CN115435941A - Support base - Google Patents

Support base Download PDF

Info

Publication number
CN115435941A
CN115435941A CN202211149250.2A CN202211149250A CN115435941A CN 115435941 A CN115435941 A CN 115435941A CN 202211149250 A CN202211149250 A CN 202211149250A CN 115435941 A CN115435941 A CN 115435941A
Authority
CN
China
Prior art keywords
shell
monitoring unit
laser
fixed
housing
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.)
Pending
Application number
CN202211149250.2A
Other languages
Chinese (zh)
Inventor
赵宝栓
张博
桑运琪
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.)
Hebei Hangke Engineering Detection Equipment Technology Co ltd
Original Assignee
Hebei Hangke Engineering Detection Equipment Technology Co ltd
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 Hebei Hangke Engineering Detection Equipment Technology Co ltd filed Critical Hebei Hangke Engineering Detection Equipment Technology Co ltd
Priority to CN202211149250.2A priority Critical patent/CN115435941A/en
Publication of CN115435941A publication Critical patent/CN115435941A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/24Measuring force or stress, in general by measuring variations of optical properties of material when it is stressed, e.g. by photoelastic stress analysis using infrared, visible light, ultraviolet
    • EFIXED CONSTRUCTIONS
    • E01CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01DCONSTRUCTION OF BRIDGES, ELEVATED ROADWAYS OR VIADUCTS; ASSEMBLY OF BRIDGES
    • E01D19/00Structural or constructional details of bridges
    • E01D19/04Bearings; Hinges
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/12Measuring force or stress, in general by measuring variations in the magnetic properties of materials resulting from the application of stress
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/20Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress
    • G01L1/22Measuring force or stress, in general by measuring variations in ohmic resistance of solid materials or of electrically-conductive fluids; by making use of electrokinetic cells, i.e. liquid-containing cells wherein an electrical potential is produced or varied upon the application of stress using resistance strain gauges
    • G01L1/2206Special supports with preselected places to mount the resistance strain gauges; Mounting of supports

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

The invention discloses a support, which relates to the technical field of bridge engineering monitoring and comprises the following components: an upper support plate and a lower support plate; a main body part arranged between the upper support plate and the lower support plate; the sensors are respectively detachably arranged between the upper supporting plate and the lower supporting plate of the support; the sensor comprises a first shell, a second shell, a first monitoring module, a third shell, a fourth shell and a second monitoring module, wherein the second shell is sleeved in the first shell in a longitudinally movable mode, the first monitoring module is arranged in a first containing cavity formed by the first shell and the second shell and used for acquiring distance information of the first shell and the second shell, the fourth shell is fixedly connected with the first shell and sleeved with the third shell in a transversely movable mode, and the second monitoring module is arranged in a second containing cavity formed by the third shell and the fourth shell and used for acquiring sensor data. The support disclosed by the invention is simple in structure and can be used for monitoring a bridge in real time.

Description

Support base
The application is a divisional application of an invention patent with a parent name of 'sensor and support'; application of parent application
The application numbers are: CN201811146812.1; the application date of the parent application is as follows: 2018-09-29.
Technical Field
The invention relates to the technical field of bridge engineering monitoring, in particular to a support.
Background
The support is an important part for bearing the upper part and the lower part of engineering such as a bridge, and the force of the upper part is transmitted to the foundation of the lower part through the support. The bridge at home and abroad is frequently collapsed or locally damaged in the operation and use period or the bridge construction period, and each accident can cause huge loss to the lives and properties of people. The main reason for the collapse of the bridge is that the load borne by the bridge is changed and accumulated to a certain extent by various external factors, and exceeds the bearing capacity of the structure. In order to ensure the stress of the bridge and the running safety of vehicles, the stress state and the use state of the bridge need to be monitored in real time so as to find accident potential in time and eliminate the potential.
At present, the existing monitoring mode is to design a dynamometric support in advance according to bridge construction or design requirements before bridge construction, install the dynamometric support between a bridge and an abutment, and monitor the stress condition of the bridge. The force measuring components such as the sensor of the force measuring support are arranged in the support and are integrated with the support, so that the force measuring support can only be used in the bridge construction process and cannot be used in the constructed bridge. Meanwhile, when the sensor of the force measuring support breaks down, the bridge cannot be continuously monitored by maintaining or replacing a new sensor.
Disclosure of Invention
The invention aims to provide a support which is used for solving the technical problems in the prior art, can monitor an operated bridge in real time and can replace a failed support in time.
In order to achieve the purpose, the invention provides the following scheme:
the invention discloses a support, comprising:
an upper support plate and a lower support plate;
a main body portion provided between the upper support plate and the lower support plate;
sensors detachably disposed between the upper support plate and the lower support plate of the cradle, respectively;
the sensor comprises a first shell, a second shell, a first monitoring module, a third shell, a fourth shell and a second monitoring module, wherein the second shell is sleeved in the first shell in a longitudinally movable mode, the first monitoring module is arranged in a first accommodating cavity formed by the first shell and the second shell and used for acquiring distance information of the first shell and the second shell, the fourth shell is fixedly connected with the first shell, the fourth shell is sleeved with the third shell in a transversely movable mode, and the second monitoring module is arranged in a second accommodating cavity formed by the third shell and the fourth shell and used for acquiring sensor data;
the first monitoring module comprises a first monitoring unit and a second monitoring unit, the first monitoring unit is fixed in the first shell, the second monitoring unit is arranged opposite to the first monitoring unit, and the second monitoring unit is fixed in the second shell;
the second monitoring module comprises a third monitoring unit and a fourth monitoring unit, the third monitoring unit is fixed in the third shell, the fourth monitoring unit is arranged opposite to the third monitoring unit, and the fourth monitoring unit is fixed in the fourth shell;
the fourth shell is arranged on the top of the first shell, and a gap is formed between the fourth shell and the first shell.
Preferably, the cross sections of the upper support plate and the lower support plate are larger than the cross section of the main body part, so that a communicated groove is formed between the outer side of the main body part and the upper support plate and the lower support plate;
the upper supporting plate is provided with a plurality of groups of first grooves, the lower supporting plate is provided with second grooves at positions corresponding to the first grooves, and the sensors are fixed in the first grooves and the second grooves.
Preferably, the number of the sensors is four, and the sensors are symmetrically arranged on the outer side of the main body part in pairs.
Preferably, go up the backup pad with be equipped with fixed panel on the extending direction of backup pad down, be equipped with the recess on the fixed panel, the sensor can install in the recess.
Preferably, the first monitoring unit is a laser transmitter, the laser transmitter is fixedly connected with the first shell through a fixing rod, the second monitoring unit is a laser receiver, and the laser receiver is arranged opposite to the laser transmitter along a laser emission light path.
Preferably, a laser emission light path of the laser emitter is parallel to the bottom surface of the second housing, and the laser receiver is fixed on the inner wall of the second housing along the laser emission light path;
and the laser receiver and the bottom surface of the second shell form a preset included angle.
Preferably, the laser emission light path of the laser emitter is perpendicular to the bottom surface of the second housing, the laser receiver is fixed on the bottom surface of the second housing along the laser emission light path, and the size of the laser receiver is the same as that of the bottom surface of the second housing.
Preferably, the first monitoring unit is a laser transmitting and receiving all-in-one machine, and the laser transmitting and receiving all-in-one machine is configured to enable the laser transmitting optical path to be perpendicular to the bottom surface of the second shell;
the second monitoring unit is a laser reflector and is fixed on the bottom surface of the second shell along the laser emission light path; or
The first monitoring unit is a grating sliding rod, the second monitoring unit is a grating detection device, the grating detection device is provided with a detection hole, and when the grating sliding rod moves along the detection hole, the grating detection device acquires sensor data; or
The first monitoring unit is a magnetic conduction device, the second monitoring unit is an excitation coil, and the magnetic conduction device and the excitation coil move relatively; or
The first monitoring unit is a trigger device, and the second monitoring unit is a resistance strain device;
wherein the resistive strain device comprises:
the resistance strain bracket is fixed in the second shell;
the strain circuit is arranged in the resistance strain bracket;
the resistance strain gauge is arranged at the top of the resistance strain bracket and is electrically connected with the strain circuit; or alternatively
The first monitoring unit is a movable polar plate, the second monitoring unit is a fixed polar plate, and the fixed polar plate is fixed on the inner wall of the second shell and is opposite to the movable polar plate.
Preferably, the third monitoring unit has the same structure as the first monitoring unit, and the fourth monitoring unit has the same structure as the second monitoring unit.
Compared with the prior art, the invention achieves the following technical effects:
the application discloses support, in the first casing was located to the second casing cover of sensor, first monitoring module set up in the first holding cavity that first casing and second casing formed, through the distance information of monitoring first casing and second casing, acquireed sensor data. The sensor is simple in structure, can be detachably mounted on a support of an operated bridge, and monitors the bridge in real time.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
FIG. 1 is a first schematic perspective view of a sensor according to a first embodiment of the present application;
FIG. 2 is a second perspective view of a sensor according to the first embodiment of the present application;
FIG. 3 is a third schematic perspective view of a sensor according to the first embodiment of the present application;
FIG. 4 is a schematic perspective view of a sensor according to a second embodiment of the present application;
FIG. 5 is a schematic perspective view of a sensor according to a third embodiment of the present application;
FIG. 6 is a schematic perspective view of a sensor according to a fourth embodiment of the present application;
FIG. 7 is a schematic perspective view of a sensor according to a fifth embodiment of the present application;
FIG. 8 is a schematic perspective view of a sensor according to a fifth embodiment of the present application;
FIG. 9 is a front view of a sensor of a sixth embodiment of the present application;
FIG. 10 is a front view of a sensor of a seventh embodiment of the present application;
FIG. 11 is a front view of a sensor of a seventh embodiment of the present application;
FIG. 12 is a perspective view of a support base of an eighth embodiment of the present application;
FIG. 13 is a front view of a mount of an eighth embodiment of the present application;
FIG. 14 is a top view of a mount of an eighth embodiment of the present application;
FIG. 15 is a partial cross-sectional view of a mount of an eighth embodiment of the present application;
FIG. 16 is a second partial cross-sectional view of a standoff according to an eighth embodiment of the present application;
FIG. 17 is a third partial cross-sectional view of a mount of the eighth embodiment of the present application;
in the figure: 1-a sensor; 11-a first housing; 111-a first opening; 12-a second housing; 121-a second opening; 13-a first monitoring module; 131-a first monitoring unit; 132-a second monitoring unit; 1321-detection well; 133-a fixing bar; 134-a fixed seat; 14-a second monitoring module; 141-a third monitoring unit; 142-a fourth monitoring unit; 15-a third housing; 151-third opening; 16-a fourth shell; 161-a fourth opening; 17-a gap; 2-an upper support plate; 21-a first groove; 3-a lower support plate; 31-a second groove; 4-a body portion; a-a resistive strain mount; a C-resistance strain gage; d-groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without making any creative effort based on the embodiments in the present invention, belong to the protection scope of the present invention.
The invention aims to provide a sensor and a support, which are used for solving the technical problems in the prior art, can monitor a running bridge in real time and can replace a failed support in time.
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in further detail below.
The first embodiment is as follows:
fig. 1-3 are schematic structural views of a sensor according to an embodiment of the present application. As shown in fig. 1 to 3, the sensor 1 includes a first housing 11, a second housing 12, and a first monitoring module 13. The second housing 12 is longitudinally movably sleeved in the first housing 11, and the first housing and the second housing form a first accommodating cavity. The first monitoring module 13 is disposed in the first accommodating cavity and used for monitoring and acquiring sensor data. When the first housing 11 and the second housing 12 are subjected to an external force, the first housing 11 and the second housing 12 can move longitudinally relative to each other, so as to drive the first monitoring module 13 to move in the first accommodating cavity for monitoring and acquiring sensor data.
The first housing 11 includes a first opening 111, and the first opening 111 is disposed downward. The second housing 12 includes a second opening 121, and the second opening 121 is disposed upward. The cross-sectional dimension of the second opening 121 is smaller than the cross-sectional dimension of the first opening 111, so that the second housing 12 is sleeved in the first housing 11, and the second housing and the first housing surround to form a first accommodating cavity with variable volume. Preferably, elastic members having elasticity such as springs are provided in the first housing 11 and the second housing 12, and the first housing 11 and the second housing 12 can be in the first state and the second state by the elastic members. In the first state, that is, when no external force is applied to the first housing 11 and the second housing 12, the elastic member is not subjected to force; the second state is that the first housing 11 and the second housing 12 are moved relatively by the elastic force of the elastic member after receiving an external force. When the external force disappears, the first housing 11 and the second housing 12 are switched from the second state to the first state by the elastic force of the elastic member. The first housing 11 and the second housing 12 may be provided in a cylindrical opening structure having an arbitrary shape in cross section. Preferably, the first housing 11 and the second housing 12 are provided in a cylindrical opening structure.
The first monitoring module 13 includes a first monitoring unit 131 and a second monitoring unit 132. The first monitoring unit 131 is disposed in the first housing 11 and is fixedly connected to the top of the first housing 11. The second monitoring unit 132 is disposed in the second housing 12, and is opposite to the first monitoring unit 131. When the first housing 11 is subjected to a downward external force, the first housing 11 drives the first monitoring unit 131 to move downward, and a relative distance between the first monitoring unit 131 and the second monitoring unit 132 changes, so that the sensor data obtained by monitoring changes.
In this embodiment, the first monitoring unit 131 is a laser transmitter, and the second monitoring unit 132 is a laser receiver. The laser receiver is arranged opposite to the laser transmitter along a laser emission light path of the laser transmitter and used for receiving laser and converting received light energy into electric energy, then corresponding electric signal parameters are sent to the data processor in a wireless or wired mode to be processed and analyzed, whether the bridge is in a normal load bearing range is judged, and measures such as maintenance, reinforcement and the like are taken in time according to the stress state of the bridge. In this embodiment, the material of the laser receiver is graphene, which can absorb photon energy. The laser receiver is characterized in that a metal electrode is evaporated on the graphene layer and is connected with a detection circuit through the metal electrode. The working principle of the laser receiver is that a Schottky barrier is formed at a contact part of metal and graphene, and in a space electric field area of the Schottky barrier, surplus electrons and holes excited by light are separated by an electric field to form photocurrent. When the relative distance between the laser transmitter and the laser receiver is different, the laser receiver receives different photon energy, and the generated photocurrent is different.
In this embodiment, the laser emitter is fixedly connected to the first housing 11 through a fixing rod 133, and is disposed in a central area of the first housing 11. The laser emitting path of the laser emitter 131 is horizontal and parallel to the bottom surface of the second housing 12, as indicated by the arrows in fig. 1 and 2. The laser receiver is fixed on the inner wall of the second shell 12 along the laser emission optical path, so that the laser emitted by the laser emitter is positioned in the laser receiving range of the laser receiver. Wherein, the surface of the laser receiver for receiving the laser is arranged to have a certain slope from top to bottom, i.e. the surface forms a predetermined included angle α with the bottom surface of the second housing 12, as shown in fig. 1. In this embodiment, the predetermined included angle α is smaller than 90 degrees or greater than 90 degrees, when an external force is applied to the first housing 11 and the second housing 12, and the first housing 11 and the second housing 12 move relatively, the distance from the laser emitted by the laser emitter to the surface of the laser receiver changes, so that the intensity of the light received by the laser receiver changes, and further the internal electrical signal changes, and the electrical signal is transmitted to the data processor for calculation and analysis, so as to calculate the external force borne by the first housing 11 and the second housing 12.
Preferably, the laser receiver may be provided as a columnar structure having a through hole provided therein, a surface of the through hole being for receiving the laser light. The outer wall of the laser receiver is the same shape as the inner wall of the second housing 12 so that the laser receiver and the second housing 12 can be fixedly connected more closely. The through hole in the laser receiver can be a circular truncated cone structure. Preferably, the upper end surface of the circular truncated cone structure is larger than the lower end surface, as shown in fig. 2. When the first housing 11 and the second housing 12 are subjected to a complex external force, the first housing 11 drives the laser transmitter to generate lateral deviation, and the laser receiver can still receive laser at the moment, so that the purpose of monitoring is achieved.
In another implementation, the laser emission optical path of the laser emitter is vertical and perpendicular to the bottom surface of the second housing 12, as shown by the arrow in fig. 3. The laser receiver is arranged in a plane structure and fixed on the bottom surface of the second housing 12 along the laser emission optical path, so that the laser emitted by the laser emitter is located in the laser receiving range of the laser receiver, as shown in fig. 3. When the shell is stressed, the laser transmitter and the laser receiver are driven to move relatively, so that the relative distance from the laser transmitted by the laser transmitter to the laser receiver is changed, the laser receiver can change the internal electric signal, the electric signal is transmitted to the data processor for operation and analysis, and the bearing load of the shell is calculated. Preferably, the size of the laser receiver is the same as that of the bottom surface of the second housing 12, and when the laser transmitter moves laterally, the laser receiver can still receive laser, so that the sensor acquires sensor data, and the monitoring accuracy of the sensor is improved.
Example two:
the present embodiment differs from the first embodiment only in that the first monitoring module 13 of the sensor 1 is different, specifically: the first monitoring unit 131 is a laser transceiver, and the second monitoring unit 132 is a laser reflector, as shown in fig. 4. The working principle of the laser transmitting and receiving all-in-one machine is that a laser transmitting unit and a laser receiving unit are arranged in the same direction to form an integral structure. When the laser emitting unit is electrified to emit laser, the laser is reflected to the laser receiving unit through the laser reflector, so that a circuit connected with the laser receiving unit is conducted, and an electric signal is generated. Wherein, the laser emitting unit can be a laser emitting diode, and the laser receiving unit can be a photosensitive diode or the like.
In this embodiment, the laser transmitter-receiver is fixedly connected to the first housing 11 through a fixing rod 133, and a laser transmitting light path of the laser transmitter-receiver is perpendicular to the bottom surface of the second housing 12. The laser reflector is arranged in a planar structure and fixed on the bottom surface of the second housing 12 along the laser emission optical path, so that the laser emitted by the laser emission unit is positioned in the laser receiving and reflecting range of the laser reflector, as shown in fig. 4. When the shell is stressed, the laser transmitting and receiving all-in-one machine and the laser reflector are driven to move relatively, so that the relative distance from the laser transmitted by the laser transmitting and receiving all-in-one machine to the laser reflector is changed, meanwhile, the angle of the laser reflected by the laser reflector is also changed, the intensity of the light received by the laser receiving unit is changed, the internal electric signal is further changed, the electric signal is transmitted to the data processor for operation and analysis, and the bearing load of the shell is calculated. Preferably, the size of the laser reflector is the same as that of the bottom surface of the second shell 12, and when the laser transmitting and receiving all-in-one machine moves transversely, the laser reflector can still receive laser to reflect, so that the sensor acquires data of the sensor, and the monitoring accuracy of the sensor is improved.
Example three:
the present embodiment differs from the first and second embodiments only in that the first monitoring module 13 of the sensor 1 is different, specifically: the first monitoring unit 131 is a grating sliding rod, and the second monitoring unit 132 is a grating detection device. The grating sliding rod is fixedly connected with the first shell 11 and is perpendicular to the bottom surface of the second shell 12. The optical grating detection device is fixed on the bottom surface of the second housing 12 through a fixing seat 134, and a detection hole 1321 is formed thereon, as shown in fig. 5. The grating sliding rod is coaxial with the detection hole 1321, the diameter of the detection hole 1321 is larger than that of the grating sliding rod, and the grating sliding rod can move longitudinally along the detection hole 1321.
The grating slide bar has grating stripes. The grating detection device comprises a light source, a convergent lens, an indication grating, a photoelectric element, a driving circuit and the like. When the grating sliding rod moves longitudinally along the detection hole 1321, an included angle is formed between grating stripes of the grating sliding rod and grating stripes of the indication grating, and light and dark stripes are formed under the irradiation of a light source. Along with the relative movement of the grating sliding rod and the indication grating, the formed light and dark stripes move along with the relative movement, and different light and dark stripes are directly irradiated on the photoelectric element to output different digital pulse signals.
When the housing is stressed, the first housing 11 of the sensor drives the grating sliding rod and the grating detection device to move relatively, digital pulse signals are output, and the digital pulse signals are processed and analyzed by the data processor, so that various forces borne by the first housing 11 and the second housing 12 are calculated. The embodiment detects through the grating, and has the characteristics of high detection precision and high response speed.
Example four:
the present embodiment is different from the first, second, and third embodiments only in that the first monitoring module 13 of the sensor 1 is different, specifically: the first monitoring unit 131 is a magnetic conductive device, and the second monitoring unit 132 is an excitation coil. The magnetic conduction device is an iron rod or an iron core, is fixed in the first shell 11, and is perpendicular to the bottom surface of the second shell 12. The excitation coil is disposed opposite to the magnetic conductive device and fixed to the bottom surface of the second housing 12. The coil dimensions of the exciter coil are larger than the magnetically permeable means, which are relatively movable within the exciter coil, as shown in fig. 6. The magnet exciting coil generates a magnetic field after being electrified, and when the magnetic conduction device moves relatively in the magnet exciting coil, the magnetic resistance can be changed, so that the current in a circuit connected with the magnet exciting coil is changed.
When the shell is stressed, the first shell 11 drives the magnetic conduction device to move relatively in the excitation coil, and at the moment, the magnetic conduction of the excitation coil changes, so that the current in a circuit connected with the excitation coil is changed. The second monitoring unit transmits the current signal to a data processor for processing and analysis, so as to calculate various forces borne by the first shell 11 and the second shell 12.
Example five:
the present embodiment is different from the first, second, third and fourth embodiments only in that the first monitoring module 13 of the sensor 1 is different, specifically: the first monitoring unit 131 is a trigger device, and the second monitoring unit 132 is a resistance strain device. The trigger device is used for applying force to the resistance strain device so as to enable the resistance strain device to deform and further change the resistance of the resistance strain device. The triggering device can be a rod-shaped structure, and the end part of the triggering device is provided with a circular structure so as to avoid damaging the resistance strain device. The trigger device is fixed in the first housing 11 and is perpendicular to the bottom surface of the second housing 12. The resistive strain device is disposed opposite the trigger device and is fixed to the bottom surface of the second housing 12, as shown in fig. 7 and 8.
The resistance strain device comprises a resistance strain support A, a strain circuit B (not shown in the figure) and a resistance strain gauge C. The resistance strain gauge C is disposed on the top of the resistance strain bracket a, so that when the trigger device 131 and the resistance strain device 132 move relatively, the trigger device 131 and the resistance strain gauge C can directly contact each other, and further the resistance strain gauge C deforms to change the resistance. The strain circuit B is arranged in the resistance strain bracket A and is electrically connected with the resistance strain gauge C. When the resistance strain gauge C deforms, the resistance changes, and the voltage or current in the strain circuit B is changed. In this embodiment, the resistance strain bracket a is provided in a cylindrical shape, the top portion thereof has good elasticity, and the resistance strain gauge C is adhered to the surface of the top portion, as shown in fig. 8. When the resistance strain gauge C is subjected to external force, the resistance strain gauge C can deform along with the top of the resistance strain support A, and damage to the resistance strain gauge C is avoided. In another implementation manner, the top of the resistance strain bracket a may be provided as a hollow structure, and the resistance strain gauge C is provided on the top of the resistance strain bracket a, and the resistance strain gauge C is larger than the area of the top of the resistance strain bracket a, as shown in fig. 7. When the resistance strain gauge C is subjected to external force, the resistance strain gauge C moves into the hollow structure of the resistance strain support A and deforms.
When the shell is stressed, the first shell 11 drives the trigger device and the resistance strain device to move relatively, at the moment, the trigger device applies external force to the resistance strain gauge, the resistance strain gauge C deforms, the resistance changes, and voltage or current in the strain circuit B is further changed. The current or voltage signal is transmitted to a data processor for processing and analysis, so as to calculate the external force borne by the first shell 11 and the second shell 12.
Example six:
the present embodiment differs from the first to fifth embodiments only in that the first monitoring module 13 of the sensor 1 is different, specifically: the first monitoring unit 131 is a movable plate, and the second monitoring unit 132 is a fixed plate. The movable pole plate is fixed to the first housing 11 by a fixing rod 133. The fixed plate is disposed on the inner wall of the second casing 12, and is disposed opposite to the movable plate in parallel to form a capacitor, as shown in fig. 9. When the movable polar plate and the fixed polar plate move transversely relatively, the voltage between the movable polar plate and the fixed polar plate changes.
When the housing is subjected to an external force, the first housing 11 drives the movable polar plate and the fixed polar plate to move relatively, so that the voltage between the movable polar plate and the fixed polar plate changes. The voltage signal is transmitted to a data processor for processing and analysis, so as to calculate the external force borne by the first shell 11 and the second shell 12.
Example seven:
fig. 10 is a schematic structural diagram of a sensor according to an embodiment of the present application. The present embodiment is different from the first to sixth embodiments in that the sensor 1 further includes a second monitoring module 14, a third housing 15, and a fourth housing 16. The fourth casing 16 is disposed on the top of the first casing 11, and has one side fixedly connected to the first casing 11 and the other side provided with a fourth opening 161. Wherein a gap 17 is formed between the fourth housing 16 and the top of the first housing 11, so that the third housing 15 can be sleeved on the outer side of the fourth housing 16 in a laterally movable manner. Preferably, the height of the gap 17 is the same as the wall thickness of the third housing 15. A side of the third casing 15 is provided with a third opening 151 opposite to a fourth opening 161 of the fourth casing 16, so that the third casing 15 and the fourth casing 16 form a second receiving cavity.
The second monitoring module 14 is disposed in the second accommodating cavity, and is configured to monitor and acquire sensor data. When the third housing 15 and the fourth housing 16 are subjected to an external force, the third housing 15 and the fourth housing 16 can move transversely relative to each other, so as to drive the second monitoring module 14 to move in the second accommodating cavity for monitoring and acquiring sensor data.
In this embodiment, the first monitoring module 13 and the second monitoring module 14 have the same structure, and may have the same structure as any one of the first monitoring module 13 in the first to sixth embodiments. The first monitoring module 13 is mounted in the same manner as in the first to sixth embodiments. The second monitoring module 14 is mounted in a manner perpendicular to the first monitoring module 13. The second monitoring module 14 includes a third monitoring unit 141 and a fourth monitoring unit 142. The third monitoring unit 141 is fixed in the third housing 15 in parallel with the bottom of the third housing 15. The fourth monitoring unit 142 is disposed opposite to the third monitoring unit 141, and is fixed in the fourth housing 16.
Preferably, elastic members having elasticity such as springs are provided in the third casing 15 and the fourth casing 16, and the third casing 15 and the fourth casing 16 can be in the first state and the second state by the elastic members. In the first state, that is, when no external force is applied to the third casing 15 or the fourth casing 16, the elastic member is not subjected to a force; the second state is that the third casing 15 and the fourth casing 16 are subjected to an external force and then relatively move in the lateral direction by the elastic force of the elastic member. When the external force disappears, the third casing 15 and the fourth casing 16 are switched from the second state back to the first state by the elastic force of the elastic member. The third and fourth housings 15 and 16 may be provided in a cylindrical or square opening structure. Preferably, the third and fourth housings 15 and 16 are provided in a square opening structure.
When the shell is subjected to a longitudinal external force, the third shell 15 transmits the external force to the first shell 11, so that the first shell 11 and the second shell 12 move longitudinally relative to each other, the distance between the first monitoring unit 131 and the second monitoring unit 132 is shortened, corresponding sensor data is generated and sent to the data processor for analysis and processing, and the magnitude of the longitudinal external force applied to the current shell can be obtained.
When the shell is subjected to a lateral external force, the third shell 15 and the fourth shell 16 move laterally relative to each other, the distance between the third monitoring unit 141 and the fourth monitoring unit 142 is shortened, and the currently acquired sensor data is sent to the data processor for analysis and processing, so that the magnitude of the lateral external force applied to the current shell can be obtained.
When the shell is subjected to the transverse external force and the longitudinal external force simultaneously, the third shell 15 and the fourth shell 16 move transversely relative to each other, and the third shell 15 transmits the longitudinal external force to the first shell 11, so that the first shell 11 and the second shell 12 move longitudinally relative to each other, and at the moment, the data processor can calculate the specific condition of the current external force applied to the shell according to the sensor data acquired by monitoring through the first monitoring module 13 and the second monitoring module 14.
In another implementation manner, the fourth housing 16 is fixedly connected to the first housing 11 and disposed on the top of the first housing 11, and the third housing 15 can be sleeved in the fourth housing 16 in a laterally movable manner. As shown in fig. 11. The third monitoring unit 141 is fixed in the fourth housing 16 in parallel with the bottom of the fourth housing 16. The fourth monitoring unit 142 is disposed opposite to the third monitoring unit 141, and is fixed in the third housing 15.
When the housing receives a longitudinal external force, the fourth housing 16 transmits the external force to the first housing 11, so that the first housing 11 and the second housing 12 move longitudinally relative to each other, the distance between the first monitoring unit 131 and the second monitoring unit 132 changes, corresponding sensor data is generated and sent to the data processor for analysis, and the magnitude of the longitudinal external force received by the current housing can be obtained.
When the shell is subjected to a lateral external force, the third shell 15 and the fourth shell 16 move laterally relative to each other, the distance between the third monitoring unit 141 and the fourth monitoring unit 142 changes, and the currently acquired sensor data is sent to the data processor for analysis and processing, so that the magnitude of the lateral external force applied to the current shell can be obtained.
When the shell receives a transverse external force and a longitudinal external force at the same time, the third shell 15 and the fourth shell 16 move transversely relative to each other, and meanwhile, the fourth shell 16 transmits the longitudinal external force to the first shell 11, so that the first shell 11 and the second shell 12 move longitudinally relative to each other, and at the moment, the data processor can calculate the specific condition of the current external force received by the shell according to the sensor data monitored and acquired by the first monitoring module 13 and the second monitoring module 14.
In other implementation manners, the first monitoring module 13 and the second monitoring module 14 may be configured as the first monitoring module with any two different structures in the first to sixth embodiments.
Embodiments one to seven the sensor 1 may be fixedly provided in a structure having upper and lower clamp plates, respectively. When sensor 1 and punch holder installation, can set up the recess in the relative one side of punch holder for sensor 1 can be embedded in the recess, and when punch holder received external force and takes place to warp, sensor 1 can not break away from punch holder, can monitor the external force that obtains punch holder received simultaneously. The sensor may be mounted on a support between the bridge and the pier. To the bridge that has moved, because the structure of support has been fixed, sensor 1 can't directly install rather than, can be through the last backup pad of support and the fixed panel of the extending direction welding of bottom suspension fagging, then set up the recess on fixed panel, utilize sensor 1's flexible performance to install in the recess, can carry out the atress monitoring to the bridge that has moved. When the sensor 1 is damaged, the sensor can be simply and conveniently replaced through the telescopic performance of the sensor, the operation of a bridge is not influenced, and meanwhile, the cost is saved.
Example eight:
fig. 12-17 are schematic structural views of a support according to an embodiment of the present application. As shown in fig. 12 to 17, the support includes at least one sensor 1, an upper support plate 2, a lower support plate 3, and a body portion 4. The main body 4 is provided between the upper support plate 2 and the lower support plate 3. The cross sections of the upper supporting plate 2 and the lower supporting plate 3 are larger than that of the main body part 4, so that the outer side of the main body part 4 and the upper supporting plate 2 and the lower supporting plate 3 form a communicated groove D. That is, the upper support plate 2, the lower support plate 3 and the main body 4 have an i-shaped cross section in any longitudinal direction. The sensor 1 is arranged in the groove D (i.e. in the frame on both sides of the i-shaped structure) and is detachably arranged between the upper support plate 2 and the lower support plate 3, as shown in fig. 13. Wherein, it is provided with first recess 21 and second recess 31 respectively to go up backup pad 2 and the relative one side of bottom suspension fagging 3, the top and the bottom of sensor 1 are embedded in first recess 21 and second recess 31 respectively, make sensor 1 is fixed in go up between backup pad 2 and the bottom suspension fagging 3. When the upper support plate 2 and the lower support plate 3 are subjected to relative movement by an external force, the sensor 1 may be used to detect the external force applied to the upper support plate 2 and the lower support plate 3.
In this embodiment, the structure of the sensor 1 may be the same as any one of the sensor structures of the first to seventh embodiments. When the sensor 1 is configured to have the same structure as that of the first embodiment to the sixth embodiment, the first recess 21 corresponds to the top structure of the first housing 11 of the sensor 1, and the second recess 31 corresponds to the bottom structure of the second housing 12 of the sensor 1, as shown in fig. 15 and 16. When the sensor 1 is configured to be the same as the sensor structure in the seventh embodiment, the first recess 21 is adapted to the top structure of the third housing 15 or the fourth housing 16 of the sensor 1, and the second recess 31 is adapted to the bottom structure of the second housing 12 of the sensor 1, as shown in fig. 17.
In this embodiment, the support may comprise a plurality of sensors 1. A plurality of sets of first grooves 21 and second grooves 31, which are the same in number as the sensors 1, are provided on opposite sides of the upper support plate 2 and the lower support plate 3, respectively. A plurality of sensors 1 are respectively fixed in the first recess 21 and the second recess 31. Preferably, when the upper support plate 2 and the lower support plate 3 are square plates, a first groove 21 and a second groove 31 are respectively formed at positions of the upper support plate 11 and the lower support plate 13 near four sides, respectively, for fixing the sensor 1, as shown in fig. 14. Wherein the grooves on opposite sides are symmetrical so that the two sensors 1 on opposite sides are symmetrical. When the support bears pressure to stretch out and draw back, rotate or slide, the data processor can carry out analysis and processing according to the data of a single sensor 1, and can also carry out processing and analysis with the sensor data of two symmetrically arranged sensors 1 so as to improve the monitoring accuracy. When the upper support plate 2 and the lower support plate 3 are circular plates, a set of first grooves 21 and second grooves 31 may be provided every 90 degrees of the circular plates.
The support of the embodiment is an important part for bearing the upper part and the lower part in engineering such as a bridge, and the force of the upper part is transmitted to the lower part foundation through the support. The upper supporting plate 2 of the support is used for being connected with a steel plate at the bottom of the bridge, and the lower supporting plate 3 is used for being connected with a steel plate at the top of the bridge pier. When the beam body is deformed, the beam body transmits force to the support, the upper supporting plate 2 and the lower supporting plate 3 of the support move relatively to change the sensor data of the sensor 1 on the support, and the data processor can analyze the stress state of the bridge according to the sensor data. Specifically, when the support is not subjected to external force, the sensor data acquired by the sensors 1 on the support are respectively calibrated, meanwhile, a database is established, and the future safety state of the support or the bridge is deduced through the processing and analysis of big data. When the support bears external force, the data processor compares and analyzes the sensor data currently acquired by the sensor 1 with the big data to determine the stress state of the current bridge, so that measures such as maintenance and reinforcement of the unsafe bridge can be carried out in time, and the normal operation state of the bridge is ensured.
The application discloses sensor and support, in first casing was located to the second casing cover of sensor, first monitoring module set up in the first holding cavity that first casing and second casing formed, is used for acquireing the distance information of first casing and second casing through the monitoring, acquires sensor data. The sensor is simple in structure, can be detachably mounted on a support of an operated bridge, and monitors the bridge in real time.
The principle and the implementation mode of the present invention are explained by applying specific examples in the present specification, and the above description of the embodiments is only used to help understanding the method and the core idea of the present invention; meanwhile, for a person skilled in the art, according to the idea of the present invention, the specific embodiments and the application range may be changed. In view of the above, the present disclosure should not be construed as limiting the invention.

Claims (9)

1. A mount, comprising:
an upper supporting plate and a lower supporting plate;
a main body part disposed between the upper support plate and the lower support plate;
sensors detachably disposed between the upper support plate and the lower support plate of the support, respectively;
the sensor comprises a first shell, a second shell, a first monitoring module, a third shell, a fourth shell and a second monitoring module, wherein the second shell is sleeved in the first shell in a longitudinally movable mode, the first monitoring module is arranged in a first accommodating cavity formed by the first shell and the second shell and used for acquiring distance information of the first shell and the second shell, the fourth shell is fixedly connected with the first shell, the fourth shell is sleeved with the third shell in a transversely movable mode, and the second monitoring module is arranged in a second accommodating cavity formed by the third shell and the fourth shell and used for acquiring sensor data;
the first monitoring module comprises a first monitoring unit and a second monitoring unit, the first monitoring unit is fixed in the first shell, the second monitoring unit is arranged opposite to the first monitoring unit, and the second monitoring unit is fixed in the second shell;
the second monitoring module comprises a third monitoring unit and a fourth monitoring unit, the third monitoring unit is fixed in the third shell, the fourth monitoring unit is arranged opposite to the third monitoring unit, and the fourth monitoring unit is fixed in the fourth shell;
the fourth shell is arranged on the top of the first shell, and a gap is formed between the fourth shell and the first shell.
2. A mount, as claimed in claim 1, wherein: the cross sections of the upper supporting plate and the lower supporting plate are larger than that of the main body part, so that a communicated groove is formed between the outer side of the main body part and the upper supporting plate and the lower supporting plate;
the upper supporting plate is provided with a plurality of groups of first grooves, the lower supporting plate is provided with second grooves at positions corresponding to the first grooves, and the sensors are fixed in the first grooves and the second grooves.
3. A mount, as claimed in claim 1, wherein: the number of the sensors is four, and the sensors are symmetrically arranged on the outer side of the main body part in pairs.
4. A mount, as claimed in claim 1, wherein: go up the backup pad with be equipped with fixed panel on the extending direction of backup pad down, be equipped with the recess on the fixed panel, the sensor can install in the recess.
5. A mount, as set forth in claim 1, wherein: the first monitoring unit is a laser transmitter, the laser transmitter is fixedly connected with the first shell through a fixing rod, the second monitoring unit is a laser receiver, and the laser receiver is arranged opposite to the laser transmitter along a laser emission light path.
6. The mount of claim 5, wherein: a laser emission light path of the laser emitter is parallel to the bottom surface of the second shell, and the laser receiver is fixed on the inner wall of the second shell along the laser emission light path;
and the laser receiver and the bottom surface of the second shell form a preset included angle.
7. The mount of claim 5, wherein: laser emitter's laser emission light path with the bottom surface of second casing is perpendicular, laser receiver follows laser emission light path is fixed in on the bottom surface of second casing, laser receiver with the bottom surface size of second casing is the same.
8. A mount, as set forth in claim 1, wherein: the first monitoring unit is a laser transmitting and receiving all-in-one machine which is configured to enable the laser transmitting light path to be vertical to the bottom surface of the second shell;
the second monitoring unit is a laser reflector and is fixed on the bottom surface of the second shell along the laser emission light path; or
The first monitoring unit is a grating sliding rod, the second monitoring unit is a grating detection device, the grating detection device is provided with a detection hole, and when the grating sliding rod moves along the detection hole, the grating detection device acquires sensor data; or
The first monitoring unit is a magnetic conduction device, the second monitoring unit is an excitation coil, and the magnetic conduction device and the excitation coil move relatively; or
The first monitoring unit is a trigger device, and the second monitoring unit is a resistance strain device;
wherein the resistive strain device comprises:
the resistance strain bracket is fixed in the second shell;
the strain circuit is arranged in the resistance strain bracket;
the resistance strain gauge is arranged at the top of the resistance strain bracket and is electrically connected with the strain circuit; or
The first monitoring unit is a movable polar plate, the second monitoring unit is a fixed polar plate, and the fixed polar plate is fixed on the inner wall of the second shell and is arranged opposite to the movable polar plate.
9. A mount, as claimed in claim 1, wherein: the third monitoring unit has the same structure as the first monitoring unit, and the fourth monitoring unit has the same structure as the second monitoring unit.
CN202211149250.2A 2018-09-29 2018-09-29 Support base Pending CN115435941A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202211149250.2A CN115435941A (en) 2018-09-29 2018-09-29 Support base

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202211149250.2A CN115435941A (en) 2018-09-29 2018-09-29 Support base
CN201811146812.1A CN109029802A (en) 2018-09-29 2018-09-29 sensor and support

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CN201811146812.1A Division CN109029802A (en) 2018-09-29 2018-09-29 sensor and support

Publications (1)

Publication Number Publication Date
CN115435941A true CN115435941A (en) 2022-12-06

Family

ID=64614963

Family Applications (2)

Application Number Title Priority Date Filing Date
CN201811146812.1A Pending CN109029802A (en) 2018-09-29 2018-09-29 sensor and support
CN202211149250.2A Pending CN115435941A (en) 2018-09-29 2018-09-29 Support base

Family Applications Before (1)

Application Number Title Priority Date Filing Date
CN201811146812.1A Pending CN109029802A (en) 2018-09-29 2018-09-29 sensor and support

Country Status (1)

Country Link
CN (2) CN109029802A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114993522A (en) * 2022-07-22 2022-09-02 广西大学 Calibration method for intelligent bridge support

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2836069Y (en) * 2005-09-30 2006-11-08 陈昌铭 Digital torque controlled display tool
JP4964099B2 (en) * 2006-11-22 2012-06-27 公益財団法人鉄道総合技術研究所 Contact force measuring device for sliding plate
CN100561155C (en) * 2008-02-02 2009-11-18 北京交通大学 Temperature-insensitive optical fiber optical grating stress sensor
CN101819075B (en) * 2010-04-26 2012-07-25 清华大学 One-way support shearing force measuring device and method
CN201915329U (en) * 2010-12-29 2011-08-03 衡水宝力工程橡胶有限公司 Bridge support capable of monitoring horizontal stress state
CN102410888B (en) * 2011-06-29 2013-03-06 浙江华铁建筑安全科技股份有限公司 Steel support stress monitoring terminal
CN103776519B (en) * 2012-10-22 2016-08-03 梅特勒-托利多(常州)精密仪器有限公司 Weighing box
CN104280162B (en) * 2013-07-12 2016-12-28 纳米新能源(唐山)有限责任公司 Pressure transducer based on triboelectricity
CN103643628A (en) * 2013-11-16 2014-03-19 姬志刚 Bridge support with pressure monitoring function
CN103790105A (en) * 2014-01-23 2014-05-14 河海大学 Pot bearing and system for monitoring transverse overturn of bridge
CN204422112U (en) * 2015-01-30 2015-06-24 韩丙虎 A kind of strain transducer
CN104697710B (en) * 2015-02-12 2017-03-08 洛阳理工学院 A kind of pressure sensor calibrating device with graininess solid as medium
CN205825946U (en) * 2016-07-15 2016-12-21 长沙理工大学 Bridge rubber support deformation monitoring device
CN107059606A (en) * 2017-06-14 2017-08-18 中国铁路设计集团有限公司 A kind of bridge health monitoring bearing and its monitoring method

Also Published As

Publication number Publication date
CN109029802A (en) 2018-12-18

Similar Documents

Publication Publication Date Title
KR101136801B1 (en) Impact Test Device and Impact Test Method of Battery Cell
CN114252838B (en) MEMS vertical probe comprehensive test platform and test method
CN115435941A (en) Support base
CN109030772A (en) Self-powered side slope condition monitoring system and monitoring method
KR20160037494A (en) Concrete Pole Diagnostic Testing Apparatus
US20230213049A1 (en) Bolting device
CN110906877A (en) Bridge monitoring device and monitoring method
CN112968628A (en) Piezoelectric vibration energy collecting and converting device for railway vehicle
JP2015021846A (en) Load cell and method of manufacturing the same
JP2013171041A (en) Apparatus, system, and method for monitoring earthquake
CN106768295A (en) A kind of fiber grating microseismic sensors and preparation method
CN114777727A (en) Steel truss chord member three-dimensional deformation monitoring and early warning device and installation method thereof
CN104364623A (en) Electret-type vibration detection system, method for generating external vibration information, method for generating transfer function information relating to external vibration, program for generating external vibration information, and program for generating transfer function information relating to external vibration
KR101243645B1 (en) Airborne dust particles monitoring device and airborne dust particles detecting method using the same
CN103456528B (en) Electronic switching device and the method for the manufacture of electronic switching device
CN108152556B (en) Passive excitation self-powered wireless non-contact current sensing measurement device and measurement method
CN104251921A (en) Sensing test clamp
CN213402851U (en) Miniature power generation device utilizing impact vibration
CN102288261B (en) Floating pontoon type fiber liquid level meter
CN103017890A (en) Introduced capacitive device for measuring horizontal ground micro-vibration
CN109596299B (en) Vertical and horizontal dual-purpose vibrating table
KR101553911B1 (en) Energy harvester
CN113419106A (en) Vertical compression power generation module test system
KR101339735B1 (en) Burying type sensor node for detecting dynamiccharateristic of structure
CN114323996B (en) Micro sample bending fatigue test device and method based on acoustic radiation force

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination