Vibrating sensor

Abstract: A vibrating sensor comprises an elongate element (18) arranged to vibrate at a frequency dependent upon an external stress applied to the sensor, and an optical fibre (15) for coupling light into an end of the element (18) to excite it into vibration. A light-absorbing layer (19) is provided on a longitudinal surface of the element (18) such that the element (18) will change its configuration (e.g. by bending) as the layer (19) absorbs light and heats that side of the element (18), this alteration in configuration causing a reduction of radiation which is absorbed so that the element (18) restores. The element (18) may define a Fabry-Perot interferometer between its opposite ends.

Description: This invention relates to a vibrating sensor for responding to physical stress, for example due to forces of pressure or acceleration. Sensors are known for sensing physical parameters such as pressure or acceleration in which a resonant beam is formed across a cavity in a semiconductor substrate. The beam is excited to cause it to vibrate at a predetermined frequency: the means for providing the excitation may be optical, thermal, electrostatic, electromagnetic, piezo-electric or acoustic. Stresses applied to the beam through causes such as acceleration or pressure cause the beam to change in frequency of vibration. This change in frequency can be measured and from known data the magnitude of the applied stress can be calculated. Optically-excited vibrating beam sensors are known, eg. from GB-A-2185106, which utilise a Fabry-Perot interferometer to modulate light which is incident on the beam, and thereby vibrate the beam using thermal effects. The semi-reflective end of an optical fibre is disposed a precise distance from and perpendicular to a semi-reflective side surface of the beam. Light transmitted down the fibre is incident on the beam, thus heating the beam and causing it to bend. The distance between the end of the optical fibre and the semi-reflective surfaces of the beam therefore alters and the light incident on the beam is reduced. As the beam cools and returns to its rest position, the intensity of light incident on the beam once again increases: the beam is therefore alternately heated and cooled and accordingly caused to vibrate at a predetermined frequency. In the above-described sensor, the distance between the end of the optical fibre and the semi-reflective side surface of the beam is particularly critical in order to define the Fabry-Perot interferometer. However, it is difficult to mount the optical fibre precisely enough relative to the beam. We have now devised a vibrating sensor which overcomes these drawbacks. In accordance with this invention there is provided a vibrating sensor comprising an elongate element which is arranged to vibrate, and means for coupling electromagnetic radiation into an end of said elongate element, the elongate element having along a longitudinal surface thereof a layer which absorbs electromagnetic radiation, the elongate element being arranged to alter its configuration as said layer absorbs radiation, which alteration reduces the energy of radiation absorbed by said layer. The elongate element vibrates in a cycle as follows: in one position or configuration of the elongate element, the electromagnetic radiation is coupled into the absorbing layer, which therefore absorbs the radiation and heats the adjacent region of the elongate element and so causing displacement of the latter. However, the coupling of the radiation is thereby reduced, so that the elongate element cools and restores, whereupon the coupling increases and the elongate element is heated again. The opposite ends of the elongate element may be formed with semi-reflective surfaces to define a Fabry-Perot interferometer cavity within the element between the two end surfaces. In one configuration of the elongate element, the incident and reflected waves at each end of the element constructively interfere: this constructive interference increases the radiation intensity within the cavity. The radiation is absorbed by the absorbing layer to cause heating of the elongate element: the change in configuration of the element thus produced alters the distance between the interferometer surfaces and the incident and reflected waves at each end no longer constructively interfere. The cavity is no longer resonant for this wavelength of light. The elongate element therefore cools and restores its configuration, whereupon the cycle repeats. Alternatively, the elongate element may be arranged so that as it is heated and changes configuration, less of the electromagnetic radiation is coupled into the end of the element, so that therefore it will cool and restore its configuration, whereupon the cycle repeats. Preferably the absorbing layer is disposed along one longitudinal side of the elongate element, so that the element is heated adjacent this side and caused to bend because its opposite side remains cool. The electromagnetic radiation may be of any frequency within the electromagnetic spectrum, but preferably comprises radiation within the optical range of frequencies. In a preferred embodiment the vibrating element comprises a beam which has been micromachined from a wafer of silicon, quartz, silicon dioxide, silicon nitride or other suitable material. Preferably the selected material is transparent to the frequency of electromagnetic radiation used. Preferably the electromagnetic radiation is coupled into the beam by an optical fibre which has its end disposed adjacent the end of the beam. An embodiment of the invention will now be described by way of example only, and with reference to the accompanying drawings in which: FIGURE 1 is a perspective view of a body of semiconductor material formed with an optical vibrating sensor; FIGURE 2 is a diagrammatic side view of the vibrating sensor of Figure 1; FIGURE 3 is a diagrammatic side view of the vibrating sensor of Figure 1 shown in its relaxed and excited states; FIGURE 4 is a diagram showing light being coupled into an optical vibrating sensor as shown in Figure 1, in order to excite it, and reflected light being picked up from the sensor, for determining its frequency of vibration; and FIGURE 5 is a diagram showing an arrangement having a plurality of vibrating elements excited at different wavelengths of light. Referring to Figure 1 of the drawings there is shown a semiconductor substrate 10 which has been micromachined to form a vibrating sensor. A portion 11 of the substrate 10 is formed with a V-shaped groove 13 which is provided with an end stop 14. An optical fibre 15 is bonded into the groove 13, and its end abuts the end stop 14. A portion 12 of the semiconductor substrate is formed with two supports 16, 17 which lie across the width of the substrate. The supports 16, 17 taper towards their upper edges and support an optically transparent beam 18. The beam 18 lies perpendicular to the supports 16, 17 and these are inset from the opposite ends of the beam. The beam 18 is aligned on the same axis as the groove 13 and its optical fibre 15. The end of the optical fibre 15 is therefore directed at an end face 20 of the beam 18. The opposite ends 20, 21 of the beam 18 are polished or coated to render them semi-reflective, or the micromachining process may leave them in appropriate polished condition. The upper surface of the beam 18 has a thin layer of optically absorbent material 19 formed on it. In use monochromatic or narrow bandwidth light is transmitted down the optical fibre 15 from a light source 40, as shown in Figure 4. The light emitted from the fibre 15 is coupled into the end of the optically transparent beam 18. The beam 18 forms a Fabry-Perot interferometer cavity between its semi-reflective end faces 20, 21. Any light of the resonant wavelength entering the cavity will be reflected between the two surfaces 20, 21 and the light internally reflected from one such surface will interfere with the light incident on that surface: if the reflected and incident light waves are in phase (as shown in Figure 2) then they will constructively interfere and produce light of a higher intensity. If they are out of phase then they will partially cancel each other out and reduce the intensity of light passing lengthwise within the beam 18. The length of the beam 18 is such that, at rest, the incident and reflected waves constructively interfere. The resulting high light intensity is absorbed by the absorbent material 19 formed on the upper surface of the beam. This causes the beam 18 to be heated adjacent its upper surface, causing the beam to expand in length adjacent its upper surface and therefore the beam bends. As the beam bends the distance between the two reflective surfaces 20, 21 increases, so that the incident and reflected light waves becomes out of phase and the absorbent layer 19 and adjacent region of the beam cool. As this cooling occurs the beam returns to its original position. The process then repeats itself: as a result the beam vibrates at a resonant frequency. Alternatively a broad-band light source may be used in which case the absorbent layer may comprise a material which better absorbs a particular frequency of light than other frequencies. Preferably the layer preferentially absorbs light of the near infrared frequency. This selective absorption characteristic may be achieved by applying an optical filter layer between the surface of the beam and the absorbing layer. The absorbing layer may have a characteristic such that its absorption decreases with increasing wavelength. Thus as the beam heats and bends and so increases in length, the standing wave between the opposite ends of the beam is based on progressively longer wavelengths: the energy absorbed therefore decreases progressively as the beam bends, causing it to cool in due course and restore. Figure 3 shows the beam 18 at different positions during its cycle of vibration, but exaggerated for the sake of illustration. The beam bends from its at-rest position (solid line) to an excited position (broken line 30) as it is heated. Then as it cools the beam 18 restores to its rest position. In an alternative mode of use the beam may be caused to vibrate by modulation of the intensity of light which is coupled into the beam rather than using the effect of the Fabry-Perot interferometer. In this case the Fabry-Perot interferometer effect is inhibited by using a broadband optical source. Referring to Figure 3 it can be seen that as the beam 18 bends due to light being absorbed by the absorbent layer 19, less light is coupled into the end of the beam 18 from the optical fibre 15. The beam therefore cools and straightens again, whereupon more light is coupled into the beam and the process repeats itself: the effect is that the beam vibrates at a predetermined frequency. This mode of operation is simpler than the above-described mode. In use of the sensor, the beam 18 is caused to vibrate at a predetermined frequency as described above. Some of the incident light is reflected from the end surface 20 of the beam and returns up the optical fibre 15: the returning light has thus been modulated by the vibrating beam. A fibre optic Y-coupler 42 is used (Figure 4) to separate the reflected beam and direct it to a detecting device 44. A semi-silvered beam splitting mirror may be used, instead of the Y-coupler 42, to separate the reflected beam. External stresses applied to the beam, such as acceleration or pressure, cause the beam to change its frequency of vibration. This change in frequency is detected by the device 44 and measured from the modulated, reflected light returned through the optical fibre and from known data the magnitude of the applied stress can be calculated. As shown in Figure 5, the beams 18 of a plurality of sensors may be coupled to a common optical fibre 15, the different sensors being excited by different wavelengths of light. Alternatively the plurality of beams 18 may be formed on a single substrate. The intensity of the beam returned up the optical fibre is monitored by the detecting device 44 at the different wavelengths to determine changes in frequency of vibration of the different sensor beams 18. The plurality of beams 18 may be arranged to have different natural resonant frequencies of mechanical vibration, but to be excited all by the same wavelength of light. In this case, the light source 40 in Figure 5 is a single wavelength source: the detecting device 44 includes a plurality of narrow bandpass filters, arranged to pass separate frequency bands centred on the respective natural resonant frequencies of the beams 18.

Claims: A vibrating sensor comprising an elongate element (18) which is arranged to vibrate, and means (15) for coupling electromagnetic radiation into an end (20) of said elongate element, the elongate element having along a longitudinal surface thereof a layer (19) which absorbs electromagnetic radiation, the elongate element (15) being arranged to alter its configuration as said layer (19) absorbs radiation, which alteration reduces the energy of radiation absorbed by said layer (19). A vibrating sensor as claimed in claim 1, in which a Fabry-Perot interferometer is defined within said elongate element (18) between its opposite ends (20, 21), so that incident and reflected waves of the electromagnetic radiation at each end of the element (18) constructively interfere when the element is in its at-rest configuration. A vibrating sensor as claimed in claim 1, in which the elongate element (18) is arranged so that, as it alters configuration from its at-rest configuration, less of said electromagnetic radiation is coupled into said end (20) of the element. A vibrating sensor as claimed in any preceding claim, in which the absorbing layer (19) is disposed along one longitudinal side of the elongate element (18), so that absorbtion of electromagnetic radiation by said layer causes heating of the elongate element (18) adjacent said longitudinal side and thereby bending of said element. A vibrating sensor as claimed in any preceding claim, in which the absorbing layer (19) absorbs electromagnetic radiation of a predetermined frequency preferentially to other frequencies. A vibrating sensor as claimed in any one of claims 1 to 4, in which the absorbing layer (19) has a characteristic such that it absorbs less with increasing wavelength of radiation. A vibrating sensor as claimed in any preceding claim, in which the means (15) for coupling electromagnetic radiation into said end (20) of the elongate element comprises an optical fibre having an end directed at said end (20) of the elongate element. A vibrating sensor as claimed in any preceding claim, comprising means arranged to receive a portion of the electromagnetic radiation which is reflected from said end (20) of the elongate element (18), said reflected portion being modulated in accordance with the vibration of said elongate element (18), said means being responsive to said reflected portion to monitor variations in the frequency of vibration of said elongate element (18). A vibrating sensor as claimed in any preceding claim, in which the elongate element comprises a beam which has been micromachined from a wafer of material. A vibrating sensor as claimed in any preceding claim, comprising a plurality of said elongate elements excited by different wavelengths of electromagnetic radiation. A vibrating sensor as claimed in any one of claims 1 to 9, comprising a plurality of said elongate elements having different natural resonant frequencies of mechanical vibration, said elongate elements being excited by a common wavelength of electromagnetic radiation.

Inventors: COOK ALAN JAMES, PINNOCK ROBERT ANDREW, COOK, ALAN JAMES, PINNOCK, ROBERT ANDREW
Applicants: LUCAS IND PLC, LUCAS INDUSTRIES PUBLIC LIMITED COMPANY
Application year: 1992
Main classification: G01L1
IPC codes: G01L9, G10K15, G01L1, G01P15