CN2231412Y - Claw type elastic sensitive element load cell - Google Patents
Claw type elastic sensitive element load cell Download PDFInfo
- Publication number
- CN2231412Y CN2231412Y CN 95242856 CN95242856U CN2231412Y CN 2231412 Y CN2231412 Y CN 2231412Y CN 95242856 CN95242856 CN 95242856 CN 95242856 U CN95242856 U CN 95242856U CN 2231412 Y CN2231412 Y CN 2231412Y
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- sensing element
- elastic sensing
- sensitive element
- pressure
- claw
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- 210000000078 claw Anatomy 0.000 title claims abstract description 12
- 239000011888 foil Substances 0.000 claims 2
- 238000012856 packing Methods 0.000 claims 2
- 239000000203 mixture Substances 0.000 claims 1
- 230000035945 sensitivity Effects 0.000 abstract description 10
- 230000006835 compression Effects 0.000 abstract description 6
- 238000007906 compression Methods 0.000 abstract description 6
- 238000005452 bending Methods 0.000 abstract description 4
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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- Force Measurement Appropriate To Specific Purposes (AREA)
Abstract
Description
本实用新型属于测力传感器设计制造技术领域,特别涉及一种应变式测力传感器。The utility model belongs to the technical field of design and manufacture of force-measuring sensors, in particular to a strain-type force-measuring sensor.
现有的应变式测力传感器内部弹性敏感元件的结构形式,大致可划分为两大类,一类是以圆筒式或圆柱式为特征的轴心受力型弹性敏感元件,其特点是刚度大,但灵敏度低;另一类是以梁式、板式或环式为特征的弯曲受力型,这类弹性敏感元件的特点是灵敏度高,但刚度低。由于上述两类弹性敏感元件受其结构形式所限,刚度与灵敏度二者无法兼顾,因而很难满足某些对刚度和灵敏度都有严格要求的使用场合,造成了此类测力传感器的使用局限性。The structural forms of the elastic sensitive elements inside the existing strain gauge load cells can be roughly divided into two categories. One is the axially stressed elastic sensitive element characterized by a cylindrical or cylindrical type, which is characterized by stiffness Large, but low sensitivity; the other is the bending force type characterized by beam, plate or ring type, this type of elastic sensitive element is characterized by high sensitivity, but low stiffness. Since the above two types of elastic sensitive elements are limited by their structural forms, the stiffness and sensitivity cannot be balanced, so it is difficult to meet some use occasions that have strict requirements on stiffness and sensitivity, resulting in the use of this type of load cell. sex.
本实用新型的目的是提供一种能同时兼顾刚度和灵敏度要求的爪瓣式弹性敏感元件测力传感器。The purpose of the utility model is to provide a claw flap type elastic sensitive element force measuring sensor which can meet the requirements of stiffness and sensitivity at the same time.
本实用新型由以下技术方案实现:将底部带有通孔的圆筒腰部经车削形成环形凹槽,从圆筒口沿轴向对称开十字或米字槽后,圆筒壁形成非均匀壁厚的径向弧形爪瓣式结构,在爪瓣外表面凹槽内粘贴应变片组成全桥测力机构,带有球台面的芯杆穿过弹性敏感元件的通孔和承压垫圈、球台面压力环,用锁紧螺母固定,芯杆有螺纹端与拉压头联接,当施加拉力时芯杆一端的球台面受力并作用于圆筒底部,爪瓣表面的应变片受拉变形,施加压力时芯杆螺纹端压力环球台面受力,通过承压垫圈作用于爪瓣端部,其表面凹槽内的应变片受压变形。这种结构形式,使原来由圆筒底部中心受压状态转化为爪瓣受压弯组合的偏心承压状态,使测力机构应变量增大,灵敏度提高。,由于轴向位移远小于侧向位移的变形特点,使测力机构有较高的轴向压缩刚度。The utility model is realized by the following technical solutions: turning the waist of the cylinder with a through hole at the bottom to form an annular groove, and after opening a cross or Pozider groove symmetrically in the axial direction from the cylinder mouth, the cylinder wall forms a non-uniform wall thickness. Radial arc-shaped claw structure, the strain gauge is pasted in the groove on the outer surface of the claw to form a full-bridge force measuring mechanism, the core rod with the ball surface passes through the through hole of the elastic sensitive element and the pressure washer, the pressure of the ball table surface The ring is fixed with a lock nut. The threaded end of the core rod is connected with the tension and pressure head. When the tension is applied, the ball table surface at one end of the core rod is stressed and acts on the bottom of the cylinder. When the threaded end of the core rod is under pressure on the surface of the ring, it acts on the end of the claw valve through the pressure washer, and the strain gauge in the groove on the surface is deformed under pressure. This structural form transforms the original state of compression at the center of the bottom of the cylinder into an eccentric pressure state of the combination of claw flaps under compression and bending, which increases the strain of the force-measuring mechanism and improves the sensitivity. , due to the deformation characteristics that the axial displacement is much smaller than the lateral displacement, the force measuring mechanism has a high axial compression stiffness.
本实用新型与现有技术相比的效果和优点在于它保留了圆筒式或柱式弹性敏感元件结构紧凑、抗压刚度大的特点,同时具备了板式、梁式弯曲受力型弹性敏感元件灵敏度高的特点,特别适用于既需要承受较大压力,又需要灵敏度高的测力场合。Compared with the prior art, the utility model has the effect and advantage that it retains the characteristics of compact structure and high compressive stiffness of the cylindrical or column elastic sensitive elements, and at the same time has the elastic sensitive elements of plate type and beam type bending force The characteristic of high sensitivity is especially suitable for force measurement occasions that need to bear high pressure and high sensitivity.
本实用新型的附图说明。Description of drawings of the utility model.
图1为本实用新型的正视剖视图。Figure 1 is a front sectional view of the utility model.
图为本实用新型的A-A向剖视图。The figure is an A-A sectional view of the utility model.
下面通过附图对本实用新型作进一步描述,该测力传感器主要由芯杆[1]、弹性敏感元件[2]、护套[3]、应变片[4]、承压垫圈[5]、带球台面的压力环[6]、锁紧螺母[7]、护套端盖[10]等组成,弹性敏感元件[2]是用底部带有通孔的圆筒经车削加工成环形凹槽,从圆筒口沿轴向对称开十字或米字槽后,圆筒壁形成非均匀壁厚的径向弧形爪瓣式结构,在爪瓣外表面弧形凹槽内粘贴应变片组成全桥测力机构。带有球台面的芯杆[1]穿过弹性敏感元件[2]底部通孔和承压垫圈[5]、球台面压力环[6],用锁紧螺母[7]固定后,再用护套端盖[10]、钉[8]封装在护套[3]内,传感器安装孔[9]可与加力头支架固定,但压力环[6]与承压垫圈[5]之间有1~2毫米间隙,弹性敏感元件[2]和承压垫圈[5]的周边与护套[3]的内壁为间隙配合,弹性敏感元件[2]的底端面与护套[3]的底部有1~2毫米间隙,当芯杆[1]受压力作用时该间隙顶死。因此,无论施加拉力还是压力,弹性敏感元件总处于受压状态,但应变片测到的应变量由于测力机构偏心承压状态不同而得到大小相等方向相反的两个参数。The utility model will be further described below through the accompanying drawings. The pressure ring [6], the lock nut [7], the sheath end cover [10], etc. on the surface of the ball table are composed, and the elastic sensitive element [2] is a cylinder with a through hole at the bottom, which is turned into an annular groove. After the cross or Pozi groove is symmetrically opened in the axial direction from the cylinder mouth, the cylinder wall forms a radial arc claw structure with non-uniform wall thickness, and the strain gauges are pasted in the arc groove on the outer surface of the claw to form a full bridge measurement force mechanism. The core rod [1] with the ball table surface passes through the through hole at the bottom of the elastic sensitive element [2], the pressure washer [5], the ball table surface pressure ring [6], and is fixed with the lock nut [7] The sleeve end cover [10] and the nail [8] are packaged in the sheath [3], and the sensor installation hole [9] can be fixed with the booster head bracket, but there is a gap between the pressure ring [6] and the pressure washer [5]. 1 to 2 mm gap, the elastic sensitive element [2] and the pressure washer [5] are in a clearance fit with the inner wall of the sheath [3], the bottom end surface of the elastic sensitive element [2] is in contact with the bottom of the sheath [3] There is a gap of 1 to 2 millimeters, and the gap is pushed to death when the core rod [1] is under pressure. Therefore, regardless of the tension or pressure applied, the elastic sensitive element is always in a compressed state, but the strain measured by the strain gauge is two parameters of equal magnitude and opposite direction due to the different eccentric pressure bearing state of the force measuring mechanism.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 95242856 CN2231412Y (en) | 1995-03-11 | 1995-03-11 | Claw type elastic sensitive element load cell |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 95242856 CN2231412Y (en) | 1995-03-11 | 1995-03-11 | Claw type elastic sensitive element load cell |
Publications (1)
Publication Number | Publication Date |
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CN2231412Y true CN2231412Y (en) | 1996-07-17 |
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Family Applications (1)
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CN 95242856 Expired - Fee Related CN2231412Y (en) | 1995-03-11 | 1995-03-11 | Claw type elastic sensitive element load cell |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101561326B (en) * | 2009-06-02 | 2010-09-22 | 李连秀 | Multi-directional load transducer |
CN102327902A (en) * | 2011-10-17 | 2012-01-25 | 北京中冶设备研究设计总院有限公司 | Device and method for measuring axial force of working roll of slab strip hot rolling mill |
CN107976267A (en) * | 2017-12-18 | 2018-05-01 | 中国石油大学(北京) | A kind of outer force measuring device of marine riser and measuring method |
CN112145511A (en) * | 2020-09-25 | 2020-12-29 | 长安大学 | Movement mechanism locking device and locking method based on inverse flexoelectric effect |
-
1995
- 1995-03-11 CN CN 95242856 patent/CN2231412Y/en not_active Expired - Fee Related
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101561326B (en) * | 2009-06-02 | 2010-09-22 | 李连秀 | Multi-directional load transducer |
CN102327902A (en) * | 2011-10-17 | 2012-01-25 | 北京中冶设备研究设计总院有限公司 | Device and method for measuring axial force of working roll of slab strip hot rolling mill |
CN102327902B (en) * | 2011-10-17 | 2013-03-06 | 北京中冶设备研究设计总院有限公司 | Device and method for measuring axial force of working roll of slab strip hot rolling mill |
CN107976267A (en) * | 2017-12-18 | 2018-05-01 | 中国石油大学(北京) | A kind of outer force measuring device of marine riser and measuring method |
CN107976267B (en) * | 2017-12-18 | 2023-05-05 | 中国石油大学(北京) | A kind of riser external force measuring device and measuring method |
CN112145511A (en) * | 2020-09-25 | 2020-12-29 | 长安大学 | Movement mechanism locking device and locking method based on inverse flexoelectric effect |
CN112145511B (en) * | 2020-09-25 | 2021-11-12 | 长安大学 | A kind of kinematic mechanism locking device and locking method based on inverse flexoelectric effect |
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Legal Events
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |