US2433539A - Blowpipe nozzle - Google Patents

Blowpipe nozzle Download PDF

Info

Publication number
US2433539A
US2433539A US525657A US52565744A US2433539A US 2433539 A US2433539 A US 2433539A US 525657 A US525657 A US 525657A US 52565744 A US52565744 A US 52565744A US 2433539 A US2433539 A US 2433539A
Authority
US
United States
Prior art keywords
nozzle
recess
gas
oxygen
passages
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
US525657A
Inventor
Earl E Westerman
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.)
Linde Air Products Co
Original Assignee
Linde Air Products Co
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 Linde Air Products Co filed Critical Linde Air Products Co
Priority to US525657A priority Critical patent/US2433539A/en
Application granted granted Critical
Publication of US2433539A publication Critical patent/US2433539A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles
    • F23D14/52Nozzles for torches; for blow-pipes
    • F23D14/54Nozzles for torches; for blow-pipes for cutting or welding metal
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49348Burner, torch or metallurgical lance making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49428Gas and water specific plumbing component making
    • Y10T29/49432Nozzle making

Definitions

  • Flame machining includes cutting, gouging, and surface conditioning. Since flame cutting is based on a chemical reaction, the thickness of the metal to be cut imposes relatively little difficulty. Flame cutting thus provides a rapid and economical method for severing steel, wrought iron and cast iron. Special techniques have been developed for flame cutting cast iron and certain alloy steels as well as for certain special cutting operations such as removing rivets, preparation of plate edges for welding, and cutting heavy Flame gougin provides a means for quickly and accurately removing a narrow strip of surface metal from steel plates, forgings, and castings. The principle of flame gouging is based on the fact that the nozzle is designed to deliver process is variously known as deseaming, scarfing, or conditioning. Generally, however, the term deseaming, i.
  • Fig. 9 is a view similar to Fig. 7 after the two longitudinal preheating oxygen passages have been formed in the nozzle.
  • Fig. 10 is a fragmentary view similar to Fig. 8,
  • each fuel-gas passage i1 is composed of a relatively long inlet section I 8 of constant diameter, and a relatively short outlet section IQ of substantially smaller constant diameter than that of the inlet section l8.
  • the inlet section may be made with a No. 54 drill (0.055 inch in diameter), and the outlet section IS with a No. 59 drill (0.041 inch in diameter).
  • the end face 20 of the nozzle N is counterbored to provide a separate recess 2
  • Preheat oxygen is supplied to the annular channel 24 by at least two longitudinally extending preheat oxygen supply passages 26 which are disposed along opposite sides of the longitudinal axis of the nozzle N. These passages, in the lilustrated example, are preferably made with a No. 42 drill. Radial inlets 27 of the same diameter are provided between frusto-conical seats 28 and 29 for feeding preheating oxygen to the inlet ends of the passages 26, the end portions of the passages 28 being hermetically sealed by plugs 30.
  • some prior post-mixed nozzles have another disadvantage in that it is possible to force oxygen up the acetylene orifices. This is possible when a piece of slag or scale plugs up acetylene, may be fed to of carbon is inhibited as is any tendency ofthe' passages to become plugged with slag. Still further, there is no possibility of preheat oxygen being forced back up the acetylene discharge passages because the preheat oxygen and acetylene the end of the nozzle. It is also possible when the v oxygen fiow is great enough to cause a pressure on the external opening of the preheat orifice which is greater than the acetylene pressure. It can be readily understood that this causes a burning back in the acetylene supply. It has been further found that a soft carbon deposition is left on the seats of some prior post-mixed nozzles which causes them to plug up.
  • the shape of the oxidizing gas passage may be changed to adapt the stream of oxygen discharged from the nozzle for any desired use, such as cutting or gouging, or such passage may be omitted in which case one or any number of the oxy-fuel gas flames may be used for welding or any other function involving high temperature flames.

Description

E. E. WESTERMAN BLOWPIPE NOZZLE Filed March 9, 1944 2 Sheets-Sheet 1 f Q 1 1 V//AV////l// /W l4 l7 [Z 17 Z 1 Z4 g5 27 2g EARL .E. WESTERMAN sections.
Patented Dec. 30, .1947
titan F ElCE BLOWPIPE NOZZLE Earl E. Westerman, Gary,
Ind., asslgnor to The Linde Air Products Company, a corporation of Ohio Application March 9, 1944, Serial No. 525,657 7 Claims. (Cl. 158-27.4)
This invention relates to blowpipe nozzles and more particularly to flame machining nozzles.
Above a red heat, iron combines with pure oxygen so rapidly that it actually burns. Thus, if a spot on a piece of iron or steel is heated to the kindling temperature, and a jet of oxygen directed at the heated spot, the iron will burn vigorously with the generation of heat. Although the result of such combination of iron and oxygen is the formation of iron oxide, a product that is solid at ordinary temperatures, the iron oxide melts at a temperature somewhat below the melting point of iron or steel. During flame machining, the heat generated by the burning iron is sufli cient to melt the iron oxide so that it runs 01? as a molten slag, not only exposing more iron to the action of the oxygen stream, but also carrying away with it some iron that has become molten at the temperature of the operation, but which has not actually become oxidized. The result of this combination of circumstances makes it possible to flame machine iron andsteel.
In flame machining, radiation at the surface, pieces of dirt, paint or scale on the metal, and the fact that heat is conducted away from the relatively cold metal beside the out make it necessary for additional heat to be supplied or the reaction will stop. Therefore, the flame machining blowpipe nozzle is provided with a number of small orifices for oxy-fuel gas heating flames surrounding a central opening that supplies the oxygen stream. Such preheat flames are used to heat a spot on the work, to a red heat. The machining operation is then started by opening a valve controlling the oxygen stream and directing such stream at the heated spot. The preheating flames remain burning while cutting is in progress to make up for the heat that is lost during the operation.
Flame machining includes cutting, gouging, and surface conditioning. Since flame cutting is based on a chemical reaction, the thickness of the metal to be cut imposes relatively little difficulty. Flame cutting thus provides a rapid and economical method for severing steel, wrought iron and cast iron. Special techniques have been developed for flame cutting cast iron and certain alloy steels as well as for certain special cutting operations such as removing rivets, preparation of plate edges for welding, and cutting heavy Flame gougin provides a means for quickly and accurately removing a narrow strip of surface metal from steel plates, forgings, and castings. The principle of flame gouging is based on the fact that the nozzle is designed to deliver process is variously known as deseaming, scarfing, or conditioning. Generally, however, the term deseaming, i. e., the removal of scams or cracks, is used when the operation is performed In such case, only those with a hand blowpipe. defects that are visible are removed. In mechanized steel conditioning the entire surface of the billet, bloom or slab is removed by a flame conditioning machine set into the rolling mill line. Such machine is adapted to remove thermochemically a thin layer containing surface defects from one, two, or all si es of the body simultaneously, the operation being performed while the metal is still hot and without interrupting the rolling operation. Secondary conditioning involving the removal of deeper defects may be performed by hand deseaming after the work has cooled down.
It has been customary in the past to supply the preheating flames in flame machining with a fuel gas such as acetylene and a combustion-supporting gas suchas oxygen, through a blowpipe or nozzle equipped with internal means for mixing such gases before the gas mixture is delivered to the nozzle or a mixed-gas passage in the nozzle. In any case the combustible gas mixture is highly explosive and such premixed blowpipe apparatus is subject to backfire and flashback. Either phenomenon is highly undesirable, because the internal passages of the apparatus become fouled with carbon in the case of backflre, and burned in the case of flashback, necessitating costly repair'and dismantling of the entire apparatus for cleaning. A premixed flame or nozzle is one wherein the combustible mixture for the flame is formed by mixing a fuel gas and a combustionsupporting' gas before these gases are discharged from a nozzle.
In order to overcome such difliculty it has been proposed in the past to mix the fuel gas and combustion-supporting gas externally of the nozzle to form post-mixed preheating flames. A postmixed flame or nozzle is one wherein the combustible mixture for the flame is formed by mixing a fuel gas and a combustion supporting gas substantially upon discharge or after these gases are discharged from a nozzle. However, postmixed nozzles which have been made in the past,
especially nozzles for flame machining, are difligouged out of I lene discharge passages. This happens, for example, when a piece of slag or scale plugs up the end of the nozzle. It is also possible, when the oxygen flow. is great enough, to cause a pressure on the external opening of the preheat orifice which is greater than the acetylene pressure. It can be readilyunderstood that this causes a burning back or flashback in the acetylene supply passages. It has also been found that a soft carbon deposit is formed on the seats of some prior postmixed nozzles which causes such nozzles to plug up and become ineflective.
The main-objects of this invention are to provide an improved blowpipe nozzle which overcomes the difficulties and disadvantages of the prior art, which nozzle is adapted to be used efhciently for scarfing, cutting, gouging and similar functions involving the thermochemical working or machining of ferrous metals and the like with oxy-fuel gas flame and oxygen, such expensive to manufacture, because of Fig. 2 is a similar view of the nozzle taken on I line 22 of Fig. 3;
Fig. 3 is a view in front end elevation of the nozzle;
Fig. 4 is a cross-sectional view taken on line seaming nozzle;
Fig. 7 is a view in longitudinal section taken on line 1| of Fig. 6;
Fig. 8 is a view similar to Fig. 6 of the nozzle after the preheating gas passages have been modiimproved nozzle being simple and economical to backs and backfires of the preheating flames are inhibited by introducing the preheat oxygen at an inclination to the wall of a recess or counterbore through which the fuel gas is discharged.
The dimensions of such recess are critical, being such that burning of the mixed gases takes place at the extreme outlet of the recess.
More particularly, there is provided according to the invention a desurfacing nozzle having an axial oxidizing gas discharge passage, a group of acetylene discharge passages disposed on each side of such oxidizing gas passage in arcs concentric with the longitudinal axis of the nozzle and terminating in counterbores the depth of which is of the order of twice the diameter thereof. The cross-sectional area of each counterbore is of the order of twice that of the acetylene discharge passage. Each counterbore is provided with a relatively short inclined preheat oxygen discharge passage terminating in the side wall adjacent the bottom of the counterbore. Communicating with the preheat oxygen discharge passages is an annular preheat oxygen distributing channel or passage to which preheat oxygen is supplied by a pair of preheat oxygen supply passages which extend longitudinally of the nozzle. A removable cover is provided for the preheat oxygen distributing channel, providing ready access to such channel and all of the preheat oxygen discharge passages.
In the accompanying drawing:
Fig. l is a fragmentary longitudinal cross-sectional view taken on line l-i of Fig. 3 of a desurfacing blowpipe nozzle exemplifying-the invention;
Fig. 9 is a view similar to Fig. 7 after the two longitudinal preheating oxygen passages have been formed in the nozzle; and
Fig. 10 is a fragmentary view similar to Fig. 8,
showing the discharge end portion of the nozzle after the annular recess, the preheat oxygen distribution channel, and the inclined preheat oxy gen outlet passa es have been formed, and a crosssectional view of the cover about to be telescoped in position on the nozzle.
Referring to the drawings/a nozzle N is shown which comprises an elongated body of metal, such as copper, the surface of which may be chromium plated if desired. Extending longitudinally through the nozzle N is a cutting oxygen or oxidizing gas passage l0 composed of an inlet section ll of constant diameter, a frust0-conica1section l2, a relatively short medial section l3 of constant diameter larger than that of said inlet section l2, 2. section M the cross-section of which changes gradually from circular to oblong shape, and an outlet section l5 having flared side walls l6, It. The oxidizing gas passage l0 thus is adapted to discharge a characteristic stream of cutting oxygen which is suitable for deseaming, desurfacing, scarfing, and the like. The shape of the oxygen discharge passage l0 may be changed, as desired, depending upon the work to be done.
In suitable arcs, concentric with the longitudinal axis of the nozzle N, above and below the ML dizing gas passage 10, a plurality of longitudinally extending fuel-gas passages I! are provided in the nozzle N. Each fuel-gas passage i1 is composed of a relatively long inlet section I 8 of constant diameter, and a relatively short outlet section IQ of substantially smaller constant diameter than that of the inlet section l8. By way of example, the inlet section may be made with a No. 54 drill (0.055 inch in diameter), and the outlet section IS with a No. 59 drill (0.041 inch in diameter). The end face 20 of the nozzle N is counterbored to provide a separate recess 2| in axial alignment with each of the fuel-gas passages i7. Where the fuel-gas discharge passage I9 is made with a No. 59 drill, the recess 2i is preferably made with a No. 54 drill, the depth of the recess being of the order of twice the diameter thereof, in this case, of the order of a: inch deep, since equals 0.0937, and 2 times 0.055 equals 0.110. The cross-sectional area of the recess 2i is of the order of twice that of the acetylene discharge passage I9.
A peripheral recess 22 of constant diameter ex tending rearwardly from the end face of the nozzle 20 is provided for receiving a ring or sleeve 23 which may be press-fitted in place, the rear edge of the ring engaging the shoulder provided by the recess 22 to prevent rearward displacement 'the recess 22. Extending assasse of the ring when the nozzleis in use. Such ring constitutes a removable cover for an annular preheat oxygen distribution passage or channel 24 in theperiphery of the nozzle N in the area of from the channel 24 to the side Wall Of each reces 2l and adjacent the bottom thereof, is a slightly inclined preheat oxygen discharge passage 25. All of the passages 26 communicate with the channel 2t.
Preheat oxygen is supplied to the annular channel 24 by at least two longitudinally extending preheat oxygen supply passages 26 which are disposed along opposite sides of the longitudinal axis of the nozzle N. These passages, in the lilustrated example, are preferably made with a No. 42 drill. Radial inlets 27 of the same diameter are provided between frusto- conical seats 28 and 29 for feeding preheating oxygen to the inlet ends of the passages 26, the end portions of the passages 28 being hermetically sealed by plugs 30.
Thus, fuel gas, such as the inlet ends of the fuel-gas supply passages l'l between the frusto-conical seat 29 and a frustoconical seat 3|. Cutting oxygen is delivered to the inlet end of the oxidizing gas passage ill by any suitable connection.
In operation, preheat oxygen and acetylene are delivered to the passages 26 and, respectively, at suitable pressures, so that the recesses 2| discharge streams of combustible gas mixture composed of oxygen and acetylene, which streams, when ignited, produce work-preheating flames of high eiliciency. The nozzle N is positioned so that such oxy-acetylene flames heat the work to the ignition temperature, whereupon oxygen is supplied to the oxidizing gas passage ll) of the nozzle, being discharged from the nozzle at a suitable velocity for thermochemical reaction with the heated work. The nozzle N is then moved with respect to the surface of the work so as to thermochemically condition or remove a layer of surface metal therefrom in the usual way.
The preheat flames of the present nozzle simulate those of a standard premixed type of nozzle, but such flames do not have the unsatisfactory flame pattern produced by prior post-mixed nozzles. Prior post-mixed nozzles do not work satisfactorily on high alloy steels due to the lack of' preheat. When it is necessary to increase the oxygen flow through such prior post-mixed nozzles, the preheat flame becomes dispersed and the acetylene fans out so as to become fairly ineffectlve. With the nozzle of the present invention, however, the preheat flame pattern may be adiusted to conform to any satisfactory arrangement.
Furthermore, some prior post-mixed nozzles have another disadvantage in that it is possible to force oxygen up the acetylene orifices. This is possible when a piece of slag or scale plugs up acetylene, may be fed to of carbon is inhibited as is any tendency ofthe' passages to become plugged with slag. Still further, there is no possibility of preheat oxygen being forced back up the acetylene discharge passages because the preheat oxygen and acetylene the end of the nozzle. It is also possible when the v oxygen fiow is great enough to cause a pressure on the external opening of the preheat orifice which is greater than the acetylene pressure. It can be readily understood that this causes a burning back in the acetylene supply. It has been further found that a soft carbon deposition is left on the seats of some prior post-mixed nozzles which causes them to plug up.
Although, in the present nozzle, which may be designated an open mixed nozzle to distinguish it from prior post-mixed nozzles, no carbon is deposited at any point in the nozzle, it can be carbon may be removed by simply drilling it out,
'to a depth of a", inch since are supplied at very nearly equal pressures.
e depth of the counterbores or recesses 2i constituting the preheat orifices in the front end of the nozzle N is very important. If such counterbore is too deep, the preheat acetylene and oxyen tend. to burn within the counterbore and cause overheating of the nozzle. In'the preferred example, it is necessary to limit such counterbore this Just permits the burning of the mixed gas at the extreme outlet of the counterbore. The cross-sectional area of each of the heatingfiame recesses is also critical, being less than that of the sum of the cross-sectional areas of the preheat oxygen and acetylene discharge passages 25 and i9, but greater than the cross-sectional area of either one of such two passages. The cross-sectional area of the recess 2| should as discharge passage IQ for good results.
Nozzles may be'made embodying the principles of this invention, by converting a standard premixed type of nozzle having standard preheat drillings, to the present type. complished by a back drilling and a front drilling with a No, 59 drill to form the inlet section l8 and outlet section l9, respectively, of the fuel-gas passages H. The preheat oxygen supply passages 25 are drilled through their entire length with the largest size drill permissible without damaging the seat 29, which in thepresent example is a No. 54 drill. Such two drilled holes 25, which are used for the preheat oxygen, are closed adjacent the seat 29 with plugs 30. The cross drillings 21 are then made apart with a No. 54 drill between the preheat seating surface 29 of the nozzle N and a nozzle nut ring or flange 32. The front ends of the remaining open preheat drillings I 9 are then counterbored with a No. 54 drill, to a depth of the order of 3% inch. to provide the recesses 2i. down to provide the annular recess 22 and the channel 24. The preheat oxygen discharge passages 25 are then made with a No. 60 drill so as to join the preheat oxygen distribution channel 24 with each of the ten preheat flame recesses 2|. All exterior holes are then plugged with copper. Any suitable block or head may be usd to deliver This may be acwith a No. 54' drill preheating oxygen and ,aceteylene, as well as the cutting oxygen, to their respective inlets at the rear end of the nozzle.
The cover 23 for the annular preheat oxygen distribution passage 24 is preferably in the nature of a slip ring or sleeve which is adapted frictionally to engage the annular recess 22 at opposite sides of the channel 24 so as to prevent any leakage of the preheat oxygen. It is not necessary to solder or weld such ring to the nozzle, it being preferably press-fitted in place. The preheat oxygen orifices or passages 25 are preferably large enough to permit the passage of enough oxygen to produce a neutral flame. The length and diameter of the preheat flames are dependent upon the diameter of the counterbores 2 l.
The open mixed nozzle of the present invention has a great many advantages over prior postmixed. nozzles. Such advantages include the novel method of introducing preheat oxygen to be of the order of twice that of the fuel-- The nozzle is turned.
the flamerend of the nozzle, This makes it easier to manufacture the nozzle than prior post-mixed nozzles, and provides a nozzle the internal passages of which can be readily cleaned. It will be understood that this advantage is equally applicable to cutting nozzles, as well as desurfacing nozzles. The recessed flame ports 2f require less precision from a manufacturing standpoint than where the oxygen and acetylene ports intersect at a surface of the nozzle as in prior post-mixed nozzles. Nozzles of the present invention also have substantially the same operating characteristics as premixed nozzles, without being subject to backfire or flashback difficulties.
The shape of the oxidizing gas passage may be changed to adapt the stream of oxygen discharged from the nozzle for any desired use, such as cutting or gouging, or such passage may be omitted in which case one or any number of the oxy-fuel gas flames may be used for welding or any other function involving high temperature flames.
Whatis claimed is:
1. A flame machining blowpipe nozzle having an end face, a work oxidizing gas discharge passage terminating in said end face, a work preheating flame recess spaced from said oxidizing gas discharge passage in said end face, a fuel gas discharge passage terminating in the bottom of said recess, and a combustion-supporting gas discharge passage terminating in the side wall of said recess adjacent the bottom or said recess, the shape of said recess being such that, when fuel gas and combustion-supporting gas are discharged into said recess from said fuel-gas and combustionsupporting gas discharge passages, a highly combustible' gas mixture is formed within and discharged in the form of a stream from said recess, such stream, when ignited, being adapted to produce a work preheating flame which is not subject to flashback or backfire, said recess having an annular side wall concentric with a prolongation of the longitudinal axis of said fuel-gas discharge passage,the cross-sectional area of said recess in a plane at right angles to said axis being equal to a value which is less than the sum of the crosssectional areas of said fuel-gas discharge passage and said combustion-supporting gas passage, but greater than the cross-sectional area of either one of such two passages, being of the order of twice that of the fuel-gas discharge passage, and the depth of said recess being of the order of twice the diameter of said recess.
2. A flame machining blowpipe nozzle having an end face, a work oxidizing gas discharge passage terminating in said end face, a plurality of work preheating flame recesses spaced from and disposed about said oxidizing gas discharge passage in said end face, a fuel-gas discharge passage terminating in the bottom of each recess, and a combustion-supporting gas discharge passage terminating in the side wall of each recess adjacent the bottom of said recess, the shape of each recess being such that, when fuel-gas and combustionsupporting gas are discharged into said recess from the fuel-gas and combustion-supporting gas discharge passages, a highly combustible gas mixture is formed within and discharged in the form of a stream from said recess, such stream, when ignited, being adapted to produce a work preheating flame which is not subject to flashback or backfire, each recess having an annular side wall concentric with a prolongation of the longitudinal axis of the fuel-gas discharge passage, the crosssectional area of each recess in a plane at right angles to said axis being of the order of twice the cross-sectional area of said fuel-gas discharge passage, and the depth of each recess being of the order of twice'the diameter of such recess.
3. A blowpipe nozzle having an end face, an annular combustion-supporting gas distribution passage, a plurality of combustion-supporting gas supply passages communicating with said gas distribution passage, a plurality of recesses in said end face, a separate fuel-gas discharge passage terminating in the bottom of each recess, a separate inclined combustion-supporting gas discharge passage communicating with said gas distribution passage and terminating in the side wall adjacent the bottom of each recess, and a work-oxidizing gas discharge passage terminating in said end face, each recess being adapted to discharge a stream of combustible gas mixture composed of fuel gas and combustion-supporting gas, which streams, when ignited, produce work heating flames adapted to cooperate with the work-oxidizing gas discharged from said work-oxidizing gas discharge passage, each recess having a depth and a diameter such that flame flashback and backfire are prevented, the cross-sectional area of each recess being less than the sum of the cross-sectional areas of the fuel-gas passage and combustion-supporting gas passage, and greater than the cross-sectional area of either one of such two passages, and the depth of each recess being of the order of twice thediameter of such recess.
4. A blowpipe nozzle having an end face, an annular combustion-supporting gas distribution passage, a plurality of combustion-supporting gas supply passages communicating with said gas distribution passage, a plurality of heating flame recesses in said end face, a separate fuel gas discharge passage tcrminating in the bottom of each recess, a separate inclined combustiomsupporting gas discharge passage communicating with said gas distribution passage and terminating in the side wall adjacent the bottom of each recess, each recess being adapted to discharge a stream of combustible gas mixture composed of fuel gas and combustion-supporting gas, which streams, when ignited, produce heating flames, each recess having a depth and a diameter such that flame flashback and backfire areprevented, the cross-sectional area of each recess being less than the sum of the cross-sectional areas of the fuel-gas passage and combustion-supporting gas passage, and greater than the cross-sectional area of either one of such two passages, and the depth of each recess being of the order of twice the diameter of such recess, and a removable cover for said annular combustion-supporting gas distribution channel comprising a ring embracing the periphery of the nozzle.
5. A blowpipe nozzle having an end face, an open recess in said end face, a fuel-gas discharge passage terminating in the bottom of said recess,
and a combustion-supporting gas discharge passage terminating in the side wall adjacent the bottom of said recess, the cross-sectional area of said recess being of the order of twice that of said fuel-gas discharge passage, and the depth of said recess being of the order of twice the diameter of said recess.
6. A blowpipe nozzle having an end face, an open recess in said end face, a. gas-discharge passage terminating in the bottom of said recess, and a gas-discharge passage terminating in the side wall adjacent the bottom of said recess, the crosssectlonal area of said recess being of the order of twice that of said first-named discharge passage,
and the depth of said recess being of the order of twice the diameter of said recess, and gas-supply passage means for conducting oxygen to one of said gas-discharge passages and acetylene to the other of said gas-discharge passages, so that the oxygen and acetylene mix in said recess to form a combustible oxy-acetylene gas stream which, when ignited, produces a flame that is not subject to either backfire or flashback.
7. A blowpipe nozzle for cutting or deseaming metal members, such nozzle comprising an elongated body having a longitudinal cutting or deseaming oxygen passage provided with a discharge orifice in one face of said body, said body having a group of relatively short recesses arranged substantially parallel to the axis of said orifice and providing combustible mixture outlets in said face to produce oxy-fuel gas preheating flames substantially parallel to the cutting or deseaming oxygen stream discharged from said orifice, fuel gas passages in said body having the discharge ends thereof severally opening axially into said recesses and of smaller cross-sectional area than said recesses, and combustion-supporting gas passages in said body severally opening into said recesses between said discharge ends of the fuel gas passages and said outlets of the recesses, each gas discharge recess thus being provided with one central fuel gas inlet and one lateral combustionsupporting gas inlet.
EARL E. WESTERMAN.
REFERENCES crrnn The following references are of record in the file of this patent:
UNITED STATES PATENTS Germany May 31, 1819
US525657A 1944-03-09 1944-03-09 Blowpipe nozzle Expired - Lifetime US2433539A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US525657A US2433539A (en) 1944-03-09 1944-03-09 Blowpipe nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US525657A US2433539A (en) 1944-03-09 1944-03-09 Blowpipe nozzle

Publications (1)

Publication Number Publication Date
US2433539A true US2433539A (en) 1947-12-30

Family

ID=24094117

Family Applications (1)

Application Number Title Priority Date Filing Date
US525657A Expired - Lifetime US2433539A (en) 1944-03-09 1944-03-09 Blowpipe nozzle

Country Status (1)

Country Link
US (1) US2433539A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2655988A (en) * 1947-05-24 1953-10-20 Daniel A Marra Gas torch tip having protective terminal shoe
US2694851A (en) * 1948-04-28 1954-11-23 Daniel A Marra Method of forming torch tips
US3836081A (en) * 1973-05-14 1974-09-17 Goss Gas Inc Torch tip and method of fabricating the same
US4535518A (en) * 1983-09-19 1985-08-20 Rockwell International Corporation Method of forming small-diameter channel within an object

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE300705C (en) *
US400827A (en) * 1889-04-02 Gas-furnace
US880099A (en) * 1907-04-05 1908-02-25 Camille Rodrigues-Ely Heating and welding metals.
GB113032A (en) * 1917-03-30 1918-02-07 Josiah Mower Wallwin Improved Method of and Means for Mixing and Controlling Air and Gas as Supplied under Pressure to Burners used for Heating Purposes.
US1283157A (en) * 1917-06-07 1918-10-29 Merton C Green Burner.
US1371309A (en) * 1918-05-18 1921-03-15 Jenkins Alexander Frederick Nozzle for oxyacetylene-torches
CH181091A (en) * 1934-07-16 1935-11-30 Manz Dietrich Fritz Burner head for a device for removing crusts of all kinds on heating surfaces of steam boilers, boilers and the like.
US2286191A (en) * 1939-04-18 1942-06-16 Linde Air Prod Co Mineral piercing and cutting
US2363250A (en) * 1942-09-25 1944-11-21 Alexander F Jenkins Torch tip
US2367316A (en) * 1937-02-27 1945-01-16 Linde Air Prod Co Blowpipe and nozzle therefor

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE300705C (en) *
US400827A (en) * 1889-04-02 Gas-furnace
US880099A (en) * 1907-04-05 1908-02-25 Camille Rodrigues-Ely Heating and welding metals.
GB113032A (en) * 1917-03-30 1918-02-07 Josiah Mower Wallwin Improved Method of and Means for Mixing and Controlling Air and Gas as Supplied under Pressure to Burners used for Heating Purposes.
US1283157A (en) * 1917-06-07 1918-10-29 Merton C Green Burner.
US1371309A (en) * 1918-05-18 1921-03-15 Jenkins Alexander Frederick Nozzle for oxyacetylene-torches
CH181091A (en) * 1934-07-16 1935-11-30 Manz Dietrich Fritz Burner head for a device for removing crusts of all kinds on heating surfaces of steam boilers, boilers and the like.
US2367316A (en) * 1937-02-27 1945-01-16 Linde Air Prod Co Blowpipe and nozzle therefor
US2286191A (en) * 1939-04-18 1942-06-16 Linde Air Prod Co Mineral piercing and cutting
US2363250A (en) * 1942-09-25 1944-11-21 Alexander F Jenkins Torch tip

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2655988A (en) * 1947-05-24 1953-10-20 Daniel A Marra Gas torch tip having protective terminal shoe
US2694851A (en) * 1948-04-28 1954-11-23 Daniel A Marra Method of forming torch tips
US3836081A (en) * 1973-05-14 1974-09-17 Goss Gas Inc Torch tip and method of fabricating the same
US4535518A (en) * 1983-09-19 1985-08-20 Rockwell International Corporation Method of forming small-diameter channel within an object

Similar Documents

Publication Publication Date Title
US2451422A (en) Thermochemical removal of metal with a flux-forming powder in the oxygen cutting stream
US2210402A (en) Method of removing metal from metallic bodies
US2286191A (en) Mineral piercing and cutting
US1958044A (en) Torch for removing defects from billets
US5944915A (en) Cutting nozzle assembly for a postmixed oxy- fuel gas torch
US2470999A (en) Thermochemical metal removal
US6277323B1 (en) Cutting nozzle assembly for a postmixed oxy-fuel gas torch
US3347660A (en) Method for refining metals
US2378346A (en) Apparatus for mixing and burning fuel
US2376413A (en) Blowpipe nozzle
US2290295A (en) Method and apparatus for desurfacing metal
US3966504A (en) Method and apparatus for thermochemical gas scarfing
US2433539A (en) Blowpipe nozzle
US2425710A (en) Blowpipe nozzle
US2356197A (en) Blowpipe device
US2444900A (en) Blowpipe apparatus
US2356196A (en) Blowpipe apparatus
US2365411A (en) Deseaming apparatus
US2536201A (en) Thermochemical metal removal method and apparatus
US2425709A (en) Blowpipe nozzle
US2484891A (en) Post-mixed blowpipe and method of thermochemically cutting metal
US2210403A (en) Method of removing metal from metallic bodies
US2181135A (en) Multiple flame nozzle
US2897884A (en) Cutting torch tip construction
US2334257A (en) Method of making blowpipe nozzles