AU603834B2 - Optical-fibre smoke detection/analysis system - Google Patents

Description

60u"38347

AUSTRALIA

PATENTS ACT 1952 COMPLETE SPECIFICATION

(ORIGINAL)

FOR OP'FICE USE Application Ni~rber: Lodged: Complete Specification Lodgedi Accepted: Published: T1is do u;n r.'t contains the ameunments maidc under Section 49 and is corf;ect for pirintin~

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t~I Priori ty: Related Art: TO BE COMPLETED BY APPLICANT t Name of Applicant: Address of Applicant: Actual Inventor: Address for' Servlce: ALAN LEITCH 11 Hampden Street, BEVERLY HILLS NSW 2209 ALAN LEITC.1 ARTHURI S. CAVTE CO.

Patent Tradb Mat'k Attorneys Goldfields House 1 Alfred Street SYDNEY N.S.W. 2000

AUSTRALIA

*I I '4.

t~ Complete Specification for the invention entitled OPTICAL-FIBRE SMOKE DETECTION/ANALYSIS SYSTEM.

The following statement is a full description of this invention including the best method of performing it known to met- 1 ASC 49 AMD/1069P ii;il( ^lii .F II--I( OPTICAL-FIBRE SMOKE DETECTION/ANALYSIS SYSTEM The present invention relates to the field of fibre-optic technology, to spectrophotometery and reflectometry, and more particularly to their application to a sensing system for the detection and analysis of smoke, gas or the combustion products of fire.

The technology of fibre-optics finds application in a wide variety of fields, most notably in the communications and medical fields. -The principal reasons for the explosive growth 1 of the fibre-optics industry are due to the low loss, wide S0 bandwidth communication achievable using optical fibres. Other unique characteristics of optical fibres include their immunity to electromagnetic interference and their ability to withstand high temperature environments, All these characteristics o. render the optical fibre as an ideal component in a smoke, gas and fire detecting system in accordance with the arrangement of the present invention.

The science of spectrophotometery allows the composition of a sample gas to be determined. A spectrophotometer, in the strict sense, is a device for measuring tLa distribution of electromagnetic energy over a spectrum. Basically, a 'spectrophotumeter consists of a light source, chosen for the S special range of interest, a sampling cell, a detector and a readout device. Measurements may be carried out at particular wavelengths of interest, or the spectrum may be scanned automatically and a graph or printout of the absorption/ emission at various wavelengths produced.

Gaseous molecules have natural frequencies of vibration, -2 0722E so each type of molecule absorbs electromagnetic radiation in different wavebands. Spectra of gases are therefore unique to particular gases, so, by mapping their transmission at various wavelengths the composition of a sample gas may be deduced.

Spectrophotometery has particular application to this invention in that not only can the presence of smoke, gas, and/or the combustion products of fire be detected, but the particular composition and nature of the smoke, gas or fire can be analysed.

i.O This renders the present invention particularly useful in S0o. a wide variety of applicationb including chemical and gas o manufacturing and processing plants, where not only is the 0 *0O. presence of fire able to be detected, but also, unusually high concentrations of gases or chemical vapours may be detected and o 0 analysed, Reflectometry is also utilised in the present invention to provide an integrated sensing system. Since fibre-optic cables have a finite velocity constant, and the transit time of a a pulse of electromagnetic energy of specific wavelength through t,1, a network of fibre-optic cables and detection cells can be measured accurately, the transmission of such a pulse through a network and the detection of the returned signal relative to a time frame and the measurement of the amplitude of the signal at specific wavelengths, allows the exact location and the nature of the smoke, gas or fire to be determined by the microprocessor. The location of the smoke, gas or fire, (combustion products), may then be signaled by digital communication over optical fibre or other communication media, 3 0722E as may be appropriate to a given installation, to a central watching station where an appropriate alarm is raised. Mimic diagrams/computer generated displays of the floor plan, specific instructions for those premises in the event of alarm are activated, and the location and type of the smoke, gas, or combustion products of fire are displayed.

The present invention seeks to provide a sensing system for detection and analysis of smoke, gas or fire.

The present invention also seeks to provide an 1 0 intrinsically safe smoke, gas and fire sensing system which is Scapable of withstanding high temperature environments with no 000 .oo adverse effects.

o o o 0 The present invention also seeks to provide a smoke, gas and fire sensing system which does not only detect the presence S0OO o11%l of smoke, gas and fire, but also is able to analyse the exact nature of said smoke, gas or fire.

The present invention also seeks to provide a smoke, gas and fire sensing system, which is capable of not only detecting the presence of fire within a particular environment, but is 0. also able to pin-point the exact location of said smoke, gas or fire.

In one broad-ff--t-h3 pres int i system comprising: detection means having at least one ection cell for the detection of smoke, gas or the e; and, analyser mean o-electrically connected ti o each of said detectiiLfe s of said detection means via an optical fibre P h r m i'nrin the o ii -m ,m 4 -in C'i i-

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In one broad form, the present invention provies a sensor system, comprising: a light source adapted to emit electromagnetic energy signals of predetermined frequencies; detection means having at least one detection cell adapted to admit gaseous substances into the path of said electromagnetic energy signals; a receiver adapted to receive resultant electromagnetic energy signals after transmission of said electromagnetic energy signals through said detection means; an optical fibre circuit adapted to transmit said oOOo electromagnetic energy signals between said detection means, 0 a Ssaid light source, and said receiver; and o.0. microprocessor means adapted to control the emission of SO, said predetermined frequencies of said electromagnetic energy signals from said light source and to process said resultant electromagnetic energy signals returned from said detection *means to said receiver by spectrophotometry to identify the Be composition of said gaseous substance.

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1238a _134fa ceatctcad. by ride ,,ltet6i-nmeans- The present invention will become more fully understood by consideration of the following detailed description of preferred embodiments thereof in connection with the accompanying drawings, in which: Fig. 1 shows a preferred embodiment of the sensing system of the present invention; Fig. 2 illustrates an embodiment of a simple detection cell for the detection of gas, smoke or the like; '0 Fig. 3 details the manner in which an optical fibre is .o 0 mounted in the rear of a parabolic mirror of the detection cell 000 a 0o.* of Fig. 2; 0 0 oo«oo Fig. 4 shows the operation of a fibre-optic splitter/ combiner; o*°1 Fig. 5 illustrates a temperature sensor which may be used in conjunction with the present invention if information ao, regarding the temperature is to be monitored; 0 09 Fig. 6 shows an alternative embodiment of the sensing o0*o system of the present invention; 0 0 e0000 Fig. 7 illustrates the basic feature of an embodiment of a St microprocessor used to analyse the presence and nature of gas, 0

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e e smoke or the like in accordance with the present invention; Fig. 8 details an embodiment of an optical spectrophotometer analyser suitable for analysing the composition of gas, smoke or the like; Fig. 9 details a block diagram of a microprocessor and the associated control logic for the transmission and reception and analysis of the electromagnetic radidtion; and, 5 MM PM_-- Fig. 10 shows a detection cell designed in the shape of a torus, illustrating a preferred embodiment thereof.

In Fig. 1, the sensor system is comprised of detection means, gene-ally designated by the numeral 1 and analyser means, generally designated by the numeral 2. The present embodiment shows the detector 1 comprising a plurality of fibre-optic cables 3, 11, 12, a plurality of fibre-optic splitters 4, fibre-optic combiners 5, and a plurality of detection cells 6. The analyser 2 comprises a light source 7, 1.0 a receiver 8 and a microprocessor 9. A communications link °o links the system to a control panel, alarm or the like to indicate the presence of smoke, gas or fire to an operator.

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o In operation, the coherent light source 7, which may, for instance, be a laser or a laser diode, emits a pulse of *60o o0.Fg electromagnetic energy into the fibre-optic cable 3. If more than one detection cell 6 is required, a fibre-optic splitter 4 S is used to direct part o the energy into the detection cell 6 S ia optical fibre 12 and part of the energy to the next detection cell stage. The detection cell 6, which will be S3. described hereinafter in more detail, detects the presence of smoke, gas or the like by changing the spectral properties of a S pulse of electroagnetic energy. The resultant electromagnetic energy conducted out of the detection cell 6 is returned via the fibre-optic combiner 5 from each of the detection stages.

The resultant electromagnetic enegy returned to the receiver 8 is then supplied to the microprocessor 9 for processing and analysis.

0722E 0722E -4 By changing the wavelength of the light source 7, the presence and concentration of gas, smoke or the like can be identified by the attenuation of the signal as it travels through the detection cell. It is also possible to determine the presence of particular substances by the stimulated emission of electromagnetic radiation of certain wavelengths following the application and removal of the pulse of electromagnetic energy. This may be determined by sensing both the absorption and emission spectra of the substance in the '0 detection cell 6.

Sos The analyser 2 utilises time domain reflectometry to "0 o determine the particular location of the smoke, gas or fire.

o0 Q.000 The nature of the smoke, gas or fire is determined by 0 o0 0 controlling the wavelength of the emitted light source to 0 identify particular substances and the concentrations thereof at the detection cells 6. The microprocessor unit 9 may be °o programmed to control the transmission of a particular sequence 6 of electromagnetic signals from the light source 7. The ooo resultant electromagnetic signal returned to the receiver 8 may then be compared to the transmitted signal and analysed by spectrophotometery to identify the particular substances and d i

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t their concentrations.

The particular location of the smoke, gas or the like is calculated by the microprocessor 9 by measuring the time elapsed between the transmission of the electromagnetic energy pulse from the source 7 and the reception of the resultant electromagnetic energy pulse at the receiver 8. Since the fibre-optic cable transmission is of finite velocity, a pulse 7 0722E of electromagnetic energy will take a finite time to traverse the optical path to and from each detector cell 6. By measuring the time elapsed between transmission and reception of an electromagnetic energy pulse, it is therefore possible to determine which detection cell the pulse travelled through, and thus the exact location of the smoke, gas or fire.

The microprocessor 9 controls the emission of the pulses of electromagnetic energy from the coherent light source 7 as well as analysing the resultant electromagnetic energy returned 10 to the receiver, to determine both the nature of the smoke, gas °0 o or fire as well as the particular location of the smoke, gas or oa 0 o o° fire. The microprocessor is preferably packaged in a 0QQ gas-tight/explosion-proof housing in hazardous environments.

000: The communications within the microcomputer may be either made l by optical fibres or hardwired.

The function of the device is inherently fail-safe and intrinsically safe, in that a pulse of light of known spectra is transmitted through a fibre-optic cable to a detection cell in which the said pulse of light is used to probe the c absorption and emission spectra of gaseous substances which may be present in the detection cell. Certain wavelengths of light J will be absorbed by the normal atmosphere in the detection cell and by the fibre-optic cable. However these absorptions will be known and this information is used as a reference of the normal or non-fire state. Tho light pulse is returned by another fibre-optic cable or by reflection into the first fibre-optic cable to an analysing system whirch can determine which wavelengtha have been absorbed and from this information 8 22E w mu nn n^ i7 determine the molecular signature of the substance in the detection cell and its concentration.

For example, in the early stages of certain fires there is an abrupt increase in the presence of hydroxyls which have a strong absorption lines at certain infra-red wavelengths.

Absorption at these wavelengths can be detected with the apparatus described below.

The light source employed in this device may be a broad spectrum source such as a xenon flash tube which has a known spectra, a carbon dioxide laser which has been designed to 1 produce a comb spectra, or a multiplicity of hetero-junction 0 0 a 0 0 oo lat;ers of different wavelengths, the outputs of which have been optically combined to produce a pulse or pulses of light of the o so o°0* desired spectra or any other light source of known spectra.

00oo °.185 The selection of the light source is dependant on the application of the detection system and the absorption and emission spectra of the gaseous substances of interest.

cel In Fig. 2, is shown an embodiment of a simple detection cell 6. The detection cell 6 in Fig. 2(a) comprises two cassegrain parabolic mirrors 13 and 14 facing each other with the focal point of each mirror falling in the centre of each opposing mirror. The optical fibres 15 and 16 enter the rear of the centre of each mirror 13 and 14 on the focal axis, as shown more clearly in Fig. 3. Fig. 2(b) shows a variation of the detection cell 6, to improve the coupling. Interferance rings occur within the detection call 6 due to interaction of wavefronts at the intersection of the dispertion angle of the optical fibre and the angle of the focal core of the mirror, 0722E Fig. 2(b) shows the inclusion of a probe 67 and an obscuration disc 68, consequently making the arrangment directional.

In Fig. 3, the optical fibre 17 is shown entering the rear of the parabolic mirror 16. A microsphere 19 receives the electromagnetic energy such that it provides an efficient interface to receive the electromagnetic energy for further transmission through the optical fibre 17. An identical construction may be used to transmit the electromagnetic energy from the optical fibre to the detection cell 6. The detection cell 6 is preferably mounted in a labyrinthine 46 housing such that all ambient light and dust particles are *aO 0 Poo o 00 o qO O excluded, whilst admitting gaseous substances.

The detection cell, in its simplest form, is an 9 arrangement of two identical, opposing, concave mirrors mounted on a common axis and separated by a distance which is slightly less than the focal length of the mirrors to ensure stability of the arran~goent.

te Electromagnetic energy is coupled into the detection cell 4k via a co-axially mounted optical fibre on the same axis as the O mirrors and coupled out of the cell by a similar arrangement on the opposing mirror. Tp ensure maximum coupling efficiency the position of the output fibre on the mirror axis is adjusted in manufacture such that it falls at the focus of the interference rings which occur within the detection cell. A short focal length lens may be inserted ir the optical path at this point to further increase the coupling efficiency. The inclusion of an obscuration disc on the axis of the mirrors between the input fibre and output probe attenuates direct rays on the Wxis 10 0722E ^-i-w-^.j^^^g-awTOajiaacgj^.S^^WM^'J^wii^^ and minimises reflections into the input fibre which could disturb the operation of the system. This is, in effect, an optical directional coupler.

In most applications of this invention it is desirable, for both economic and engineering considerations, that a multiplicity of detection cells be connected to one fibre-optic highway. This is achieved by the insertion of fibre-optic splitter combiners in the transmit and receive optical fibres at the desired detection location. It also provides an 0 economical method whereby detection cell/s, which is/are geographically removed from the main fibre-optic highway, may 0 a to *ti. be connected on a spur fibre-optic circuit. The fibre-optic i splitter combiners have been designed as an integral part of U t the detection cell assembly to simplify installation of the system. They also provide a method to prevent reflections, j( which occur at interfaces of differing refractive indices, from disturbing the operation of the system. The splitter combiners are directional deviees in that the gradient of the refractive index changes along the length of the device, that is, there S.0 an abrupt change to a higher refractive index in the core o.

the optical fibre at the input end of the device, followed by a gradual decrease in refractive index along the length of ithe device, such that, at the output end, the refrar-tive index to equal to that of the core of the optieal fibre.

By controlling the refractive index in this manner it is possible to construct a number of useful optical dvi<?eo which have application to this inveniton such devices incluo circulators* directional eouplets, signal spliter 07229 and optical impedance matching devices.

These devices are used, individually or in combination, to direct the returning light pulse on to the return fibre-optic highway and thence to the analyser.

In Fig. 4 is shown a detail of an optical fibre splitter/combiner. In the case when it is being used as a splitter, one end 20 is mounted adjacent the light source, whilst the other ends 21 and 22 are both illuminated with minimal losses. When using it as a combiner, the ends 21 and .i B 22 are utilised as the inputs, and the output is end <i In Fig. 5, a temperature sensor is shown. A temperature o, u sensor may be utilised in connection with the sensing system to 4 o. provide data on the change of temperature at a remote location, a a due to, for example, heat build-up caused by a fire. The a 15J temperature sensor can be connected by an optical fibre link to the microprocessor 9 for analysis. The temperature sensor a, comprises the input fibre 23 and the output fibre 24 connected together wikh a microsphere of temperature dependent optical S. material 26. The microsphere is connected via a thermal a connection 25 to a thermal sensing plate 27. As the ambient temperature changes, the thermal sensing plate 27 recognises this change and conveys same to the microsphere 26 via the thermal connection 25. The optical properties of the microsphere 26 of temperature dependent optical material consequently change, thus altering the optical properties of the path between the optical fibres 23 and 24. The microprocessor 9 can then analyse the differences between the electromagnetic energy supplied to the optical fibre 23 and the 12 0722Z electromagnetic energy received at the output of the optical fibre 24. The temperature, or th5;, rate of change of temperature may consequently be determined by calculation wi~thin the microprocessor.

Numerous other modifications may be made to the inven'tion as herein described. For example, the system shown in Fig. 1 may be modified to the simpler serially-connected system shown in Fig. 6. In Fig. 6, each1 of the detector cells 28 is linked in ~a 'series' connection with the adjacent detector cells by optical fibres 29. In this' alternate embodiment, an electromagnetic energy pulse may be transmitted from the ligjht 0~ 0 S source 7 and may pass through each of the detector cells 28. A 0006 suitable termination may be supplied, for instance of highly a~ sO reflective material at the last of the detector cells 28. The ,4 electromagnetic energy pulse would travel through each of the detector cells 28 and optical fibre links 29, and be reflected at the end of the optical link to the receiver 8. Since the S amount of energy returned to the receiver under the conditions 0 when there is no smoke, gas or fire present i~s known by the Aw~ microprocessor, the microprocessor can then analyse the received signal iri a similar way to the embodiment shown in c r Fig. 1 to determine the nature of the smoke, gas or fire.

In Fig. 7, is shown the basic features of an embodiment of an analyser system in block diagram form. The system comprises the control microprocessor unit 30 which controls the system and analyses the results. The microprocessor 30 has an output to a control interface 31. The control interface 31 controls the emission of electromagnetic energy, shown as lasers 32., 13 0722t into the detection system. After the electromagnetic energy has passed through the series of optical fibres and detection cells, the electromagnetic energy returns to the analyser system either, unchanged indicating the absence of smoke, gas or fire, or, at changed intensity indicating the p':esence of smoke, gas or fire. On reception of the electromagnetic energy signal from the detection system, the signal is firstly converted into an electrical signal by a suitable photodetector 33. The electrical signal may then pass through an amplifier 34 before being converted into a digital signal for processing 'lot. by the microprocessor 30. Typioally, this may be implemented by the system shown in Fig. 7 consisting <f a sample-and-hold block 35, a multiplexer 36, an amplifier 37 Und an analog-to-

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digital converter 38. The microcomputer may then be linked by L a hardwire or optical-fibre link to a communications interface for display on a screen, or activation of an alarm or the like, indicating of the presence of smoke, gas or fire. The analysis t system is preferably connected to both a mains power supply as well as a standby battery for occasions when there is a power .0.1 failure or an emergency situation.

In Fig. 8, is shown an analyser 39 which acts as an optical spectrophotometer. Fig. 8(a) illustrates an end view of the analyser 39 showing concave mirrors 41 and 43, Fig. 8(b) details a plan view of the analyser 39 showing the optical paths of electromagnetic radiation of tho system, and, Fig.

8(c) shows an end view of the analyser 39, wherein the electromagnetic radiation enters the slit 40, is reflected onto the diffraction grating 42 and focussod onto the detector array 14 0722E i- 44. Light returning from the detection cell via the fibre-optic cable is directed into an optical system which has been machined from material having the same refractive index as the core of the optical fibre. This ensures that losses due to reflections from intGrfaces of differing refractive indices are minimised. The light from the optical fibre passes through the entrance slit 40, and is reflected from the concave mirror 41, onto the diffraction grating 42, where the light is diffracted at different angles corresponding to the wavelengths of the f0 spectra of the light. The diffracted light falls on the O concave mirror 43, and is focussed onto the detector array 44, 99 where the image of the slit appears as a series of lines at the wavelengths of the spectra of the light source. The intensity S of these lines will vary, dependant on the degree of absorption t of the light at the wavelengths of interest.

The letters f, r and x in Fig. 8 illustrate the preferred S optical lengths of the system. The radius of curvature of the concave mirrors is represent by r, r being, for example, t typically 112mm. The focal length f of the concave mirror is I0' equal to 0.5 r, and x is the optimum distance between a mirror i and a diffraction grating in a Czerny-Turner spectrophotometer mount which gives the most compact design, which is equal to 0.423r. The mirrors may be off-axis paraboloids.

The detector array 44, may be scanned by a charge coupled device shift register, under control of a microprocessor, and the output of the charged coupled device being an analogue video signal in which the amplitude of the signal is an analogue representation of the intensity of light falling on 15 0722E *t-2 the detectors and the position in time represents the location of an element in the detector array. Since the location of each of the elements in the detector array is known relative to the diffraction wavelength then this video signal may be said to represent a spectrograph of light returned from the detection cell.

The amplitude of the video signal at various wavelengths is influenced by the transmission characteristics of the fibre-optic cable and any device or substance in the optical path including the characteristics of the light source and the detector array. To compensate for these variations an is equalising video amplifier is preferably included in the signal path, described hereinafter with reference to Figs. 9(a) and 4 9(b).

L 0* In Fig. 9, comprising Figs. 9(a) and is shown a block diagram of.the microprocessor and the associated control tit 8 l logic for the transmission and reception and analysis of the electromagnetic radiation.

ft As there are critical timings which cannot be determined by the microprocessor 46 alone it is necessary to implement this design using a high frequency crystal controlled oscillator, 47, and timebase circuit 48, to provide all the critical timing and sequencing signals for the system. The timebase circuit 46 also monitors the operation of the microprocessor 46 in that it maintains a 'watchdog' circuit which will raise a 'fault' alarm should the microprocessor 46 fail or become locked in program loop.

At power up, the microprocessor 46 is reset and then 16 0722E vectors to a start address from where it performs a hardware configuration routine and a self test diagnostic to ensure that the hardware is correctly configured and operational, as defined by tables in the ROM 50. The communications interface, 56, is activated so that an engineer may interact with the system. The random access memory 51, resides on the Data bus 61, and the Address bus 57. A fast memory controller 52, and a bus switch 54, are interposed between the data and address buses 61 and 57 respectively, and the video memory 53. The bus switch 54, is necessary to prevent bus contention between the memories. The video memory is required to buffer the output of the A/D convertor 60, which has a conversion rate of 2.0E7/Sec.

9 (20,000,000). The microprocessor 46 loads the timebase 48 with the transmit and receive parameters; wavelength, pulse width, pulse repetition frequency, receiver gating time, and the top end of the video memory with the gain control tables for the control the video equalising amplifier 58, which verifies the information and then initiates the transmit and receive I t sequence. The timebase 48 executes the sequence, starting the 0 3 A/D convertor 60 and timing the reception of the returned j signals. The results of the conversions are time-tagged and stored in the video memory 53.

At the completion of the transmit/receive sequence, which may be one or a number of iterative cycles of the timebase, the results of the conversions are down loaded to the RAM, 51. The microprocessor 48 then analyses this data, stores the results, and signals an appropriate response to a poll from the watching station.

17 0722E 4 The gain of the equalising video amplifier 58 may be controlled by a digital signal from a gain control unit 59 which is derived by the microprocessor 46 from a set of tables stored in memory of the microprocessor 46 at the time of commissioning of the installation. These tables are not fixed but are variable within defined limits. The microprocessor 46 may be provided with auxilliary inputs such that it is able to learn the environment of the detection cells 44 and automatically adjust the system performance to optimise the detection and minimise false alarms. Because the system is dynamic, that is, continuously testing the functionality of the detectors 44, it is able to actively monitor its own performance by testing the absorption of known substances in 0*0 the optical paths.

The equalised video signal is converted to digital form by a very fast analogue to digital convertor 60 and the results of a these conversions are passed by bus 55 and stored in a multiport video memory 53. This information is analysed by the t "l signal processor 45. The analysis may be performed by simply matching the current information with !he detection tables as in a set-point controller. A more sophisticated approach is to use an adaptive predictive algorithm which will not only compensate for changes in the environment but be able to enhance the detection of specific substances by correlating the absorption spectra at a number of wavelengths.

At this time, the computational speed of most available microprocessors is not sufficiently fast to enable this design to be economically implemented without the addition of high 18 0722B r speed ancillary logic to control the transmission and reception of the nanosecond pulses of electromagnetic energy required in the realisation of the reflectometry section of the design. To overcome this limitation a high speed timebase circuit design has been implemented such that all critical timings are independant of the microprocessor cycle time.

These timings include, the initiation of a transmission, the width of the transmitted pulse, the selection of the wavelength or the transmitted signal, the gating of the receiving section, the timing of the transit of a pulse through t ii the network of detectors, the adjustment of the gain of the S equalising video amplifier 58 and other such timings as may be S considered critical to the proper operation of the system.

"There are circumstances in which the absorption wavelengths of certain substances of interest fall outside the passband of the available optical fibre. In these cases a modified form of the detection cell has been designed in which a band of wavelengths which would normally fall outside the passband of the fibre-optic cable are translated within the S0 passband of the optical fibre. To achieve this effect a crystal of non-linear optical material, such as KDP, is included in the optical path. This crystal is pumped by coherent radiation at two or more wavelengths to produce the sum and difference wavelengths of the pump beams. The desired spectra is selected by filters or gratings and then used to probe the absorption spectra of the substances in the detection cell. The resultant absorption spectra is translated by similar means or be reflected onto the crystal to a band of 19 0722E q. 4 wavelengths which fall within the passband of the optical fibre.

In Fig. 10, is shown a preferred embodiment of a detection cell design. Whilst the detection cell of the present invention may take a variety of forms to achieve the required functions of the present invention, a torus, as illustrated in Fig. 10 achieves an optimum design choice. Whilst the arrangement of Fig. 2 demonstrates the principle of the detection cell, it is not the most optimum arrangement for both production and aesthetic considerations. A more compact design is to fold the optics into a truncated torus. This is a much improved packaging method which achieves optimum gas flow and o 9 which is much more suitable for mass production, for instance, by injection molding.

A possible variation to the basic concepts of the detection cells of Figs. 2a and 2b, is to arrange the mirrors as surfaces of a modified torus, generally designated by the numberal 62 in Fig. 10(a). The torus is comprised of essentially an inner mirrored surface 63 and an outer mirrored surface 64 in facing relationship. In Fig. 10(a) is shown an isometric view of a detection cell 62, provided with an input 71, output 72, a port 69 to the next detection cell and a port from the next detection cell. Fig. 10(b), illustrates an isometric sectional view of the torus-shaped detection cell.

Rather than the torus being fully enclosed, the upper and lower ends thereof, 65 and 66 respectively are vented to the surrounding environment, such that smoke, gas or the like to be detected may pass through the detection cell 62. The 20 0722E input 77 is passed via 3 fibre-optic splitter 76 to the launcher 73 provided circumferentially around the outer mirror 64. The resultant optical signal is received by the probe 74, provided circumferentially around mirror 63, to be transmitted to the output 78 via the fibre-optic combiner 75. Fig. is a representation of the preferred design choices of the optical path therein. In Fig. 10(c), AB represents the radius of curvature of mirror 64, CD represents the radius of curvature of mirror 65, and DB is the focal length of mirrors 63 and 64, which is equal to half the radius of curvature, for this design. Whilst Figs. 2(a) and 2(b) incorporate i rI S microspheres in the optical path to improve the coupling through the detection cell, when the detection cell is arranged in the torus form of Fig. 10, these are preferably replaced by a ring launcher 73 on the mid plane of the detection cell 62, S and, as in Fig. the probe 67 is equivalently replaced by j a concentrator ring 74. The pattern of operation of light rays within the torus 62 is equivalent to those shown in Figs. 2(a) S 4 and 2(b) in the vertical plane, but the interferance rings will i now lie in the horizontal plane, i Applications of the sensing system for the detection and analysis of smoke or fire in accordance with the present invention are numerous, and include the following: Industrial and commercial premises; Petroleum refineries; Mines and mine processing plants; Ordinance and munitions factories; Explosives factories; 21 0722E -II U

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Natural gas wells and processing plants; Gasworks; Oil rigs and gas wells; Dangerous goods stores; S 5 Explosives magazines; K Chemical works; Sewage works; Hospitals; and, Hotels and residential premises.

S0 In fact, any general situation wherein the detection of gas, smoke or fire is required, would render the present Sinvention useful.

S Although there have been described herein specific arrangements of a sensing system for detection and analysis of j 15 gas, smoke or fire in accordance with the present invention for the purpose of illustrating the manner in which the invention i may be used to advantage, it will be appreciated that the invention is not limited thereto. Accordingly, numerous variations and modifications will be apparent to those skilled t 0 in the art which should be considered to be within the spirit and scope of the invention as herein described.

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Claims (2)

1. A sensor system, comprising: a light source adapted to emit electromagnetic energy signals of predetermined freqvtencies; detection means having at least one detection cell adapted to admit gaseous substances into the path of said electromagnetic energy signals; a receiver adapted to receive resultant electrc~inagnetic energry signals after transmission of said electromagnetic energy signals through said detection means; an optical fibre circuit adapted to transmit said 00 electromagnetic energ~y Signals between said detection meansf said light source, and said receiver; and Microprocessor means adapted to control the emission of said predetermined freguencies of said electromagnetic energy signals from paid light source and to proneos said res4tant electromagnetic energy signals returned from. said detection toot: means to said receive4 by spectrophotometry to ident~fy the osition of said gaseous substance, A sensor systom a§ claimed In claim 1 Wherein said detection Means is comprised of at least two dotoction calls connected in. parall.el relati~onohi, by means of flbre-optc splitters /combiners, and wherein said. microp~aoestor moans is A further adapted to cont~rol the timing or emission of said electromagnetic en, xgy signals from said light source and to analyse said resultant elecitromagnetic energy signals retturned to said receiver by refloctometry, such that the particular detection cell from which the components of said resutant

23- >9/0238a electromagnetic energy signals are returned therefrom can be identified. 3. A sensor system, comprising: a light source adapted to emit electromagnetic energy signals; detection means having at least two detection cells adapted to admit gasous substances into the path of said electromagnetic energy signals; a receiver adapted to receive resultant electromagnetic energy signals after transmission of said electromagnetic energy signals through said detection means; an optical fibre circuiit adapted to transmit said electromagnetic energy signals between said detection means, said light source, and said receiver; and Microprocessor means adapted to control -the timing of emission of said eloctromagnetic energy signals from said light sour~ce, and to analyse said resultant electromagnetic energy signal returned from said detection means to said recoivor by reflectometrye such that the particular detection cell from which -the components of said resultant electromraqnetic energy signals are returned theroerom can be Ictontifiod. 4. A sensor system as olaimed In claim 3 wherein said micro~ _$eor means is tiirkher adapted to control the emissionl af predetrmtined frequondies of said 0loctOM4ao energy signals from said light ooutcot And to analyso said resultant 0lectrtomagnotic energy signals returned to said receiver by specitrophotQMotry to identify the Ooniposltion of said gaseous -24 A sensor system as claimed in claims 1 to 4, wherein each of said detection cells comprise two concave mirrors placed in opposed relationship, each of said mirrors being provided with a microsphere to transmit and receive electromagnetic radiation 'through optical fibres connected thereto. 6. A sensor system as claimed in claim 5, wherein each of i said concave mirrors are mounted on a common axis and separated I by a distance which is slightly less than the focal length of the mirrors. 7. A ,ensor system as claimed in claims 5 or 6, wherein each of said de,:ection cells is mounted in a labyrinthine housing. 0 8. A sensor system as claimed in claims 5 to 7, wherein each of Said detection cells includes an obscuration disc on -aid t (ia *o axis of said mirrors such as to attenupte direct rayn on said o avis and minimize reflections into said optical fibres. 9. A sensor system as claimed in claims 1 to 8, further comprising temperature sensing means for detecting thermal changes at a remote location. A sensor system as claimed in claim 9, wherein said temperature sensing means compcises a thermal sensing plate for sensing ambient temperature changes, and a microsphere of temperature dependent optical material provided within said optical fibre circuit, wherein thermal changes sensed by said S thermal sensing plate are conveyed to said microsphere to consequently change the optical properties of said optical fibre circuit. 25 <423 A sensor system as claimed in claims 1 to 4, wherein each of said detection cells comprise two concave mirrors placed in opposed relationship, each of said mirrors being provided with a microsphere to transmit and receive electromagnetic radiation through optical fibres connected thereto. 6. A sensor system as claimed in claim 5, wherein each of said concave mirrors are mounted on a common axis and separated by a distance which is slightly less than the focal length of the mirrors. 7. A sensor syst claimed in claims 5 or 6, wherein each of said detection cells is mounted in a labyrinthine housing. 8. A sensor system as claimed in claims 5 to 7, wherein each of said detection cells includes an obscuration disc on said oo, axis of said mirrors such as to attenuate direct rays on said axis and minimize reflections into said optical fibres. 9. A sensor system as claimed in claims 1 to 8, further uomprising temperature sensing means for detecting thermal changes at a remote location. 10. A sensor system as claimed in claim 9, wherein said temperature sensing means comprises a thermal sensing plate for sensing ambient temperature changes, and a microsphere of temperatuze dependent optical material provided within said 44 optical fibre circuit, wherein thermal changes sensed by said thermal sensing plate are conveyed to said microsphere to consequently change the optical properties of said optical fibre circuit. 25 i 2 AMOZV23a -r r _Id-i~ I 11. A sensor system as claimed in claims 5 to 10, wherein said detection cells are provided in the shape of a torus. 12. A sensor system, substantially as herein described with reference to the accompanying drawings. DATED this 23rd day of August, 1990 ALAN LEITCH By His Patent Attorneys ARTHUR S. CAVE CO. et ,a CL Si '38