US2553179A - Detection of toxic gases, particularly carbon monoxide - Google Patents

Description

May 15, 1951 w. H. FARR ETAL 2,

DETECTION OF TOXIC GASES, PARTICULARLY CARBON MONOXIDE Filed Oct. 15, 1948 s Sheefs-Sheet 1 K I v 20 @6702,

May 15, 1951 w. H. FARR ET- AL DETECTION OF TOXIC GASES, PARTICULARLY CARBON MONOXIDE Filed Oct. 15. 1948 3 Sheefcs-Sheet 2 FARR ET AL TOXIC GASES, PARTICULARLY CARBON MONOXIDE 5 Sheets-Sheet Filed Oct. 15, 1948 Q vez alozzLL,

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JIZ/azaowukd 6M Patented May 15, 1951 DETECTION OF TOXIC GASES, PARTICU- LARLY CARBON MONOXIDE Willard H. Farr, Chicago, 111., William F. Fagen, Gainesvillc, Fla., and Stanley C. Kclanowski, Chicago, Ill., assignors to Stewart-Warner Corporation, Chicago, 111., a corporation of Virginia Application October 15, 1948, Serial No. 54,802

2 Claims. 1

The present invention relates to improvements in the detection of toxic gases, particularly carbon monoxide and is a continuation in part of our earlier application Serial No. 478,324, filed March 6, 1943, now abandoned.

The primary object of the present invention is to provide new and improved apparatus for detecting the presence of toxic gases, especially carbon monoxide.

A further object of the present invention is to provide apparatus of this character that may be easily constructed, and which is extremely sensitive.

A further object of the present invention is the provision of apparatus of the character described, which is particularly adapted for detecting the presence of carbon monoxide in the cabins of airplanes, especially airplanes heated by means of the airplane engine exhaust gases.

A further object of the present invention resides in the provision of new and improved apparatus for detecting carbon monoxide which includes a substance having a photocharacteristic preferably the light transmission characteristicthat changes when it is subjected to the presence of carbon monoxide.

Another object of the present invention resides in the provision of new and improved apparatus for detecting carbon monoxide wherein the sensitive substance is placed in a pair of transparent tubes arranged equidistantly from a single light source and controlling the passage of light to a pair of photosensitive devices and wherein heated air is passed through one tube and unheated air through the other.

Another object of the invention is to provide an apparatus as set forth in the previous para- I for equal or difierent light intensities impinging upon the devices.

Another object of the present invention is to provide an improved apparatus of the character described, wherein the sensitivity of the apparatus to the presence of carbon monoxide may be readily adjusted.

A further object of our invention is to provide a carbon monoxide detector which will not respond to the presence of carbon monoxide if the carbon monoxide is in the fresh air to be heated, as might be the case when the airplanes are flying in formation and some of the exhaust gases from one plane enter the cabin of a following plane.

Another object of our invention is to provide a carbon monoxide detection apparatus wherein provision is made to eliminate any possible errors resulting from temperature differences between the heated and unheated air supplied to the tubes containing the sensitive substance.

Another object of our invention is to provide apparatus of the character specified so constructed and arranged as to give indication of the presence of carbon monoxide and also of the operative condition of the electrical circuits and photosensitive devices associated therewith.

A still further object of the invention resides in the physical construction of the apparatus, in the construction of a heat exchanger utilized to bring to an equal temperature the heated and unheated air supplied to the sensitive substance containing tubes, and in an apparatus wherein the tubes may be readily replaced.

Another object of the invention resides in the provision of a new and improved carbon monoxide detecting apparatus capable of being operated from a low voltage electric power source such as that commonly utilized in an airplane.

Other objects and advantages of the present invention will become apparent from the ensuing description, in the course of which reference is had to the accompanying drawings, in which:

Fig. l is a diagrammatic representation of an installation of the apparatu of our invention relative to an exhaust type airplane heater;

Fig. 2 is a view similar to Fig. 1 of an alternative installation requiring no connections to the airplane heatin system and thus making it less vulnerable to gunfire;

Fig. 3 is a vertical cross sectional View illustrating the physical construction of the detection apparatus, the view being taken alon the broken line 3-3 of Fig. 4;

Fig. 4 is a horizontal cross sectional view of the apparatus shown in Fig. 3, the view being taken along the line 5- 3 of that figure;

Fig. 5 is a fragmentary horizontal cross sectional view of the apparatus taken along the broken line 5-5 of Fig. 3 and illustrating details of construction of a novel heat'exchanger incorporated therein;

Fig. 6 is a fragmentary vertical cross sectional view of the apparatus illustrating further details Before considering the details of the physical construction of and the electrical circuits embodied in the apparatus, it may be well briefly to consider their general character. In brief, apparatus of the present invention utilizes a pair of photosensitive devices preferably connected in a balanced difierential bridge circuit and upon which impinges light from a single light source preferably located equidistantly between the devices. Between the light source and each of the two devices is located a transparent tube of material, such as glass, containing a substance, a photocharacteristic-preferably the light trans- Initting characteristic-of which changes in response to the presence of the substance to be detected, in this case carbon monoxide. Fresh air is passed through one of the tubes, which tube acts as a standard, while the air to be analyzed, in this case the heated air, i passed through the second tube. Inasmuch as the photosensitive devices are connected in a balanced bridge circuit, the unbalance of the circuit resulting from the change in color transmitting characteristics of the tube through which the heated air is passed is utilized to control an electronic tube. The electronic tube may be rendered either more or less conductive as a result of the unbalance to operate a relay or to return the relay to its nonoperated position. The operation of the relay in either of these two ways may be used to perform some control operation, for instance the lighting of a warning signal lamp, the operation of a valve to cut off the further supply of heated air into the cabin, or the like.

The substance within the tube which is responsive to the presence of carbon monoxide is one known as the National Bureau of Standards Colorimetric Carbon Monoxide Indicating Gel. The chemical description and method of making this gel are fully disclosed in an article under the title of Rapid Determination of Small Amounts of Carbon Monoxide (Preliminary Report on the NBS Colorimetric Indicating Gel) by Martin Shepherd. This article appeared in Industrial and Engineering Chemistry (Analytical Chemistry) volume 19, page 77, February 1947. This gel is yellow in color until exposed to carbon monoxide when its color changes from yellow progressively toward a dark blue-green.

' Thus, in the event there is carbon monoxide present in the heated air supplied to the airplane cabin which may result from leakage from the heat exchanger, the substance in one of the glass tubes between the light source and one of the photosensitive devices changes progressively from yellow color to a dark blue-green color, thereby decreasing the amount of light impinging upon that photosensitive device. As a result, the bridge circuit becomes unbalanced, and this unbalance is utilized to operate a warning device, or the like.

In the further detailed description of the invention, attention will first be directed to Fig. 1 showing diagrammatically an installation upon an airplane having a heater of the exhaust type often used in airplanes. The exhaust gases are passed through a heat exchanger H], which they enter through a conduit I2 and leave through a conduit Id. The air to be heated and to be supplied to the interior of the cabin flow to the heat exchanger through a cold air intake or duct Hi. This air may be, and usually is, cold air taken from outside the cabin. The heated air is supplied to the interior of the cabin through an outlet conduit or hot air manifold l8. Inasmuch as the primary purpose of the present invention is to provide an apparatus for detecting the leakage of carbon monoxide from the exhaust gases into the fresh air supplied to the interior of the cabin, it is desirable to compare the quantity of carbon monoxide in the inlet conduit [6 and the outlet conduit 65. The fresh 'air sample is continuously passed through a both of which contain the carbon monoxide responsive substance referred to above.

The fresh air flows from the inlet conduit IE to tube 20 through a conduit 25, a flow restrictor 26, a tube 28 containing silica gel, a heat exchanger chamber 30 forming part of a heat exchanger 32, and a conduit 34 connected to the lower end of tube 20. In a similar manner, heated air is supplied to tube 22 from the outlet conduit 18 through a conduit 36, a flow restrictor 38, a tube li) also containing silica gel, a chamber 42 also forming part of heat exchanger 32, and a'conduit i l connected to the lower end of tube 22. The air in each case passes through the upper end of its associated tube, which is open to atmosphere-i. e., the interior of the cabin, or the wing of the airplane, or some other suitable place where the apparatus may be most conveniently located.

The flow of air through the tubes '20 and 22 is preferably continuous and is caused by the air pressures obtaining in the inlet and outlet conduits I 6 and i8. It is preferred that the velocity be such as to maintain a positive flow of air without creating any undue physical disturbance. This flow is readily determinable by the flow restrictors 26 and 38, which may be in the nature of orifices or tube sections containing some restricting material such as glass or steel wool.

In order to prevent gasoline, alcohol or water vapors from affectin the operation of the apparatus, the tubes 28 and 40, filled with silica gel, are utilized to absorb these vapors. The vapors, thus, will not change the color of the substance within the tubes 20 and 22 to any marked degree. Even though the color of the substance be affected, the color change will usually be the same in both tubes because the unheated and heated air supplies are obtained from the same inlet conduit. The apparatus, also, will not be affected if the fresh air supplied to the interior of the cabin through the heat exchanger should contain some carbon monoxide, as might possibly be the case when one plane is flying very close behind another. Under these circumstances the change in the light transmitting characteristics in the same direction will have no effect thereon.

In order to avoid inaccurate readings because of temperature differences and in order to decrease the temperature of the heated air (which may be desirable in some instances, since excessive temperatures have a tendency to reduce the sensitivity of the sensitive substance), the samples are passed through the heat exchanger 32 for the purpose of bringing them to more or less the same temperature. The heat exchanger, it may be seen, is of the character where the two chambers 30 and 42 are in close contact with each other, whereby the air flowing therethrough is brought to much the same temperature. This heat exchanger is described in greater detail hereinafter.

The sensitive substance containing tubes 20 and 22 are mounted in a housing 59 to be described in greater detail hereinafter, centrally of which is also supported a single light source 52, which may be of any suitable construction and energized in any convenient manner.

The variations in the photocharacteristic, in this case the light transmitting characteristics, of the substance within the tubes 20 and 22 are measured by the photosensitive devices 54 and 56, between which and the light source the tubes are located. In order to provide the greatest sensitivity possible, these photosensitive devices are of the photoelectric type. Excellent results have been obtained with the type 923 photoelectric tubes.

Instead of utilizing the pressure of the air in the air inlet and outlet conduits to provide the requisite pressure for creating a flow of air through the tubes, this flow can be induced by means of a pump or aspirator or simply a connection to a region of low pressure. An alternate construction of this character utilizing a pump, illustrated in Fig. 2, enables the air samples to be taken directly from the outside of and interior of the cabin, respectively. This construction eliminates long connection conduits that might otherwise be necessary and makes the installation less vulnerableto gunfire.

Referring now to Fig. 2, it may be seen that fresh air is drawn through the tube 20 by a pump 66, the inlet end 62 of which is connected to the top of the tube by a conduit 64. The fresh air is supplied to the lower end of tube 29 from outside the cabin through a conduit 66, the flow restrictor 26, the silica gel tube. 28, the heat exchanger chamber 30, and conduit 34. In like manner heated air from the interior of the cabin is drawn through tube 22 by the pump, 60, the inlet conduit $2 of which is connected to the top of the tube through a conduit 68. The lower end of tube '22 communicates with the interior of the cabin through conduit 10, the flow restrictor 38, the silica gel tube 40, heat exchanger chamber 32 and conduit 44.

Attention will next be directed to the physical construction of the apparatus and particularly to the glass tube, lamp, electron tube, and photosensitive devices assembly, which is best illustrated in Figs. 3170 6, inclusive.

Referring now more particularly to Figs. 3 and 4, it may be seen that the apparatus is housed in a portable structure comprisin a chassis l4 and a removable cover 16. The chassis comprises a bottom plate l8, provided with a series of ventilating apertures 80, and an upper plate 82 upon which various elements are mounted. The bottom and upper plates of the chassis are suitably secured together as by brackets 84 to provide a space for the heat exchanger 32 and its connections.

The heat exchanger, which is of novel construction, has a generally triangular configuration as may best be noted from Fig. 5 and comprises an upper plate 86 and an intermediate plate 88 that are spaced apart to form the heretofore referred to heat exchanger chamber 30. The inter- 6o mediate plate 88 and a bottom plate 90 are-also spaced apart to form the second heat exchanger chamber 52. The top and bottom plates 86 and st, respectively, are provided with spaced apart, inwardly extending channels or ribs 9| extending into contact with the intermediate plate 38 to provide baflles so that the air must follow a sinuous path through the heat exchanger. This construction provides a more uniform and equal temperature for both the heated and unheated air entering the glass tubes and lowers the temperature of the heated air.

The unheated, or fresh, air is supplied to the sensitive substance containing tube 20 through the silica gel containing tube 28, which is supported immediately outside the unit upon a nipple 92 extending within and secured to the chassis. The inner end of the nipple is provided with a head 95 secured to the upper plate 86 of the heat exchanger near one base corner, as best shown in Figs. 3 and 6. The'heated air is supplied to the heat exchanger chamber 52 through the silica gel containing tube 48, a nipple 96 similar to nipple 92, the head 98 of which is secured to both the upper and intermediate plates near another base corner, as best illustrated in Fig. 6. The plates are all held together by the reversely bent-over peripheral edge 99 of plate 86.

The tubes 2e and 22 containing the carbon monoxide sensitive substance communicate with the heat exchanger chambers 3!] and 42 through the conduits 3t and 44 and through rubber bushings 2&2 and M5, respectively. The bushings are secured to the top plate 82 of the chassis and fixedly receive the upper ends of the conduits 34 and at, respectively. The upper ends of the rubber bushings E32 and its are flared, as indicated by reference characters H35, in order more readily and reniovably to receive the tubes. The lower end of conduit 3 is secured to the upper plate 65 of the heat exchanger so that it communicates with heat exchanger chamber 35 and the lower end of conduit li is secured to bcth the upper and intermediate plates 86 and 88 near their apices so that it communicates with chamber 42.

The glass tubes 29 and 22 are removably held in place by the bushings I92 and its and by rubber grommets ii -d and HE! apertured closely to receive the tubes and secured to the top 'wall I 52 of the lamp housing as. The lamp housing 58 is constructed of two symmetrical parts, each of which is secured to the top plate of the chassis by bolts Ht (see Fig. 4). The light bulb 52 is mounted centrally of this housing in suitable manner, as in a socket 5 l6 (see Fig. 3)

To reduce the quantity of carbon monoxide sensitive substance that must be placed in the tubes 28 and 22, the lamp housing is so constructed and arranged relative to tubes that light from the lamp passes through but. a limited portion of the length of the tubes. Thus, the lamp housing parts are constructed With central oppositely extending parts H3 (see Fig. 4) that are spaced apart and configured to receive the tubes 23 and 22, respectively.

The tubes 28 and 22 thus need be filled with but a limited amount of the carbon monoxide sensitive substance, as shown in Fig. 3, where central portions of the tubes are filled by the substance as indicated by the reference characters A. To each side of the sensitive substance there is placed a quantity of silica gel, the extents of which are indicated by the reference characters B, and the ends of the tubes are filled with some inert material such as glass wool, as indi- 7. cated by the reference characters C, which does not materially impede the flow of air through the tubes.

In order to prevent the temperature within the lamp housing from rising too high, the housing is provided in its exterior with radiator fins I28.

The photoelectric tubes 54 and 56 are mounted on the chassis immediately adjacent the lamp housing in such manner that the photoelectric tubes, lamp and glass tubes are all in a straight line. The photoelectric cells are substantially fully enclosed by metal shields I22 detachably secured to the lamp housing as by a sliding connection constituted by flanges I24 and I26 on the housin and shields, respectively. The air passing upwardly through the tubes flows outside the cover 16 through suitable apertures I21 formed in the cover.

The chassis also supports an electron tube I28, a relay I 30,.a battery I32 and a pair of adjustable resistors I34 and IE6, the functions of which will be described shortly. The relay I38 is of the plug-in type, and the battery is held in place by a pair of straps I38 and I40. The resistors are adjustable by means of adjusting screws I42 and I44. The electrical conductors, through which power is supplied, and/or through which the control functions are exercised may be led within the chassis through a sleeve I46.

The location of the battery I32 in the same enclosure with the light source and electron tube permits the utilization of the heat generated by them to heat the battery and keep it from being frozen, as might be the case when the airplane flies in extremely cold weather or at high altitude. If the heat generated by the lamp and tube is not sufiicient, additional heat may be provided for preventing freezing of the battery. No heating would, of course, be required if the apparatus was located in the normally heated cabin of an airplane.

The photoelectric tubes are arranged in a balanced differential circuit, whereby the sensitive substance in one tube can be used as a standard, and any gradual drift in color of both tubes is balanced out. Referring now more particularly to Fig. 7, it may be seen that the photoelectric tubes 54 and 56 constitute two legs of a bridge, the other two legs of which are constituted by portions I58A and I58B of the resistor I734. Because of the low voltage supply (24 volts) usually found in airplanes, it is preferred, in order to provide a balanced circuit arrangement, to utilize a separate source of potential for the bridge circuit such as, for

instance, a 45 volt battery I32, the positive terminal of which is connected to anodes of the photoelectric tubes and the negative terminal of which is connected to the resistor I34 through a connection I 54 adjustable by adjustment of the screw I42, which connection is utilized for the purpose of balancing the bridge circuit. The junction between the photoelectric tube 54 and resistor portion I58--A is connected by the conductor I56 to the grid I58 of the electron tube I28 which may be of the high vacuum type (of the 25B6G type). The junction between resistor portion I58--B and photoelectric tube 56 is connected by a connection I62 adjustable by adjustment of the screw I44 to the bias resistor I36 in circuit with the cathode I66 of the electron tube. This connection is utilized to adjust the sensitivity of the apparatusi. e., the change in light transmitting characteristics of the substance in tube 22 associated with the photoelecplane cabin.

tric'tube 56 necessary to operate a relay or the like. i

In adjusting the apparatus the adjustable connection I54 is first adjusted to balance the bridge circuit, after which the connector I62 is adjusted to bring the grid bias applied to grid i58 to a desired point below the value of plate current required to operate a relay I30 in the plate circuit of the tube. In the illustrated embodiment the relay includes a winding I68 and a normally closed contact I10. The winding I68 is connected to the positive terminal'of the usual 24 volt supply found on the airplane through a normally closed relay resetting switch I12 and a main switch I14, which is closed when the apparatus is in operation.

One of the features of the present invention, as already indicated, resides in the effective utilization of the low voltage supply of the airplane. To provide a suflicient negative bias to the grid of the control tube independently of the flow of current through the tube, there is provided a bleeder resistor I16 connected to the positive power supply line through conductor I18 and to the cathode I66 by a conductor I80. The current through the bleeder resistor thus flows through the bias resistor I36 to the negative power supply conductor I80. The cathode heater I82 is connected across the power supply lines H4 and I86 by the conductor I18 and a conductor I84.

The relay switch I18 may be utilized to control a suitable indicating device or some device controlling the flow of heated air into the air- In the indicated arrangement the switch controls the warning light I86, which is normally connected across the power supply lines through the switch I18 and a current limiting resistor I88.

Before proceedin with the description of the alternate forms of circuit, it is thought best to review the operation of the embodiment of the invention described above. illustrated in Fig. 1 is utilized, then fresh air obtained from the inlet conduit I6 is passed through the sensitive substance containing tube 26 and air obtained from the hot air duct I8 is passed through the sensitive substance-containing tube 22, through the passages heretofore described in detail. Or, if the arrangement of Fig. 2 is utilized, air from outdoors is passed through the tube 28, and air from within the cabin is passed through the tube 22. In either case, the air flows through the tubes at a relatively slow velocity and the two air samples are brought to approximately the same temperature by passing the air through the heat exchanger 32. Alcohol or gasoline vapors are removed from the air stream by the silica gel in the instrument entrance tubes 28 and 40, which are located just ahead of the heat exchanger.

The light source 52 is usually energized continuously although, if desired, it can be energized simultaneously with the remainder of the apparatus through the power switch H14. Light from the lamp passes through the portions of tubes 20 and 22 containing the substance sensitive to carbon monoxide and impinges upon the photoelectric cells 54 and 56.

It is possible to insert new tubes 20 and 22 at desired intervals or just before each flight of the airplane, in order to make certain that the tubes have not been previously discolored. If they have not been discolored, then they both possess the same light transmitting character- If the installation of small quantities of carbon istics with the result that the photoelectric tubes have the same amount of light impinging thereon. However, if the light transmitting characteristics are not exactly the same, the bridge circuit may be balanced by adjustment of the connection I54. When so balanced any gradual drift or change in color of the carbon monoxide sensitive substance will not afiect the flow of current through the relay winding I63, since the currents flowing through the resistor portions III-A and I5ll-B are equal and opposite. Consequently, the potential applied to grid I58 is unafiected by the drift or change in color.

The sensitivity of the apparatus is readily adjustable by movement of connection I62 to vary the effective portion of the voltage drop across bias resistor I36 applied to the grid I553. The grid is biased to a desired point-usually a point just below that at which the flow of current through the relay winding I68 is insuflicient to operate the relay. This grid potential is such that current normally flows through the relay winding and also through the tube and the bias resistor. This current how is, however, insufiicient to provide the necessary bias for the grid, but the flow of current through the bias resistor is increased and made more constant by use of the bleeder resistor I76.

When there is no carbon monoxide present in the heated air, the light I86 is connected across the power supply lines by the relay switch Ill! and glows continuously. However, when there is carbon monoxide present in the heated air, as might be the case when the heat exchanger is punctured by a bullet, then the carbon monoxide changes the light transmitting characteristics of the sensitive material in the tube 22. As a result less light passes through the tube and the photoelectric tube 56 produces a smaller electron flow. The net result is that the current flow through the local circuit connected across battery I32 and including the tube 56 and resistor portion I5flB is reduced. This reduction in current flow through resistor portion I5ll-B results in the application of an increased positive potential on the grid I58, with the further result that the tube I28 becomes more conductive. As the current flow through the tube I23 increases to a point determined by the sensitivity adjustment, the relay winding Hi8 becomes energized sufiiciently to open the switch I'm whereupon the lamp I86 is disconnected from its power supply to give an indication of the presence of carbon monoxide.

An apparatus constructed in accordance with this invention has proved to be very sensitive and, indeed, is capable of detecting the presence monoxide in a relatively short period. Y

After operation of the relay, the apparatus may be reset for further detection and indication of the presence of carbon monoxide upon balancing the bridge circuit, which is accomplished by adjustment of the connection I54, and the momentary opening of switch I72. The switch H2 is provided so that the relay may be reset without cutting down the current flow through the tube by adjustment of the grid bias to a value below the release current of the relay, which is usually much less than the operating current. If the switch were not provided, it would be necessary to adjust the bias resistor I 35 to some point whereat the current flow through the tube would be cut down to an extent suilicient to release the relay.

The balanced bridge circuit arrangement may be arranged to maintain the relay in its operated position when the amount of carbon monoxide does not exceed some predetermined value and to release the relay when the amount of carbon monoxide exceeds the aforesaid value. An advantage of this type of circuit arrangement is that it indicates also whether or not the circuit is operative, since, if the circuit should be inoperative, the relay is released to give an indication. An arrangement of this character is illustrated in Fig. 8, to which reference is now had.

The circuit of Fig. 8 corresponds quite closely to that illustrated in Fig. 7 with exception of the adjustment of the sensitivity control I62 relative to the bias resistor I36 and in the transposition of the photoelectric tubes 54 and 56. The aforesaid adjustment is so made that the normal grid potential maintains the relay operated switch lit in its operated position, whereb the signal lamp I 86 is normally lightedin other words, the grid is normally more positive than in the first described embodiment and is rendered more negative when the presence of carbon monoxide is detected. The photoelectric tube 55 is placed in series with resistor portion I 5Ii-A so that when less light is transmitted to the tube as carbon monoxide changes the color of the sensitive gel in tube 22, less current flows through the resistor portion I5IlA and the grid I 58, which is connected to the junction of the cell and resistor portion, is rendered more negative. Thus, when the unbalance reaches a point determined by the setting of the grid bias adjustable connection I62, the flow of current through the relay winding I68 is decreased to a point where the switch I'II] is released and the lamp I86 de-energized to give an indication of the presence of carbon monoxide.

In order to reset the relay without the necessity of increasing the flow of current through the electron tube I28 to a high value, there is provided a normally open switch I90 which, when closed, connects the relay winding across the power supply lines through a current limiting resistor 592; thus, momentary closure of the switch I!!!) after the bridge has been rebalanced resets the apparatus for a further detection operation.

The balanced bridge circuit arrangement'may also be used in connection with gas tubes, as illustrated in Fig. 9, wherein a gas tube Bill! of the 2051 type is used. The bridge circuit of this arrangement is identical with that illustrated and described in the embodiment of Fig. 7, i. e., the photoelectric cell 54 is connected, in series with resistor portion I5i3-A, while the photoelectric cell "ili is connected in series with resistor portion ltd-B. The junction of resistor I5IlA and cell as is also connected to the grid 262 of the gas tube and the junction of resistor portion I5@-B and cell Elli is connected by conductor 2G4 to an adjustable contact 2% associated with a bias resistor 208. The cathode ZIEl of the tube is connected by a conductor 2I2 to the resistor and the cathode heater 2M is also connected across a portion ofthe resistor by the conductors The lamp 5?! associated with the photoelectric cells is connected. between the upper terminal and the bias resistor 208 and the positive power supply line through a resistor 2 I8.

The relay winding IE3 is in circuit with the anode 22b of the tube and the relay switch I'II! controls a circuit 222 leading to a signal light or to some device for controlling the operation of the heater or the supply of heated air into the cabin.

. ll V In order to neutralize stray electron grid current and to provide a more perfect balancing of the bridge circuit, there is provided a neutralizing circuit between the anode and the grid in- :cluding a high resistance resistor 224. This resistor is desirable in some cases and not necessary in others, dependent upon the characteristics of particular tubes.

The'bridge circuit of the embodiment of Fig. 9 is balanced and the sensitivity adjusted in the same manner as these adjustments are made in the previously described embodiments. When the bridge circuit becomes unbalanced because of less light being transmitted to photoelectric cell 54, the grid 262 of the gas tube is rendered -more positive with the result the relay winding 168 is energized more strongly until, at a point determined by the sensitivity adjustment 2%, the relay operates to close switch we to indicate the presence of carbon monoxide or to shut off the supply of heated air or the like. If desired, the apparatus may be utilized to perform both functions, that is, both to give the signal and to operate some control apparatus to shut off the supply of heated air into the interior of the cabin.

From the foregoing detailed description of the details of apparatus embodying the invention, it 'may-be noted that the apparatus may take various forms. It should be understood, therefore, the details of the variousembodiments are not intended to be limitative of the invention except in so far as set forth in the accompanying claims.

Having thus described our invention what we claim as new and desire to secure by Letters Patent of the United States is:

1. Apparatus for detecting the presence of a contaminating substance in a, gas which comprises means forming a case, a light source disposed within said case, a housing enclosing said light source, said housing having a pair of open- .ings therein substantially equally spaced from said source, a pair of photosensitive devices disposed beyond said openings and adapted to receive light fromv said light source each through one of said openings, shielding means to exclude light from said photosensitive devices other than .light passing through said openings, a pair of glass tubes larger in diameter than said openings, means forming guides to facilitate positioning of said glass tubes before said openings so that all of the light. passing through one of said openings passes through one of said tubes while light passing through the other. of said openings passes through the other of said tubes, sockets disposed beyond said guide means and adapted to embrace one end each of said tubes in airtight engagement so that said tubes can be inserted in said guide means with one end engaged in said sockets, each of said tubes containing a substance which undergoes a photocharacteristic change in the presence of .the contaminant to be detected, a pair of inlet fittings disposed on said case, one of said fittings ,being adapted for connection to a source of gas known not to be contaminated and the other of said fittings being adapted for connection to a, source of gas to be tested for the contaminant, conduit means connecting one of said fittings to one of said sockets and the other of said fittings to the other of said sockets, said conduits comprising together a heat exchanger to exchange heat from one of said conduits to the other of said conduits so as to equalize the temperature of gases flowing through said conduits, circuit means including amplifying means for balancing the outputs of said photoelectric devices against each, other and relay means operable upon a predetermined amount of unbalance in said outputs, said relay being adapted for actuating an alarm when so operated, and circuit means for energizing said light source.

2. Apparatus for detecting the presence of a contaminating substance in a gas which comprises means providing a light source, a housing enclosing said light source, said housing having a pair of openings therein, a pair of photosensitivedevices disposed beyond said openings and adapted to receive light from said light source each through oneof said openings, a pair of glass cells sufficiently large to cover said openings, means forming guides to facilitate removable positioning of said glass cells before said openings so that all of the light passing through one of said openings passes through one of said cells while light passing through the other of said openings passes through the other of said cells, sockets adapted to connect to one end of each of said cells in airtight engagement so that said cells can be easily inserted in said guide means with one end engaged in said sockets, each of said cells containing a substance which undergoes a photocharacteristic change in the presence of the contaminant to be detected. a pair of inlet fittingsone of said fittings being adapted for connection to a source of gas known not to be contaminated and the other of said fittings beind adapted for connection to a source of gas to be tested for the contaminantconduit means connecting one of said fittings to one of said sockets and the other of said fittings to the other of said sockets, circuit means for energizing said light source and for balancing the outputs of said photoelectric devices against each other and including means operable upon a predetermined amount of unbalance in said outputs, the last said means being adapted for actuating an alarm when so operated, whereby gradual change in the photocharacteristic of said substance due to aging will not operate the last said means but relative change due to contamination of one of said gas sources will operate the last said means.

WILLARD H. FARR.

WILLIAM F. FAGEN.

STANLEY C. KOLANOWSKI.

REFERENCES CITED The following references are of recordin the file of this patent:

UNITED STATES PATENTS Number Name Date 1,594,264 Howard July 27, 1925 1,919,858 Pettingill July 25, 1933 1,943,684 Martin et al. Jan. 16, 1934 1,977,359 Styer Oct. 16, 1934 1,993,665 Holt Mar. 5, 1935 2,019,871' Pettingill Nov. 5, 1935 2,036,251 Boynton Apr. 7, 1935 2,111,301 Schroter -2. Mar. 15, 1933 2,123,573 McFarlan et a1. July 12, 1933 2,411,672 Van Den Akker Nov. 26, 1945

Claims (1)

1. 2. APPARATUS FOR DETECTING THE PRESENCE OF A CONTAMINATING SUBSTANCE IN A GAS WHICH COMPRISES MEANING PROVIDING A LIGHT SOURCE, A HOUSING ENCLOSING SAID LIGHT SOURCE, SAID HOUSING HAVING A PAIR OF OPENINGS THEREIN, A PAIR OF PHOTOSENSITIVE DEVICES DISPOSED BEYOND SAID OPENINGS AND ADAPTED TO RECEIVE LIGHT FROM SAID LIGHT SOURCE EACH THROUGH ONE OF SAID OPENINGS, A PAIR OF GLASS CELLS SUFFICIENTLY LARGE TO COVER SAID OPENINGS, MEANS FORMING GUIDES TO FACILITATE REMOVABLE POSITIONING OF SAID GLASS CELLS BEFORE SAID OPENINGS SO THAT ALL OF THE LIGHT PASSING THROUGH ONE OF SAID OPENINGS PASSES THROUGH ONE OF SAID CELLS WHILE LIGHT PASSING THROUGH THE OTHER OF SAID OPENINGS PASSES THROUGH THE OTHER OF SAID CELLS, SOCKETS ADAPTED TO CONNECT TO ONE END OF EACH OF SAID CELLS IN AIRTIGHT ENGAGEMENT SO THAT SAID CELLS CAN BE EASILY INSERTED IN SAID GUIDE MEANS WITH ONE END ENGAGED IN SAID SOCKETS, EACH OF SAID CELLS CONTAINING A SUBSTANCE WHICH UNDERGOES A PHOTOCHARACTERISTIC CHANGE IN THE PRESENCE OF THE CONTAMINANT TO BE DETECTED, A PAIR OF INLET FITTINGS, ONE OF SAID FITTINGS BEING ADAPTED FOR CONNECTION TO A SOURCE OF GAS KNOWN NOT TO BE CONTAMINATED AND THE OTHER OF SAID FITTINGS BEIND ADAPTED FOR CONNECTION TO A SOURCE OF GAS TO BE TESTED FOR THE CONTAMINANT, CONDUIT MEANS CONNECTING ONE OF SAID FITTINGS TO ONE OF SAID SOCKETS AND THE OTHER OF SAID FITTINGS TO THE OTHER OF SAID SOCKETS, CIRCUIT MEANS FOR ENERGIZING SAID LIGHT SOURCE AND FOR BALANCING THE OUTPUTS OF SAID PHOTOELECTRIC DEVICES AGAINST EACH OTHER AND INCLUDING MEANS OPERABLE UPON A PREDETERMINED AMOUNT OF UNBALANCE IN SAID OUTPUTS, THE LAST SAID MEANS BEING ADAPTED FOR ACTUATING AN ALARM WHEN SO OPERATED, WHEREBY GRADUAL CHANGE IN THE PHOTOCHARACTERISTIC OF SAID SUBSTANCE DUE TO AGING WILL NOT OPERATE THE LAST SAID MEANS BUT RELATIVE CHANGE DUE TO CONTAMINATION OF ONE OF SAID GAS SOURCES WILL OPERATE THE LAST SAID MEANS.

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