• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A bolt (100) which deforms when subjected to stress comprises a cavity (104), intelligence and means (105) for determining elongation and alarm at specific values.
    公开号:SE1630260A1
    申请号:SE1630260
    申请日:2015-04-02
    公开日:2016-10-26
    发明作者:Widin Klasén Lena
    申请人:Strain Labs Ab；
    IPC主号:
    专利说明:

    [1] The invention relates to the measurement of elongation in mechanical components, such as fasteners, e.g. bolts.
    [2] It is earlier edge, e.g. in US 4553124, to install wire strain gauges in bolts for jugging of strain. However, these known donors are complicated and therefore expensive. Another disadvantage is that they are temperature dependent.
    [3] JP-A-lll83280 describes a fastening and tightening method for bolts, during which the elongation of the bolt is measured when tightening the bolt. The fastening or tightening operation ends when the extension reaches a predetermined value. The method used to measure the elongation includes a step of controlling a laser. In this known method, the extension of the bolt is monitored when the bolt is fastened / tightened, but after tightening, no further information about extension is available.
    [4] Additional background is described in US2010 / 0050778 and US2007 / 0204699 SUMMARY
    [5] An object of the invention is to increase safety and to provide a new type of elongation measuring equipment which has communication means and which allows intelligent analysis, which is better than in the prior art and which eliminates or at least reduces the disadvantages discussed above.
    [6] This object has now been achieved with the technique defined in the following, independent claims, wherein preferred embodiments appear from the dependent claims.
    [7] According to a first aspect of the invention there is provided a mechanical component which has a portion which is deformed, i.e., elongated, when subjected to elongation. The party has encavity. The component further has an optical unit, which is arranged to send light into the cavity. The optical unit is also arranged to detect reflected light. The component further has a control unit which is connected to the optical unit. The control unit is arranged to determine the characteristics of the signal response provided by the emitted light traveling from the optical unit into the cavity, reflected and traveled back to the optical drive. Furthermore, the control unit is arranged to determine the physical deformation of the portion of the mechanical component on the basis of the properties of the signal response in order to determine the strain data. The component further has a single communication unit, which is connected to the control unit and arranged to communicate strain data for the mechanical component to an external device. It is advantageous to determine the physical deformation of the mechanical component since it can be used to determine the elongation of the component. It is also advantageous for the component to have a communication device, which enables the component to send and receive data, e.g. elongation data.
    [8] The control unit can be arranged to determine physical deformation by means of the time-of-ightight method or interferometry. It is advantageous to determine monophysical deformation of the mechanical component as it can be used to determine the elongation at the component.
    [9] The optical unit may have a light emitter and a light detector for the purpose of being able to both emit and receive light. It may also include reactors, beam splitters and / or other optical components. Furthermore, the control unit can be a microcontroller circuit, which can be arranged to control the light transmitter in addition to other components. It is an advantage to have a single control unit in order to be able to control the other components present in the mechanical component.
    [10] Preferably, the optical unit has a laser. It is advantageous to use a single laser as an optical device because it emits coherent light. It is possible to illuminate the bottom of the cavity without illuminating the walls, which would otherwise result in an incorrect calculation of elongation data.
    [11] The mechanical component may comprise a charging unit arranged to collect energy from the environment. The mechanical component may also comprise an energy storage unit arranged to store energy collected by the charging unit and the pre-control unit and the communication unit with energy. The energy storage unit may comprise an accumulator, preferably a rechargeable battery. That mechanical component is probably mounted in a remote location and inaccessibly placed. It is therefore preferred that the component can extract and store energy in order to be able to supply both the control unit and the communication unit and not be dependent on a certain battery life.
    [12] In another embodiment, the component has a memory unit arranged to be stored.ex. preset fabrication data, determined elongation data and / or processed elongation data or elongation data. This allows different data to be stored and wait for further communication or for future purposes.
    [13] In one embodiment, the communication unit is wireless. This is advantageous when the mechanical component is located at a remote location, as no technician needs to travel to the mounting site to collect stored data from that mechanical component. In another embodiment, the mechanical component may utilize a fixed link. This is preferable when the mechanical component is located in a location where such infrastructure exists.
    [14] In one embodiment, the mechanical component has a support sensor unit. This unit can provide the control unit with additional input data to be used when determining the elongation of the component. The support sensors may be more than one and the type of sensors may be a combination of suitable sensors for each particular field of application of the mechanical component.
    [15] An example of a support sensor is a temperature sensor, which is advantageous if the mechanical component is placed in an environment with high or low temperatures which can affect the elongation determination.
    [16] Another example of a support sensor is a positioning device, which is advantageous if the mechanical component is installed in a vehicle. It is then possible to determine where the component is located and as an example at which of the vehicle's planned stops the component needs to be tightened.
    [17] A further example of a support sensor is a moisture sensor which is advantageous if the mechanical component is placed in an environment of high or low humidity, which may affect the elongation determination or cause corrosion.
    [18] In a preferred embodiment, the mechanical component is included in a network, which also comprises central software arranged to monitor the strain data of all components included in the network. The central software is also arranged to automatically report normal function, malfunction and deviations. The mechanical component is arranged to communicate with other corresponding components included in the network. It is advantageous to have a network of components for the purpose of sharing or sending information between or to components.
    [19] The mechanical component may be a fastening element, such as a bolt, a screw or a rivet, arranged to clamp or clamp two parts. With the features previously described and described below, it is possible to estimate whether a fastener has come loose and needs to be tightened, and if so, when it becomes critical to take this action. It is also possible to avoid defects in joints due to fatigue, separation of clamped parts or movement between them.
    [20] In a preferred embodiment, the cavity of the mechanical component is elongate drilling. An elongated borehole is advantageous because it allows a light pulse train to travel a certain distance before it is reflected at the bottom of the borehole and starts the journey back. A longer drilling provides better measurement accuracy and calculations.
    [21] In one embodiment, the cavity comprises an optical fiber. An advantage of this construction is that the fiber acts as a fuse. If for some reason the component is extended more than the optical fiber can be stretched, the fiber will break and it will be impossible to perform a measurement, whereby the component may report that a fault has occurred. Furthermore, it is possible to program the sensor to warn if the component is overloaded even if fiber is not broken.
    [22] According to a second aspect of the invention, there is provided a method of feeding elongation into a mechanical component having a cavity. This method comprises the steps of emitting a light pulse train from an optical unit into the cavity, detecting a reflected light pulse train by the optical unit, determining the properties of the signal responses arising from the emitted light passing from the optical unit into the cavity, summer fl passed and passed back to the optical unit, determining the physical deformation of the mechanical component based on the determined properties of the signal response in order to determine the strain data, and communicating the determined strain data to an extreme device.
    [23] In one embodiment, the physical deformation is determined by the maturity method or interferometry.
    [24] In one embodiment, strain data is sent to a portable device. This is advantageous when the mechanical component is accessible and when an operator on site is preferred for any reason. This is also preferable during assembly.
    [25] In one, a wireless communication system is sent. This method of communication is preferred when the component other embodiment of strain data via is inaccessibly located or when an on-site operator is not preferred.
    [26] In yet another embodiment, strain data is sent to a network of mechanical components. This is advantageous when the components are located inaccessible and there is no possibility of wireless communication with an external device and when it is convenient to send data from several components as a packet.
    [27] According to a third aspect of the invention, there is provided a system comprising a number of mechanical components as described above. The system also has central software and infrastructure that is arranged to monitor strain data from all mechanical components in the system and also report normal function, errors and deviations.
    [28] In one embodiment, the information can be read from / written to the mechanical components of the system. About t.eX. preset data turns out to be incorrect, new and correct data can then be uploaded to all components in the system.
    [29] According to a fourth aspect of the invention, there is provided a structural element, such as a pl plane plane wing, which has a number of mechanical components as described above. The components of the structural element may be connected in a network. An advantage of having components in a construction element is that the entire element can be manufactured with the components and delivered in the stable to deliver the construction in parts for assembly on site.
    [30] According to one aspect, an arrangement is provided which comprises a mechanical component which deforms when subjected to elongation. The component has a cavity. The system further has an optical unit arranged to emit light in the cavity and a detected light. It further has a control unit connected to the optical unit and arranged to determine the characteristics of the signal responses arising from the emitted light which has passed from the optical unit into the cavity, which has been reflected and which has returned to the optical unit. The control unit is further arranged to determine the physical deformation of the mechanical component on the basis of the determined properties of the signal response in order to determine the strain data deriving from the physical deformation. The system further has a communication unit connected to the control unit and arranged to communicate strain data for the mechanical component to an external device.
    [31] Embodiments of the invention will be described below; References are made to the accompanying schematic drawings, which illustrate non-limiting examples of how the inventive concept can be condensed into practical applications. Own. 1 is a section of a bolt according to an embodiment
    [33] Eig. 2 shows a number of bolts on an eye plane wing according to an embodiment of the invention.
    [34] Eig. 3 shows a number of bolts on an eye plane wing according to another embodiment of the invention.
    [35] Eig. 4 shows a fate diagram of an elongation determination process utilizing the maturity method.
    [36] Pig. 5 shows a fate diagram of an elongation determination process utilizing interferometry. Pig. 6 shows a bolt according to an alternative embodiment.
    [38] Pig. 7 is a graph of measured elongation data.
    [39] Specific embodiments will now be described in more detail below with reference to the accompanying drawings. However, the invention may be practiced in many different ways and should not be construed as limited by the embodiments described below. These embodiments should rather be seen as examples which make the description more credible and complete and will fully convey the scope of the invention to those skilled in the art.
    [40] Referring to Figs. l shows a mechanical component or arrangement in the form of an intelligent bolt schematically and in section. The bolt 1 has a shaft 2 and a head 3 with an elongate bore or cavity 4 extending from the head 3 into the shaft 2. The bore 4 is preferably made as long and narrow as possible while maintaining the strength of the bolt 1. Drilling 4 ends with a bottom. Preferably, the cross section of the borehole is cylindrical. The diameter of the bore 4 is preferably as small as possible within e.g. range 0.1 μm to 1 cm.
    [41] The bolt 1 has an upper portion 5 which receives a control unit 6, a memory unit 7, a single charge unit 8. An energy storage unit 9, a communication unit 10, a single support sensor unit 1 and an optical unit 12. In another embodiment, the components 6-12 may just as well be mounted inside the head 3 of the bolt 1 or may in any other way be connected to the bolt 1. The bolt 1 may also comprise another group of components depending on what the bolt is to be used for. The upper part 5 will hereinafter be called an electronics package.
    [42] The control unit 6 controls the optical unit 12, the memory unit 7, the communication unit 10 and the support sensor unit 11. It can be realized by using suitable controller technology, such as but not limited to a microcontroller, a CPU, a microchip or the like. The control unit 6 is implemented with the aid of RFID technology and is preferably small in size, e.g. 2x3 mm.
    [43] The optical unit 12 is arranged to send out a light pulse train in the bore 4 of the bolt. It is preferably a light emitting unit and more particularly a laser, but a diode or other suitable light source can be used. The optical unit 12 also has a light detector arranged to detect reflected light.
    [44] The charging unit 8 comprises an energy absorbing element having any suitable components for absorbing energy from the environment, e.g. but not limited to, from external stress on the bolt, solar energy, thermal energy, wind energy, salinity gradients or kinetic energy. The charging unit 8 is arranged to supply the energy storage unit 9 with energy.
    [45] Other energy recording options are charging with a photosensor, which converts sunlight into energy, or recording vibrational energy.
    [46] Another possibility is charge by induction. A galvanically separated charging coil (not shown) is placed on top of the bolt 1 head, in which the electronics package is arranged. The coil transmits induction to energy through the energy storage unit.
    [47] The energy storage unit 9 has a battery (not shown) for energy storage. The bolt 1 can also be connected to the mains or can use any combination thereof.
    [48] The communication unit 10 operates via a wireless connection, a wire interface or a combination thereof. The wireless connection can use any wireless transmission technology, e.g. WLAN, Bluetooth®, radio, audio, electromagnetic induction. The communication unit 10 is preferably implemented with Bluetooth® technology and is arranged to send specific strain data to, for example, a handheld device 14 or central software 13 which is part of a network.
    [49] The memory unit 7 is implemented by means of memory technology, such as but not limited to ROM, RAM, SRAM, DRAM, CMOS, FLASH, DDR, SDRAM or the like. This unit 7 is arranged to store determined elongation data and or preset manufacturing data.
    [50] The support sensor unit ll can e.g. be a temperature or humidity sensor, a positioning device or other sensor that can provide the measurements with relevant input data. The unit 11 may comprise a number of sensors / devices for measuring various variables, such as humidity and temperature.
    [51] In most embodiments, the bolt 1 is programmed to log and report the elongation is sufficient to maintain the specific tension of the bolt 1. This can e.g. caused by a green light visible on the bolt itself (not shown). In the förest embodiments, factory settings of the preferred elongation limits are stored in the memory unit 7. The factory settings may include but are not limited to manufacturer name, serial number, unique bolt ID, date and time of series, elongation window, name of fitter, torque used, elongation temperature, ambient temperature installation date, deviation over time in a database and / or maintenance alarm.
    [52] In one embodiment, the bolt 1 must be calibrated. If the bolt 1 is to be placed in a place with difficult weather conditions, e.g. with low / high temperatures, it is preferable to take this into account when determining elongation data. The calibration can be a single-process calibration, which is performed at the factory and / or an on-site calibration. The factory calibration can e.g. take into account what materials the bolt will tighten as well as the manufacturing series.
    [53] One embodiment is focused on basic strain detection. It is possible to use t.eX. a hand-held device 14 for recovering strain data from the bolt 1 for the purpose of determining whether the strain is within the preset limit values. This is done via the control unit 6, which receives the strain value from the memory unit 7 and sends strain data to the handheld device 14 via the communication unit 10. The bolt 1 is based on a self-charging system, an eXtem communication device being used to inquire about the status of the bolt. In this embodiment, the bolt 1 is preferably equipped with a control unit 6, a communication unit 10, an energy storage unit 9 and a charging unit 8. The external communication device may be a hand-held device 14. The bolt 1 checks whether the elongation is within the groove and if so indicates correct tightening .
    [54] In another embodiment, the bolt 1 is part of an automatic system. In addition to the charging unit 8, the bolt according to this embodiment has a wireless communication unit 10. The bolt 1 operates on the principle that it is in a rest position for a certain, adjustable period of time, which may depend on the battery level, wakes up, determines the elongation status, communicates a certain elongation status and falls back to the rest state. It is also possible to communicate with the bolt 1 via a single communication device, which may be a hand-held communication device. After mounting and indicating correct elongation, it is possible to load data, e.g. manufacturing limit values, via the communication device and charge to the bolt memory unit 7. When this is done, an indication that the information received and stored can be obtained. The strain indicator can be downloaded manually from the bolt 1 by means of the communication device. It can also be performed automatically by the bolt checking whether the elongation is within the limits, indicating the correct tightening and sending information if necessary, e.g. determined elongation data.
    [55] In yet another embodiment, the bolt 1 has knowledge of strain through storage of strain data in the memory unit 7 together with manufacturing data and it can remember deviation which is also stored in the memory unit 7. An alarm signal can be sent when the strain falls below / exceeds a threshold value. Bolt l is part of a network or system of bolts. The bolts l included in the system monitor elongation with a frequency interval of between once per second to once a year and can automatically report normal function, deviations and malfunction as well as determine the time to a potential maintenance. The system further comprises central software and infrastructure 13. After mounting and indicating correct elongation, it is possible to address the bolt 1 from a computer. It is also possible to write / read information to / from the bolt l. From the central software it is possible to administer the bolts l and get an overview of the status of all the bolts that are connected in the system. The bolt 1 determines if the strain is within the limit range, indicates correct tightening or deviation / malfunction, sends information when needed or at regular time intervals and is part of an intelligent system with log and memory. 11
    [56] Elongation data measured from the elongation of the bolt 1 can be communicated in any combination of the above-mentioned communication methods. For example. strain data can be retrieved from the bolt 1 with a handheld device 14 during assembly and during operation, data can be sent between different components to a final bolt 1, which either forwards data via wireless communication or stores data until an operator retrieves it with a handheld device 14.
    [57] In the embodiment of Fig. 1, an optional optical fiber is inserted into the bore 4 of the bolt 1 to conduct the light from the optical unit 12. The principal measuring method in this embodiment is to send a light pulse train down the bore of the bolt 1, through the optical fiber 20. The pulse train will pass through the fiber 20 arranged in the bore 4, reflect a bottom wall of the bore and return through the fiber 20 to the detector in the optical unit 12 . The control unit 6 determines the time it took and determines the elongation data of the mating time method. In addition, the optical fiber 20 can act as a fuse or security check. The fiber 20 is very brittle when subjected to longitudinal strain. Thus, when the bolt 1 is subjected to an excessive strain, the optical fiber 20 will come off and thus the strain measurement will no longer work. This will be an indication that something has gone wrong.
    [58] In the embodiments in Fig. 1, the control unit 6 determines the signal response characteristics pre-bolt 1 in order to determine a physical deformation, e.g. extension, using the expiration method. This method is based on the principle of measuring the time it takes for a light pulse train, which includes a single light pulse, to go from the optical unit 12 to the bottom of the cavity 4, where it is reflected and back to the optical unit. The maturity method can be used both with and without an optical fiber in the cavity.
    [59] In another embodiment, the control unit 6 determines the signal response characteristics pre-bolt 1 in order to determine a physical deformation, e.g. extension, by means of optical communication in free space, FSO. FSO is a technique which means that the cavity 4 is used in the same manner as previously described with the optical fiber 20 but without fiber.
    [60] In yet another embodiment, the control unit 6 determines the signal response characteristics of the bolt 1 in order to determine a physical deformation, e.g. extension. Using interferometry, preferably optical interferometry. 12 Interferometry is a measurement method in which waves are superimposed in order to retrieve information about the waves.
    [61] The physical deformation, e.g. elongation, in the above embodiments the elongation is longitudinal but it can also be other physical deformations, such as torsion or rupture caused by an external force. The measurement methods above can also be used mooring control, ie. the method is used to detect deviations or malfunctions, such as e.g. torque, disturbances or incorrect results.
    [62] Referring to Fig. 2, it is shown that system 14 of intelligent bolts 1 mounted on a structural element, in this case a plane plane wing W. The system further has central software and infrastructure 13. The bolts 1 in system 14 monitor elongation with a frequency range of e.g. between once per second and once a year using any of the measurement methods above. The bolts 1 communicate with each other, one bolt 1 receiving data from all other bolts. The bolt 1 which receives data from all other bolts 1 sends the collected information from all the bolts 1 in the system to the central software. This particular method is advantageous when no wireless network connection is available. An example may be bolts 1 installed along a railway tunnel, one bolt communicating with the next and so on. for example. via Bluetooth® until the data reaches a bolt outside the tunnel, which can then use a wireless network communication to transmit all data to the central software 13.
    [63] Fig. 3 shows a similar construction as in Fig. 2 with a system 14 de-intelligent bolts 1 attached to a plane plane wing W. The system 14 further has central software and infrastructure 13. The bolts 1 in the system 14 monitor elongation frequently but this embodiment communicates each intelligent bolt 1 directly with the central software 13.
    [64] Fig. 4 shows a fate diagram, in which a method 400 for measurement according to the maturity method is described with reference to a bolt 1 of the type described above.
    [65] In the first set 401, the control unit 6 controls the light emitter to emit a light pulse train inside the cavity 4 in the mechanical component 1 and at the same time the control unit 6 starts a time measurement by starting a clock at the time T1. The emitted light pulse train 13 passes through the cavity 4 and in step 402 reaches the bottom, where it is reflected. From there, the starter light pulse train makes its way back through the cavity 4 in the direction of the detector. In step 403, the reflected light pulse train is detected by the detector and the time measurement ends at time T2.
    [66] In step 404, the control unit 6 analyzes the signal response characteristics of the pulse train, i.e. signal strength, amplitude and pulse shape. Step 409 describes the case when no pulse train is detected within a certain time or if the detected signal is disturbed in any way. The control unit then controls an error message. This can be done via the communication unit l0or t.eX. with a visual organ, e.g. with a diode (not shown) that changes color from green to red. On the other hand, if the detected pulse is OK, as described in step 405, the controller 6 determines the time it took for the pulse to go from the upper part of the cavity 4, the bottom and back to the upper part again as T2-T1. It uses this time and the maturity method to determine physical deformation, in this case strain or elongation, of the bolt.
    [67] In step 406, the controller 6 compares determined elongation data, or elongation, with a reference value. If the strain data is within a preset, accepted range, the controller can either control the communication unit l0 to send the determined value to the eXtem unit l3, l4, t.eX. a computer, and / or activating a green diode, step 407, or also storing said determined strain data in the memory unit 7, step 408. In some embodiments, it may perform both step 407 and step 408.
    [68] In step 41, determined elongation data is not within the preset, accepted range and the controller sends some form of alarm regarding insufficient elongation. Dettakan t.eX. caused by an error message to an eXtem device 13, 14, such as a computer, or by lighting a red diode. The control unit 6 can also, step 41 l, store determination elongation data in the memory unit 7. In certain embodiments it can perform both steps 41 and 41.
    [69] Fig. 5 shows a flow chart in which a method 500 for measurement according to the interferometry method is described with reference to a bolt 1 of the type described above. 14
    [70] The first step 501 is that the control unit controls the light transmitter to emit a light pulse train in the cavity 4 of the mechanical component 1 and that at the same time the control unit initiates one-time measurement by starting a clock at time T1. The emitted light pulse train passes through the cavity 4 and in step 502 reaches the bottom, where it is reflected. From there, the starter light pulse train makes its way back through the cavity 4 in the direction of the detector. In step 503, the reflected light pulse train is detected by the detector and the time measurement ends at time T2.
    [71] In step 504, the control unit 6 analyzes the signal response characteristics of the pulse, i.e. e.g., interference pattern, signal strength, amplitude and pulse shape. Step 509 describes the case when the reflected pulse train is detected within a certain period of time or if that detected signal is disturbed in some way. The control unit 6 then controls an error message. This may be via the communication unit 10 or t.eX. with a visible organ, e.g. a diode (not shown), which changes color from green to red. On the other hand, if the detected pulse is OK, as described in step 505, the controller 6 analyzes the interference pattern. It then uses interferometry to determine physical deformation, in this case elongation or elongation, of the bolt.
    [72] In step 506, the controller compares determined strain data with a reference value. Stretch data is within a preset, accepted range, the controller 6 can either control the communication unit 10 to send the determined value to an external unit 13,14, such as a computer, and / or it can light a green diode, step 507, or it can also store determined strain data in the memory unit 7, step 508. In some embodiments, it may perform both step 507 and step 508.
    [73] In step 510, determined elongation data is not within the preset, accepted range and the controller 6 controls any type of alarm regarding insufficient elongation. This can be done, for example, with an error message to an eXtem unit 13, 14, such as a computer, or by lighting a red diode. The control unit 6 can also, step 511, store determination elongation data in the memory unit 7. In certain embodiments it can perform both step 510 and step 511.
    [74] Fig. 6 shows a subsurface application of the bolt 100 developed underwater use. This bolt 100 has a head 103 and a shaft 102 with an elongate cavity 104 extending from the head 103 into the shaft 102. The bolt 100 is provided with an electronics package 105, which contains basically the same components as the previously described bolt 1 and which has the same features such as this bolt but it is further equipped with a hood or cover 101 on the head of the bolt 100. Inside the hood 101 there is a receiver 107 for receiving radio signals. The signals may come from a Bluetooth® transmitter, possibly a low energy type Bluetooth® transmitter (not shown), or any other suitable transmitter provided with the electronics package 105. The hood 101 is provided with a coil 108 for contactless, inductive energy transfer to the electronics package 105. The bolt 101 is provided with a conduit 106 connected to another bolt or directly to an extreme data collection device.
    [75] The electronics package 105 and the hood 101 thus have no direct contact with each other, no galvanic contact but communication and energy transfer between the two boats is still possible. The electronics unit 105 is sealed inside the head 103 of the bolt 100 and is thus protected from external elements. The bolt 100 is therefore adapted for pre-use deep underwater; and manages fl your thousand meters below the surface. This is very useful in e.g. offshore industry.
    [76] An example of a graphical presentation of measured values is shown in Fig. 7. When a controller or inspector uses a handheld device for checking strain data from a bolt, he can have this graphical presentation on the display. In another embodiment, it can be displayed on a display of an external device, either when a measured value is requested or at regular intervals.
    [77] The diagram shows bias on the y-axis and time on the x-axis. In a real case, the rabbit units on the shoulders are customized for the case in question. Both bias and time can be expressed with suitable respective units. The diagram includes three fields, which represent high, low and accepted bias. All measured values, which are represented by pollutants, are desired to fall within the accepted range. If a value appears in the low range, the bolt may be loose. If a value ends up in the high range, the bolt may be damaged due to too much bias and in the worst case went off in two parts.
    [78] When a measurement is made, i.e. the controller reads the elongation value from a bolt, a mark is shown in the diagram, here in the form of a stem. The next time a value for the same 16 bolt is measured, a new mark is shown in the diagram. The example diagram in the figure thus shows six measured values for a specific bolt. The first four cairns as well as the last are ok; they lie well within the accepted range. However, the fourth value is on the verge of being too low and the fifth value is definitely too low. This is a pre-controller help tool; he can see how the preload changes over time and also predict when the bolt needs will be tightened. Collected bias data can also be processed by the external device and the time when the bias voltage will be close to the low range can be calculated and predicted, e.g. by eXtrapolation of the measured values. To further assist the inspector, values outside the accepted range may be color-coded, e.g. markings in red if the value is too low.
    [79] It will be appreciated that the concept of the invention is not limited to the embodiments described above and many modifications are reasonable within the scope of the invention as defined in the appended claims. As understood from the description, the system according to the invention is not only applicable to fasteners but also to other mechanical components, such as threaded fasteners, e.g. screws, bolts, studs, specially shaped male threaded fasteners or threaded rods. The technique for determining the elongation of a mechanical component as described above is applicable to many different areas requiring high safety, e.g. in the oil, nuclear power, wind power, g yg, automotive, process or mining industries but also in areas such as measurement technology and vibration measurements.
    权利要求:
    Claims (27)
    [1]
    A mechanical component having a portion which deforms when subjected to strain and having a cavity (4; 104), the component further having an optical unit (12) arranged to emit light into the cavity (4) and detect reflected light; a control unit (6) connected to the optical unit (12) and arranged to determine the characteristics of the signal response provided by the emitted light which passes from the optical unit (12) into the cavity (4; 104), is reflected and returns to the the optical unit (12), the control unit (6) further being arranged to determine physical deformation of the portion of the mechanical component (1; 100) on the basis of the properties of the signal response and determination elongation data from the physical deformation; and a communication unit (10) connected to the control unit (6) and arranged to send strain data for the mechanical component (1; 100) to an external device (13; 14).
    [2]
    Mechanical component according to claim 1, wherein the control unit (6) is arranged to determine physical deformation by means of the maturity method or interferometry.
    [3]
    A mechanical component according to claim 1 or 2, wherein the optical unit (12) has a single light transmitter and a light detector; and wherein the control unit (6) has a microcontroller arranged to control the light transmitter.
    [4]
    A mechanical component according to any one of the preceding claims, wherein the optical unit (12) is a laser.
    [5]
    A mechanical component according to any one of the preceding claims, further comprising a charging unit (8) arranged to collect energy from the environment.
    [6]
    A mechanical component according to claim 5, further comprising an energy storage unit (9) arranged to store energy absorbed by the charging unit (8) and supply energy to the control unit (6) and the communication unit (10).
    [7]
    Mechanical component according to claim 6, wherein the energy storage unit (9) comprises an accumulator, preferably a battery. 18
    [8]
    A mechanical component according to any one of the preceding claims, further comprising a memory unit (7) arranged to store preset manufacturing data and said strain data.
    [9]
    A mechanical component according to any one of the preceding claims, wherein the communication unit (10) is wireless.
    [10]
    A mechanical component according to any one of the preceding claims, further comprising a support sensor unit (1 1).
    [11]
    A mechanical component according to claim 10, wherein the support sensor unit (11) comprises a temperature sensor.
    [12]
    A mechanical component according to claim 10, wherein the support sensor unit (11) comprises a positioning device.
    [13]
    A mechanical component according to claim 10, wherein the support sensor unit (11) comprises a moisture sensor.
    [14]
    A mechanical component according to any one of the preceding claims, wherein the component (1; 100) is part of a network which also has central software (13) arranged to monitor said strain data for all components (1; 100) included in the network (15) and automatically report normal function, malfunction or deviations.
    [15]
    A mechanical component according to claim 14, wherein the component (1; 100) is arranged to communicate with corresponding components (1; 100) included in the network.
    [16]
    A mechanical component according to any one of the preceding claims, wherein the component (1; 100) is a fastening element, such as a bolt, a screw or a rivet arranged to clamp parts together.
    [17]
    A mechanical component according to any one of the preceding claims, wherein the cavity is an elongate bore (4; 104) in the component (1; 100).
    [18]
    A mechanical component according to any one of the preceding claims, wherein the cavity (4; 104) contains an optical fiber (20). 19
    [19]
    A method of measuring elongation in a mechanical component (1; 100) having a cavity (4: 104); comprising the steps of: riveting a light coil train from an optical unit (12) into a cavity (4; 104); detecting a reflected light coil train with the optical unit (12); determining the properties of the signal response produced by the emitted light from the optical unit (12), which enters the cavity (4; 104), is reflected and returns to the optical unit (12), and determining the physical defornation in the mechanical component ( 1; 100) based on the properties of the determined signal response, for determining strain data based on the physical deformation; and sending strain data to an external device (13,14).
    [20]
    A method according to claim 19, wherein the physical deformation is determined by the open time method or interferometry.
    [21]
    A method according to claim 19 or 20, wherein said strain data is sent to a hand-held communication device (14).
    [22]
    A method according to any one of claims 19-21, wherein said strain data is transmitted via a wireless communication system.
    [23]
    A method according to any one of claims 19-22, wherein said elongation data is transmitted in a network of mechanical components.
    [24]
    A system comprising: a plurality of mechanical components (1; 100) according to any one of claims 1-18; and centers1 software and infrastructure (13) arranged to monitor strain data for all components included in the system and automatically report normal function, malfunction or deviations.
    [25]
    A system according to claim 24, wherein information is read from / written to the mechanical components (1; 100).
    [26]
    A structural element, such as a bearing swing (W), having a plurality of mechanical components (1; 100) according to any one of claims 1-18.
    [27]
    A construction element according to claim 26, wherein the mechanical components (1; 100) are connected in a network.
    类似技术:
    公开号 | 公开日 | 专利标题
    SE1630260A1|2016-10-26|Intelligent bult och system för denna
    US8596134B2|2013-12-03|Bolt tension monitoring system
    JP4248567B2|2009-04-02|Valve device monitoring system
    CN109563866B|2020-10-30|Intelligent bolt and using method thereof
    RU2013150507A|2015-05-20|SENSOR SYSTEM FOR TORQUE MEASUREMENT AND SHAFT WITH SENSOR SYSTEM FOR TORQUE MEASUREMENT
    JP4264891B2|2009-05-20|Structure condition inspection system
    CA2890884C|2018-07-17|System and method for evaluating remaining life of an operative sub-system of a vehicle
    US20130132032A1|2013-05-23|System, device and associated methods for monitoring a physical condition or operating performance of a structure
    WO2016078595A1|2016-05-26|Solar battery wireless integrated load cell and inclinometer
    CN104516302A|2015-04-15|Tool and method for monitoring state of tool
    US10302510B2|2019-05-28|Wireless axial load cell and sensor assembly
    JP6556474B2|2019-08-07|Fastening unit, fastening structure and inspection method
    JP2012197938A|2012-10-18|Valve device monitoring system
    RU172963U1|2017-08-02|Automatic device for controlling displacements of the near-edge rock mass of mine workings
    JP5210532B2|2013-06-12|Simple rope abnormality detection device
    CN205719090U|2016-11-23|Pitshaft monitoring and warning system
    US20200173423A1|2020-06-04|Lightning detection and measurement system and method for location detection of lightning strikes on a wind turbine blade
    JP2015045329A|2015-03-12|Method and system for monitoring load and stress of floating body facility
    CN207194883U|2018-04-06|Drilling rod Parameters Instrument
    CN103322958A|2013-09-25|Length sensor and detecting method thereof
    KR20210030520A|2021-03-18|a structure for measuring the axial force of bolts
    JP2009063171A|2009-03-26|Monitoring system of valve apparatus
    CN102809631A|2012-12-05|Truss structure damage diagnosis method
    CN105738407A|2016-07-06|Thermal expansion coefficient detection method and device for anchor cup
    CN210265612U|2020-04-07|Temperature early warning system and power assembly of heavy truck AMT transmission clutch
    同族专利:
    公开号 | 公开日
    WO2015150544A2|2015-10-08|
    CN105960582A|2016-09-21|
    CN105960582B|2019-04-26|
    US10066930B2|2018-09-04|
    SE541238C2|2019-05-14|
    WO2015150544A3|2016-02-04|
    US20170167857A1|2017-06-15|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US4553124A|1983-09-16|1985-11-12|Carron & Company|Strain gauge transducer assembly|
    DE59804600D1|1997-02-12|2002-08-01|Thomas Loeffler|METHOD AND DEVICE FOR PRODUCING SCREW CONNECTIONS|
    US5945665A|1997-05-09|1999-08-31|Cidra Corporation|Bolt, stud or fastener having an embedded fiber optic Bragg Grating sensor for sensing tensioning strain|
    JP3407069B2|1997-12-25|2003-05-19|株式会社サンノハシ|Bolt fastening device and fastening method|
    DE19819301C1|1998-04-30|1999-12-30|Thomas Loeffler|Method and device for checking the preload force of screw connections|
    CN1950617A|2004-03-16|2007-04-18|远程接合技术公司|Fastener networks|
    JP2007178232A|2005-12-27|2007-07-12|Honda Motor Co Ltd|Method for measuring shearing load of fastening implement|
    US20070204699A1|2006-03-02|2007-09-06|General Electric Company|Remote strain measurement|
    FR2916838B1|2007-05-29|2009-08-14|Schneider Electric Ind Sas|INTEGRATED DEVICE FOR MONITORING THE DEFORMATIONS OF AN ELECTRICALLY INSULATING WORKPIECE AND METHOD OF MANUFACTURING SUCH A DEVICE.|
    US8683869B2|2008-09-04|2014-04-01|The Boeing Company|Monitoring fastener preload|
    US8433160B2|2009-01-30|2013-04-30|Cleveland Electric Laboratories|Smart fastener and smart insert for a fastener using fiber Bragg gratings to measure strain and temperature|
    US8810370B2|2010-01-22|2014-08-19|The Boeing Company|Wireless collection of fastener data|
    US8596134B2|2011-09-21|2013-12-03|King Fahd University Of Petroleum And Minerals|Bolt tension monitoring system|
    AU2011235942B2|2011-10-11|2015-01-22|Nicholas Charles Dooner|Safetytrim nut locking device|
    WO2013117954A1|2012-02-09|2013-08-15|Osmos Sa|A monitoring device, system and method for the monitoring of an area of building or land, using at least one light waveguide|SE540526C2|2016-08-08|2018-09-25|Strain Labs Ab|An intelligent bolt, a method of using an intelligent bolt and a sensor arrangement for the intelligent bolt|
    EP3290721A1|2016-08-30|2018-03-07|HILTI Aktiengesellschaft|Distance sensor on anchor tip|
    EP3366931B1|2017-02-22|2021-06-16|SFS Intec Holding AG|Sleeve comprising a sensor arrangement with rfid|
    CN108303240B|2017-12-20|2019-11-15|华东交通大学|A kind of bolt looseness detection of rail joint union piece and warning device|
    CN110388951B|2018-04-20|2021-05-25|中车株洲电力机车研究所有限公司|Device and method for monitoring bolt looseness of wind generating set|
    KR102177113B1|2018-10-31|2020-11-11|한국철도기술연구원|Apparatus for measuring the axial force of bolt and method for measuring the axial force of bolt using the same|
    CN109632006A|2019-01-11|2019-04-16|重庆大学|A kind of intelligent wireless bolt and on-line monitoring system|
    CN110487470A|2019-08-29|2019-11-22|江铃控股有限公司|On-vehicle safety monitoring method and system based on bolt torque monitoring|
    CN110987254A|2019-11-25|2020-04-10|北京宇航系统工程研究所|Bolt load wireless monitoring system and monitoring method|
    CN113008149A|2019-12-20|2021-06-22|奥动新能源汽车科技有限公司|Looseness monitoring device and system for bolt or nut|
    CN113008150A|2019-12-20|2021-06-22|奥动新能源汽车科技有限公司|Looseness monitoring device and system for bolt or nut|
    DE102020210859A1|2020-08-27|2022-03-03|Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung eingetragener Verein|screw|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    SE1450415|2014-04-04|
    PCT/EP2015/057369|WO2015150544A2|2014-04-04|2015-04-02|Intelligent bolt and system therefor|
    [返回顶部]