CN101059381A - Piezoelectric film cantilever beam type micro-force sensor micro-force loading device - Google Patents

Piezoelectric film cantilever beam type micro-force sensor micro-force loading device Download PDF

Info

Publication number
CN101059381A
CN101059381A CN 200710011275 CN200710011275A CN101059381A CN 101059381 A CN101059381 A CN 101059381A CN 200710011275 CN200710011275 CN 200710011275 CN 200710011275 A CN200710011275 A CN 200710011275A CN 101059381 A CN101059381 A CN 101059381A
Authority
CN
China
Prior art keywords
micro
micrometer
slide block
displacement platform
linear slide
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN 200710011275
Other languages
Chinese (zh)
Other versions
CN100507483C (en
Inventor
崔岩
董维杰
王兢
陈会林
王立鼎
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dalian University of Technology
Original Assignee
Dalian University of Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dalian University of Technology filed Critical Dalian University of Technology
Priority to CNB2007100112755A priority Critical patent/CN100507483C/en
Publication of CN101059381A publication Critical patent/CN101059381A/en
Application granted granted Critical
Publication of CN100507483C publication Critical patent/CN100507483C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

The invention relates to a micro force load device of piezoelectric film suspension beam micro force sensor, belonging to sensor and test technical field, used for the static and quasi-static test and label of piezoelectric film suspension beam micro force sensor, wherein a micro force load device is composed of a one-dimension micro displacement table, a two-dimension micro displace table, a piezoelectric dual-crystal micro force generator, and a damping device. The one-dimension micro displacement table is composed of an X-axis micrometer element and a one-dimension micro displacement table base. The two-dimension micro displace table is composed of a Y-axis micrometer element, a Z-axis micrometer element, a two-dimension micro displacement table base, a support plate and a socket head cap screw. The piezoelectric dual-crystal micro force generator III is composed of a micro probe, a fixing block, two piezoelectric ceramic plates, an aluminum plate, a clamping plate and a socket head cap screw. The invention has simple and reliable structure, easy operation, and improved resolution of micro force loading system, to resolve the problems as instability and hard control of micro Newton force load.

Description

The micro-force loading device of piezoelectric film cantilever beam type micro-force sensor
Technical field
The invention belongs to sensor and technical field of measurement and test, particularly the static state of piezoelectric film cantilever beam type micro-force sensor and quasi static test and demarcation.
Background technology
Piezoelectric film cantilever beam type micro-force sensor is based on a kind of novel sensor of MEMS technology, has been widely used in the fine measuring instruments such as scanning force microscopy.Whether reach desired technical performance index in order to detect force transducer, before using force transducer, must once comprehensively check it on technology and performance, promptly the sound attitude is demarcated.At present, adopt the vertical loading method that cantilever beam type micro-force sensor is carried out in the system of static and quasistatic demarcation, its small power generally is to be applied on the metal needle point by mass or spring, and the direction by mechanical guide rail confining force is perpendicular to sample surfaces then.The load mode of these two kinds of power, the size of power is at 0-20N, for resolution is the small power of little newton's magnitude, and there is following several respects shortcoming in its loading system: because the factor that machinery loading device exists additional force etc. to be difficult to eliminate, increased the instability and the control difficulty of loading force; These chargers are lower to the accuracy requirement of loading force, limited the demarcation of piezoelectric film cantilever beam type micro-force sensor in little newton's magnitude power.
Summary of the invention
The objective of the invention is to invent the small force loading device of a kind of Simple and Reliable, evaded the shortcoming that exists in the above-mentioned force loading device, improved the resolution of small force loading system.Utilize the micron dimension micrometer respectively on X-axis, Y-axis and Z-direction, accurately control the loading position of microprobe on piezoelectric film cantilever beam type micro-force sensor to be measured; Adopt the piezoelectric ceramic piece of drive power supply for piezoelectric ceramics excitation band microprobe, utilize the micrometric displacement of the inverse piezoelectric effect generation vertical direction of piezoelectric, microprobe is delivered to micrometric displacement on the piezoelectric film cantilever beam type micro-force sensor to be measured, realize the loading of small power, and then small power is demarcated.The charger of whole small power adopts the loading section rigid structure, utilizes micrometric displacement to realize the transmission of small power, and finishes the loading of little newton's magnitude power.Instability and the difficult problem of control that little newton's magnitude power loads have been solved.
The technical solution used in the present invention is a kind of micro-force loading device of piezoelectric film cantilever beam type micro-force sensor, by one-dimensional micro-displacement platform I, and two-dimentional micrometric displacement platform II, little forcer III of piezoelectric bimorph and shock attenuation device IV form; One-dimensional micro-displacement platform I is by X-axis micrometer assembly, one-dimensional micro-displacement platform base 6 is formed, wherein, X-axis micrometer assembly is by X-axis micrometer knob 1, dial sleeve 2 in the X-axis micrometer, socket head cap screw 3, X is to linear slide block 4, X-axis micrometer main shaft 5 is formed, the X-axis micrometer knob 1 that has EXT scale is connected with the threaded one end of X-axis micrometer main shaft 5, X-axis micrometer knob 1 and interior dial sleeve 2 clearance fit of X-axis micrometer, the X of dial sleeve 2 and band guide pin bushing is to linear slide block 4 interference fit in the X-axis micrometer, and be fixed on X on the guide pin bushing of linear slide block 4 by socket head cap screw 3, one-dimensional micro-displacement platform base 6 is shaped as perpendicular type, horizontal bottom is a guide pass, match to the end of linear slide block 4 guide pass with X, the vertical plane of one-dimensional micro-displacement platform base 6 is that Z is to the plane, be fixed in by 4 socket head cap screws 7 on the right plane of two-dimentional micrometric displacement platform base 18, in one-dimensional micro-displacement platform base 6 inner chambers, spring 30 is housed, spring 30 1 ends are fixed in one-dimensional micro-displacement platform base 6 inner chambers, and the other end and X are affixed to linear slide block 4;
Two dimension micrometric displacement platform II is by Y-axis micrometer assembly, Z axle micrometer assembly, two dimension micrometric displacement platform base 18, support plate 19 and socket head cap screw 20 are formed, wherein, Y-axis micrometer assembly is by Y-axis micrometer knob 8, dial sleeve 9 in the Y-axis micrometer, socket head cap screw 10, Y is to linear slide block 11, Y-axis micrometer main shaft 12 is formed, have on the Y-axis micrometer knob 8 of EXT scale and be connected with Y-axis micrometer main shaft 12 threaded one ends, Y-axis micrometer knob 8 and interior dial sleeve 9 clearance fit of Y-axis micrometer, dial sleeve 9 and the Y of band guide pin bushing be to linear slide block 11 interference fit in the Y-axis micrometer, and be fixed on Y on the guide pin bushing of linear slide block 11 by socket head cap screw 10; Z axle micrometer assembly is made up of to linear slide block 16, Z axle micrometer main shaft 17 dial sleeve 14, socket head cap screw 15, Z in Z axle micrometer knob 13, the Z axle micrometer, the Z axle micrometer knob 13 that has EXT scale is connected with Z axle micrometer main shaft 17 threaded one ends, Z axle micrometer knob 13 and interior dial sleeve 14 clearance fit of Z axle micrometer, dial sleeve 14 and the Z of band guide pin bushing be to linear slide block 16 interference fit in the Z axle micrometer, and be fixed on Z on the guide pin bushing of linear slide block 16 by socket head cap screw 15; Two dimension micrometric displacement platform base 18 is shaped as square, and horizontal direction is a Y-axis, and vertical direction is the Z axle, and two-dimentional micrometric displacement platform base 18 horizontal bottom and vertical plane are guide pass, respectively with Y to linear slide block 11 and Z to the guide pass of linear slide block 16 to cooperating; Along continuous straight runs and vertical direction are equipped with spring 31 and spring 32 respectively in the inner chamber of two-dimentional micrometric displacement platform base 18, one end of spring 31 and spring 32 is separately fixed in the inner chamber of two-dimentional micrometric displacement platform base 18, the other end of spring 31 and Y are affixed to linear slide block 11, the other end of spring 32 and Z are affixed to linear slide block 16, and two-dimentional micrometric displacement platform base 18 is affixed by socket head cap screw 20 with support plate 19;
The little forcer III of piezoelectric bimorph is by microprobe 21, fixed block 22, two piezoelectric ceramic pieces 23, aluminum sheet metal 24, intermediate plate 25, socket head cap screw 26 is formed, wherein, aluminum sheet metal 24 is sandwiched in the middle of two rectangular piezoelectric ceramic sheets 23, and it is bonding by bonding agent, probe 21 is installed in the center of fixed block 22 by bonding agent, fixed block 22 is bonded in an end of piezoelectric ceramic piece 23 by bonding agent, with the end of the little forcer III of intermediate plate 25 clamping piezoelectric bimorphs, and the little forcer III of piezoelectric bimorph is installed on the baseplane of one dimension displacement platform base 6 by socket head cap screw 26 away from probe 21; Two piezoelectric ceramic pieces 23 are drawn an electrode A jointly, and aluminum sheet metal 24 is drawn another electrode B;
Shock attenuation device IV is by piezoelectric film cantilever beam type micro-force sensor 27, objective table 28 and damped platform 29 are formed, on damped platform 29, be fixed with objective table 28, piezoelectric film cantilever beam type micro-force sensor 27 is installed on objective table 28, and piezoelectric film cantilever beam type micro-force sensor 27 free ends are aimed at microprobe 21.
Effect of the present invention is to drive micrometer with X-axis, Y-axis and Z axle respectively position and the exposure level of microprobe on cantilever beam type micro-force sensor to be measured to be carried out manually grand moving control, has controlled pre-load force well, measures and calibration range thereby enlarge; Adopt piezoelectric ceramic piece that microprobe is carried out automatically controlled fine motion, small power loading accuracy height can reach little newton's magnitude, has improved the stated accuracy of piezoelectric film cantilever beam type micro-force sensor; Manual adjustments and automatically controlled mode combine, and cooperate necessary surveying instrument and bracing or strutting arrangement, promptly can realize the demarcation of piezoelectric film cantilever beam type micro-force sensor under static and quasistatic, and be simple and reliable for structure, and easy to operate.
Description of drawings:
Accompanying drawing 1 is a piezoelectric film cantilever beam type micro-force sensor micro-force loading device front view.
Accompanying drawing 2 is a piezoelectric film cantilever beam type micro-force sensor micro-force loading device vertical view.
Accompanying drawing 3 is a piezoelectric film cantilever beam type micro-force sensor micro-force loading device right view.
Accompanying drawing 4 is the little forcer III of a piezoelectric bimorph structure enlarged drawing.
Wherein, dial sleeve in the 1-X axle micrometer knob, 2-X axle micrometer, 3-socket head cap screw, 4-X be to linear slide block, 5-X axle micrometer main shaft, 6-one-dimensional micro-displacement platform base, the 7-socket head cap screw, dial sleeve in the 8-Y axle micrometer knob, 9-Y axle micrometer, the 10-socket head cap screw, 11-Y is to linear slide block, 12-Y axle micrometer main shaft, 13-Z axle micrometer knob, dial sleeve in the 14-Z axle micrometer, 15-socket head cap screw, 16-Z be to linear slide block, 17-Z axle micrometer main shaft, 18-two dimension micrometric displacement platform base, the 19-support plate, 20-socket head cap screw, 21-microprobe, the 22-fixed block, the 23-piezoelectric ceramic piece, 24-aluminum sheet metal, 25-intermediate plate, the 26-socket head cap screw, the 27-piezoelectric film cantilever beam type micro-force sensor, 28-objective table, 29-damped platform, the 30-spring, the 31-spring, 32-spring, A-electrode A, the B-electrode B, I-one-dimensional micro-displacement platform, II-two dimension micrometric displacement platform, the little forcer of III-piezoelectric bimorph, the IV-shock attenuation device, X-X direction coordinate axis, Y-Y direction coordinate axis, Z-Z direction coordinate axis.
Embodiment:
Describe enforcement of the present invention in detail below in conjunction with accompanying drawing.At first, utilize body silicon process technology and Surface-micromachining process processing piezoelectric film cantilever beam type micro-force sensor 27.Cantilever beam type micro-force sensor 27 is fixed on the objective table 28, places on the damped platform 29 objective table 28 to be measured again.Measure and timing signal, be fixed on the damped platform 29 after all devices are integrated, cover all devices and device with hurricane globe.
Thisly be used for the micro-force loading device that piezoelectric film cantilever beam type micro-force sensor is demarcated, suit in the ultra-clean chamber work of 23 ℃ isoperibol.Be the blind hole of 1mm at first, microprobe 21 be fixed in the blind hole with bonding agent at square fixed block 22 center drill diameters; After treating that microprobe 21 fixes, with the fixed block 22 of band microprobe 21, at piezoelectric ceramic piece 23 non-electrode leads to client, bearing is positioned at the middle position at the about 5mm of piezoelectric ceramic piece 23 non-electrode leads to client place with adhesive; Treat fixed block 22 after fixing on the piezoelectric ceramic piece 23, use the piezoelectric ceramic piece 23 of intermediate plate 25 clamping band microprobes 21, and be fixed on the one-dimensional micro-displacement platform base 6 by 4 socket head cap screws 26; Electrode A and electrode B are drawn by lead, and link to each other with drive power supply for piezoelectric ceramics, realize voltage drive, and before the use, the little forcer III of piezoelectric bimorph need demarcate.Before carrying out the demarcation of static state and quasistatic, the piezoelectric effect of utilizing piezoelectric is produced the micrometric displacement of vertical direction, microprobe 21 is delivered to micrometric displacement on the piezoelectric film cantilever beam type micro-force sensor 27 to be measured, realizes the loading of small power, and then small power is tested and demarcated.The charger of whole small power adopts the loading section rigid structure, utilizes micrometric displacement to realize the transmission of small power, and finishes the loading of little newton's magnitude power.Package unit is fixed on the damped platform 29, carries out the location and the demarcation of microprobe 21 and pressure measurement conductive film cantilever beam type micro-force sensor 27 then.
During loading, regulating X-axis micrometer knob 1 driving X moves to the guide pass upper edge directions X of linear slide block 4 in one-dimensional micro-displacement platform base 6, regulate Y-axis micrometer knob 8 and Z axle micrometer knob 13 more respectively, driving Y respectively moves along Y and Z direction respectively on the guide pass of linear slide block 16 in two-dimentional micrometric displacement platform base 18 to linear slide block and Z, make microprobe 21 arrive piezoelectric film cantilever beam type micro-force sensors 27 directly over, make needle point over against the load(ing) point place, regulate Z axle micrometer knob 13 again, microprobe 21 has just been contacted with piezoelectric film cantilever beam type micro-force sensor 27 to be measured.Then according to the needs of testing and demarcating, by electrode A and electrode B, by the ceramic driving power supply the little forcer III of the piezoelectric bimorph of having demarcated is applied direct current or ac-excited voltage, by the loading section rigid structure, utilize micrometric displacement to realize the transmission of small power, and finish the loading of little newton's magnitude power, and then piezoelectric film cantilever beam type micro-force sensor 27 is carried out static state and quasi-static demarcation.

Claims (1)

1, a kind of micro-force loading device of piezoelectric film cantilever beam type micro-force sensor, by one-dimensional micro-displacement platform (I), two-dimentional micrometric displacement platform (II), little forcer of piezoelectric bimorph (III) and shock attenuation device (IV) are formed; It is characterized in that, one-dimensional micro-displacement platform (I) is by X-axis micrometer assembly, one-dimensional micro-displacement platform base (6) is formed, wherein, X-axis micrometer assembly is by X-axis micrometer knob (1), dial sleeve (2) in the X-axis micrometer, socket head cap screw (3), X is to linear slide block (4), X-axis micrometer main shaft (5) is formed, the X-axis micrometer knob (1) that has EXT scale is connected with the threaded one end of X-axis micrometer main shaft (5), X-axis micrometer knob (1) and interior dial sleeve (2) clearance fit of X-axis micrometer, the X of dial sleeve (2) and band guide pin bushing is to linear slide block (4) interference fit in the X-axis micrometer, and be fixed on X on the guide pin bushing of linear slide block (4) by socket head cap screw (3), one-dimensional micro-displacement platform base (6) is shaped as perpendicular type, horizontal bottom is a guide pass, match to the end guide pass of linear slide block (4) with X, the vertical plane of one-dimensional micro-displacement platform base (6) is that Z is to the plane, be fixed in by 4 socket head cap screws (7) on the right plane of two-dimentional micrometric displacement platform base (18), in one-dimensional micro-displacement platform base (6) inner chamber, spring (30) is housed, spring (30) one ends are fixed in one-dimensional micro-displacement platform base (6) inner chamber, and the other end and X are affixed to linear slide block (4);
Two dimension micrometric displacement platform (II) is by Y-axis micrometer assembly, Z axle micrometer assembly, two dimension micrometric displacement platform base (18), support plate (19) and socket head cap screw (20) are formed, wherein, Y-axis micrometer assembly is by Y-axis micrometer knob (8), dial sleeve (9) in the Y-axis micrometer, socket head cap screw (10), Y is to linear slide block (11), Y-axis micrometer main shaft (12) is formed, the Y-axis micrometer knob (8) that has EXT scale upward is connected with Y-axis micrometer main shaft (12) threaded one end, Y-axis micrometer knob (8) and interior dial sleeve (9) clearance fit of Y-axis micrometer, dial sleeve (9) and the Y of band guide pin bushing be to linear slide block (11) interference fit in the Y-axis micrometer, and be fixed on Y on the guide pin bushing of linear slide block (11) by socket head cap screw (10); Z axle micrometer assembly is made up of to linear slide block (16), Z axle micrometer main shaft (17) dial sleeve (14), socket head cap screw (15), Z in Z axle micrometer knob (13), the Z axle micrometer, the Z axle micrometer knob (13) that has EXT scale is connected with Z axle micrometer main shaft (17) threaded one end, Z axle micrometer knob (13) and interior dial sleeve (14) clearance fit of Z axle micrometer, dial sleeve (14) and the Z of band guide pin bushing be to linear slide block (16) interference fit in the Z axle micrometer, and be fixed on Z on the guide pin bushing of linear slide block (16) by socket head cap screw (15); Two dimension micrometric displacement platform base (18) is shaped as square, horizontal direction is a Y-axis, vertical direction is the Z axle, and the bottom surface of two-dimentional micrometric displacement platform base (18) is guide pass in level and vertical direction, respectively with Y to linear slide block (11) and Z to the guide pass of linear slide block (16) to cooperating; Along continuous straight runs and vertical direction are equipped with spring (31) and spring (32) respectively in the inner chamber of two-dimentional micrometric displacement platform base (18), one end of spring (31) and spring (32) is separately fixed in the inner chamber of two-dimentional micrometric displacement platform base (18), the other end of spring (31) and Y are affixed to linear slide block (11), the other end of spring (32) and Z are affixed to linear slide block (16), and two-dimentional micrometric displacement platform base (18) is connected by socket head cap screw (20) with support plate (19);
The little forcer of piezoelectric bimorph (III) is by microprobe (21), fixed block (22), two piezoelectric ceramic pieces (23), aluminum sheet metal (24), intermediate plate (25), socket head cap screw (26) is formed, wherein, aluminum sheet metal (24) is sandwiched in the middle of two rectangular piezoelectric ceramic sheets (23), and it is bonding by bonding agent, probe (21) is installed in the center of fixed block (22) by bonding agent, fixed block (22) is bonded in an end of piezoelectric ceramic piece (23) by bonding agent, with the end of the little forcer III of intermediate plate (25) clamping piezoelectric bimorph, and the little forcer III of piezoelectric bimorph is installed on the baseplane of one dimension displacement platform base (6) by socket head cap screw (26) away from probe (21); Two piezoelectric ceramic pieces (23) are drawn an electrode (A) jointly, and aluminum sheet metal (24) is drawn another electrode (B);
Shock attenuation device (IV) is by piezoelectric film cantilever beam type micro-force sensor (27), objective table (28) and damped platform (29) are formed, on damped platform (29), be fixed with objective table (28), piezoelectric film cantilever beam type micro-force sensor (27) is installed on objective table (28), and piezoelectric film cantilever beam type micro-force sensor (27) free end is aimed at microprobe (21).
CNB2007100112755A 2007-05-10 2007-05-10 Piezoelectric film cantilever beam type micro-force sensor micro-force loading device Expired - Fee Related CN100507483C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2007100112755A CN100507483C (en) 2007-05-10 2007-05-10 Piezoelectric film cantilever beam type micro-force sensor micro-force loading device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2007100112755A CN100507483C (en) 2007-05-10 2007-05-10 Piezoelectric film cantilever beam type micro-force sensor micro-force loading device

Publications (2)

Publication Number Publication Date
CN101059381A true CN101059381A (en) 2007-10-24
CN100507483C CN100507483C (en) 2009-07-01

Family

ID=38865598

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2007100112755A Expired - Fee Related CN100507483C (en) 2007-05-10 2007-05-10 Piezoelectric film cantilever beam type micro-force sensor micro-force loading device

Country Status (1)

Country Link
CN (1) CN100507483C (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101798226A (en) * 2010-03-19 2010-08-11 中国电子科技集团公司第二研究所 High-precision transporting device for processing multi-layer green ceramic chip
CN102359844A (en) * 2011-07-27 2012-02-22 合肥工业大学 Differential horizontal micro force loading device and loading method
CN102359843A (en) * 2011-07-27 2012-02-22 合肥工业大学 Differential type horizontal micro-force measuring device and measuring method thereof
CN102496391A (en) * 2011-11-18 2012-06-13 江苏大学 Assembled two-dimensional micro-displacement platform
CN102519646A (en) * 2011-12-15 2012-06-27 大连理工大学 Micro-power loading test method of nonlinear piezoelectric micro-energy collector
CN102889963A (en) * 2011-07-27 2013-01-23 合肥工业大学 Loading method of differential type horizontal micro-force loading device
CN104714123A (en) * 2013-12-13 2015-06-17 旺矽科技股份有限公司 Electrical property detection device
CN105628269A (en) * 2015-12-25 2016-06-01 湖南师范大学 Micro force and micro displacement amplification sensor
CN105720858A (en) * 2016-04-18 2016-06-29 南京理工大学 Friction force precisely adjustable impact type piezoelectric driving device
CN106370366A (en) * 2016-08-19 2017-02-01 西北工业大学 Angular rigidity testing bench based on piezoelectric translation table feeding
CN106783656A (en) * 2016-12-05 2017-05-31 武汉新芯集成电路制造有限公司 A kind of probe structure for WAT detection machines
CN107144397A (en) * 2017-05-05 2017-09-08 中国计量科学研究院 Adding mechanism for the small force value standard set-up of dead weight type safe
CN111044180A (en) * 2019-12-12 2020-04-21 华侨大学 Continuous radial pressure device of semiconductor substrate piece
CN111982676A (en) * 2020-07-28 2020-11-24 宁波大学 Micro-force loading device
CN115342866A (en) * 2022-10-18 2022-11-15 中国空气动力研究与发展中心高速空气动力研究所 Piezoelectric ceramic actuator detection device and system

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101798226A (en) * 2010-03-19 2010-08-11 中国电子科技集团公司第二研究所 High-precision transporting device for processing multi-layer green ceramic chip
CN102889963A (en) * 2011-07-27 2013-01-23 合肥工业大学 Loading method of differential type horizontal micro-force loading device
CN102359844A (en) * 2011-07-27 2012-02-22 合肥工业大学 Differential horizontal micro force loading device and loading method
CN102359843A (en) * 2011-07-27 2012-02-22 合肥工业大学 Differential type horizontal micro-force measuring device and measuring method thereof
CN102889963B (en) * 2011-07-27 2014-08-06 合肥工业大学 Loading method of differential type horizontal micro-force loading device
CN102359844B (en) * 2011-07-27 2013-01-09 合肥工业大学 Differential horizontal micro force loading device and loading method
CN102359843B (en) * 2011-07-27 2013-01-09 合肥工业大学 Differential type horizontal micro-force measuring device and measuring method thereof
CN102496391A (en) * 2011-11-18 2012-06-13 江苏大学 Assembled two-dimensional micro-displacement platform
CN102519646A (en) * 2011-12-15 2012-06-27 大连理工大学 Micro-power loading test method of nonlinear piezoelectric micro-energy collector
CN104714123A (en) * 2013-12-13 2015-06-17 旺矽科技股份有限公司 Electrical property detection device
CN104714123B (en) * 2013-12-13 2018-03-20 旺矽科技股份有限公司 Electrical property detection device
CN105628269A (en) * 2015-12-25 2016-06-01 湖南师范大学 Micro force and micro displacement amplification sensor
CN105628269B (en) * 2015-12-25 2019-01-18 湖南师范大学 A kind of micro- power and micro-displacement amplify sensor
CN105720858A (en) * 2016-04-18 2016-06-29 南京理工大学 Friction force precisely adjustable impact type piezoelectric driving device
CN106370366A (en) * 2016-08-19 2017-02-01 西北工业大学 Angular rigidity testing bench based on piezoelectric translation table feeding
CN106370366B (en) * 2016-08-19 2019-02-01 西北工业大学 A kind of angular rigidity testboard based on the feeding of piezoelectricity translation stage
CN106783656A (en) * 2016-12-05 2017-05-31 武汉新芯集成电路制造有限公司 A kind of probe structure for WAT detection machines
CN106783656B (en) * 2016-12-05 2019-11-29 武汉新芯集成电路制造有限公司 A kind of probe structure for WAT detection machine
CN107144397A (en) * 2017-05-05 2017-09-08 中国计量科学研究院 Adding mechanism for the small force value standard set-up of dead weight type safe
CN107144397B (en) * 2017-05-05 2020-05-05 中国计量科学研究院 Loading mechanism for dead weight type micro force value standard device
CN111044180A (en) * 2019-12-12 2020-04-21 华侨大学 Continuous radial pressure device of semiconductor substrate piece
CN111982676A (en) * 2020-07-28 2020-11-24 宁波大学 Micro-force loading device
CN111982676B (en) * 2020-07-28 2023-09-12 宁波大学 Micro-force loading device
CN115342866A (en) * 2022-10-18 2022-11-15 中国空气动力研究与发展中心高速空气动力研究所 Piezoelectric ceramic actuator detection device and system
CN115342866B (en) * 2022-10-18 2023-01-31 中国空气动力研究与发展中心高速空气动力研究所 Piezoelectric ceramic actuator detection device and system

Also Published As

Publication number Publication date
CN100507483C (en) 2009-07-01

Similar Documents

Publication Publication Date Title
CN100507483C (en) Piezoelectric film cantilever beam type micro-force sensor micro-force loading device
CN104297065B (en) A kind of Piezoelectric Driving micro-stretching test device
EP1829050B1 (en) Scanner for probe microscopy
CN101520389B (en) Super-precision trans-scale in-situ nanometer indentation marking test system
US7685869B2 (en) Nanoindenter
CN108760548B (en) Double-stroke hybrid driving micro-nano indentation/scratch testing device
CN203405372U (en) Flexible hinge type mechanics performance testing platform for in-situ nanoindentation scratching materials
CN204101217U (en) A kind of micro-nano force value standard set-up based on electrostatic force principle
US8281648B2 (en) Material testing apparatus with non-contact sensor
CN101216390A (en) Micro-element dynamic performance off-chip tensile test experimental bench
CN100470230C (en) Suspension type static and dynamic material testing machine of tiny tensile
CN110595880A (en) Mesoscale cantilever beam bending fatigue testing device and testing method
EP2960637A1 (en) Design and interface of a microfabricated scanning force sensor for combined force and position sensing
CN107990859B (en) Micro-displacement sensor calibration device and application thereof
CN103163024A (en) Film loading device
US20060243079A1 (en) Device for high-precision generation and measurement of forces and displacements
CN101710006A (en) Three-dimensional micro-force measuring device
CN100453964C (en) Electric capacity method testing device for electrostrictive material characteristic
CN103293065B (en) Outward bending testing device of microstructural mechanical property sheet
CN116930554A (en) Speed sensor calibration system and calibration method for precision instrument vibration isolator
Chetwynd et al. A controlled-force stylus displacement probe
CN1975335A (en) Universal precision displacement measurement auxiliary device and measuring method
CN108169029B (en) Electromechanical thermal coupling stress corrosion in-situ fatigue performance test device
CN204882204U (en) Tensile fatigue test device of normal position triaxial under many field couplings
RU2306621C1 (en) Two-coordinate micro-positioner

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090701

Termination date: 20130510