Structure to absorb, dissipate and measure a force

Abstract

A structure to absorb, dissipate and measure a force includes a plurality of distinct layers. The layers include a first impact absorbing material having an outer face facing the direction of expected impact and an opposite inner face, an impact dissipating layer adjacent to the inner face of the first impact absorbing material and having a higher flexural rigidity than the first impact absorbing material, a second impact absorbing material having an outer face adjacent to the impact dissipating layer and an opposite inner face, and having a lower hardness than the impact dissipating layer, and a pressure sensor arranged across the inner face of the second impact absorbing material. An impact on the outer face is partially absorbed by that material, dissipated by the impact dissipating layer and further absorbed by the second impact absorbing material, with the remaining transmitted force being sensed by the pressure sensor.

Claims

1. A combination of a structure to absorb, dissipate and measure a force, a means to calculate an impact force on the structure, and a control module, the structure comprising a plurality of distinct layers including: a first impact absorbing material having an outer face facing the direction of expected impact and an opposite inner face; an impact dissipating layer adjacent to the inner face of the first impact absorbing material and having a higher flexural rigidity than the first impact absorbing material; a second impact absorbing material having an outer face adjacent to the impact dissipating layer and an opposite inner face, and having a lower hardness than the impact dissipating layer; and a pressure sensor arranged across the inner face of the second impact absorbing material, wherein an impact on the outer face of the first impact absorbing material is partially absorbed by that material, dissipated by the impact dissipating layer and further absorbed by the second impact absorbing material, with the remaining transmitted force being sensed by the pressure sensor; the means to calculate the impact force on the structure comprising a means to calculate the impact force on the outer face of the first impact absorbing material based on the force measured by the pressure sensor; and the control module comprising an electrical connection to the pressure sensor and a processing unit to receive the sensed data and carry out any required calculation of the incident force and control the transmission of data as required, wherein the processing unit calculates a received impulse by integrating the detected force over time.

2. The combination according to claim 1, the structure further comprising an inner fabric layer covering the face of the pressure sensor on the opposite side of the pressure sensor from the second impact absorbing material.

3. The combination according to claim 1, the structure further comprising an outer fabric layer covering the outer face of the first impact absorbing material.

4. The combination according to claim 1, wherein the pressure sensor is in the form of a matrix array which is able to detect pressure changes across a substantial portion of the width of the structure.

5. The combination according to claim 1, wherein the first and second impact absorbing materials and impact dissipation layer together have a dampening factor of greater than 10%, preferably greater than 50%, most preferably greater than 85%.

6. The combination according to claim 5, wherein the means to calculate the impact force comprises a control system which is programmed with the dampening factor.

7. A combination according to claim 6, wherein the control module further comprises a transceiver which is able to transmit data wirelessly.

8. A combination according to claim 6, wherein the control module comprises a lithium ceramic battery.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) An example of a structure in accordance with the present invention will now be described with reference to the accompanying drawings, in which:

(2) FIG. 1A is a front view of a garment in a structure according to the present invention;

(3) FIG. 1B is a back view of the garment of FIG. 1A;

(4) FIG. 1C is a perspective view of the garment of FIGS. 1A and B;

(5) FIG. 1D is a top view of the garment of the previous figures;

(6) FIG. 2 is a schematic cross-section through various layers of the pad, sensor and garment;

(7) FIG. 3A is an exploded perspective view of a pressure sensor;

(8) FIG. 3B is an assembled plan view of the same sensor;

(9) FIG. 4 shows the layout of the control module; and

(10) FIG. 5 is a flow chart showing the general operation of the system.

(11) FIG. 6A is a cross-section through a tackle bag incorporating a structure according to the present invention;

(12) FIG. 6B is a plan view of the bag of FIG. 6A;

(13) FIG. 7A is a cross-section through a scrummaging machine incorporating a structure according to the present invention;

(14) FIG. 7B is a front view of the scrummaging machine of FIG. 7A;

(15) FIG. 8 is a schematic drawing of a drill incorporating a structure according to the present invention; and

(16) FIG. 9 is a plan view of a crash barrier incorporating the structure according to the present invention.

DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS OF THE INVENTION

(17) FIGS. 1A to D show a padded top which is a type of padded underlayer intended for use by a rugby player. As described elsewhere in this application, the invention is applicable to wearable garments in general and other items where impact protection is required. Whilst the top illustrated in FIGS. 1A to D is being used as an illustration, it will be readily understood that, for other such garments, the impact absorbing pads are placed in the areas most likely to receive an impact.

(18) As shown in FIGS. 1A to C, the garment 1 comprises five impact absorbing pads 2 comprising a pair of shoulder pads, a pair of upper arm pads and a chest pad. Towards the upper part of the back of the garment 1 is a control module 3. This is surrounded by a soft layer 4 to provide comfort for the person wearing the garment as well as anyone impacting on them. The control module 3 is connected via an electrically conductive line 5 to each of the pads 2. The line 5 may simply be a wire which is retained between layers of the garment so that it does not impede the wearer.

(19) The number and positioning of pads is provided as one example only. There may be fewer pads, for example just the shoulder pads, or additional pads, such as pads which protect the ribs.

(20) FIG. 2 shows the structure of the pad 2 in greater detail. The pad is sandwiched between an outer fabric layer 10 and an inner fabric layer 11. The pad consists of an impact absorbing layer 12. This may be made of a material such as foamed elastomers, thermoplastic elastomers, foamed thermoplastic elastomers or any suitable compliant material. This layer 12 will generally be less than 100 mm thick, more preferably less than 50 mm thick and most preferably less than 20 mm thick. Within the impact absorbing material 12 is an impact dissipating layer 13. This may be embedded in the impact absorbing material at the point of manufacture. Alternatively, the impact absorbing material 12 may be formed of two parts which are sandwiched around the impact dissipating layer 13. The impact dissipating layer 13 may be high impact engineering polymers (such as polycarbonate or nylon), glass or carbon fibre composites, bi-axial oriented films or any other material which provides high flexural strength, high puncture resistance and flexibility.

(21) Between the impact absorbing material 12 and the inner fabric layer 11 is a sensor 14. This sensor is shown in greater detail in FIGS. 3A and 3B. Another suitable sensor is shown in US2014/0083207.

(22) The sensor 14 comprises two substrate layers 14a, 14b between which is provided a spacer layer 14c and, optionally, one or more dielectric layers 14d, 14e. The facing surfaces of the substrate layers 14a, 14b may carry conductive traces of known resistance printed thereon such that when contacting the substrate layers 14a, 14b provide a variable resistance that depends on the force of contact. Preferably, an array of such force sensing resistor elements is arranged in a grid pattern on the substrates 14a, 14b. The sensor can be designed in any desired pattern (the grid pattern does not have to be a regular pattern) with the effective sensing grid arranged within.

(23) The layout of the control module 3 is shown in FIG. 4.

(24) This module contains the following components.

(25) An accelerometer (e.g. ADXL375) which is a three axis accelerometer. This will measure the acceleration of the wearer during normal motion as well as measuring an abrupt change upon impact.

(26) A gyroscope 51 (e.g. ADXRS290). This is a dual axis gyroscope which is able to detect changes in orientation of the wearer.

(27) A processor 53 (e.g. ARM Cortex M3) which will receive the readings from the pressure sensors 14 from the accelerometer 50 and gyroscope 51 and carry out various calculations and output diagnostic information as set out below.

(28) A connector 54 to connect to the matrix sensor.

(29) A power management integrated circuit 55.

(30) A transceiver 56 such as a Bluetooth device.

(31) A socket 57 via which a battery can be recharged.

(32) An LED 58 which is preferably a multicolour device to provide an indication of device status such as on/off, low battery, charging or the like. It may also be used to provide visual output depending on the magnitude of the impact.

(33) An on/off switch 59 for activating the device.

(34) A battery connection 60 for attachment to a battery such as a lithium ceramic battery which provides a relatively large power source in relatively small volume. Although shown as a separate connection, the battery is preferably part of the control module 3.

(35) The operation of the present invention will now be described with reference to FIG. 5. The controller 53 receives a number of inputs as described below in order to assess the nature of an impact and to carry out various calculations and to provide useful output.

(36) Certain information is provided by a user before first wearing the garment. This can conveniently be done by providing a user interface 70 such as an app or a website that a user can access when they first use the garment. Information is required on a number of parameters specific to the user such as their weight, height and dimensions such as chest and waist measurements. These are all used in determining the nature of the impact. There may also be an age input to allow the software to determine what might be considered to be an acceptable level of impact.

(37) The software is pre-installed with data 71 concerning the threshold levels of peak pressure and impulse which are considered acceptable. These will include values for an individual impact as well as data concerning cumulative impact. Such values can be set based on existing medical research on safe levels of impact. This aspect of the software is updatable to allow for new information gathered from the latest medical research.

(38) The input from the or each pressure sensor 14 is designated by numeral 72. The sensed value is the normal component of the transmitted force. The pressure sensor 14 provides an indication of the impact force F.sub.N as well as the area A.sub.pad over which this force has been applied.

(39) The inputs from the accelerometer 50 and the gyroscope 51 are designated by numeral 73. The padding dampening factor 74 is programmed into the software based on the calibration of the material.

(40) This may be as simple as applying an impact of a known magnitude to the pad and measuring the transmitted force. A more sophisticated calibration may be carried out by applying impacts of different magnitudes to the pad.

(41) All of this information is then received by the processor 53 which can calculate the impulse felt by a user. This is achieved by integrated the force detected by the pressure sensor 14 over time.

(42) Using this data, together with the individual user date, the accelerometer and gyroscope data as well as the padding dampening factor, the algorithm is able to calculate the incident force F.sub.i by solving the equations of motion using laws of momentum and energy conservation.

(43) The output values can include the impulse and the peak pressure both as felt on the outside of the pad and as a peak pressure transmitted to the user, as well as an indication of the risk of injury and an indication of the effectiveness of the padding.

(44) FIGS. 6A and 6B show a pad 2 in a tackle bag 80. As shown in FIG. 6B, the pad is positioned on one side of the bag and can be clearly marked so that it can be targeted by a user of the bag. The pad has the same structure as previously described that is able to absorb the force and measure the force downstream of the pad at the sensors 14.

(45) FIGS. 7A and 7B show the incorporation of four pads 2 into a scrummaging machine 90 which has four cushioned areas 91 as is well known in the art. Pads 2 are incorporated (one per cushion) into an area approximately at shoulder height to absorb and measure the impact.

(46) FIG. 8 shows the incorporation of two pads 2 into a drill 100 which is otherwise of a conventional structure. The pads are shown in the areas of the drill which are most vulnerable to being damaged by being dropped. However, the pads could be applied to other areas if necessary. Such pads may be useful, for example, if the tool or the work piece are particularly sensitive to damage as they can protect both the tool and the work piece from damage. They are also able to measure the impact force to which the tool has been subjected and provide an alert to a user should the tool need to be recalibrated or serviced. Whilst a drill had been illustrated in FIG. 8, it will be understood that this can be applied to any tool where the tool and/or work piece require protection.

(47) FIG. 9 shows a convention crash barrier 110 to which a pad 2 has been applied. The same layered structure allows the impact to be absorbed and dissipated and the sensors 14 will measure the force transmitted to the crash barrier which may be useful for accident investigation purposes and/or to determine whether the barrier requires maintenance.