US2586899A - Gas analysis apparatus - Google Patents

Gas analysis apparatus Download PDF

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US2586899A
US2586899A US703980A US70398046A US2586899A US 2586899 A US2586899 A US 2586899A US 703980 A US703980 A US 703980A US 70398046 A US70398046 A US 70398046A US 2586899 A US2586899 A US 2586899A
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gas
pressure
gases
temperature
heat
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US703980A
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Florian F Yanikoski
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N11/00Investigating flow properties of materials, e.g. viscosity, plasticity; Analysing materials by determining flow properties
    • G01N11/02Investigating flow properties of materials, e.g. viscosity, plasticity; Analysing materials by determining flow properties by measuring flow of the material
    • G01N11/04Investigating flow properties of materials, e.g. viscosity, plasticity; Analysing materials by determining flow properties by measuring flow of the material through a restricted passage, e.g. tube, aperture
    • G01N11/08Investigating flow properties of materials, e.g. viscosity, plasticity; Analysing materials by determining flow properties by measuring flow of the material through a restricted passage, e.g. tube, aperture by measuring pressure required to produce a known flow

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  • This invention relates to gas analysis apparaf tus of the type that continuously 'determines the percentage of one gas in a mixture of two or more gases.
  • One object of the invention' is to provide a gas analysis apparatus capableof Avery high speeds in responding to a change in the corniposition of the sample.
  • Another object is to provide an apparatus of simple construction which provides accurate analyses substantially independent of the temperature and pressure of the surrounding atmosphere.
  • Still vvanother object is to provide an apparatus capable o f safely analyzing explosive mixtures of gases.
  • Still -another object is to provide a gas analysis apparatus which utilizes the fact that the relaitive viscosities of gases change as a function 'of temperature.
  • Still another object is to provide an apparatus which utilizes the fact'thatth viscosity of gas apparently changes when the width of the flow path is reducedy to values approaching that of the mean free moleculair path.
  • Fig. 1 is a sectional view of the preferred form ofthe invention shown connected to one type of pressure differential indicator;
  • Fig. 2 is an exploded view of some o f the parts shown in Fig. 1;
  • Fig. 3 is an enlarged sectional viewof the orif fice plate
  • FIG 4 is a sectional vieW of an alternate type of heat exchanger
  • Fig. 5 is a sectional view of an alternate Ytype of restriction to flow
  • Fig. 6 is a sectional View of another alternate type of heat exchanger.
  • Fig. 7 is a sectional view of another alternate type of restriction.
  • My invention is embodied in various combinaf tions of apparatus which cause a samplff g'aslto undergo pressure changes depending .0X1 tlie chemical n-ature of the sample, ⁇ Yand indicating or recording apparatus operatedbythe saidiprsfsure change.
  • the pressure-operated'I ratus may be calibrated ⁇ directlyin terirs percentage of each gas present in. ⁇ .th ⁇ e.s
  • the measured pressure drop occurs as th'e'sample passes through restrictions which cause viscous drag, ⁇ the volumetric oW rateth'rough the said restrictions being determinedV by causing the sample' gas to pass through an orifice at the maximum rate.
  • the maximum rate of 'flow for some gases is considerably'diiferent from that of other gases, but is substantially independent of the pressure upstream of the tonev provided the absolute pressure downstream of oriice does not exceed approximately'one-half the absolute' pressure upstream of the oriiice. Since the viscosity of gases is also substantially independent of the pressure, the viscous pressure 'drop' developed in the restriction is substantially independent of the pressure'of the sample.
  • Equation 4 VS/Triting Ras :154/molecularweight and combining all constants, (.2.) becomes Substituting the value of lo into Equation .1, and combining constants
  • the long radical in Equation 4 may be replaced by approximate values tabulated below:
  • the pressure drop developed by viscous flow through a resistance is, in addition to the temperature, also a function of the mean free path of the gas molecules provided the cross section of the flow path is not large compared to the length of the molecular free path.
  • the average cross section of the ow path may be reduced to the point where the relative pressure drops may be changed slightly to cause two or more gases to have an identical pressure drop for the purpose of determining the percentage of still another gas having a substantially different pressure drop.
  • still other groups of gases may be caused to develop identical pressure drops for the purpose of analyzing for one gas in a mixture of more than two gases.
  • Fig. 1 A thermostatic control of any type known to the art. but in this instance e tuations in temperature.
  • thermostatic switch I represented by a thermostatic switch I and heater winding 2 operates to maintain all the internal parts at substantially a certain constant temperature.
  • Any suitable insulation 3 minimizes heat exchange between the ambient air and the internal parts of the analyzer.
  • a main body 4, hereafter known as the heat reservoir, provides a heat capacity sufficiently large to prevent sudden fluc-
  • a further function of the heat reservoir is to conduct heat to all the internal parts.
  • Still another function of the heat reservoir is to provide a convenient body to which other parts are secured.
  • the heat exchanger preferably formed of porous metal, but which can alternatively be formed of porous ceramic, glass or other material, efficiently heats the gas passing through its numerous channels.
  • a heat exchanger so constructed is highly preferred to others because of its ability to change the temperature of a sample as much as 200 F. in a fraction of a second and yield a terminal temperature within a fraction of a degree of the desired temperature. Accuracy combined with speed in temperature control provides response not obtainable with heat exchangers commonly used.
  • the retainer 'I made of any heat conducting material, has a preferably tapered hole into which the porous material is fitted.
  • An alternate type of heat exchanger illustrated in Fig. 4 consists of individual pieces of material 8 packed into a retainer 9 and held in place by end plugs I0 and II which have passages to pass gas but to retain solids.
  • the material 8 may be beads, chips, strands, or other small shapes of any material, but preferably good heat conductors.
  • Still another heat exchanger which may be used but which is not preferred is illustrated in Fig. 6.
  • This heat exchanger 29 consists of any heat conducting material through which is formed one or more holes to conduct the sample.
  • Gasket I2 serves as a pressure seal and as a means of exerting force on the threads of parts 4 and 'I to insure efficient heat transfer.
  • a restriction I3 to flow is made of porous mal terial having numerous flow paths of small cross section.
  • porous metal is superior, but alternately porous ceramic, glass or other materials may be used.
  • a retainer I4 held tightly against a gasket I5 by a spring I6, preferably fits freely in the heat reservoir 4 so that it may be easily interchanged with other retainers.
  • Such construction permits quick changes in the operating characteristics of the analyzer if retainers containing various types of restrictive material are made available.
  • Other restrictions shown in Fig. 5 and Fig. 7 may be used.
  • the restriction in Fig. 5 is structurally similar to that of the heat exchanger in Fig. 4, consisting of particles of material 24, retainer 25, and end plugs 2B and 2l.
  • the restriction 28 shown in Fig. 7 represents many possible arrangements of one or more capillary channels, but in this case consists of a metal plug through which holes of small diameter are formed.
  • Fittings I 'I and I8 provide means to connect any suitable device for measuring pressure drops developed in the restriction I3.
  • a manometer I9 is representative of numerous indicators, re-
  • corders, or controllers known to the art which operate on a pressure differential For example, a diaphragm operated by the diierential pressure at ttings I1 and I8 could control valves in such a manner that the analyzer apparatus tends to maintain a mixture of definite proportions downstream of the said valves.
  • Antician 20 in an orifice plate 2l passes a volume of gas substantially independent of the pressure of the gas provided the absolute pressure downstream of the saudow does not exceed approximately one-half the absolute pressure upstream of the orifice.
  • An outlet tting 22 serves as a mounting for thetician plate, as a thermal insulator, and as a means to connect to any suitable evacuating pump (not shown). No evacuating pump is required if the gas sample enters the analyzer at a pressure high enough above atmospheric pressure to satisfy the conditions for critical ow.
  • a gasket 23 prevents leakage of gas around the threads of tting 22.
  • a gas analysis apparatus comprising an insulated heat reservoir through which is formed a passage for the ow of gas to be analyzed, a heater winding adjacent to the said heat reservoir, a thermostatic switch operating in a manner to close and open a circuit including the said heater winding.

Description

Feb. 26, 1952 F. F. YANlKosKl GAS ANALYSIS APPARATUS F1ed 00b. 18, 1946 IMI Patented Feb. 26, 1952 UNITED PATENT OFFICE assasse Qns .finntxsls APPARATUS` Florian Yanilkxoski, ChiagQ Hight Aphlicaation Qctgber 18, 1956, Serial No. 703.980
i clavier. (o1. ca -2s) (Granted `under the act of March 3, 1883, as
amended April 3Q, 192g: 370'0. G. "757) The invention described herein may -be manufactured and used by or for the Government `for governmental purposes Without paymentt me of any royalty thereon.` f
This invention relates to gas analysis apparaf tus of the type that continuously 'determines the percentage of one gas in a mixture of two or more gases. One object of the invention'is to provide a gas analysis apparatus capableof Avery high speeds in responding to a change in the corniposition of the sample. Another object is to provide an apparatus of simple construction which provides accurate analyses substantially independent of the temperature and pressure of the surrounding atmosphere. Still vvanother object is to provide an apparatus capable o f safely analyzing explosive mixtures of gases. Still -another object is to provide a gas analysis apparatus which utilizes the fact that the relaitive viscosities of gases change as a function 'of temperature. Still another object is to provide an apparatus which utilizes the fact'thatth viscosity of gas apparently changes when the width of the flow path is reducedy to values approaching that of the mean free moleculair path.
These and other objects will be vapparent to those skilled in the art from theiollowing'description and the related drawings. 'i
In the drawings:
Fig. 1 is a sectional view of the preferred form ofthe invention shown connected to one type of pressure differential indicator;
Fig. 2 is an exploded view of some o f the parts shown in Fig. 1;
Fig. 3 is an enlarged sectional viewof the orif fice plate;
"Fig 4 is a sectional vieW of an alternate type of heat exchanger;
Fig. 5 is a sectional view of an alternate Ytype of restriction to flow;
Fig. 6 is a sectional View of another alternate type of heat exchanger; and
Fig. 7 is a sectional view of another alternate type of restriction.
Similar reference numerals indicate the saine parts throughout the several views. v
My invention is embodied in various combinaf tions of apparatus which cause a samplff g'aslto undergo pressure changes depending .0X1 tlie chemical n-ature of the sample,` Yand indicating or recording apparatus operatedbythe saidiprsfsure change. When considering a"m`ix'tu`re""of two definite gases the pressure-operated'I ratus may be calibrated `directlyin terirs percentage of each gas present in.`.th `e.s
More specically, the measured pressure drop occurs as th'e'sample passes through restrictions which cause viscous drag,` the volumetric oW rateth'rough the said restrictions being determinedV by causing the sample' gas to pass through an orifice at the maximum rate. The maximum rate of 'flow for some gases is considerably'diiferent from that of other gases, but is substantially independent of the pressure upstream of the oricev provided the absolute pressure downstream of oriice does not exceed approximately'one-half the absolute' pressure upstream of the oriiice. Since the viscosity of gases is also substantially independent of the pressure, the viscous pressure 'drop' developed in the restriction is substantially independent of the pressure'of the sample.
-` Both the viscosity and the maximum ow rate of all gases are functions Vof temperature, therefore preferable combinations of apparatus include means to correct the temperature of the sample to within a fraction of a degree of a predetermined temperature before the sample passes through the restriction and the orifice; Assuming a'constant temperature,4 the pressure drop developed by viscous ow through the restricis' (l) C, G1, C2, Cs-constants A-"orilice' area; ft2. g`gravtational const. IL-degrees Rankine.` R-gas constant. lc-ratio of'spec.' heats. ruf-#molecular weight.
4 VS/Triting Ras :154/molecularweight and combining all constants, (.2.) becomes Substituting the value of lo into Equation .1, and combining constants The long radical in Equation 4 may be replaced by approximate values tabulated below:
For inert gases (helium and argon) .725
For diatomic gases (N2, O2, air, CO, HC1,
NO, etc.) .685
For complex gases (hydrocarbons, etc.)-
varies .64 to .67
Values of pressure drop relative to air are listed below for certain common gases:
Pressure drop relative to .air for a certain analyzer operating at 100 F.
While this list is far from complete, it serves to illustrate the wide difference in pressure drops developed in some cases. The pressure drop for each of the gases listed above is sufciently different from others that mixtures of any two could be analyzed. A complete table of gases would lead to innumerable other combinations that could be analyzed. Certain groups of gases, such as CO, N2, and air, have substantially identical pressure drops and may be treated in any proportions as a single gas when analyzing for one other gas, such as CO2, which has a substantially different pressure drop.
Since viscosity is a function of temperature, the relative values would be somewhat different if the operating temperature of the analyzer were changed. By choosing the proper temperature it is possible in some cases to cause two or more gases t undergo an identical pressure drop, and under these circumstances any proportions of said gases may be treated as a single gas when analyzing for still another gas. When seeking such a temperature it is only necessary to plot curves of pressure drop against temperature for the various gases concerned and choose the temperature at which the pressure curves cross or become tangent.
The pressure drop developed by viscous flow through a resistance is, in addition to the temperature, also a function of the mean free path of the gas molecules provided the cross section of the flow path is not large compared to the length of the molecular free path. By means described later in this discussion, the average cross section of the ow path may be reduced to the point where the relative pressure drops may be changed slightly to cause two or more gases to have an identical pressure drop for the purpose of determining the percentage of still another gas having a substantially different pressure drop. Furthermore, by combining the effect of changing the operating temperature and the effect of changing the cross section of the flow path, still other groups of gases may be caused to develop identical pressure drops for the purpose of analyzing for one gas in a mixture of more than two gases.
The means used to accomplish the operations described above are combinations of apparatus which will now be described.
The preferred embodiment of my invention is illustrated in Fig. 1. A thermostatic control of any type known to the art. but in this instance e tuations in temperature.
represented by a thermostatic switch I and heater winding 2 operates to maintain all the internal parts at substantially a certain constant temperature.
Any suitable insulation 3 minimizes heat exchange between the ambient air and the internal parts of the analyzer. A main body 4, hereafter known as the heat reservoir, provides a heat capacity sufficiently large to prevent sudden fluc- A further function of the heat reservoir is to conduct heat to all the internal parts. Still another function of the heat reservoir is to provide a convenient body to which other parts are secured.
An inlet fitting 5-insulates the internal parts from externally connected parts such as a filter, drier, saturator, chemical absorber or other preparatory apparatus well known in the art while conducting the gas sample from the said preparatory apparatus to a heat exchanger 6. The heat exchanger, preferably formed of porous metal, but which can alternatively be formed of porous ceramic, glass or other material, efficiently heats the gas passing through its numerous channels. A heat exchanger so constructed is highly preferred to others because of its ability to change the temperature of a sample as much as 200 F. in a fraction of a second and yield a terminal temperature within a fraction of a degree of the desired temperature. Accuracy combined with speed in temperature control provides response not obtainable with heat exchangers commonly used. The retainer 'I, made of any heat conducting material, has a preferably tapered hole into which the porous material is fitted. An alternate type of heat exchanger illustrated in Fig. 4, consists of individual pieces of material 8 packed into a retainer 9 and held in place by end plugs I0 and II which have passages to pass gas but to retain solids. The material 8 may be beads, chips, strands, or other small shapes of any material, but preferably good heat conductors. Still another heat exchanger which may be used but which is not preferred is illustrated in Fig. 6. This heat exchanger 29 consists of any heat conducting material through which is formed one or more holes to conduct the sample. Gasket I2 serves as a pressure seal and as a means of exerting force on the threads of parts 4 and 'I to insure efficient heat transfer.
A restriction I3 to flow is made of porous mal terial having numerous flow paths of small cross section. For many purposes porous metal is superior, but alternately porous ceramic, glass or other materials may be used. A retainer I4 held tightly against a gasket I5 by a spring I6, preferably fits freely in the heat reservoir 4 so that it may be easily interchanged with other retainers. Such construction permits quick changes in the operating characteristics of the analyzer if retainers containing various types of restrictive material are made available. In addition to the type of restriction made of molded porous materials, other restrictions shown in Fig. 5 and Fig. 7 may be used. The restriction in Fig. 5 is structurally similar to that of the heat exchanger in Fig. 4, consisting of particles of material 24, retainer 25, and end plugs 2B and 2l. The restriction 28 shown in Fig. 7 represents many possible arrangements of one or more capillary channels, but in this case consists of a metal plug through which holes of small diameter are formed.
Fittings I 'I and I8 provide means to connect any suitable device for measuring pressure drops developed in the restriction I3. A manometer I9 is representative of numerous indicators, re-
corders, or controllers known to the art which operate on a pressure differential. For example, a diaphragm operated by the diierential pressure at ttings I1 and I8 could control valves in such a manner that the analyzer apparatus tends to maintain a mixture of definite proportions downstream of the said valves.
An orice 20 in an orifice plate 2l passes a volume of gas substantially independent of the pressure of the gas provided the absolute pressure downstream of the orice does not exceed approximately one-half the absolute pressure upstream of the orifice. An outlet tting 22 serves as a mounting for the orice plate, as a thermal insulator, and as a means to connect to any suitable evacuating pump (not shown). No evacuating pump is required if the gas sample enters the analyzer at a pressure high enough above atmospheric pressure to satisfy the conditions for critical ow. A gasket 23 prevents leakage of gas around the threads of tting 22.
It is understood that the details of construction are not necessarily limited to those described above in the preferred embodiment of my invention.l The invention consists in certain improvements and combinations of parts set forth in the following claim.
What I claim as my invention:
A gas analysis apparatus comprising an insulated heat reservoir through which is formed a passage for the ow of gas to be analyzed, a heater winding adjacent to the said heat reservoir, a thermostatic switch operating in a manner to close and open a circuit including the said heater winding. an elongated porous mass heat exchanger removably mounted in the said gas passage, a retainer for the said heat exchanger removably mounted in the said passage, an elongated porous restriction removably mounted in the said gas passage, a retainer for the said elongated restriction removably mounted in the said passage, insulating fittings mounted in the said heat reservoir in such a manner that their internal openings connect to the said passage at opposite ends of the said elongated porous restric tion, an insulating gas connector at the outlet end of the said passage, and a restrictive orifice plate mounted in the said connector between the orice plate and outlet, and means to maintain on opposite sides of the said orice plate a pressure drop sufficient to cause maximum flow.
FLORIAN F. YANIKOSKI.
' REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,272,059 Lacey July 9, 1918 1,633,352 Tate June 21, 1927 1,884,896 Smith Oct. 25, 1932 2,154,862 Olshevsky Apr. 18, 1939 2,163,730 Goetzl June 27, 1939 FOREIGN PATENTS Number Country Date 435,176 Great Britain Dec. 8, 1933 OTHER REFERENCES Physics Text Book- Hausmann and Slack (Van Nostrand) published September 1935.
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2825226A (en) * 1954-08-25 1958-03-04 Jr Joseph A Daley Combustible gas detector
US3916672A (en) * 1972-11-27 1975-11-04 Solartron Electronic Group Apparatus for measuring the specific gravity of gases
CN101865109A (en) * 2009-04-20 2010-10-20 安捷伦科技有限公司 Serial type pump comprising a heat exchanger
US9182381B2 (en) 2013-03-15 2015-11-10 Meggitt Safety Systems, Inc. Apparatus and methods for measuring concentrations

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1272059A (en) * 1916-09-20 1918-07-09 Roessler & Hasslacher Chemical Separation of the constituents of gaseous mixtures.
US1633352A (en) * 1926-02-23 1927-06-21 Taylor Instrument Co Gas-analysis apparatus
US1884896A (en) * 1927-07-29 1932-10-25 John M Hopwood Fluid analysis
GB435176A (en) * 1933-12-08 1935-09-16 Carlo Padovani Indicating-measuring apparatus for the delivery of gaseous currents and other coefficients
US2154862A (en) * 1937-02-12 1939-04-18 Eclipse Aviat Corp Gas analysis apparatus
US2163720A (en) * 1937-07-20 1939-06-27 Union Carbide & Carbon Res Lab Preparation of acetylenic alcohols

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1272059A (en) * 1916-09-20 1918-07-09 Roessler & Hasslacher Chemical Separation of the constituents of gaseous mixtures.
US1633352A (en) * 1926-02-23 1927-06-21 Taylor Instrument Co Gas-analysis apparatus
US1884896A (en) * 1927-07-29 1932-10-25 John M Hopwood Fluid analysis
GB435176A (en) * 1933-12-08 1935-09-16 Carlo Padovani Indicating-measuring apparatus for the delivery of gaseous currents and other coefficients
US2154862A (en) * 1937-02-12 1939-04-18 Eclipse Aviat Corp Gas analysis apparatus
US2163720A (en) * 1937-07-20 1939-06-27 Union Carbide & Carbon Res Lab Preparation of acetylenic alcohols

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2825226A (en) * 1954-08-25 1958-03-04 Jr Joseph A Daley Combustible gas detector
US3916672A (en) * 1972-11-27 1975-11-04 Solartron Electronic Group Apparatus for measuring the specific gravity of gases
CN101865109A (en) * 2009-04-20 2010-10-20 安捷伦科技有限公司 Serial type pump comprising a heat exchanger
US20100299079A1 (en) * 2009-04-20 2010-11-25 Agilent Technologies, Inc. Serial type pump comprising a heat exchanger
CN101865109B (en) * 2009-04-20 2015-02-18 安捷伦科技有限公司 Serial type pump comprising a heat exchanger
US9803627B2 (en) * 2009-04-20 2017-10-31 Agilent Technologies, Inc. Serial type pump comprising a heat exchanger
US9182381B2 (en) 2013-03-15 2015-11-10 Meggitt Safety Systems, Inc. Apparatus and methods for measuring concentrations

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