This invention relates generally to the measurement and/or measuring of gas atmospheres used in conjunction with heat treating apparatus.
In a typical heat treatment system a single gas or a mixture of gasses, comprise the heat treating atmosphere. The flow rate of these gasses are typically sensed by rotometers. The rotometer can include a visual flow indicator, which comprises a ball or float that is lifted within a tapered tube by the moving/flowing gas volume, the amount of the lift being proportional to the magnitude of the gas flow rate. A rotometer of this kind can be purchased, e.g., from Waukee Engineering Company, Inc, Milwaukee, Wis.
A rotometer needs to be calibrated for a specific gas at a known gas temperature and a known gas pressure to accurately correlate the lift distance of the ball or float within the tube to the gas flow rate. However, ambient changes in gas temperature and/or gas pressure can, or course, alter this correlation and lead to incorrect indicated readings.
Mass flow meters are used outside the heat treating field for measuring and controlling the specific amount of flow of a fluid, necessary for a particular process, e.g., in semiconductor manufacturing processes, such as chemical vapor deposition or the like. Mass flow controllers are known to be capable of sensing the flow occurring through the controller and modifying or controlling that flow as necessary to achieve the required control of the flow rate of the fluid delivered to the particular process. Mass flow controllers are not sensitive to gas temperature variations and/or gas pressure variations.
According to conventional wisdom, mass flow controllers require low volume, laminar (i.e., non-turbulent) gas flow conditions, to assure a linear relationship between monitored mass flow and actual gas flow rate. Laminar flow conditions require relatively large inlet pressures and can lead to relatively large pressure drops across the mass flow controller. On the other hand, heat treating is characterized by the existence of high volume, turbulent flow conditions. These conditions are not laminar and do not accommodate the large pressure drops required for mass flow measurements.
By way of example, in heat treating, gas flow into the heat treating furnace is typically turbulent, and at relatively low pressures, e.g., <1 psi, and occurs at relatively high flow volumes, which are measured in cubic feet per hour (CFH) with magnitudes of several hundred CFH and often much higher, e.g., 1000 to 5000 CFH. In contrast, in a semiconductor manufacturing process, laminar (non-turbulent) flow conditions and significantly lower flow rates are encountered, which are measured in cubic centimeters per minute (cc/min), with magnitudes, e.g., up to about 100 cc/min. Thus, the flow volumes typically encountered in heat treating are at least three orders of magnitude higher than those encountered in semiconductor manufacturing conditions.
Thus, processing conditions typical for heat treating inherently mitigate against the use of conventional mass flow sensing devices.
One aspect of the invention provides systems and methods for measuring a gas flow rate—or that include a flow rate measuring assembly—which are based, at least in part, upon sensing of mass gas flow conditions.
In one embodiment, the flow rate measuring assembly shunts a relatively small volume of turbulent gas flow in a main flow path through a gas flow sampling path for mass flow measuring. The gas flow sampling path includes an in-line mass flow sensor. The low volume mass flow conditions within the sampling path mirror the turbulent flow conditions within the high volume main flow path. As a result, the raw output of the mass flow sensor in the sampling path is not linear with respect to the main gas flow rate. The flow rate measuring assembly includes a conversion function that electronically processes the raw non-linear output and converts it into a flow rate output that can be linearly related to the main flow rate with surprising accuracy.
In one arrangement, the conversion function can, e.g., include a correlation that fits the raw non-linear output of the particular mass flow sensor in use to a generalized linear construct or curve to yield a flow rate. The generalized linear construct or curve can be developed empirically to function with acceptable accuracy in association with a family or families of mass flow sensors, even though the outputs, given the same mass flow conditions, may vary somewhat among them. In this arrangement, the generalized linear conversion will also need to assume the same specific gravity or range of specific gravities conditions for the measured gas, as well as common units of measurement in which the outputs are expressed.
In another arrangement, the flow rate measuring assembly includes a compensation function. The compensation function generates a linear correlation between non-linear mass flow outputs of a given mass flow sensor in use and corresponding gas flow rates based upon actual existing gas flow conditions. The compensation function thereby develops for the conversion function a linear construct or curve that is reflects the actual gas flow conditions and the actual performance characteristic of the in-line mass flow sensor in use. Use of the compensation function eliminates loss of accuracy due to performance variations among different flow sensors, or variations in gas flow conditions, such as specific gravity for the measured gas, change or degradation of the sensor over time, or differences among units of measurement that may exist for the outputs of different types of mass flow sensors.
By physically placing the mass flow sensor in a gas flow sample path outside the main flow path, and by electronically processing the raw output of the mass flow sensor, the flow rate measuring assembly establishes a virtual laminar flow condition for the main flow, where there is a linear relationship between sensed mass flow and the actual gas flow rate.
The invention may be embodied in several forms without departing from its spirit or essential characteristics. The scope of the invention is defined in the appended claims, rather than in the specific description preceding them. All embodiments that fall within the meaning and range of equivalency of the claims are therefore intended to be embraced by the claims.
A heat treating atmosphere is conveyed through a supply line 14 into the furnace 12. A mixer 16 (e.g., a fan or the like) circulates the heat treatment atmosphere within the furnace 12.
A heat source 18 heats the interior of the furnace 12, and thus the heat treating atmosphere itself. The heated atmosphere reacts with rigid loads 64, e.g., metal, placed into the furnace 12, to achieve the desired heat treatment objectives.
A conventional in situ oxygen sensor 20, in association with a thermocouple, is typically installed in the heat treating furnace 12 in direct contact with the heated gas atmosphere. The sensor 20 outputs a voltage signal which is related to the condition of the gas atmosphere within the furnace 12, such as percent oxygen, dew point, or percent carbon. Maintaining the desired oxygen content at some specific temperature within the furnace controls the heat treating atmosphere. Metal Handbook, Vol. 4, pp. 417-431 (9th Edition 1981) contains a further discussion of atmosphere control in a heat treating furnace.
The system 10 includes sources 22, 24, 26, and 28 of the various gases that, when mixed, comprise the heat treating atmosphere. The type of source gases 22, 24, 26, 28 can vary according to the heat treatment objectives. For example, one of the source gases 22 can comprise an endothermic gas. Another source gas 24 can comprise natural gas. Another source gas 26 can comprise air (oxygen). Another source gas 28 can comprise ammonia. Other types of source gases can be used, depending upon the nature and type of heat treating desired.
The measured gases 22, 24, 26, and 28 are mixed within a manifold 30 and then conveyed by the supply line 14 to the furnace 12. Each source gas 22, 24, 26, and 28 is conveyed into the manifold 30 through an individual inlet line 32. As earlier explained, due to the nature of heat treating, flow within an individual inlet line 32 is characterized by turbulence, low pressure, and relatively high flow volumes, which are measured in cubic feet per hour (CFH) with magnitudes approaching 100 CFH and typically much higher, e.g., 1000 to 5000 CFH.
To control the relative high flow rates of gases 22, 24, 26, and 28 into the manifold 30, and thus the composition of the atmosphere itself, each individual inlet line 32 includes a control valve 34. The control valve 34 can be manually adjusted by an operator, or it can be electrically controlled from a remote control station.
To measure the flow rate, each inlet line 32 includes its own flow rate measuring assembly 36. The flow rate measuring assembly 36 senses the rate of gas flow through the line 32 and may provide an output related to the magnitude of the flow rate.
In the illustrated embodiment, at least one of the flow rate measuring assemblies 36 includes a mass flow sensor 38 (see
The flow rate measuring assembly 36 includes a signal processing device or microprocessor 42, which is coupled to the outlet of the mass flow sensor 38. The signal processing device 42 includes a conversion function that applies preprogrammed logic or an algorithm, to convert the output of the mass sensor 38 to a gas flow rate in the supply line 32.
The microprocessor 42 can include or otherwise be coupled to a display device 44, which visually displays the flow rate and other meaningful derived information, as well as to data registers 45, which collect and organize the data for off-line storage and/or printing for record keeping purposes. The microprocessor 42 can also be coupled by a feedback loop 70 to the control valve 34, to automatically maintain an actual flow rate according to a predetermined set point, and thereby provide automated control of gas delivery.
In one illustrated embodiment (see
To promote flow out of the main path 46 into the sample measuring path 47, the mass flow sensor 38 can also include a restricting orifice 48, which is positioned in the main path 46 of gas flow within inlet line 32 in juxtaposition with the sample measuring path 47. The orifice 48 creates a pressure differential between the inlet and outlet ends of the sample measuring path 47, which is believed to be helpful, particularly when the flow rates are low, e.g., about 100 CFH and below. At higher flow rate conditions within the main path 46, e.g., in excess of about 100 CFH, use of a restricting orifice 48 is optional.
In a representative embodiment, given a main flow path 46 having an area of about 0.4 in2, and the low volume sampling path 47 having an area of 0.003 in2, the orifice 48 can have a volume of about 0.2 in2, i.e., about half of the main flow path 46.
In the arrangement shown in
Alternatively, as shown in
The small diameter shunt lines 50 and 52 (on the upstream and downstream sides of the flow restricting orifice 48, if present) direct a fraction of the total flow of gas in the main path 46 through the temperature resistance device 40 for measurement. Conventional thought believes that laminar flow is a prerequisite for using conventional mass flow sensors. According to conventional thought, a laminar flow is required so that the output of the mass flow sensor is linearly proportional to the total flow. As
More particularly, the flow rate measuring assembly 36 includes a conversion function 80 that resides within the processing device 42 (see
In the illustrated embodiment, the conversion function 80 (see
Flow Rate=(M*X)+B
The table items for the linearization table 98 shown in
In the embodiment shown in
The compensation function 100 can operate in various ways. In the embodiment shown in
The compensation function 100 can also operate during the initialization or “teaching” mode based upon a manual selection of a process values (flows), and registering the corresponding sensor output when the desired process value (flow) is verified by other means. This registered value and the manually selected flow value is incorporated in the linearization table 98.
In this arrangement, a steel housing defines the passage 46. The orifice 48 is fitted into the housing 46 through a formed access opening 54. A top plate 56 and o-ring 58 fit over and seal the access opening 54. In this arrangement, gas flow in the passage 46 proceeds from inlet to outlet in a dog-leg path through the orifice 48, as shown by arrow 72.
The temperature resistance device 40 (which, e.g., can comprise a Mass Airflow Sensor AWM3100V made by Honeywell) is mounted on the top plate 56. The device 40 is enclosed within a formed top cover 78.
In this embodiment, the inlet shunt line 50 comprises a rigid tube 60 and a hose 62, which can be made of a flexible material but need not be. The rigid tube 60 has an end that extends into the top cover 78 near the temperature resistance device 40. The rigid tube 60 has another end that extends through the top plate 56 and opens into the gas passage 46 upstream of the orifice 48. The hose 62 couples the near end to the inlet of the temperature resistance device within the cover 78.
In this embodiment, the outlet shunt line 52 comprises a rigid tube 66 and a hose 68, which can be made of a flexible material but need not be. The rigid tube 66 has an end that extends into the top cover 78 near the temperature resistance device 40. The rigid tube 66 has another end that extends through the top plate 56 and opens into the gas passage 46 downstream of the orifice 48. The hose 68 couples the near end 70 to the outlet of the temperature resistance device 40 within the cover 78.
Lead wires 74 electrically connect the output of the temperature resistance device 40 to a plug 76 carried by the cover 78. A cable 82 inserted into the plug 76 couples the output of the temperature resistance device 40 to the microprocessor 42 (see
In the illustrated embodiment, the microprocessor 42 is also mounted to the assembly 90, so that the three components 38, 92, and 42 comprise an integrated unit. The microprocessor 42 can include an integrated display device 44, which displays the processed, linearized main flow rate based upon the measured sample of mass flow of gas through the mass flow sensor 38. It should be appreciated, however, that the microprocessor 42 and/or the display device 44 can be located remote from the joined assembly of the mass flow sensor 38 and the rotometer 92.
The assembly 90 combines traditional visual and/or non-electrically powered flow indication (i.e., the rotometer 92) with the output obtained by mass flow sensing (i.e., the mass flow sensor 38) in a convenient, compact package that can be easily handled and installed. Use of the mass flow sensor 38 provides the advanced benefits of digital mass flow technology. The flow rate information shown on a digital display 44 is immune to possible error from gas pressure and gas temperature variations. However, the presence of the rotometer 92 provides familiar visual and/or non-electrically powered flow indication and the benefits of well-known analog flow sensing technology. The assembly 90 provides the best of analog and digital worlds in a compact, convenient package.
The foregoing is considered as illustrative only of the principles of the invention. Furthermore, since numerous modifications and changes will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation shown and described. While the preferred embodiment has been described, the details may be changed without departing from the invention, which is defined by the claims.
This application claims the benefit of U.S. Provisional Patent Application Ser. No. 60/611,903, filed Sep. 21, 2004, titled “Systems and Methods for Sensing and/or Measuring Flow Rate of Gases Based Upon Mass Flow in Heat Treating Environments.”
Number | Date | Country | |
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60611903 | Sep 2004 | US |