CN210487142U - Fiber grating type three-dimensional force sensor - Google Patents
Fiber grating type three-dimensional force sensor Download PDFInfo
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- CN210487142U CN210487142U CN201921992575.0U CN201921992575U CN210487142U CN 210487142 U CN210487142 U CN 210487142U CN 201921992575 U CN201921992575 U CN 201921992575U CN 210487142 U CN210487142 U CN 210487142U
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Abstract
The utility model relates to the technical field of multidimensional force sensing, in particular to a fiber grating type three-dimensional force sensor, which comprises an upper elastic disc, a lower elastic disc, a force transmission column and a fiber grating component; the upper elastic disc comprises a disc body I with a cavity arranged therein and a plane strain beam I positioned in the cavity, wherein the plane strain beam I is of a cross-shaped structure and is provided with four branch beams I; the lower elastic disc comprises a disc body II with a cavity and a plane strain beam II positioned in the cavity, and the plane strain beam II is of a cross-shaped structure and is provided with four branch beams II; the lower end of the force transmission column is vertically connected to the center of the plane strain beam II, the upper end of the force transmission column penetrates out of the through hole I, and the force transmission column is in clearance fit with the through hole I; the fiber grating component comprises a first fiber grating, a second fiber grating, a third fiber grating and a fourth fiber grating. The utility model discloses can anti electromagnetic interference, corrosion-resistant, reduce the dimension and couple, increase sensitivity, can realize temperature compensation simultaneously, its simple structure, easily processing.
Description
Technical Field
The utility model relates to a multidimension force sensing technical field especially relates to a three-dimensional force transducer of fiber grating formula.
Background
The multidimensional force sensor is one of the most important sensors of the robot, and plays a key role in feedback of control of flexibility, force, remote operation and the like of the robot. Install in the multidimensional force transducer of joints such as robot wrist, fingertip, ankle for the space information when perception robot receives external environment power to do all can for the better cognitive environment of robot, so that the corresponding work of accurate completion, if: contour tracing, zero force teaching, workpiece grabbing and placing or carrying, and the like.
At present, most of the existing multidimensional force sensors adopt resistance strain gauges as sensing elements, and the number of the resistance strain gauges is more than ten, even tens, so that the wiring is complex and strong electromagnetic interference exists, for example, as shown in CN 105973521 a; in addition, the traditional multidimensional force sensor has a complex structure, so that the coupling between dimensions is large, and the strain beam is mostly a traditional rectangular beam, so that the sensitivity of the sensor is low.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model aims at providing a fiber grating formula three-dimensional force transducer, but anti-electromagnetic interference, corrosion-resistant, reduce the dimension and couple, increase sensitivity, can realize temperature compensation simultaneously, its simple structure, easily processing.
The utility model provides a fiber grating type three-dimensional force sensor, which comprises an upper elastic disc, a lower elastic disc, a force transmission column and a fiber grating component;
the upper elastic disc comprises a disc body I with a cavity arranged therein and a plane strain beam I positioned in the cavity, the plane strain beam I is of a cross structure and is provided with four branch beams I, the outer ends of the four branch beams I are connected to the inner wall of the disc body I, and a through hole I for a force transmission column to pass through is formed in the center of the plane strain beam I;
the lower elastic disc comprises a disc body II with a cavity and a plane strain beam II positioned in the cavity, the plane strain beam II is of a cross structure and is provided with four branch beams II, the outer ends of the four branch beams II are connected to the inner wall of the disc body II, the disc body I is connected with the disc body II through a supporting component, the plane strain beam is arranged in parallel to the plane strain beam I, and the four branch beams II are respectively and correspondingly arranged right below the four branch beams I;
the force transmission column is of an elastic upright column structure capable of bending along the radial direction and stretching along the axial direction, the lower end of the force transmission column is vertically connected to the center of the plane strain beam II, the upper end of the force transmission column penetrates out of the through hole I, and the force transmission column is in clearance fit with the through hole I;
the fiber grating component comprises a first fiber grating, a second fiber grating, a third fiber grating and a fourth fiber grating which are sequentially connected through optical fibers, the first fiber grating and the second fiber grating are respectively connected to two perpendicular branch beams I of the plane strain beam I, the third fiber grating is suspended between the disk body I and the disk body II, and the fourth fiber grating is connected to one branch beam II and located under the second fiber grating.
As a preferred technical scheme, the disc body I and the plane strain beam I are of an integral structure and are made of elastic materials.
As a preferred technical scheme, the disc body II and the plane strain beam II are of an integral structure and are made of elastic materials.
As a preferred technical scheme, the branch beam I and the branch beam II are both of the same I-beam structure.
As an optimal technical scheme, the connection positions of the inner ends of the four branch beams I form a central circular truncated cone I, and the through hole I and the central circular truncated cone I are coaxially arranged.
As an optimal technical scheme, the connection positions of the inner ends of the four branch beams II form a central circular truncated cone II, the central circular truncated cone II is coaxially provided with a first screw hole, and the lower end of the force transmission column is provided with a first threaded part which is matched and screwed with the first screw hole.
As a preferred technical scheme, the first fiber bragg grating and the second fiber bragg grating are respectively pasted on the upper surface of the corresponding branch beam I and are arranged near the center of the plane strain beam I, and the fourth fiber bragg grating is pasted on the upper surface of the branch beam II and is arranged near the center of the plane strain beam II.
As a preferred technical scheme, the sensor further comprises a loading cap used for bearing load, a second screw hole is formed in the loading cap, a second threaded portion matched and screwed with the second screw hole is formed in the upper end of the force transmission column, and a set distance is reserved between the loading cap and the plane strain beam I after the loading cap and the force transmission column are connected stably.
As a preferred technical scheme, the supporting assembly comprises four supporting rods with rigid structures, the four supporting rods are uniformly arranged along the circumferential direction, the upper ends of the four supporting rods are fixed on the tray body I, and the lower ends of the four supporting rods are fixed on the tray body II.
As a preferable technical scheme, the tray body I is provided with third screw holes which are in one-to-one correspondence with the support rods, and the upper ends of the support rods coaxially extend into the third screw holes and are in threaded connection; through holes II which are in one-to-one correspondence with the support rods are formed in the tray body II, and the lower ends of the support rods coaxially extend into the through holes II and are positioned through nuts positioned at the upper end and the lower end of the through holes II; and a mounting hole for mounting a sensor is also formed between two adjacent through holes on the disk body II.
Compared with the prior art, the utility model provides a pair of three-dimensional force transducer of fiber grating formula has following beneficial technological effect:
firstly, the utility model discloses utilize fiber grating wavelength drift volume as the output signal of sensor, compare with the three-dimensional force transducer of traditional resistance variation formula with voltage as output signal, have advantages such as anti-electromagnetic interference, stronger corrosion resistance and no zero drift;
secondly, the four fiber gratings used by the utility model form the central wavelength difference of three groups of fiber gratings as the output signal of the sensor, which can realize the temperature self-compensation, thereby solving the cross sensitivity problem of temperature and strain;
thirdly, the utility model uses four fiber gratings as the sensitive elements of the sensor, compared with dozens of resistance strain gauges used by the traditional resistance strain type three-dimensional force sensor, the number of the sensitive elements of the sensor is greatly reduced, and the problem of complex wiring caused by excessive number of the resistance strain gauges is solved;
fourthly, the upper elastic disc and the lower elastic disc are separated up and down, so that the interference of the vertical direction to the transverse direction and the longitudinal direction can be eliminated, and the inter-dimensional coupling of the multi-dimensional sensor is effectively reduced;
fifthly, the elastic disc and the lower elastic disc are of an integrated cross beam structure, so that the repeatability error of the sensor can be reduced;
sixthly, the branch beam I and the branch beam II are I-beam structures, and the sensitivity of the sensor is improved.
Drawings
Fig. 1 is a front view of the present invention;
fig. 2 is a left side view of the present invention;
fig. 3 is a top view of the upper flexible disk of the present invention;
fig. 4 is a top view of the lower elastic disc of the present invention.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings of the present invention; obviously, the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention based on the embodiments of the present invention.
As shown in fig. 1 to 4: the embodiment provides a fiber grating type three-dimensional force sensor which comprises an upper elastic disc 1, a lower elastic disc 2, a force transmission column 3 and a fiber grating component.
The upper elastic disc 1 comprises a disc body I11 with a cavity 12 arranged therein and a plane strain beam I positioned in the cavity 12, the plane strain beam I is of a cross structure and is provided with four branch beams I13, the outer ends (one ends far away from the center of the plane strain beam I) of the four branch beams I13 are connected to the inner wall of the disc body I11, and the center of the plane strain beam I is provided with a through hole I14 for a force transmission column 3 to pass through; the disc body I11 is preferably of a circular ring structure; the four branch beams I13 are positioned on the same plane, and the adjacent branch beams I13 are mutually vertical; the disc body I11 and the plane strain beam I are of an integral structure and are made of elastic materials (such as elastic aluminum alloy), so that the repeatability error of the sensor can be reduced; wherein, the I13 of branch roof beam is I-beam structure, can improve sensor's sensitivity.
The lower elastic disc 2 comprises a disc body II 21 with a cavity 22 arranged therein and a plane strain beam II positioned in the cavity 22, the plane strain beam II is of a cross structure and is provided with four branch beams II 23, the outer ends (the ends far away from the center of the plane strain beam II) of the four branch beams II 23 are connected to the inner wall of the disc body II 21, the disc body I11 is connected with the disc body II 21 through a supporting component, the plane strain beam II is arranged in parallel to the plane strain beam I, and the four branch beams II 23 are respectively and correspondingly arranged right below the four branch beams I13; the disc body II 21 is preferably in a circular ring structure; the four branch beams II 23 are positioned on the same plane, and the adjacent branch beams II 23 are mutually vertical; the disc body II 21 and the plane strain beam II are of an integral structure and are made of elastic materials (such as elastic aluminum alloy), so that the repeatability error of the sensor can be reduced; the branch beam II 23 is of an I-beam structure, and the sensitivity of the sensor can be improved.
The force transmission column 3 is of an elastic upright column structure capable of bending along the radial direction and stretching along the axial direction, the lower end of the force transmission column 3 is vertically connected to the center of the plane strain beam II, the upper end of the force transmission column 3 penetrates out of the through hole I14, and the force transmission column 3 is in clearance fit with the through hole I14; the joint of the inner ends of the four branch beams I13 forms a central circular truncated cone I, the through holes I14 and the central circular truncated cone I15 are coaxially arranged, the inner diameter of the central circular truncated cone I15 is larger than the thickness of the branch beams I13, and the structural strength of the plane strain beam I is improved; a proper gap is reserved between the force transmission column 3 and the through hole I14; the connecting positions of the inner ends of the four branch beams II 23 form a central circular truncated cone II 24, the inner diameter of the central circular truncated cone II 24 is larger than the thickness of the branch beams II 23, the structural strength of the plane strain beam II is improved, and meanwhile, the connecting stability of the force transmission column 3 is improved; the second central round platform 24 is coaxially provided with a first screw hole 25, and the lower end of the force transmission column 3 is provided with a first screw thread part which is matched and screwed with the first screw hole 25, so that the force transmission column 3 can be conveniently mounted and dismounted.
The fiber grating subassembly includes first fiber grating FBG1, second fiber grating FBG2, third fiber grating FBG3 and fourth fiber grating FBG4 that connect gradually through optic fibre, first fiber grating FBG1, second fiber grating FBG2 are connected respectively on two mutually perpendicular branchs roof beam I13 of plane strain roof beam I, the suspension of third fiber grating 3 is arranged in between disk body I11 and disk body II 21, fourth fiber grating FBG4 is connected on a branchs roof beam II 23 and is located under second fiber grating FBG 2. The tail end optic fibre of first fiber grating FBG1 and the head end fiber connection of second fiber grating FBG2, the tail end optic fibre of second fiber grating FBG2 and the upper end fiber connection of third fiber grating FBG3, the lower extreme optic fibre of third fiber grating FBG3 and the head end fiber connection of fourth fiber grating FBG4, the head end optic fibre of first fiber grating FBG1 is worn out from the sensor top, the tail end optic fibre of fourth fiber grating FBG4 is worn out from the sensor below and can be used for linking to each other with outside demodulation equipment.
The sensor utilizes the fiber bragg grating wavelength drift amount as an output signal of the sensor, and has the advantages of electromagnetic interference resistance, strong corrosion resistance, zero drift prevention and the like compared with the traditional resistance-variable three-dimensional force sensor which takes voltage as an output signal; the four used fiber gratings form the central wavelength difference of three groups of fiber gratings as the output signal of the sensor, which can realize the temperature self-compensation, thereby solving the problem of cross sensitivity of temperature and strain; the four fiber gratings are used as sensitive elements of the sensor, compared with dozens of resistance strain gauges used by the traditional resistance strain type three-dimensional force sensor, the number of the sensitive elements of the sensor is greatly reduced, and the problem of complex wiring caused by excessive number of the resistance strain gauges is solved; the structure that the upper elastic disc 1 and the lower elastic disc 2 are separated from each other up and down can eliminate the interference of the vertical direction to the transverse direction and the longitudinal direction, and effectively reduces the inter-dimensional coupling of the multi-dimensional sensor.
In this embodiment, first fiber grating FBG1, second fiber grating FBG2 paste respectively in the upper surface of corresponding branch roof beam I13 and be close to the central setting of plane strain roof beam I, fourth fiber grating FBG4 pastes in the upper surface of branch roof beam II 23 and be close to the central setting of plane strain roof beam II, and this structure is favorable to improving the detection precision of sensor.
In this embodiment, the sensor further includes a loading cap 4 for bearing a load, a second screw hole is formed in the loading cap 4, a second threaded portion matched and screwed with the second screw hole is formed in the upper end of the force transmission column 3, and a set distance (for example, 1-2 mm) is formed between the loading cap 4 and the plane strain beam i after the loading cap 4 and the force transmission column 3 are connected stably.
In the embodiment, a parallel state with a specific interval is also kept between the tray body I11 and the tray body II 21, the support assembly comprises four support rods 5 with rigid structures, the four support rods 5 are uniformly arranged along the circumferential direction (the adjacent support rods 5 are separated by 90 degrees), the upper ends of the four support rods are fixed on the tray body I11, and the lower ends of the four support rods are fixed on the tray body II 21; third screw holes 16 which are in one-to-one correspondence with the support rods 5 are formed in the tray body I11, and the upper ends of the support rods 5 coaxially extend into the third screw holes 16 and are in threaded connection; the disc body II 21 is provided with through holes II 26 which correspond to the support rods 5 one by one, and the lower ends of the support rods 5 coaxially extend into the through holes II 26 and are positioned by nuts 6 positioned at the upper end and the lower end of the through holes II 26; and a mounting hole 27 for mounting a sensor is further formed between two adjacent through holes II 26 on the disc body II 21.
And adhering the fiber bragg grating at a specific position of the sensor, and detecting the three-dimensional force by using the wavelength drift amount of the fiber bragg grating as output. For convenience of understanding, a three-dimensional coordinate system is constructed in fig. 1 and fig. 2, the center of the bottom surface of the elastic disc 2 is taken as a coordinate origin O, the x axis and the y axis are the extending directions of the two perpendicular support beams ii 23, and the z axis is the axial direction of the force transmission column 3 (and is also the direction of the symmetrical center line of the upper elastic disc 1 and the lower elastic disc 2).
The difference value of the wavelength drift amounts of the first fiber grating FBG1 and the third fiber grating FBG3 is used for measuring Fx; the difference value of the wavelength drift amounts of the second fiber bragg grating FBG2 and the third fiber bragg grating FBG3 is used for measuring Fy; the difference between the wavelength drift amounts of the fourth FBG4 and the third FBG3 is used for measuring Fz.
Specifically, the sensor measurement principle is as follows:
when a force Fx in the x direction acts on the loading cap 4, the force transmission column 3 can bend in the x direction, the upper elastic disc 1 enables the branch beam I13 arranged in the x direction to elastically deform through the bending action of the force transmission column 3, so that the wavelength of the first fiber bragg grating FBG1 drifts, the wavelength drift conditions of the fiber bragg gratings are the same due to the change of the ambient temperature, the difference value between the wavelength drift amount of the first fiber bragg grating 1 affected by the temperature and the strain and the wavelength drift amount of the third fiber bragg grating FBG3 affected by the temperature is used as an output signal of the sensor for measuring the Fx, and meanwhile, the temperature compensation is realized;
when a force Fy in the y direction acts on the loading cap 4, the force transmission column 3 can bend towards the y direction, the upper elastic disc 1 enables a branch beam I13 arranged in the y direction to be elastically deformed through the bending action of the force transmission column 3, so that the wavelength of a second fiber bragg grating FBG2 is drifted, the wavelength drift conditions of the fiber bragg gratings are the same due to the change of the ambient temperature, the difference value between the wavelength drift amount of the second fiber bragg grating 2 affected by the temperature and the strain and the wavelength drift amount of a third fiber bragg grating FBG3 affected only by the temperature is used as an output signal of the sensor for measuring Fy, and meanwhile, the temperature compensation is realized;
when a force Fz in the z direction acts on the loading cap 4, the force transmission column 3 can move towards the z direction, because the force transmission column 3 is in clearance fit with the through hole I14 of the upper elastic disc 1, when the force in the z direction acts, the wavelengths of the first fiber bragg grating FBG1 and the second fiber bragg grating FBG2 which are arranged on the upper elastic disc 1 do not drift, and the first screw hole 25 of the lower elastic disc 2 is in threaded connection with the force transmission column 3, only the wavelength of the fourth fiber bragg grating FBG4 drifts, so that the coupling influence of the x direction and the y direction on the z direction is eliminated, and the purpose of reducing the coupling between the sensor dimensions is achieved; the difference value of the wavelength drift amounts of the fourth FBG4 and the third FBG3 is used as an output signal for measuring Fz, and meanwhile, temperature compensation is achieved.
The above description is only an example of the present invention, and the common general knowledge of the known specific structures and characteristics of the embodiments is not described herein. It should be noted that, for those skilled in the art, without departing from the structure of the present invention, several modifications and improvements can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent. The scope of the claims of the present application shall be determined by the contents of the claims, and the description of the embodiments and the like in the specification shall be used to explain the contents of the claims.
Claims (10)
1. A fiber grating type three-dimensional force sensor is characterized in that: comprises an upper elastic disc, a lower elastic disc, a force transmission column and a fiber grating component;
the upper elastic disc comprises a disc body I with a cavity arranged therein and a plane strain beam I positioned in the cavity, the plane strain beam I is of a cross structure and is provided with four branch beams I, the outer ends of the four branch beams I are connected to the inner wall of the disc body I, and a through hole I for a force transmission column to pass through is formed in the center of the plane strain beam I;
the lower elastic disc comprises a disc body II with a cavity and a plane strain beam II positioned in the cavity, the plane strain beam II is of a cross structure and is provided with four branch beams II, the outer ends of the four branch beams II are connected to the inner wall of the disc body II, the disc body I is connected with the disc body II through a supporting component, the plane strain beam is arranged in parallel to the plane strain beam I, and the four branch beams II are respectively and correspondingly arranged right below the four branch beams I;
the force transmission column is of an elastic upright column structure capable of bending along the radial direction and stretching along the axial direction, the lower end of the force transmission column is vertically connected to the center of the plane strain beam II, the upper end of the force transmission column penetrates out of the through hole I, and the force transmission column is in clearance fit with the through hole I;
the fiber grating component comprises a first fiber grating, a second fiber grating, a third fiber grating and a fourth fiber grating which are sequentially connected through optical fibers, the first fiber grating and the second fiber grating are respectively connected to two perpendicular branch beams I of the plane strain beam I, the third fiber grating is suspended between the disk body I and the disk body II, and the fourth fiber grating is connected to one branch beam II and located under the second fiber grating.
2. The fiber grating-based three-dimensional force sensor according to claim 1, wherein: disk body I just adopts elastic material to make with planar strain roof beam I structure as an organic whole.
3. The fiber grating-based three-dimensional force sensor according to claim 1, wherein: the disc body II and the plane strain beam II are of an integrated structure and are made of elastic materials.
4. The fiber grating-based three-dimensional force sensor according to claim 1, wherein: the branch beam I and the branch beam II are of the same I-beam structure.
5. The fiber grating-based three-dimensional force sensor according to claim 1, wherein: the inner end joints of the four branch beams I form a central circular truncated cone I, and the through holes I and the central circular truncated cone I are coaxially arranged.
6. The fiber grating-based three-dimensional force sensor according to claim 1, wherein: the connecting parts of the inner ends of the four branch beams II form a central circular truncated cone II, the central circular truncated cone II is coaxially provided with a first screw hole, and the lower end of the force transmission column is provided with a first threaded part which is matched and screwed with the first screw hole.
7. The fiber grating-based three-dimensional force sensor according to claim 1, wherein: first fiber grating, second fiber grating paste respectively in the upper surface of corresponding outrigger I and be close to the central setting of plane strain roof beam I, fourth fiber grating pastes in the upper surface of outrigger II and is close to the central setting of plane strain roof beam II.
8. The fiber grating-based three-dimensional force sensor according to any one of claims 1 to 7, wherein: the sensor further comprises a loading cap used for bearing load, a second screw hole is formed in the loading cap, a second threaded portion matched with the second screw hole in a threaded mode is arranged at the upper end of the force transmission column, and a set distance is reserved between the loading cap and the plane strain beam I after the loading cap and the force transmission column are connected stably.
9. The fiber grating-based three-dimensional force sensor according to any one of claims 1 to 7, wherein: the supporting component comprises four supporting rods with rigid structures, the four supporting rods are uniformly arranged along the circumferential direction, the upper ends of the four supporting rods are fixed on the tray body I, and the lower ends of the four supporting rods are fixed on the tray body II.
10. The fiber grating-based three-dimensional force sensor according to claim 9, wherein: third screw holes which correspond to the support rods one to one are formed in the tray body I, and the upper ends of the support rods coaxially extend into the third screw holes and are in threaded connection; through holes II which are in one-to-one correspondence with the support rods are formed in the tray body II, and the lower ends of the support rods coaxially extend into the through holes II and are positioned through nuts positioned at the upper end and the lower end of the through holes II; and a mounting hole for mounting a sensor is also formed between two adjacent through holes on the disk body II.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921992575.0U CN210487142U (en) | 2019-11-18 | 2019-11-18 | Fiber grating type three-dimensional force sensor |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201921992575.0U CN210487142U (en) | 2019-11-18 | 2019-11-18 | Fiber grating type three-dimensional force sensor |
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| CN210487142U true CN210487142U (en) | 2020-05-08 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110779651A (en) * | 2019-11-18 | 2020-02-11 | 重庆交通大学 | Double-cross beam type three-dimensional force sensor based on fiber bragg grating |
| CN114152374A (en) * | 2021-11-09 | 2022-03-08 | 天津大学 | High-precision micro torque sensor based on fiber Bragg grating |
-
2019
- 2019-11-18 CN CN201921992575.0U patent/CN210487142U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110779651A (en) * | 2019-11-18 | 2020-02-11 | 重庆交通大学 | Double-cross beam type three-dimensional force sensor based on fiber bragg grating |
| CN114152374A (en) * | 2021-11-09 | 2022-03-08 | 天津大学 | High-precision micro torque sensor based on fiber Bragg grating |
| CN114152374B (en) * | 2021-11-09 | 2022-10-04 | 天津大学 | High-precision micro torque sensor based on fiber Bragg grating |
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