processing on the four driving curved surfaces are completed circularly. The invention facilitates the improvement of the blade cross section position accuracy, facilitates the improvement of the blade surface profile tolerance, and facilitates the reduction of the blade torsional deformation; when compared with traditional vertical cutting with a constant allowance and spiral milling methods, the invention can solve the technical problems of large torsional deformation, poor profile precision, difficultly-controlled cross section position accuracy error, and the like, and can realize the high-efficient precise numerical control processing of thin walled blades of difficult-to-process materials.
Owner:西安三航动力科技有限公司

Push-bending forming process for hollow blade

The invention discloses a push-bending forming process for a hollow blade. The process comprises producing a mould cavity curved surface according to a finished product hollow blade appearance curved surface; machining a mould according to the mould cavity curved surface and forming a mould cavity passage with two open sides in the mould; designing a chuck according to the blade tenon shape; fixing the chuck and the mould on a hot press; coating high-temperature lubricants on the inner surface of the mould cavity and the surface of a blade blank; mounting the blade blank on the chuck. The hot press acts, the mould is closed, the chuck drives the blade to move towards the mould to push the blade into the mould cavity from one end of the mould cavity passage, and the blade is forced to be bent under the action of the mould cavity inner surface and is subjected to torsional deformation; the mould is opened after the torsional deformation is kept for certain time, and the formed blade is dismounted. According to the process, slab hollow blade blanks can be formed into complex torsional forms and are provided with required torsion angles, the forming process is stable and convenient and fast, the speed is controllable, deformation distribution of all parts are uniform, and the production efficiency is high.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Pipeline inner wall bionic groove surface machining device and machining method thereof

The invention provides a pipeline inner wall bionic groove surface machining device and a machining method thereof. The device comprises a drive mechanism used for providing drive force, a traveling mechanism used for supporting the inner wall face of a pipeline, a machining mechanism used for machining a bionic groove in the inner wall of the machined pipeline, and a controller. The drive mechanism is installed on the traveling mechanism through bolts. The machining mechanism is fixedly connected with the traveling mechanism through bolts. The drive mechanism and the machining mechanism are electrically connected with corresponding control ends of the controller. The method comprises the steps that according to the diameter of the pipeline needing to be machined, a front and back traveling unit is adjusted in a rotating manner, after the machining mechanism is moved to the position, to be machined, on the inner wall of the pipeline, the traveling unit stops moving and presses the inner wall of the pipeline, the cutter position of the machining mechanism is adjusted, and the groove in the inner wall of the pipeline begins to be machined. The device has the beneficial effects that tangential counter force borne by three tools in the cutting machining process can be offset, thus, bending deformation and torsional deformation are avoided, and meanwhile the device is high in precision, simple in structure and easy to operate.
Owner:ZHEJIANG UNIV OF TECH

Method for calculating rigidity of aircraft airfoil surface structure

The invention discloses a method for calculating the rigidity of an aircraft airfoil surface structure. The method includes the steps that an airfoil-surface-structure finite element analysis model is built, wherein the airfoil-surface-structure finite element analysis model should be corrected through a static test and can really simulate the rigidity of the structure; sections of the root are restrained in the finite element analysis model, and then finite element analysis is carried out; the torsional rigidity of the structure is reversely derived through torsional deformation of the sections, and then the rigidity center positions of the sections are determined through a torsional rigidity calculation formula; and when the bending rigidity of the structure is calculated, small-deformation assumption is adopted, the finite element analysis is fitted to obtain displacement at the rigidity centers of the sections, a structure bending rigidity calculation formula is obtained accordingly, and the rigidity, the rigidity center positions and the bending rigidity of the aircraft airfoil surface structure are rapidly and accurately calculated through the structure bending rigidity calculation formula. In this way, the rigidity, the rigidity center positions and the bending rigidity of the aircraft airfoil surface structure are rapidly and accurately calculated; and in addition, experiments in aircrafts in multiple types verify that the algorithm is correct in principle, easy and convenient to implement and capable of meeting the aircraft designing requirement.
Owner:JIANGXI HONGDU AVIATION IND GRP

Torque measurement sensor based on phase difference of photoelectric encoder signals and measuring method

The invention discloses a torque measurement sensor based on the phase difference of photoelectric encoder signals. The torque measurement sensor comprises a shell; an elastic drive sleeve is mounted in the shell by use of a ball bearing; an elastic link is arranged in the middle part of the elastic drive sleeve; a photoelectric encoder sleeves each of the two ends of the elastic link, and the central angles of the two photoelectric encoders are equal; a mounting base is fixed on the top of the shell; a photoelectric sensor A and a photoelectric second B are fixed in the mounting base, and arranged in opposition to the two photoelectric encoders. The two photoelectric encoders are arranged at the two ends of the elastic link of the elastic drive sleeve and the two photoelectric sensors are used for obtaining square wave output signals when the encoders rotate, and then the measurement of the torsional deformation and torque of the elastic drive sleeve can be realized according to the phase difference of the square wave signals output by the two encoders. The torque measurement sensor based on the phase difference of the photoelectric encoder signals is used for solving the problem that the measurement accuracy of an existing torque sensor is prone to be effected by a magnetic field and an electric field; the torque measurement sensor is simple in measurement principle, high in anti-jamming capability, and capable of realizing high-dynamic and high-accuracy torque measurement of a drive mechanism.
Owner:XIAN UNIV OF TECH

Thin-walled vane nine-point control variable-allowance milling method based on Newton interpolation

The invention provides a thin-walled vane nine-point control variable-allowance milling method based on Newton interpolation. Modeling is carried out by utilizing a three-dimensional modeling software, and an auxiliary surface and a boundary surface are formed, so that a driving surface is determined by utilizing a section line lofting process. Cutter machining paths are generated according to the driving surface, and the machining allowance of each cutter position point on each machining path is determined by adopting a Newton interpolation method. Finally, vanes are cyclically processed according to symmetrical milling rules. Compared with a traditional longitudinal fixed-allowance cutting and spiral milling method, the thin-walled vane nine-point control variable-allowance milling method has the advantages that technical problems, such as large torsional deformation, low contour precision, poor section position tolerance and difficult error control, in the machining process can be solved; and by adopting a Newton interpolation process allowance fine adjustment method, surface quality can be more comprehensively controlled, and problems, such as large bending deformation, poor section position tolerance and low surface contour precision, in the machining process can be effectively solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV
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