GB1588478A

GB1588478A - Gas flow control apparatus

Info

Publication number: GB1588478A
Application number: GB24664/78A
Authority: GB
Original assignee: Perkin Elmer Corp
Current assignee: Applied Biosystems Inc
Priority date: 1978-05-22
Filing date: 1978-05-30
Publication date: 1981-04-23
Also published as: DE2833553A1; AU516406B2; CA1108432A; IT7949134A0; IT1116208B; JPS54161989A; AU3771478A; DE2833553C2; JPS6128293B2

Description

(54) GAS FLOW CONTROL APPARATUS (71) We, THE PERKIN-ELMER CORPORA TION, a Body Corporate organised and existing under the laws of the State of New York, United States of America, having a principal place of business at Main Avenue, Norwalk Connecticut 06856, United States of America do hereby declare the invention, for which we pray that a patent may be granted to us and the method by which it is to be performed, to be particularly described in and by the following statement:- This invention pertains generally to automatic gas flow control systems and particularly to such systems for burners used in atomic absorption spectroscopy.

In atomic absorption spectroscopy the measurement of the absorption of a radiation beam at a characteristic resonant spectral line for a particular element yields a measure of the concentration of that element in an original sample solution. Presently the most common technique for atomizing an element for purposes of the absorption measurement, is by introducing a liquid sample solution of the element of interest into a gas burner wherein droplets of the solution are vaporized and the elements ultimately atomized, so as to form in the path of the apparatus radiation beam, a substantial quantity of the element of interest in its atomic state.

In order to effect appropriate burning of the element containing solution, the liquid must be converted into a fine spray by means of a nebulizer and then mixed with a fuel and oxidant gas before introduction into the burner. A nebulizer generally employs a venturi-type restriction which passes rapidly moving gas (hereinafter referred to as an oxidant) past an opening, drawing a portion of the liquid sample solution into the gas stream, effecting an atomizing of the liquid in the process. The liquid is said to be aspirated by the venturi effect caused by the rapidly moving current of gas. The sample laden gas or oxidant then passes into the burner chamber where it is mixed with additional oxidant from an auxiliary inlet, and fuel such as acetylene. It is then introduced into the burner head where it is ignited.

The sensitivity of the absorption measurement is dependent on many factors, one of which being the flame condition of the burner, i.e. the leanness or richness of the fueloxidant mixture. Also the sensitivity of the measurement requires the optimization of the setting of the nebulizer which varies the amount of liquid sample aspirated by the rapidly flowing gas. Because of the nature of the mechanism for aspirating more or less of the sample, namely varying the flow of oxidant through the venturi-type restriction, there is the obvious side effect on the flame condition which has a direct effect on the sensitivity of the measurement. In prior systems, the operator had to go back to the auxiliary inlet to the burner and vary the oxidant flow through it to compensate for the last adjustment to the nebulizer and the effect thereof on the oxidant flow into the burner.

The object of the invention is to eliminate the need for these re-adjustments due to the adjustments of the nebulizer. Thus, according to the invention an automatic gas flow control apparatus for an atomic absorption spectrometer system, including a burner for burning a mixture of fuel, oxidant and a sample containing an unknown element, comprises means for supplying a predetermined flow of fuel to the burner, means for supplying sample to the burner under the control of a first flow of oxidant which also passes to the burner, means for adjusting the first flow of oxidant so as to adjust the flow of sample and means for providing a second flow of oxidant to the burner which is controlled in accordance with variations in the flow of oxidant controlling the sample so that the total flow of oxidant to the burner remains substantially constant.

The two oxidant supplies preferably pass along separate respective conduits, the means for adjusting the second flow of oxidant including a sensor for sensing the first flow of oxidant through the respective conduit and means for adjusting the second flow of oxidant in response to the output of the sensor to compensate for changes in the first flow of oxidant.

An example of a control system in accordance with the invention will now be described, with reference to the accompanying drawings, in which: Figure 1 is an elevation of a nebulizerburner assembly, typically employed in atomic absorption spectrometer instrumentation; and Figure 2 is a block diagram of the gas control system.

Referring now to Figure 1, there is shown a typical nebulizer-burner assembly used in atomic absorption spectroscopy. It includes a chamber 10 for mixing fuel, oxidant and the unknown element-containing sample. The chamber feeds the burner 12 which ignites the fuel, oxidant and sample mixture. Feeding the chamber is a fuel line 14 which supplies a suitable gas, e.g. acetylene, from a regulated source.

Axially connected to the chamber 10 is a nebulizer 16. The internal configuration of the nebulizer is not shown, but is understood to be operatonal in a manner similar to many such devices on the market. The nebulizer introduces a variable flow of the unknown element-containing sample into the mixing chamber.

The sample solution is contained in a beaker such as 18. Typically the sample is an unknown metallic element in solution. The aspirating action of the venturi-type restriction in the nebulizer draws solution out of the beaker through capillary tubing 20. The aspiration of the sample is achieved by rapidly-moving gas, typically traveling through the venturi restriction, which draws the solution into the nebulizer and atomizes it into a fine spray. The rapidly-moving gas enters the nebulizer via tubing 22. Generally, this gas is referred to as the oxidant. In a typical situation, it might be nitrous oxide or, air.

To adjust the nebulizer for most efficient sample aspiration, the operator of the equipment, for the unit shown, would turn knob 24. This would alter the flow of sample into the assembly, but because of the nebulizer design, there will be a corresponding effect on the flow of the oxidant entering the nebulizer through tubing 22. The adjustment of the nebulizer by the operator for an optimum measured signal in the spectrophotometer will vary from unit to unit, so that differing effects on the oxidant flow rate through tubing 22 will result. Since the amount of oxidant supplied to the burner is altered, the flame condition and thus the signal measurement would be altered except for the present invention.

The nebulizer, typically, is axially joined to the mixing chamber by a sealing interface at 26.

Connected to the mixing chamber is a variable (auxiliary) supply of oxidant. This is provided through tubing 28. As will be seen hereafter in the discussion of Figure 2, the amount of oxidant supplied at this point will be equal to the difference between the total flow of oxidant predetermined, for example, by a methods analyst as necessary to insure a prescribed sensitivity, and the varying amount supplied to the chamber by the nebulizer.

In order to sense the flow of oxidant supplied to the nebulizer, in-line means, such as a restrictor, is inserted in the oxidant supply tubing 22. The restrictor is shown at 30.

The flow rate is sensed by monitoring the pressure on either side of the restrictbr. This is accomplished by pressure monitoring ports 32 and 34, connected into the tubing 22 and 82 respectively. For the indicated flow direction for the oxidant, the pressure at terminal 34 would be higher than the pressure at 32.

Ports 32 and 34 are shown as being directed to a so-called "computer relay" whose operation as it concerns the gas flow control system of the invention will be discussed with respect to Figure 2. Generally, its function is to compare the pressure differential across the restrictor 30 to a predetermined command pressure based on a prescribed sensitivity of the spectrometer and to adjust the oxidant flow between the auxiliary inlet (hereinabove referred to as inlet 28) and the nebulizer inlet (hereinabove referred to as inlet 22) to compensate for the variations of oxidant flow in 22 due to nebulizer adjustments at knob 24.

Referring now to Figure 2, there is shown in block diagram form, an arrangement of the various pneumatic components which effect the purposes of the invention. The few situations where reference numerals are identical to those employed in Figure 1, those are done to identify the same identical components or tubing even though in this latter figure they are a block diagram equivalent.

Considering the fuel supply section initially, the burner fuel, acetylene, is supplied to the system via tubing 36. Acetylene is employed because it is readily available and inexpensive.

Tubing 36 is connected to a pressure switch 38 which senses a safe level before closing.

Typically, the acetylene at the input might be of the order of 15 psig, and the threshold pressure of the switch 38 set at 7 psig. The switch directs the fuel to a pair of solenoids via tubing 40 and 42. The first such solenoid 44 is energized at start up and directs the fuel through tubing 46 to the igniter section of the burner. Once ignited, solenoid 44 is opened and the fuel is blocked from that passageway.

During subsequent burner operation, sole noid 48 is closed and the fuel directed therethrough to tubing 50 and pressure regulator 52. The output of the regulator 52, typically, would have a fuel gas pressure at 12 psig.

This pressure level is the maximum that can be employed in the burner because of the instability of acetylene above that pressure.

The regulator is connected to a volume booster 56 by tubing 54. The regulator responds to a command pressure on line 58, in order to further reduce the pressure of the acetylene from 12 psig down to a value determined previously to be optimum for spectrometer sensitivity. For example, the pressure of the gas in tubing 57, typically, will be at 6 psig. The tubing 57 is connected to the fuel inlet duct 14 previously referred to in Figure 1.

The command pressure input to the volume booster 56 is supplied by a voltage to pressure transducer 60. The latter receives an analog signal on input line 62 from a digital to analog converter 64. The D/A converter is supplied, via line 66, with a digital word permanently stored on a typical memory device such as a magnetic card or disc. The digital word represents the optimum flow of the fuel as previously determined by a methods analyst in arriving at optimum parameters for the system.

The volume booster, in a situation where acetylene is employed, for example, is a nonrelieving type, i.e., it would bleed off the necessary amount of acetylene into the burner to achieve the commanded pressure differential and not into the air as might be the case with relieving-type boosters.

The analog signal appearing on line 62 to the transducer 60, typically, is of the order of 0 to 9 volts, with the corresponding pressure out of the transducer in tubing 58, between 3 and 15 psig.

Thus there has been described means for supplying a predetermined flow rate of fuel for the burner in response to a preexisting command. Thus optimization of a critical parameter is assured.

The total oxidant supply to the system appears in tubing 68 and uses as its source either a supply of nitrous oxide entering on line 69, through pressure switch 70 and solenoid 72, or air in line 73 through pressure switch 74 and solenoid 76. The pressure switches 70 and 74, typically, have a setting at 25 psig. Depending on the oxidant to be use, either solenoid 72 or 76 would be selected by appropriate control.

The oxidant in tubing 68 is supplied to a pressure regulator 78 which maintains a pressure level in tubing 80 at, typically, 32 psig. Tubing S0 is connected by a T-connection to tubing 82 and 84. Tubing 82 (previously referred to with respect to Figure 1) is connected to restrictor 30. As discussed earlier the down stream side of the restrictor is supplied to the oxidant inlet on the nebulizer via tubing 22.

86 refers to a pneumatic computing means, known typically as a computing relay, which is generally of a non-relieving type. The computing relay includes an oxidant inlet port, S, and outlet port, P. These are connected, respectively, to tubing 84, the variable oxidant flow supply, and the auxiliary inlet 28, to the mixing chamber.

Further, the relay includes ports C and A which are connected respectively to the pressure monitoring ports on either side of the in-line restrictor 30.

Also, the computing relay includes a command pressure port B which is connected to a command pressure supply in line 88 which emanates from a voltage-topressure transducer 90. The latter provides a command pressure on its output from, typically, 3 to 15 psig in response to an analog signal of 0 to 9 volts, as received on input line 92. The analog signal is produced by a digital to analog converter 94 and is proportional to a predetermined digital word received on input electrical line 96. The digital word appearing in line 96 would be stored, much like the signal representing the predetermined fuel rate on a memory device such as a magnetic card or disc. Its value, again, would be previously determined by a methods analyst in arriving at optimum values for the various parameters necessary to be considered in optimizing the sensitivity of the instrument.

The input pressure supply for the voltage transducer 90, and the previously described transducer 60, is developed from an air supply line and is supplied to the transducer 90 by line 98. Line 98 is connected to a pressure regulator 100 which is connected by line 102 to the previously discussed pressure switch 74 in the air input line. The regulator 100 maintains the pressure in lines 98 and 104, the supply lines for the transducers, at an adequate pressure necessary for the command function performed by each. Typically, the pressure in those lines might be of the order of 20 psig.

The computing relay is a well known device which employs chambers and diaphragms to solve the equation P--A+B-C+K.

Where P is the pressure in the oxidant outlet port, A and C are the pressures on either side of the line restrictor, and B is the command pressure out of transducer 90.

K is an offset which is effected by a mechanical adjustment on the computing relay unit. It is set initially so as to ensure a sufficient pressure at port P, to provide the lowest flow rate of oxidant in response to the lowest digital command in line 96.

The computing relay is thus seen to perform the function of sensing and comparing the flow of oxidant to the nebulizer and the auxiliary oxidant supply means to a predetermined command flow rate for the oxidant as represented by the pressure on line 88. The relay adjusts the flow of oxidant to the auxiliary inlet in response to this comparison and does so and continues to readjust the flow thereto as it senses variations in the flow to the nebulizer across the restrictor 30.

Other variations of the above embodiment will be apparent in the light of the above.

For example, instead of employing a computing relay, means for sensing the flow of oxidant to the sample introducing means (nebulizer), in oxidant supply line, 22, and as well as means sensing the flow in line 28 could be employed. These might, typically, produce electrical signals which would then be compared with the command electrical signal. Valves in each of the supply lines could be provided which would be operated upon by the compared electrical signals so as to vary the amount of oxidant flowing into the auxiliary based on the compared readings.

The advantage of the present technique, is that the computing relay can both sense the variations in oxidant flow to the nebulizer and effect an adjustment in accordance therewith to the oxidant flow to the auxiliary inlet.

WHAT WE CLAIM IS: 1. An automatic gas flow control apparatus for an atomic absorption spectrometer system, including a burner for burning a mixture of fuel, oxidant and a sample containing an unknown element, the apparatus comprising means for supplying a predetermined flow of fuel to the burner, means for supplying sample to the burner under the control of a first flow of oxidant which also passes to the burner, means for adjusting the first flow of oxidant so as to adjust the flow of sample and means for providing a second flow of oxidant to the burner which is controlled in accordance with variations in the flow of oxidant controlling the sample so that the total flow of oxidant to the burner remains substantially constant.

2. Apparatus according to claim 1 wherein the two oxidant supplies pass along separate respective conduits, the means for adjusting the second flow of oxidant including a sensor for sensing the first flow of oxidant through the respective conduit and means for adjusting the second flow of oxidant in response to the output of the sensor to compensate for changes in the first flow of oxidant.

3. Apparatus according to claim 2 wherein the sensor includes a restriction in the conduit carrying the first flow of oxidant for developing a pressure differential thereacross proportional to the flow of oxidant therethrough and pressure monitoring means coupled across the restriction to control the means for adjusting the second flow of oxidant.

4. Apparatus according to claim 3 and also including means for providing a reference pressure signal, th means for adjusting the second flow of oxidant being responsive both to the reference pressure signal and a signal from the pressure monitoring means to adjust the second flow of oxidant to satisfy the equation P=A+B-C, where P is the pressure of the oxidant supplied to the burner in the second flow, B is the reference signal pressure and A and C are the pressures on the respective opposite sides of the restriction.

5. Apparatus according to claim 4 in which the means for adjusting the second flow of oxidant comprises a pneumatic computing relay including inlet and outlet ports for the oxidant whose flow is to be adjusted and means responsive respectively to the reference pressure signal and to the pressure differential across the restriction whereby to adjust the flow of oxidant in accordance with the said equation.

6. Apparatus according to claim 5 wherein the computing relay includes means for its mechanical adjustment whereby the pressure at the oxidant outlet port can be adjusted to assure the lowest required flow rate of oxidant therethrough for the minimum command pressure.

7. Apparatus according to any one of claims 4 to 6 further comprising a transducer for deriving the reference pressure signal from a corresponding electrical signal.

8. Apparatus according to any one of the preceding claims wherein the fuel supply is controlled by means responsive to pneumatic pressure derived from a transducer supplied with an electrical signal representing the predetermined flow of fuel.

**WARNING** end of DESC field may overlap start of CLMS **.

Claims

**WARNING** start of CLMS field may overlap end of DESC **. auxiliary oxidant supply means to a predetermined command flow rate for the oxidant as represented by the pressure on line 88. The relay adjusts the flow of oxidant to the auxiliary inlet in response to this comparison and does so and continues to readjust the flow thereto as it senses variations in the flow to the nebulizer across the restrictor 30. Other variations of the above embodiment will be apparent in the light of the above. For example, instead of employing a computing relay, means for sensing the flow of oxidant to the sample introducing means (nebulizer), in oxidant supply line, 22, and as well as means sensing the flow in line 28 could be employed. These might, typically, produce electrical signals which would then be compared with the command electrical signal. Valves in each of the supply lines could be provided which would be operated upon by the compared electrical signals so as to vary the amount of oxidant flowing into the auxiliary based on the compared readings. The advantage of the present technique, is that the computing relay can both sense the variations in oxidant flow to the nebulizer and effect an adjustment in accordance therewith to the oxidant flow to the auxiliary inlet. WHAT WE CLAIM IS:

1. An automatic gas flow control apparatus for an atomic absorption spectrometer system, including a burner for burning a mixture of fuel, oxidant and a sample containing an unknown element, the apparatus comprising means for supplying a predetermined flow of fuel to the burner, means for supplying sample to the burner under the control of a first flow of oxidant which also passes to the burner, means for adjusting the first flow of oxidant so as to adjust the flow of sample and means for providing a second flow of oxidant to the burner which is controlled in accordance with variations in the flow of oxidant controlling the sample so that the total flow of oxidant to the burner remains substantially constant.