Dynamometric device
专利摘要:
The measuring journal according to the invention permits the construction of a measuring body which solves the troublefree transmission of a force between the structural elements, when measuring is carried out with the conversion of forces to electric signals, while in place of the shear- and bending stress, the mechanical stress is used for measuring-technical purpose. The measuring journal contains measuring elements connected to a central body and are developed as a longer and as a shorter measuring element. The torsional axes of the measuring elements are parallel with each other, are arranged symmetrically on both sides of the plane determined by the influence lines of the force bringing about the torsion and by those of the reaction force and are eccentric in relation to the geometrical axis of the measuring journal, while the plane determined by them is perpendicular to the plane determined by the reaction force and torsional force. The two ends of the measuring elements are linked through an arm of force to the connecting element that takes up the torsional force or reaction force, while the other ends of the measuring elements are in rigid connection with each other. 公开号:SU1093262A3 申请号:SU792850255 申请日:1979-12-06 公开日:1984-05-15 发明作者:Ковач Шандор 申请人:Вашипари Кутато Интезет (Инопредприятие); IPC主号:
专利说明:
1 The invention relates to the field of devices used to monitor and determine power parameters in testing systems that load forces and torque. A dynamic device is known comprising at least one measuring cell comprising two measuring elements, made in the form of rods, whose axes are parallel, and three connected in series with the ends of the measuring elements. body elements stop zones for the application of the measured force and registration of reactions f 1. The disadvantage of this device is the impossibility of its use in various devices with different schemes of application of forces. The purpose of the invention is to ensure versatility. This goal is achieved by the fact that in a dynamometric device containing at least one measuring cell, including two measuring elements, made in the form of rods, whose axes are parallel, and three connecting elements with supporting zones rigidly connected to the ends of the measuring elements for application of the leakage force and registration-reaction., the connecting elements are disk-shaped and arranged coaxially and the reference zones for the laying of the measured force and the register tion reactions lie in a plane passing through the axis izmeritelnk elements. In addition, the middle connecting element is 1; in, the sleeve - and is made with a cutout for the passage through it of the measuring element .. In addition, a torque wrench; the device is made of several cells interconnected coaxially by means of connecting cells and arranged mirror-like with respect to each other. FIG. 1 shows the construction of a dynamometric device; in fig. 2 is the same longitudinal section J in FIG. 3 shows section A-A in FIG. 2J in FIG. 4 - mechanical forces mounted according to FIG. 1-3 dynamometric devices; 2 FIG. 5 shows a device with a mechanical model in FIG. 6 is a variant of the assembly of several elementary frame structures; in fig. 7 - the same, the second option; in fig. 8 - the same, the third optionJ in FIG. 9 is the same, the fourth embodimentJ in FIG. 10 is a montage of a variant of FIG. 7J in FIG. 11 is a section BB in FIG. 10 in FIG. 12 of FIG. 9, partly in section in FIG. 13 is a section B-B in FIG. 12. In FIG. 1-3 show the form of the execution of a dynamometer device according to the invention. The dynamometer device consists of an elongated measuring element 1 and a shortened measuring element 2, as well as from the central body 3. Measuring elements 1 and 2 by means of connecting elements. 4 and 5 are attached to the structural units. The connecting element 4 is made as a reference connection for the device, and the connecting element 5 is a disk, which contains a cutout corresponding to the measuring element t and is fitted to the cover; sleeve 7 in the bearing bracket 6. The bearing clamp 4 holding the bearing bracket 8 is fixed to the base plate 9 that holds the sleeve 7. The bearing bracket 6 is fixed during intermediate switching on the spacer elements 10 and 11 on the load-carrying structure 12. The measuring elements are connected to measuring device. Measuring elements 1 and 2 are made in the form of .Cylindrical bodies and are placed on its both sides relative to the geometrical axis of the dynamometric device. The central body 3 is a disk whose diameter is smaller than the inner diameter of the sleeve 7. The central body 3 is rigidly connected to the ends of the measuring elements 1 and 2. The central body 3 is made up of two parts that are machined together with the measuring elements 1 and 2 respectively. The elongated element 1 with the connecting element 4 and the lower part of the central body is made in one piece, while the other part is formed by the shortened measuring element 2, the connecting element 5 and the upper part of the central body. body 3. After processing the two parts are connected by a permanent connection to a rigid system. The connecting elements A and 5 can also be manufactured as separate parts, in which case the connection with the measuring elements 1 and 2 takes place by means of a hot press connection. The connecting elements can be multifaceted and prismatic bodies, and the central body 3 can be made in the willow of any rigid element. FIG. 4 is a schematic diagram of the distribution of forces shown in FIG. 1-3 forms of execution. The measured force P, which through the sleeve 7 acts on the connecting element 5, causes a pair of forces P-j-P at the installation site. As an internal reaction, the Po force on the shoulder 1p acts, as a result, a reactive moment arises, through which the sleeve 7 is held parallel to the geometric axis .14, while the force P through the corresponding eccentricity 2. the shoulder forms a twisting moment in the measuring element 1. Coupling 5 works as a boom on one end, but due to its geometrical dimensions it must be considered absolutely rigid. In the shortened measuring element 2, which is rigidly connected to the central body 3 and to the connecting element 5, a bending moment is also produced in one of the two ends of the stressed boom. This moment is perpendicular to the longitudinal axis of the measuring element 2 and has, in the plane cut off passing through P the plane of the twisted measuring element 2, the value zero. In places of attachment its value is maximum. At the point connecting the central body and the measuring element 2 with each other, the bending moment appears on the central body 3 as a twisting moment and its reaction occurs at the point of attachment of the measuring element 1. By the correct choice of the geometric dimensions of the dynamometric device & 24 the absolute stiffness of the central body 3. The twisting moment of the measuring element 2 while it acts on one end of the central body perpendicular to the geometric axis 14 and perpendicular ikul angles to an axis intersecting the axis of the measuring element, loads the central body 3 on bending. At its other end, an opposite reactive moment is produced, which causes torsion in the measuring element 1. The arising voltages are a function of the cross section S of the element inertia I as well as the equatorial and polar factors of the cross section (K and Cr) of the elements 1 and 2 and also depends on the material properties. The above factors 9 determine the strength properties of the measuring elements 1 and 2. The other end of the elongated measuring element 1 adjoins the connecting element 4 and causes in it the corresponding eccentricity I - reactive force R. The parallelism of this element of the geometric axis 14 is ensured by the moment produced by the pair of forces on shoulder br. This is the internal load of the structure and it has nothing to do with the processes passing between the forces P and R. As a result of the forces of P and R (acting on the shoulder Lp of a pair of forces), the rigid frame structure could rotate around an axis that lies in a certain measuring element 1 and 2, as well as the geometric axis 14 of the plane and located perpendicular to it. This is prevented by the forces of Pg and Rjj excited in the structure (acting on the arm Lp of a pair of reactive forces). FIG. 5 explained in FIG. 4, the ratio of forces introduced in the axle axles according to FIG. 1-3. The force P acts on the outer shell of the sleeve 7 with a diameter Dp. Inside the structure there are measuring elements 1 and 2, as well as a central body 3, which through connecting elements 4 and 5 respectively are connected with other parts of the structure. The diameter D: - shell of the connecting element 4 formed as a part of it. The caps of the connecting element 4 are affected by the reactive force R. In the construction according to FIG. 1-5 lines of action of force P and reactive force R do not coincide. This means that the structure with respect to the line of action of force P is not symmetrical. This disadvantage can be eliminated if several of these frame structures are put together in pairs. Connections can be made in a variety of ways. The examples shown in FIG. 6-9. The connection can be made with central bodies (Fig. 6), with connecting elements 4 adjacent to the measuring elements 1 (Fig. 7) or connecting elements 5 adjacent to the measuring elements 2 (Fig. 8). The combination of elements can also be combined. Thus, in FIG. 9 shows, for example, the connection of the central body with the connecting element 5 adjacent to the measuring element 2. If both elementary structures according to FIG. 6 at the central bodies are connected to each other, then the central bodies 3 should communicate with each other. Connection 15 may be made as a connector, but may be loose. The central bodies 3 are also made from one piece (the most favorable solution). The system is loaded with concentrated forces P and can be viewed as propped at both ends or a boom is strained. Forces P and P can also be resultant systems of forces. 1 Both frame structures can also be connected to the measuring elements with connecting elements 4 (see Fig. 7). Here, the connecting elements 4 are attached to each other by a connection 15 and / or a connecting sleeve 16. It is preferable to manufacture the connecting elements 4 from one piece. Both different structures can also be attached to the connecting elements 5 connected to both the short-measuring measuring elements 2. This form of execution requires special care, since absolute rigidity and lack of friction must be ensured. The connection is also carried out here by means of connection 15 or sleeve 16. The structure is backed on two sides or tensioned and in the middle can be loaded with one or several concentrated and respectively distributed forces. Elementary frameworks can also be connected to each other by a combination of these methods. FIG. 9 shows the connection of frame structures with central bodies as well as connecting elements 5 that are attached to measuring elements 2. Central bodies 3 are connected to each other by connection 15, connecting elements 5 by connecting sleeve 16. At the same time, reactive forces R and R arise, which pass approximately symmetrically to the line of action of R. From the explained variants, only presented above in FIG. 6 and 8 are suitable for special tasks. In the embodiment shown in FIG. 6 addressing the load of the measuring elements, the forces P and P can be different in magnitude. This solution is advisable if, in the measurement task, the magnitude of the forces P and p should be determined separately, since the system can be performed as independent measuring systems once and double-pointed. The reactive forces R and R are influenced by the connection of the central bodies 3, by means of which certain balancing is carried out. The latter depends on the symmetry relations of the systems (suitable for special tasks). Similar is also shown in FIG. 8 is a solution in which the force P acts not symmetrically, so that the reactive forces are also not symmetrical. This deviation must be taken into account when sizing the systems. Shown in FIG. 7 n 9 devices can be used for most measurement tasks. The measurement systems according to FIG. 7 in practice, the bottom is depicted in the FNG. 10 and 11. The hook designs are shown, the elementary frame structures are located on both sides of the crane hook 17. The connecting elements 5 7109 are placed with bushings 7 in the yoke 18 of the screen. In the block 19 located between the connecting elements 5, the connecting elements 4 are joined. The reactive force R acts in the center line of the hook 20, the forces P and p lie in the plane of symmetry of the boom l 18 (the principle of operation is not affected by the fact that the force P and reactive force R here are rearranged, as with lifting mechanisms, the useful force is the raised weight force, which manifests itself as reactive force). . In the sleeves 7 there are connecting elements 5, as well as measuring elements 1 and respectively which are connected to the central bodies 3. The measuring elements, as well as the central bodies 3, act as a result. hard bonded as one body. 57 2 A The one shown in FIG. 10 and 11, the dual dynamometric device functions as a hook hook and at the same time perceives the arising force. The practical implementation shown in FIG. 9, the principle is shown in FIG. 12 and 13. In this case, the measuring elements 1, as well as the connecting elements 4 and COOTBIET itself 5, are arranged symmetrically on both sides of the central bodies-3. Thus, the device according to the invention makes it possible to transfer forces between different parts of the structure. At the same time, a load on shear and bending can be produced, which makes it possible to use mechanical stress for measurement purposes. gDtje.7 fig.c .fO 7 7 . already / ttt fie. // if
权利要求:
Claims (3) [1] 1. DYNAMOMETRIC DEVICE containing at least one measuring cell, including two measuring elements made in the form of rods, the axes of which are parallel, and three consecutively connected connecting elements with a shear force and reaction detection, characterized in that that, in order to ensure universality, the connecting elements are made disk-shaped and arranged coaxially: and the supporting zones for the application of the measured force and registration of the reaction lie at in a plane passing through the axis of the measuring elements. [2] 2. The device according to claim 1, wherein the middle connecting element is fixed in the sleeve and is made with a cutout for passage of the measuring element through it. [3] 3. The device πό π. 1, due to the fact that it is made of several cells interconnected coaxially by means of connecting elements and located mirror-relative to each other SU <,, 1093262
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同族专利:
公开号 | 公开日 GB2039373A|1980-08-06| JPS5928847B2|1984-07-16| DE2943613A1|1980-07-17| ATA605379A|1986-12-15| JPS5594125A|1980-07-17| DD147721A5|1981-04-15| US4350048A|1982-09-21| AT383682B|1987-08-10| GB2039373B|1983-05-25| DE2943613C2|1983-10-13| HU180974B|1983-05-30| FR2446470A1|1980-08-08| FR2446470B1|1982-11-19|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题 DE173832C| FR1010506A|1948-09-01|1952-06-12|Onera |Dynamometer| DE813318C|1949-06-04|1954-09-20|Georg Reicherter O H G|Torsion bar for force measurement| GB857759A|1956-09-20|1961-01-04|Vyzk A Zkusebni Letecky Ustav|An electromagnetic force measuring device| US2983140A|1956-10-01|1961-05-09|Martin Decker Corp|Load indicating and anchoring device for cables and other lines| US3026491A|1957-10-02|1962-03-20|Vyzk A Zkusebni Letecky Ustav|Indirectly excited electromagnetic feeler| GB899105A|1959-01-05|1962-06-20|Vyzk A Zkusebni Letecky Ustav|A device for converting a rectilinearly acting force into a torsional force| US3104544A|1959-02-26|1963-09-24|Rech S Et Etudes Electroniques|Devices for measuring torques| US3205706A|1962-12-04|1965-09-14|Task Corp|Ring-type load cell| SE311573B|1967-02-08|1969-06-16|Bofors Ab| US3370296A|1967-02-23|1968-02-20|Samuel W. Greenberg|Animal activity recorder| GB1184822A|1967-03-08|1970-03-18|English Electric Co Ltd|Torque-Sensitive Machines| US4058178A|1971-09-13|1977-11-15|Tadano Ironworks Co., Ltd.|Hydraulic cylinder unit| US3853001A|1972-07-13|1974-12-10|American Hoist & Derrick Co|Crane load measuring means| US3906788A|1974-05-23|1975-09-23|Nasa|Self-supporting strain transducer| US3969935A|1974-10-29|1976-07-20|Gse, Inc.|Load cell| FR2346278B1|1975-11-03|1978-08-18|Ferodo Sa| SE400650B|1976-01-15|1978-04-03|Bofors Ab|POWER SENSOR IN THE FORM OF A CYLINDER-SHAPED BEAM ARRANGED NOT TO BE LIKE A COHINGING ELEMENT IN A MECHANICAL COUPLING| DE2639762C3|1976-09-03|1984-08-16|Mannesmann AG, 4000 Düsseldorf|Load measuring device for hoists| US4083236A|1976-11-29|1978-04-11|Harry W. Dietert Co.|Load cell| US4199980A|1978-10-30|1980-04-29|Bell & Howell Company|Folded beam structure utilization methods and apparatus|JPS5821520A|1981-08-01|1983-02-08|Nippon Soken Inc|Detecting device for liquid quantity| US4562732A|1982-04-28|1986-01-07|Nippon Soken, Inc.|Device for detecting liquid amount in a vessel| WO2000066479A1|1999-05-02|2000-11-09|Varco I/P, Inc.|System for measuring torque applied to the drum shaft of a hoist| US6398557B1|1999-09-17|2002-06-04|The University Of Iowa Research Foundation|Devices, methods and kits for training in surgical techniques| DE10302349B3|2003-01-16|2004-09-30|EBM Brosa Messgeräte GmbH & Co. KG|Force transducers for measuring axial forces|
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申请号 | 申请日 | 专利标题 HU79VA1538A|HU180974B|1979-01-10|1979-01-10|Gauge shaft for converting force to electric signal| 相关专利
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