SENSOR SKIN

Abstract

The disclosure herein relates to a measuring system for determining damage to components including at least one fiber-reinforced plastics material, comprising sensors that can be or are arranged on a component to be mutually spaced, the sensors distributed over a curved surface of the component in the use position. In order provide a measuring system by which it is possible to obtain fiber-reinforced plastics components economically and with reasonable outlay, and by which process parameters and/or state variables can be reliably obtained during production and operation of the component, it is proposed to provide the component with a substrate that is different from the component and on which the sensors can be or are arranged, the substrate being flexible, and for the sensors arranged on the flexible substrate to form a measuring device.

Claims

1. A measuring system for determining damage to components comprising at least one fiber-reinforced plastics material, comprising a plurality of sensors that can be or are arranged on a component so as to be mutually spaced, the sensors being distributed over a curved surface of the component in a use position, wherein the component is provided with a substrate that is different from the component and on which the sensors can be or are arranged, the substrate being flexible, and wherein the sensors arranged on the flexible substrate form a measuring device.

2. The measuring system according to claim 1, wherein the flexible substrate forms a material-uniting connection with a matrix of the component during production of the component.

3. The measuring system according to claim 1, wherein the flexible substrate is arranged inside the component or on the surface thereof.

4. The measuring system according to claim 1, wherein the measuring device monitors production of the component and/or operation of the component by the sensors thereof.

5. The measuring system according to claim 1, wherein the plurality of sensors of the measuring device is formed on the flexible substrate as an ultrasonic transducer.

6. The measuring system according to claim 5, wherein the ultrasonic transducer is formed as a micromachined capacitive ultrasonic transducer or as a piezoelectric thin film.

7. The measuring system according to claim 1, wherein the measuring device carries out a pulse-echo method.

8. The measuring system according to claim 1, wherein the measuring device carries out a capacitive measurement by the sensors.

9. The measuring system according to claim 1, wherein the measuring device forms, on the substrate in both planar extension directions thereof, a matrix of sensors that are in each case evenly spaced in the directions, in particular sensors having identical spacing in the directions.

10. The measuring system according to claim 1, wherein conductive tracks, multiplexers or other electronic devices are applied to and integrated in the flexible substrate.

11. The measuring system according to claim 1, wherein the flexible substrate can be or is connected to the component by a co-bonding or co-curing process.

12. The measuring system according to claim 1, wherein the substrate forms a film and is produced from a thermoplastic high-performance polymer.

13. The measuring system according to claim 12, wherein thermoplastic high-performance polymer is made of a polyimide, in particular polyetherimide, or a polysulfone, in particular polyethersulfone.

14. The measuring system according to claim 1, wherein structures applied to the flexible substrate can be or are protected from their surroundings by at least one additionally arranged layer.

15. The measuring system according to claim 1, wherein the flexible substrate and/or an additionally arranged layer is/are formed as liquid-crystal polymer (LCP).

16. A method of using an arrangement of sensors on a curved surface of a fiber-reinforced plastics component on a curved component surface, wherein the sensor arrangement is formed on a flexible substrate made of a thermoplastic high-performance polymer that is connected to a matrix of the component during production of the component.

17. The method of claim 16, wherein one or more interposer structures are arranged on the substrate during production of the component, the structures being equipped with sensors after production of the component has been completed.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0029] The disclosure herein is explained in greater detail in the following, on the basis of embodiments shown in the example drawings. In the drawings, in a schematic representation in part:

[0030] FIG. 1 is a sectional side view of a measuring system comprising a sensor skin as a flexible substrate on a CFRP component comprising piezo sensors; and

[0031] FIG. 2 is a perspective side view of an arrangement of a sensor skin comprising electronic components on the parabolic profile of a leading edge of an airfoil.

DETAILED DESCRIPTION

[0032] In all the figures, like or functionally like elements and apparatuses have been provided with the same reference numerals unless specified otherwise.

[0033] FIG. 1 first shows a measuring system, denoted as a whole by 1, for determining damage to a component 5 made of a fiber-reinforced plastics material. A film made of a flexible substrate 22 is arranged as a sensor skin 20 on the side of the component 5 that is the top for the viewer. The sensor skin 20 is provided with a plurality of sensors 24 that form a measuring device 10 on the substrate 22. In this case, the sensors 24 are formed by transducers arranged on the flexible polyetherimide substrate 22. The transducers in turn consist of or comprise two opposing electrodes 26A, 26B, between which a piezoelectric ceramic film 28 is arranged.

[0034] This arrangement of transducers as sensors 24 forms the sensor skin 20 on the flexible substrate 22, which skin is arranged on a surface of the component 5. The sensors 24 carry out a pulse-echo method on the component 5 in order to detect damage, which method is shown by the ultrasound waves moving back and forth between two opposing lateral surfaces 6a, 6b of the component 5, which waves are indicated by arrows 32b, 32b, 33a, 33b. Sound waves 32a, 32b moving back and forth and unimpeded between the lateral surfaces 6a, 6b can be seen in the left-hand region of FIG. 1, whereas the delay time thereof is reduced in the right-hand region in that the sound waves 33a, 33b encounter delamination 34 on their way through the plastics component 5 and are already reflected there.

[0035] The fact that the signal processing is also already carried out for the most part on the sensor skin 20 is due to electronic devices 36 that can be applied to and integrated in the flexible substrate 22, as can be seen in FIG. 2. This shows the leading edge 8 of a portion of an airfoil 15 of an aircraft. The inner face of the parabolic profile 16 thereof is provided with a plurality of sensor skins 20. In the present case, it can be seen in each case that the sensor skins 20 form a curved surface on the inner face of the airfoil profile 16. In turn, sensors 24 arranged uniformly over each surface can be seen on the sensor skin 20, which sensors can make ultrasound measurements on the glass-reinforced component 5.

[0036] The permanent connection between the sensor skins 20 and the component 5 achieved during the preceding production process ensures uninterrupted monitoring of the structural integrity of the component 5 in question and the associated signal processing.

[0037] Accordingly, the disclosure herein described above thus relates to a measuring system 1 for determining damage to a component 5 consisting of or comprising at least one fiber-reinforced plastics material, comprising a plurality of sensors 24 that can be or are arranged on a component 5 so as to be mutually spaced, the sensors 24 being distributed over a curved surface of the component 5 in the use position.

[0038] In order provide a measuring system 1 by which it is possible to obtain fiber-reinforced plastics components 5 economically and with reasonable outlay, and by which process parameters and/or state variables can be reliably obtained during production and operation of the component 5, the component 5 is provided with a substrate 22 that is different from the component and on which the sensors 24 can be or are arranged, the substrate 22 being flexible, and the sensors 24 arranged on the flexible substrate 22 form a measuring device 10. In a preferred development, the flexible substrate 22 also forms a material-uniting connection with the matrix of the component 5 during production of the component.

[0039] While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms “comprise” or “comprising” do not exclude other elements or steps, the terms “a”, “an” or “one” do not exclude a plural number, and the term “or” means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.

REFERENCE NUMERALS

[0040] 1 measuring system [0041] 5 fiber-reinforced component [0042] 6a, 6b lateral surfaces of the component [0043] 8 airfoil leading edge [0044] 10 measuring device [0045] 15 airfoil [0046] 16 airfoil profile [0047] 20 sensor skin [0048] 22 flexible substrate [0049] 24 sensor/transducer [0050] 26a, 26b electrodes [0051] 28 piezoelectric ceramic film [0052] 32a, 32b arrows [0053] 33a, 33b arrows [0054] 34 delamination [0055] 36 electrical devices