US3448917A - Air jet pump - Google Patents

Air jet pump Download PDF

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US3448917A
US3448917A US637179A US3448917DA US3448917A US 3448917 A US3448917 A US 3448917A US 637179 A US637179 A US 637179A US 3448917D A US3448917D A US 3448917DA US 3448917 A US3448917 A US 3448917A
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nozzle
conduit
outlet
section
air
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US637179A
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William R Dewey
Howard W Locker
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JETDRAFT Inc
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JETDRAFT Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles

Definitions

  • This invention relates to ejector systems :for fume removal and more specfically to an air ejector apparatus having an oifset discharge nozzle supported a predetermined distance from the outlet of a chimney conduit having a uniform transverse cross section and which discharges compressed air toward the chimney outlet to create an artificial gas flow.
  • Air ejector systems are commonly employed to provide an artificial draft in the chimney of commercial and industrial incnerators, boiler units, and those applications where it is necessary to transfer gases from a source such as a com bustion unit to a discharge area through a conduit.
  • Systems of this type are also employed as a material handling means wherein a' fluid such as a gas is to be transferred from a 'first area to a second area.
  • Air ejector pumping systems have a special advantage in that the materials contained in the transferring gas do not impinge upon or corrode the air pump Components.
  • the broad purpose of the present invention is to provide an eflicient air jet pump which may be incorporated within a chimney or similar conduit having a uniform cross section in the direction of its length without the necessity for the venturi throat and which has improved draft-inducing efficences.
  • the nozzle is supported with its outer side wall tangential to the axis of the conduit so that the discharge opening of the nozzle is laterally ofiset from the axis of the conduit.
  • the discharge nozzle is supported upstream from the conduit outlet a distance lying in a range between 5.5 and 16 times the diameter of the conduit. This range permits flexiblity in mounting the nozzle in a conventional stack and still insures satisfactory performance. Performance tests indicate that an optimum efficiency results 'when the discharge end of the nozzle is positoned ten times the diameter of the exhaust end of the conduit from the conduit outlet.
  • the duct from the discharge of the air 'fan to the nozzle curves in a common lateral direction from the fan to the nozzle as distinguished from an S curve flow path.
  • performance tests have indicated that improved results are obtainable by making the side walls of the nozzle convergent toward the discharge opening within an angle of convergency of 0 to 14 degrees.
  • satisfactory results can also be obtained by a non-convergent nozzle.
  • the preferred air jet pump nozzle arrangement has a number of definite advantages over air jet pumps of the prior art including its easy adaptability to existing or new, round or square, brick masonry or metal conduits; the ease in mounting the fan on the conduit; and the elimination for the requirement for a venturi throat in the conduit to provide a satisfactory draft.
  • FIGURE 1 is an elevational sectional view of an air pump apparatus mounted to a conduit with a duct and nozzle illustrating the preferred embodiment of the invention and with parts in section for purposes of clarity;
  • FIGURE 2 is a plan View of the air ejector apparatus and conduit of FIGURE 1;
  • FIGURE 3 is an elevational view of the preferred duct and nozzle separated from the other Components of the system
  • FIGURE 4 is a plan view of the duct and nozzle of FIGURE 3;
  • FIGURE 5 is a fragmentary sectional view illustrating a convergent nozzle showing an alternative ernbodiment of the invention
  • FIGURE 6 is a graphical illustration showing the performance associated with various nozzle positions relative to the conduit outlet.
  • FIGURE 7 is a graphical illustration showing the performance associated with various nozzle positions laterally displaced with respect to the conduit axis.
  • number 10 refers to a chimney or similar casing having a conduit 12 having a uniform circular cross section throughout its length.
  • the lower end of the conduit 12 is connected to a source of gas 16 which is discharged through an outlet 18 at the upper end of thet conduit 12.
  • the chimney 10 defines a conduit having a circular cross section it is to be understood that the chimney could as Well define a square conduit or other conventional shape which is symmetrical about a longitudinal axis 20;
  • a housing 22 mounted on the chimney 10 by bracket 24 supports a centrifugal air pump 26.
  • the air pump 26 provides means for supplying a source of pressurized air through a fan discharge opening 28 to a straight section of duct 30 having a rectangular cross section.
  • the duct 30 extends through the Wall of the chimney 10 in a lateral direction to the aXis 20 and merges with an elbow section 32 which directs the pressurized air upwardly through a nozzle section 34.
  • the nozzle 34 has a rectangular or preferably square discharge opening 36.
  • the duct 30 and the elbow section 32 are preferably gradually and regularly narrowed from the inlet of the duct 30 and toward the nozzle section 34.
  • the length of the straight section 30 as indicated by the letter B is preferably one and half times the thickness of the wall of the chimney 10 and in no case is it less than one inch.
  • the duct section 30 has a rectangular inlet defined by a height C and a width D.
  • the radius of the inner side wall of the elbow section 32 and indicated at R1 is preferably equal to C.
  • RZ which defines the radius of curvature of the outer side wall of the elbow 32 is preferably equal to two times the dimension C. It is to be understood that the forementioned dimensions define the flow path of the air and consider the ducting as being formed of a sheet metal having a relatvely nominal thickness.
  • the nozzle 34 preferably has a length extending in the direction of the flow path of the air and indiacted by H which corresponds to the diameter S of the nozzle discharge opening 36.
  • the discharge opening 36 is directed toward the outlet 18 with the outer wall of the nozzle 34 which forms an extension of the outer curved wall of the elbow 32 supported so that it is tangential to the conduit aXis 201
  • the discharge end 36 of the nozzle 34 is preferably positioned with respect to the outlet 18 a distance indicated at L which ranges between 5.5 and 16 times the diameter of the conduit 12. For best results, L is 10 times the diameter of the exhaust portion of the conduit 12.
  • FIGURE 1 illustrates a nozzle section 34 having side walls parallel to the longitudinal axis of the nozzle, however, as can best be seen in FIGURE 5, an alternative form of nozzle 38 has side walls converging toward a discharge opening 40 at an included angle M.
  • M lies in a range of 0-14 degrees.
  • FIGURE 6 illustrates the results achieved by positioning the nozzle 34 at various distances from the outlet 18 of the conduit. T hus it can be seen that in terms of the air horsepower achieved in the conduit for a given air jet, the optimum distance is approximately 8 to 12 times the diameter of the conduit with satisfactory results obtainable between 5.5 to 16 times the diameter of the conduit.
  • FIGURE 7 is a graphical illustration showing the improved results obtained by positioning the nozzle at a position laterally offset from the axis of the conduit 12.
  • the best performance is achieved when the outer edge of the nozzle 34 is arranged along the axis of the conduit 12.
  • an air pump apparatus for producng a draft of the gas from said source to said outlet, compris mg:
  • said duct means has an axis substantially normal to the aXis of said condut, said duct means having a rectangular 20 cross section of a width defined in the direction of the aXis of said condut and an elbow connectng said duct means and said nozzle, said elbow having an inner side formed on a radius correspondng to said width and an outer side formed on a radius corresponding to twice said width, and said nozzle having a length in the direction of said nozzle axis corresponding to the diameter of said nozzlc discharge opening.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)

Description

Sheet fi k AIR JET PUMP I m C 4 H A l w. R. DEWEY ET L VZa Jun 10, 1969 Filed May 9, 1967 FIG. l
INVENTORS /AM R. DEWEY !u LOCKER BOFIG- 30 V w w w FIGB United States Parent Oflice 3,448,9l7 Patented June 10, 1969 3,448,917 AIR JET PUMP William R. Dewey, Detroit, and Howard W. Locker, Birmingham, Mich., assignors to Jetdraft, Inc., Detroit, Mich., a corporation of Michigan Filed May 9, 1967, Ser. No. 637,179 Int. Cl. F04f 5 00 U.S. Cl. 230-95 7 Claims ABSTRACT OF THE DISCLOSURE An air ejector mounted within and near the outlet of a chimney to create an artifical draft of the chimney gases. A rectangular or square nozzle supported a predetermined distance from the outlet and otfset from the axis of the chimney discharges pressurized air toward the outlet to induce a positive gas flow.
BACKGROUND OF THE INVENTION Field of the invention This invention relates to ejector systems :for fume removal and more specfically to an air ejector apparatus having an oifset discharge nozzle supported a predetermined distance from the outlet of a chimney conduit having a uniform transverse cross section and which discharges compressed air toward the chimney outlet to create an artificial gas flow.
Description of the prior art Air ejector systems are commonly employed to provide an artificial draft in the chimney of commercial and industrial incnerators, boiler units, and those applications where it is necessary to transfer gases from a source such as a com bustion unit to a discharge area through a conduit. Systems of this type are also employed as a material handling means wherein a' fluid such as a gas is to be transferred from a 'first area to a second area. Air ejector pumping systems have a special advantage in that the materials contained in the transferring gas do not impinge upon or corrode the air pump Components.
It is common practice to mount the air nozzle on the axis of the conduit so that the pressurized air is discharged axially toward a -venturi-like throat in the conduit. This symmetrical arrangement has a number of drawbacks, particularly where it is necessary to incorporate a draft producing air jet pump in a conventional chimney having a uniforrn transverse cross section from the nozzle outlet to the chimney outlet. This is due to the expense of installing the venturi throat downstream from the nozzle.
The broad purpose of the present invention is to provide an eflicient air jet pump which may be incorporated within a chimney or similar conduit having a uniform cross section in the direction of its length without the necessity for the venturi throat and which has improved draft-inducing efficences.
SUMMARY The preferred embodiment of the invention is described with reference to a chimney conduit having a circular cross section, however it is to -be understood` compressor. An elbow within the conduit has one end connected to the duct and its opposite end terminating in a nozzle having a rectangular cross section. The discharge end of the nozzle is directed toward the outlet of the conduit. The rectangular cross section of the nozzle improves the entrainment of the gases flowing through the conduit because of the greater surface area of the air jet dscharged from the nozzle for a given cross sectional area as opposed to a circular discharge area.
The nozzle is supported with its outer side wall tangential to the axis of the conduit so that the discharge opening of the nozzle is laterally ofiset from the axis of the conduit. Preferably the discharge nozzle is supported upstream from the conduit outlet a distance lying in a range between 5.5 and 16 times the diameter of the conduit. This range permits flexiblity in mounting the nozzle in a conventional stack and still insures satisfactory performance. Performance tests indicate that an optimum efficiency results 'when the discharge end of the nozzle is positoned ten times the diameter of the exhaust end of the conduit from the conduit outlet.
Preferably the duct from the discharge of the air 'fan to the nozzle curves in a common lateral direction from the fan to the nozzle as distinguished from an S curve flow path. In addition performance tests have indicated that improved results are obtainable by making the side walls of the nozzle convergent toward the discharge opening within an angle of convergency of 0 to 14 degrees. However, satisfactory results can also be obtained by a non-convergent nozzle.
The preferred air jet pump nozzle arrangement has a number of definite advantages over air jet pumps of the prior art including its easy adaptability to existing or new, round or square, brick masonry or metal conduits; the ease in mounting the fan on the conduit; and the elimination for the requirement for a venturi throat in the conduit to provide a satisfactory draft.
It is therefore an object of the present invention to provide in combinaton with a conduit having an nlet connected to a source of a gas and an outlet for the dis charge of the gas, air ejector apparatus for inducing a draft of the gas from the inlet and toward the outlet through an exhaust section formed symmetrically about an axis and terminating with the outlet of the conduit and including a nozzle having a discharge opening and supported in the exhaust section upstream of the outlet with the discharge opening directed toward the outlet and the periphery of the discharge opening being contiguous with the axis of the conduit, a source of pressurized air and duct means connecting the pressurized air to the nozzle.
It is another object of the present invention, to provide in com-bination with a conduit having an nlet connected to a source of gas, an outlet .for the discharge of the gas and an exhaust section formed symmetrically about an axis and terminating with the outlet, air ejector apparatus for inducing a draft for the gas from the source and towards the outlet comprising a nozzle having a discharge opening supported within the exhaust section upstream from the outlet and laterally oifset from the axis of the exhaust section, the nozzle having a rectangular cross section with the discharge section opening directed toward the conduit outlet, a source of pressurized air, and duct means connecting the source of pressurized air to the nozzle.
It is a still further object of the present invention to provide means for creating an artificial draft in a conduit for exhausting a gas through the conduit and toward a conduit outlet by providing a rectangular nozzle connected to a source of pressurized air and having a discharge opening supported within the condiut and directed toward the conduit outlet, and being positioned upstream from the conduit outlet a distance between 5.5 and 16 times the diameter of the conduit.
c Still other objects and advantages of the present invention will readly occur to one skilled in the art to which the invention pertains upon reference to the detailed description.
Description of the d'awings The description refers to the accompanying drawings in which like reference characters refer to like parts throughout the several views and in which:
FIGURE 1 is an elevational sectional view of an air pump apparatus mounted to a conduit with a duct and nozzle illustrating the preferred embodiment of the invention and with parts in section for purposes of clarity;
FIGURE 2 is a plan View of the air ejector apparatus and conduit of FIGURE 1;
FIGURE 3 is an elevational view of the preferred duct and nozzle separated from the other Components of the system;
FIGURE 4 is a plan view of the duct and nozzle of FIGURE 3;
FIGURE 5 is a fragmentary sectional view illustrating a convergent nozzle showing an alternative ernbodiment of the invention;
FIGURE 6 is a graphical illustration showing the performance associated with various nozzle positions relative to the conduit outlet; and
FIGURE 7 is a graphical illustration showing the performance associated with various nozzle positions laterally displaced with respect to the conduit axis.
Description of the preferred embod'ment Now referring to the drawings, number 10 refers to a chimney or similar casing having a conduit 12 having a uniform circular cross section throughout its length. The lower end of the conduit 12 is connected to a source of gas 16 which is discharged through an outlet 18 at the upper end of thet conduit 12. Although the chimney 10 defines a conduit having a circular cross section it is to be understood that the chimney could as Well define a square conduit or other conventional shape which is symmetrical about a longitudinal axis 20;
A housing 22 mounted on the chimney 10 by bracket 24 supports a centrifugal air pump 26. The air pump 26 provides means for supplying a source of pressurized air through a fan discharge opening 28 to a straight section of duct 30 having a rectangular cross section. The duct 30 extends through the Wall of the chimney 10 in a lateral direction to the aXis 20 and merges with an elbow section 32 which directs the pressurized air upwardly through a nozzle section 34. As 'best seen in FIGURES 3 and 4, the nozzle 34 has a rectangular or preferably square discharge opening 36. In addition, the duct 30 and the elbow section 32 are preferably gradually and regularly narrowed from the inlet of the duct 30 and toward the nozzle section 34.
It has been found from performance tests that the improved air pump ducting has a close interrelationship between its various Components which contribute toward an overall optimal performance. Thus the length of the straight section 30 as indicated by the letter B is preferably one and half times the thickness of the wall of the chimney 10 and in no case is it less than one inch. The duct section 30 has a rectangular inlet defined by a height C and a width D. The radius of the inner side wall of the elbow section 32 and indicated at R1 is preferably equal to C. RZ which defines the radius of curvature of the outer side wall of the elbow 32 is preferably equal to two times the dimension C. It is to be understood that the forementioned dimensions define the flow path of the air and consider the ducting as being formed of a sheet metal having a relatvely nominal thickness.
The nozzle 34 preferably has a length extending in the direction of the flow path of the air and indiacted by H which corresponds to the diameter S of the nozzle discharge opening 36. Referring 'back to FIGURE 1, the discharge opening 36 is directed toward the outlet 18 with the outer wall of the nozzle 34 which forms an extension of the outer curved wall of the elbow 32 supported so that it is tangential to the conduit aXis 201 The discharge end 36 of the nozzle 34 is preferably positioned with respect to the outlet 18 a distance indicated at L which ranges between 5.5 and 16 times the diameter of the conduit 12. For best results, L is 10 times the diameter of the exhaust portion of the conduit 12.
The embodiment of FIGURE 1 illustrates a nozzle section 34 having side walls parallel to the longitudinal axis of the nozzle, however, as can best be seen in FIGURE 5, an alternative form of nozzle 38 has side walls converging toward a discharge opening 40 at an included angle M. Preferably M lies in a range of 0-14 degrees.
FIGURE 6 illustrates the results achieved by positioning the nozzle 34 at various distances from the outlet 18 of the conduit. T hus it can be seen that in terms of the air horsepower achieved in the conduit for a given air jet, the optimum distance is approximately 8 to 12 times the diameter of the conduit with satisfactory results obtainable between 5.5 to 16 times the diameter of the conduit.
Similarly FIGURE 7 is a graphical illustration showing the improved results obtained by positioning the nozzle at a position laterally offset from the axis of the conduit 12. Thus the best performance is achieved when the outer edge of the nozzle 34 is arranged along the axis of the conduit 12.
It can therefore be seen that an improved air jet pump arrangement for creating an artificial draft through a conduit for exhausting the gas has been described which provides an efficient performance Without the requrement of the conventional venturi-like throat. By employing a rectangular or square nozzle and arranging the edge of the nozzle contiguous with the conduit axis and a predetermined distance from the conduit outlet, a highly efficient draft-producing arrangement is available for conventional ducts. Furthermore the preferred apparatus can be readly mounted to conventional chimneys to provide an artificial draft. By providing a suitable damper and a sensor associated with the source of the gas, the discharge magnitude of the draft can be readly controlled.
Although We have described the invention in its simplest terms, it is to be understood that various changes and revsious can be made therein without departing from the spirit of the invention or the scope of the appended claims.
We claim:
1. In a conduit having a constant cross-sectional area throughout its length, an inlet connected to a source of gas, an outlet for the discharge of said gas, and an exhaust section formed symmetrically about an axis and terminat ing with said outlet, an air pump apparatus for producng a draft of the gas from said source to said outlet, compris mg:
(a) a nozzle having a discharge opening and supported within said exhaust section upstream from said outlet with 'said discharge opening laterally offset from said axis, said nozzle having a rectangular cross section with the discharge opening directed toward said conduit outlet,
(b) a source of pressurized air, and
(c) duct means connecting said source of pressurized air and said nozzle,
(d) the discharge opening of said nozzle being disposed upstream from the outlet of said conduit a distance comprised between 8 and 12 times the diameter of said exhaust section.
2. The combination as defined in claim 1, wheren said nozzle has side walls converging in the direction of the flow path of the pressurized air towards said discharge opening at an included angle comprised between O and 14 degrees.
3. The combinaton as defined in claim 1, wherein said nozzle has side walls converging in the direction of the flow path of the pressurized air towards said discharge opening at an included angle comprised between 0 and 14 degrees.
4. The combnation as defined in claim 2, wherein said nozzle has an edge located in said condut substantially at the axis of said condut.
5. The combination as defined in claim 3, wherein said nozzle has an edge located in said condut substantially at the axis of said condut.
6. The combination as defined in claim 1, wherein said duct means between said source of pressurized air and said nozzle approach the axis of said Conduit from a lateral direction, and all directional changes in the flow path of the air from said source to said nozzle are in a common lateral direction.
7. The combination as defined in claim 6, wherein said duct means has an axis substantially normal to the aXis of said condut, said duct means having a rectangular 20 cross section of a width defined in the direction of the aXis of said condut and an elbow connectng said duct means and said nozzle, said elbow having an inner side formed on a radius correspondng to said width and an outer side formed on a radius corresponding to twice said width, and said nozzle having a length in the direction of said nozzle axis corresponding to the diameter of said nozzlc discharge opening.
References Cited UNITED STATES PATENTS 569,804 10/1896 Smith 230-96 739,806- 9/ 1903 Applegarth 230- 1,172,450 2/1916 Griffin 230-95 1,386,050 8/1921 Carr et al 230-96 1,407,011 2/1922 Wolf 230-95 l,426,518 8/ 1922 Sweeny 230-95 1,533,898 4/1925 Prat 110-162 1,527,849 2/ 1925 Elliott 110-162 1,653,980 12/1927 Bjorkholm et" al 230-96 2,923,959 2/1960 Huber 230-95 X 3,371,618 3/1968 Chambers 103-258 DONLEY J. STACKING, Primary Exam'ner.
W. J. KRAUSS, Assistant Examner.
U.S. Cl. X.R. 110-162; 230-105
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4483258A (en) * 1982-07-08 1984-11-20 Clear Air, Inc. Incinerator steam generation system
US4754952A (en) * 1984-03-22 1988-07-05 Kabushiki Kaisha Komatsu Seisakusho Fluidized-bed type carburizing furnace means for use as bright heat-treating furnace
US5117531A (en) * 1989-05-08 1992-06-02 Electrostar Schottle Gmbh & Co. Suction or blowing apparatus
RU2145680C1 (en) * 1999-06-28 2000-02-20 Открытое акционерное общество "Магистральные нефтепроводы Центральной Сибири" Foam generator (versions)
US6761559B1 (en) * 2003-05-09 2004-07-13 Tangteck Equipment Inc. Gas-exhausting module structure suited for a continuous type oven
US20110030807A1 (en) * 2006-08-24 2011-02-10 Jet Stick Limited Fluid amplifier

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US569804A (en) * 1896-10-20 Stack blower attachment
US739806A (en) * 1903-04-08 1903-09-29 Robert Applegarth Steam and air injector for furnaces.
US1172450A (en) * 1905-09-11 1916-02-22 Andrew A Hancock Pneumatic cleaner.
US1386050A (en) * 1919-12-23 1921-08-02 Joseph V Carr Draft-equalizer for steam-boilers
US1407011A (en) * 1921-03-11 1922-02-21 Bert D Wolf Varnish booth
US1426518A (en) * 1921-08-18 1922-08-22 Robert P Sweeny Air-induction cleaning apparatus
US1527849A (en) * 1923-12-29 1925-02-24 Osker W Elliott Draft producer
US1533898A (en) * 1923-08-30 1925-04-14 Prat Georges Jules Arman Louis Apparatus for obtaining artificial draft
US1653980A (en) * 1926-05-24 1927-12-27 John E Bjorkholm Blower nozzle
US2923959A (en) * 1960-02-09 Compressed-air operated cleaning apparatus
US3371618A (en) * 1966-02-18 1968-03-05 Chambers John Pump

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US569804A (en) * 1896-10-20 Stack blower attachment
US2923959A (en) * 1960-02-09 Compressed-air operated cleaning apparatus
US739806A (en) * 1903-04-08 1903-09-29 Robert Applegarth Steam and air injector for furnaces.
US1172450A (en) * 1905-09-11 1916-02-22 Andrew A Hancock Pneumatic cleaner.
US1386050A (en) * 1919-12-23 1921-08-02 Joseph V Carr Draft-equalizer for steam-boilers
US1407011A (en) * 1921-03-11 1922-02-21 Bert D Wolf Varnish booth
US1426518A (en) * 1921-08-18 1922-08-22 Robert P Sweeny Air-induction cleaning apparatus
US1533898A (en) * 1923-08-30 1925-04-14 Prat Georges Jules Arman Louis Apparatus for obtaining artificial draft
US1527849A (en) * 1923-12-29 1925-02-24 Osker W Elliott Draft producer
US1653980A (en) * 1926-05-24 1927-12-27 John E Bjorkholm Blower nozzle
US3371618A (en) * 1966-02-18 1968-03-05 Chambers John Pump

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4483258A (en) * 1982-07-08 1984-11-20 Clear Air, Inc. Incinerator steam generation system
US4754952A (en) * 1984-03-22 1988-07-05 Kabushiki Kaisha Komatsu Seisakusho Fluidized-bed type carburizing furnace means for use as bright heat-treating furnace
US5117531A (en) * 1989-05-08 1992-06-02 Electrostar Schottle Gmbh & Co. Suction or blowing apparatus
RU2145680C1 (en) * 1999-06-28 2000-02-20 Открытое акционерное общество "Магистральные нефтепроводы Центральной Сибири" Foam generator (versions)
US6761559B1 (en) * 2003-05-09 2004-07-13 Tangteck Equipment Inc. Gas-exhausting module structure suited for a continuous type oven
US20110030807A1 (en) * 2006-08-24 2011-02-10 Jet Stick Limited Fluid amplifier

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