US1574677A - Ejector for the delivery of gas and air in large quantities - Google Patents

Ejector for the delivery of gas and air in large quantities Download PDF

Info

Publication number
US1574677A
US1574677A US733858A US73385824A US1574677A US 1574677 A US1574677 A US 1574677A US 733858 A US733858 A US 733858A US 73385824 A US73385824 A US 73385824A US 1574677 A US1574677 A US 1574677A
Authority
US
United States
Prior art keywords
nozzle
air
ejector
gas
walls
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US733858A
Inventor
Mulder Jakob
Endert Dirk Christiaan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US733858A priority Critical patent/US1574677A/en
Application granted granted Critical
Publication of US1574677A publication Critical patent/US1574677A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F04F5/466Arrangements of nozzles with a plurality of nozzles arranged in parallel
    • 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
    • F04F5/461Adjustable nozzles

Definitions

  • the object of this invention is to considerably improve the useful effects when dealing ⁇ with the delivery of very large quantities of. air or gas.
  • the object of this invention is to reduce this consumption of steam in ejections for large deliveries and such result is obtained by an absolutely exact centering of the outer and inner. walls of an annular nozzle and the extension of the surface of contact between the active medium and the gas or air to be delivered.
  • the outer and the inner walls of the .annular nozzlel which are independent run concentrically for a considerable distance up to the point of smallest cross sect-ion.
  • the annular space between said walls isl divided into a circle of channels by radial ribs extending in an axial directionvwhich ribs may be helically arranged whilst the Ytwo cylindrical nozzle walls are centered relativelyy to eachother by said ribs.
  • the outer nozzle Wall or the inner, one or both on that portion of the annular nozzle which widens towards the .orifice can be provided with grooves extending in an axial gas or the effective medium and the medium to be delivered.
  • the cross section of the grooves provided in the nozzle walls may conveniently be gradually enlarged towards the outlet orifice of the nozzle ⁇
  • the depth ot the groove may be graduallv increased in the direction ot' the orifice ot the nozzle.
  • a 'nozzle uiade in accordance with this invention is illustrated by way of example, iii the accompanying drawing.
  • Fig. 1 shows a longitudinal section of an ejector according to this invention.
  • Fig. 2 is a similarlongitudinal section showing a n'ioditied construction.
  • Fig. 3 is an end elevation ot the discharge end or nozzle ot the ejector shown in Fig. 2.
  • Fig. 4 is a partial perspective view of the end ot the nozzle drawn toa larger scale.
  • Fig. is a longitudinal section through one of the nozzle passages also drawn to a larger scale.
  • ot ejectors with au Aannular nozzle may be regardedl as known.
  • the drawing 1 is the casing ot the ejector which is provided with an inlet 2 t'or the active medium (steam).
  • the passage 2 leads to an annular chamber 3 to which is connected the cylindrical outer wall '4T ot' the nozzle.
  • rl'lhe inner wall ot said nozzle is formed by a tube 5 which is arranged concentrially with the wall et.
  • annular space 6 which is divided into acircle ot' passages S running in an axial direction by radial ribs 7 extending in a axial direction and it desired helically arranged.
  • the ribs 7 extend across the annular space (i so that the nozzlc walls are centered b v said ribs which iualy be made in one piece with the inner wall or with the outer wall et.
  • the ribs may also be ,connected to the outer and iiiner walls alternately.
  • the tube' 5 forming thcinncr wall is also supported at 9 by the body of the casing and made tight against the steam chamber by a stuiiing boX it. l1.
  • V The admission ot the gas delivered or of the air to be delivered occurs in two places, ⁇ centrally through the inside of the tube o by means of the apertures 12 at the rear end thereof to which it gains access through ⁇ the flanged inlet 13.
  • a flange 15 is provided at the front end of the casing 1 by means of which the ejector casing is coupled in the usual way with a conical ejector tube 16. At the rear end the ejector casing is closed by means ot a cover 17.
  • Fig. 2 illustrates a inodiied torni of construction ⁇ where the portion ot the outer wall of the nozzle which lies between the point of the smallest cross section 18 and the orifice 19 is provided with longitudinal grooves 22.
  • the said longitudinal grooves are made 'oit uniform width, whilst their depth .increases gradually towards the orilice ot the annular nozzle.
  • the ⁇ inner wall ot the annular nozzle is constructed in the saine manner as in Fig. 1 i. e. with a smooth surtace.
  • the inner walls of the nozzle instead of the outer ones may be provided with similar grooves. It desired, both walls otl the nozzle may be provided with such grooves.
  • the issuing jet of the active medium assumes an undulated sur- ⁇ face and thus provides a considerably larger surface of Contact with the gas to be delivered.
  • the useful effect of the delivery is considerably augniented so that for a given largequantity of air orgas to be delivered the consumption of 'steam i. e. the working medium isr comparatively small.
  • a 'steam gas or vapour operated gas or air ejector for the delivery of large kquantities having an annularnozzle cen trally arranged in the casing ot the ejector for the inlet of the workingmedium, characterized by the fact that in rear ot the smallest cross section (18) of the annular nozzle the outer wall (4t) and the inner wall of the nozzle (5) which is independent of the former run concentrically for a considerable distance and the space (6) between thein is divided into a circle of passages (8) by radial o r helical ribs (7) extending in an axial direction whilst both walls of the nozzleA are centered relatively to each other by said ribs.
  • one of the opposed and nozzle-defining walls is provided with axially extending grooves, which grooves provide an undulating surface for the jet issuing from the nozzle.
  • both of the opposed and nozzle-'defining walls are provided with axially extending grooves, which grooves provide an undulating surface for the jet issuing from the nozzle.
  • a casing coaxially arranged tubes in said casing and having opposed walls defining therebetween an annular space for the passage of a motive fluid, the cross section of said space contracting from the outer ends of said tubes to an intermediate section thereof, means in rear of said intermediate section for maintaining said tubes in coaxial alignment, means permitting the delivery of motive fluid to said annular space at the rear thereof, and means permitting the delivery of air or gases to the inside of the inner tube and around said outer tube.
  • a casing for delivering gas or gases, a casing, a motive fluid passage leading into said casing and terminating in an annular chamber, a wall extending forwardly from said chamber providing a cylindrical outer nozzle member, a second cylindrical nozzle member within said outer member and ribs between said members for maintaining the same'in coaxial alignment, said ribs terminating in rear ofthe outlet end of saidV nozzle, whereby an annular stream of motive fluid may be delivered therefrom.
  • a casing a motive fluid chamber within said casing, a passage extending from the exterior of said casing to said chamber for delivering motive fluid thereto, a cylindrical wall extending forwardly of said chamber to rovide an outer nozzle member, a second cyfindrical member having the rear portion thereof supported by and in Huid tight engagement with the rear wall of said chamber, and spacing ribs between said members adjacent said chamber for maintaining the same in coaxial alignment, the opposed walls of said members diverging from each other towards the outlet end of said nozzle to provide space of increasing cross-section for the passage of the motive fluid.
  • a nozzle having inner and outer members defining an annular passage through which motive fluid may be delivered, one of the opposing walls provided by said members being grooved, whereby the jet of motive fluid assumes an undulating surface.
  • a pair of tubular members defining a ⁇ nozzle, the passage through said nozzle being of smallest cross-section at' an intermediate section thereof, spacing means between said members in rear of the smallest cross-section for maintaining said members in coaxial alignment, one of the opposing walls provided by said members being formed with grooves which gradually increase in cross-section from the smallest cross-section of said nozzle towards the outlet end thereof.
  • a nozzle comprising an inner member having an .outer wall of gradually increasing diameter from the nozzle/end towards the rear thereof, and an outer member having' an inner wall provided with spaced axial grooves opposing the tapering wall of said inner member.
  • a nozzle comprising a pair of tubular members, longitudinally extending ribs between said members for maintaining the same incoaxial alignment, said ribs terminating short of the outletend of the nozzle to provide an unobstructed annular outlet for said nozzle, axial grooves of increasing cross section extending along the wall of one of said members from a point in front of said ribs to the end of said nozzle, the wall of the other member gradually diverging from said grooved wall.

Description

Feb. 23 ,1926. 1,574,677
J. MULDER ET AL EJECTOR FOR THE DELIVERY OF GAS AND AIR IN LARGE QUAN'I'ITIES` Fil ed August 23, 1924 Patented Feb. 23, 1926.
nutren srarns l1,514,531? natuur orner..
JAKOB MULDER AND DXRKv CHRSTIAAN ENDERT, OF ROTTERDAM, NETHERLANDS.
EJECTOR FOR THE DELIVERY OF GAS AND AIR IN LARGE QUANTITIES.
Application iled August 23, 1924. Serial No. 733,858.
T0 all whom, it may concern.'
Beit known that we, .lAKon MULDER and DIRK CHRISTIAAN ENDERT, subjects of the Queen ofthe Netherlands. residing at Rotterdam, in the Province of Southllolland,
in the Kingdom of the Netherlands, have invented certain new and useful Improvements in Ejectors for the Delivery of Gas and Air in Large Quant-ities, of which the following is a specification.
The operation of the 'and air ejectors hitherto in use have been based on the principle of a massive jet of steam or several separate steam jets arranged in a circle, being blown cent-rally through direrging tubes. Ejectors with annular jets ot steam are also used,kbut theyv are only suitable for Supplying small quantities of air or gas at a high vacuum.
Neither apparatus with massive steam jets nor apparatus with several. separate steam jets arranged in a circle permit the delivery of large quantities of air or gas with the consumption of a relativelji' small quantity of steam. The consumption of steam has always proved to be large, relatively to the quantity of air or gas delivered, so that in the case of large deliveries, economic working was impracticable.
The object of this invention is to considerably improve the useful effects when dealing` with the delivery of very large quantities of. air or gas.
It should be observed that an annular steam jet has already beenapplied by Parsons, but-only on a small scale, when dealing with large deliveries, the extraordinarily high consumption of steam rendered its practical application almost impossible.
The high consumption of steam due to the fact that, with the existingarrangements, it was not possible owing to the variations in shapeto which the material is subjected to obtain an accurate centering of the concentric walls of the annular nozzles which are surrounded on the 0pposite sides by the cold air or gas and by the hot steam. The factthat the medium flowing out of the nozzle with a great velocity is in contact with a comparatively small surface of the air or gas to be delivered is also one of. the main reasons of the low useful effect of such apparatus It isevident that the greater the diameter of the nozzle, the smaller in comparisonwitli said diameter the surface over which the working medium is in contact with the air to be delivered.
Experiments have shown that the outer and inner walls of an annular nozzle when the apertures of such nozzle are normal, always came into contact with one another2 so that the passage of the steam at the said points in .contact was completely prevented, whilst on the diametrically opposite .side of the nozzle the width of the annular orifice was doubled. rlhe consequence of such a deviation is naturally that no closed steamcone can be formed and therefore the action of the ejectors fails or is incomplete. Nevertheless, in order to produce under such circumstances a delivery of air or gas an ajierture had to be provided on the side where the outer and inner walls of the nozzle touch each other, so that there should be there also an adequate flow of steam from the nozzle. On the diametrically opposite side where the walls were at too great a distance from each other, .the enlarge(` cross section remained. so that there was always a very considerable flow of steam which was wasted. This explains the extraordinary high consumption of steam with the present devices.
Now the object of this invention is to reduce this consumption of steam in ejections for large deliveries and such result is obtained by an absolutely exact centering of the outer and inner. walls of an annular nozzle and the extension of the surface of contact between the active medium and the gas or air to be delivered.
l According to this invention the outer and the inner walls of the .annular nozzlel which are independent run concentrically for a considerable distance up to the point of smallest cross sect-ion. The annular space between said walls isl divided into a circle of channels by radial ribs extending in an axial directionvwhich ribs may be helically arranged whilst the Ytwo cylindrical nozzle walls are centered relativelyy to eachother by said ribs. Hence areliable centering of the nozzle walls under all circumstances 1s obtained, whilsta longitudinal displacement of said walls, with referenceto each other is also possible. l
Further and .according to the invention, the outer nozzle Wall or the inner, one or both on that portion of the annular nozzle which widens towards the .orifice can be provided with grooves extending in an axial gas or the effective medium and the medium to be delivered.
The cross section of the grooves provided in the nozzle walls may conveniently be gradually enlarged towards the outlet orifice of the nozzle` For .instance with the same width, the depth ot the groove may be graduallv increased in the direction ot' the orifice ot the nozzle. f
A 'nozzle uiade in accordance with this invention is illustrated by way of example, iii the accompanying drawing.
Fig. 1 shows a longitudinal section of an ejector according to this invention.
Fig. 2 is a similarlongitudinal section showing a n'ioditied construction.
Fig. 3 is an end elevation ot the discharge end or nozzle ot the ejector shown in Fig. 2.
Fig. 4 isa partial perspective view of the end ot the nozzle drawn toa larger scale.
Fig. is a longitudinal section through one of the nozzle passages also drawn to a larger scale. y
rIhe usual arrangement ot ejectors with au Aannular nozzle may be regardedl as known. In the'construction shown in Fig. 1 ot' the drawing 1 is the casing ot the ejector which is provided with an inlet 2 t'or the active medium (steam). The passage 2 leads to an annular chamber 3 to which is connected the cylindrical outer wall '4T ot' the nozzle. rl'lhe inner wall ot said nozzle is formed by a tube 5 which is arranged concentrially with the wall et. Between the outer wall 4 and the inner wall 5 there remains an annular space 6 which is divided into acircle ot' passages S running in an axial direction by radial ribs 7 extending in a axial direction and it desired helically arranged. The ribs 7 extend across the annular space (i so that the nozzlc walls are centered b v said ribs which iualy be made in one piece with the inner wall or with the outer wall et. The ribs may also be ,connected to the outer and iiiner walls alternately. The tube' 5 forming thcinncr wall is also supported at 9 by the body of the casing and made tight against the steam chamber by a stuiiing boX it. l1. VThe admission ot the gas delivered or of the air to be delivered occurs in two places,` centrally through the inside of the tube o by means of the apertures 12 at the rear end thereof to which it gains access through `the flanged inlet 13.
l into fcontact. with the outer surface of the AThe portion ot the gas to Vbe delivered which does not flow through the aperture 12 reaches the annular space 14' and comes conical steam jetissuing from the end of the nozzle. At the front end of the casing 1 a flange 15 is provided by means of which the ejector casing is coupled in the usual way with a conical ejector tube 16. At the rear end the ejector casing is closed by means ot a cover 17. j
lt is evident that in the construction adopted a very accurate centering ot the walls of the annular nozzle is obtained and that there is no longer any danger ot any deviation or any inequality arising in the cross section of the passage or ot' even any contact o't' the walls with the nozzle at point 18 where the cross section of the nozzle is si'nallest. ltwill be seen, that the inner diameter ot the outer wall widens conically at 20 from the point 18 ot' the narrowest cross section towards the orifice 19, whilst the outer surface of the inner wall 21 gradually decreases.
Fig. 2 illustrates a inodiied torni of construction` where the portion ot the outer wall of the nozzle which lies between the point of the smallest cross section 18 and the orifice 19 is provided with longitudinal grooves 22. The said longitudinal grooves are made 'oit uniform width, whilst their depth .increases gradually towards the orilice ot the annular nozzle. The` inner wall ot the annular nozzle is constructed in the saine manner as in Fig. 1 i. e. with a smooth surtace. However in accordance with the invention the inner walls of the nozzle instead of the outer ones may be provided with similar grooves. It desired, both walls otl the nozzle may be provided with such grooves. Y y
Owing to the particular form of the walls ot the nozzle., the issuing jet of the active medium (steam) assumes an undulated sur- `face and thus provides a considerably larger surface of Contact with the gas to be delivered. In consequence of this arrangement the useful effect of the delivery is considerably augniented so that for a given largequantity of air orgas to be delivered the consumption of 'steam i. e. the working medium isr comparatively small.
lVhat we Vclaim is:
1. A 'steam gas or vapour operated gas or air ejector for the delivery of large kquantities having an annularnozzle cen trally arranged in the casing ot the ejector for the inlet of the workingmedium, characterized by the fact that in rear ot the smallest cross section (18) of the annular nozzle the outer wall (4t) and the inner wall of the nozzle (5) which is independent of the former run concentrically for a considerable distance and the space (6) between thein is divided into a circle of passages (8) by radial o r helical ribs (7) extending in an axial direction whilst both walls of the nozzleA are centered relatively to each other by said ribs. y
2. Thevinvention as claimed in claim 1,
wherein one of the opposed and nozzle-defining walls is provided with axially extending grooves, which grooves provide an undulating surface for the jet issuing from the nozzle.
3. The invention as claimed in claim I, wherein both of the opposed and nozzle-'defining walls are provided with axially extending grooves, which grooves provide an undulating surface for the jet issuing from the nozzle.
4. In a large capacity ejector for delivering air or gases, coaxial tubular walls dyel'ining therebetween an, annular space for the passage of a motive fluid, the cross section of said annular space at an intermediate section beingsmaller than at either end thereof, a plurality of ribs between said tubes and in rear of the smaller cross section for maintaining the coaxial alignment of said tubes.
5. In a large capacity ejector for delivering air or gases, a casing, coaxially arranged tubes in said casing and having opposed walls defining therebetween an annular space for the passage of a motive fluid, the cross section of said space contracting from the outer ends of said tubes to an intermediate section thereof, means in rear of said intermediate section for maintaining said tubes in coaxial alignment, means permitting the delivery of motive fluid to said annular space at the rear thereof, and means permitting the delivery of air or gases to the inside of the inner tube and around said outer tube.
6. In an ejector for delivering gas or gases, a casing, a motive fluid passage leading into said casing and terminating in an annular chamber, a wall extending forwardly from said chamber providing a cylindrical outer nozzle member, a second cylindrical nozzle member within said outer member and ribs between said members for maintaining the same'in coaxial alignment, said ribs terminating in rear ofthe outlet end of saidV nozzle, whereby an annular stream of motive fluid may be delivered therefrom.
7. In an ejector, a casing, a motive fluid chamber within said casing, a passage extending from the exterior of said casing to said chamber for delivering motive fluid thereto, a cylindrical wall extending forwardly of said chamber to rovide an outer nozzle member, a second cyfindrical member having the rear portion thereof supported by and in Huid tight engagement with the rear wall of said chamber, and spacing ribs between said members adjacent said chamber for maintaining the same in coaxial alignment, the opposed walls of said members diverging from each other towards the outlet end of said nozzle to provide space of increasing cross-section for the passage of the motive fluid.
S, In an ejector, a nozzle having inner and outer members defining an annular passage through which motive fluid may be delivered, one of the opposing walls provided by said members being grooved, whereby the jet of motive fluid assumes an undulating surface.
9. In an ejector, a pair of tubular members defining a` nozzle, the passage through said nozzle being of smallest cross-section at' an intermediate section thereof, spacing means between said members in rear of the smallest cross-section for maintaining said members in coaxial alignment, one of the opposing walls provided by said members being formed with grooves which gradually increase in cross-section from the smallest cross-section of said nozzle towards the outlet end thereof.
lO. The invention as claimed in claim 9, wherein said grooves are of uniform width throughout their length and of graduallyincreasing depth towards the nozzle end.
11. In an ejector for air or gases, a nozzle comprising an inner member having an .outer wall of gradually increasing diameter from the nozzle/end towards the rear thereof, and an outer member having' an inner wall provided with spaced axial grooves opposing the tapering wall of said inner member.
12. In an ejector for air or gases, a nozzle comprising a pair of tubular members, longitudinally extending ribs between said members for maintaining the same incoaxial alignment, said ribs terminating short of the outletend of the nozzle to provide an unobstructed annular outlet for said nozzle, axial grooves of increasing cross section extending along the wall of one of said members from a point in front of said ribs to the end of said nozzle, the wall of the other member gradually diverging from said grooved wall.
In testimony whereof we have hereunto set our hands.
JAKoB MULDER. DIRK oHRIsTIAAN ENDERT.
US733858A 1924-08-23 1924-08-23 Ejector for the delivery of gas and air in large quantities Expired - Lifetime US1574677A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US733858A US1574677A (en) 1924-08-23 1924-08-23 Ejector for the delivery of gas and air in large quantities

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US733858A US1574677A (en) 1924-08-23 1924-08-23 Ejector for the delivery of gas and air in large quantities

Publications (1)

Publication Number Publication Date
US1574677A true US1574677A (en) 1926-02-23

Family

ID=24949391

Family Applications (1)

Application Number Title Priority Date Filing Date
US733858A Expired - Lifetime US1574677A (en) 1924-08-23 1924-08-23 Ejector for the delivery of gas and air in large quantities

Country Status (1)

Country Link
US (1) US1574677A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3047208A (en) * 1956-09-13 1962-07-31 Sebac Nouvelle Sa Device for imparting movement to gases
FR2620491A1 (en) * 1987-09-10 1989-03-17 Wiederaufarbeitung Von Kernbre JET PUMP WITH PROPELLER PIPE
US20150093261A1 (en) * 2009-05-15 2015-04-02 Ford Global Technologies, Llc Nozzle insert for boosting pump inlet pressure
US10962028B2 (en) * 2018-01-05 2021-03-30 Hamilton Sundstrand Corporation Additively manufactured ejector pump

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3047208A (en) * 1956-09-13 1962-07-31 Sebac Nouvelle Sa Device for imparting movement to gases
FR2620491A1 (en) * 1987-09-10 1989-03-17 Wiederaufarbeitung Von Kernbre JET PUMP WITH PROPELLER PIPE
BE1001124A3 (en) * 1987-09-10 1989-07-25 Wiederaufarbeitung Von Kernbre Pump jet a nozzle booster.
US20150093261A1 (en) * 2009-05-15 2015-04-02 Ford Global Technologies, Llc Nozzle insert for boosting pump inlet pressure
US10962028B2 (en) * 2018-01-05 2021-03-30 Hamilton Sundstrand Corporation Additively manufactured ejector pump

Similar Documents

Publication Publication Date Title
US2444615A (en) Eductor
US3920187A (en) Spray head
US1151259A (en) Jet apparatus.
US2486019A (en) Jet control apparatus applicable to entrainment of fluids
US1574677A (en) Ejector for the delivery of gas and air in large quantities
US2061032A (en) Jet pump
US2189532A (en) Heat transfer apparatus
US1531877A (en) Oil burner
US1543834A (en) Ejector
US355250A (en) Talmadge blass
US1267897A (en) Air-pump.
US1447103A (en) Translating device
US1175462A (en) Ejector.
US1580177A (en) Method of and apparatus for compressing fluid
US733579A (en) Hydrocarbon-burner.
US1457777A (en) Jet augmenter or ejector
US950598A (en) Spiral-jet injector.
US344480A (en) holden
JP2006334585A (en) Steam cleaning auxiliary agent ejector nozzle
US297511A (en) Injector
US1506908A (en) Jet augmenter or ejector
US1388670A (en) A corpoba
US199530A (en) Improvement in injectors
US799809A (en) Nozzle for elastic-fluid turbines.
US817620A (en) Injector.