US2517622A

US2517622A - Pierce severing

Info

Publication number: US2517622A
Application number: US756057A
Authority: US
Inventors: Roger S Babcock
Original assignee: Linde Air Products Co
Current assignee: Linde Air Products Co
Priority date: 1947-06-20
Filing date: 1947-06-20
Publication date: 1950-08-08
Anticipated expiration: 1967-08-08

Description

Aug. 8, 1950 R. s. BABCOCK PIERCE SEVERING 2 Sheets-Sheet 1 Filed June 20, 1947 laq J INVENTOR ROGER s. BABCOCK ATTORNEY R. S. BABCOCK PIERCE SEVERING Aug. 8, 1950 2 Sheets-Sheet 2 Filed June 20, 1947 lllllllllllllllllHHIIIHHH lllllllll n N m w A Patented Aug. 8, 1950 PIERCE SEVERIN G Roger S. Babcock, Plainfield, N. J., assignor to The Linde Air Products Company, a corporation of Ohio Application June 20, 1947, Serial No. 756,057

11 Claims. l

This invention relates to pierce severing of rolled metal stock, and more particularly to method and apparatus for cutting thin flat metal strip into lengths by the oxy-fuel blowpipe.

It is necessary in a number of metal fabricating procedures, for instance in the rolling of wheel rim stock, to cut strip produced in lengths of for example 125 feet into shorter lengths for more convenient handling. Mechanical shears for this purpose are expensive, and conventional methods employing an oxy-fuel cutting blowpipe to traverse the width of the strip are too slow to keep up with other units in the usual production line.

Objects of the present invention are to provide a simple, rapid and economical method and apparatus for oxy-fuel severing of thin flat metal strip, to permit preheating and cutting through the strip without movement of the nozzle or cuttin oxygen jet relative to the strip.

Other objects and features of novelty will be apparent from the following description and the accompanying drawings, in which:

Fig. 1 is a perspective view of apparatus for carrying out the method, both according to the preferred embodiment Of the present invention;

Fig. 2 is a section through the nozzle, taken along the line 2-2 of Fig.

Fig. 3 is an end elevation of the nozzle in position to project the cutting oxygen perpendicularly to the strip;

Fig. 4 is an end elevation of the nozzle in position beneath the strip, to project the heating flames perpendicularly to the strip, and. showing in dotted lines the position to project the cutting oxygen perpendicularly to the strip from below;

Fig. 5 is a plan view of the nozzle shown in Fig. 1;

Fig. 6 is a longitudinal vertical section taken along the line 6-6 of Fig. 5;

Fig. 7 is a longitudinal vertical section taken along the line l'[ of Fig. 5; and

Fig. 8 is a transverse vertical section taken along the line 8-8 of Fig. 7.

According to the present invention the thin fiat metal strip is severed by directing against one surface of the strip a sheet of oxy-fuel preheat flame extending transversely of the strip for the full width thereof to heat a narrow transverse band of the metal to oxygen ignition temperature, and thereafter directing a similar sheet of cutting oxygen against the preheated band to pierce through the metal and sever the strip.

The gases are projected by an integral or double nozzle, which has respective rows of preheat gas and oxygen passages spaced sufficiently close to project sheet or ribbon jets. The rows of passages preferably converge to the same bandon the surface of the strip. The nozzle may be stationary during the preheat and cutting steps, the separate steps being controlled by valve manipulation.

Alternatively the nozzle may be positioned to impinge the preheat flame vertically, and thereafter pivoted to project the cutting oxygen vertically against the preheated band. The nozzle may be positioned either above or below the strip for any of these operations.

As shown in Fig. 1, the strip W is supported on rolls R of a cooling bed or roll table, preferably in heated condition as delivered thereto from the rolling operation. Spaced along the roll table are a plurality of oxy-fuel bl-owpipes B terminating in transversely elongated nozzles N which extend the full width of the strip W. The nozzles N are provided with a row of closely spaced orifices which project a sheet of preheating flame P to impinge against a narrow transverse band on the surface of the strip W and heat it to oxygen ignition temperature.

The nozzles N also have anothe row of closely spaced orifices which project a sheet of cutting oxygen 0 against the preheated band, to pierce through the metal and sever the strip.

The blowpipes B are supported in spaced relation along the path of the strip W, by means of a bar in extending parallel to the strip, and mounted on a pair of brackets l2 for example secured to a channel 14 extending along or forming part of one side of the roll table.

Longitudinally movable along the bar III are a plurality of slides 13 in which the blowpipes B are vertically adjustably mounted, the slides being adjustable along the bar to adjust the spacing of the cuts.

Fuel gas such as acetylene is supplied by a pipe l5 through branch tubes l6 to the mixers I! of the blowpipes B, and preheat oxygen is supplied to these mixers through branch tubes l8 from a ,pipe [9. The pipes l5 and I 9 respectively contain

solenoid valves

20 and 2! both actuated by a switch 22.

Cooling fluid such as water is supplied by a valve 29 The nozzles N each comprise a preheat block 3| and a cutting oxygen block 32, each block being constructed as described in detail in Deck Patent No. 2,337,087. The preheat block 31 has a central bore 33 containing a bafile 34. The bore 33 receives preheat mixture from the blowpipe B, and delivers the mixture through a, row of passages 35 sufiiciently closely spaced to project the sheet of preheat flame P.

The cutting oxygen block 32 has a longitudinal bore 36 containing a bafile 31. The bore 36 receives cutting oxygen from the branch tube 28, and delivers the cutting oxygen through a row of passages 39 suificiently closely spaced to project the cutting oxygen sheet 0.

The preheat block 3i has a longitudinal side channel Ml for cooling medium, and the cutting oxygen block 252 has a similar longitudinal side channel 42. A third channel 43 is located between the blocks. As shown in Fig. 8, these channels are connected by transverse passages l i. Cooting medium such as water from the tube 25 flows through the passages M, channels til, 42, and 33 and out through the return tube 25.

In operation, the strip W delivered from the rolling step is arrested in a stationary position with respect to the nozzles, the slides iii having been adjusted according to the spacing of the cuts desired. The switch 22 is closed to open simultaneously the solenoid valve 2i? for preheat fuel and solenoid valve 2! for preheat oxygen, thus simultaneously projecting the sheets of preheat gases, which, when ignited, deliver sheets of preheat flames from the nozzle N against the respective bands on the strip W. After these bands have been heated to oxygen ignition temperature, the switch 30 controlling cutting oxygen is closed to open the solenoid valve 2e for the cutting oxygen, thus simultaneously projecting sheets of cut" ting oxygen against the preheated bands to pierce through the metal and simultaneously sever the strip at the several bands.

In the procedure shown in Fig. 2, the nozzle N is maintained stationary during the preheating and cutting steps, the preheat flame P being first projected against the strip W at an obtuse angle thereto in a vertical longitudinal plane, and the oxygen sheet later projected against the preheated band at an angle inclined in the opposite direction. In the procedure shown in Fig. 3, the preheat flame P is first projected against the strip at a sharper angle, and the cutting oxygen sheet 0 is projected vertically at right angles to the strip. In Fig. in the position shown in full lines, the nozzle is positioned below the strip W, and the preheat flame P is first projected vertically against the underside of the strip. The nozzle N is then moved to the position shown in dotted lines, to project the cutting oxygen sheet vertically against the underside of the preheated band.

What is claimed is:

1. Method of thermochemically severing thin fiat metal strip, to separate a length of said strip from the remainder thereof which comprises directing against one surface of the strip a sheet of oxy-fuel preheat flame extending transversely Of the strip for the full width thereof to heat a narrow transverse band of the metal to oxygen ignition temperature, thereafter directing a similar sheet of cutting oxygen against said preheated band in a plane intersecting the plane of said strip, and maintaining said cutting oxygen sheet so directed until it penetrates the metal of said preheated narrow transverse band on one side of said strip, pierces through the metal of the entire thickness and width of said strip, completely severs the length of said strip ahead of said preheated narrow transverse band from the length of said strip behind said narrow transverse band, and emerges at the other side of said strip between the severed edges of the separatelengths of said strip.

2. Method of thermochemically severing thin fiat metal strip into separate lengths, which comprises simultaneously directing against one surface of the strip a plurality of longtudinally spaced rows of coplanar oxy-fuel jets transversely suficiently closely spaced to project flat sheets of preheat flame extending for the full width of the strip in planes intersecting the plane of the strip to heat longitudinally spaced narrow transverse bands of the metal to oxygen ignition temperature, and thereafter simultaneously directing rows of coplanar cutting oxygen jets similarly spaced to project fiat sheets of cutting oxygen against said preheated bands, and maintaining said rows of coplanar cutting oxygen jets so directed until said fiat sheets of cutting oxygen penetrate the metal of said preheated narrow transverse bands on one side of said strip, pierce through the metal of the entire thickness and width of said strip, completely sever the length of said strip between adjacent narrow transverse bands from the lengths respectively ahead or" and behind the same, and emerge at the other side of said strip. between the severed edges of the separate lengths of said strip.

3. Method as claimed in claim 1, in which said sheets Of preheat name and cutting oxygen respectively are directed against the underside of the strip.

4. Method as claimed in claim 1, in which said sheets of preheat flame are directed against the strip at an obtuse angle in the vertical longitudinal plane of the strip, and said sheets of cutting oxygen are directed against the preheated band at right angles to the strip.

5. Method as claimed in claim 1, in which said sheets of preheat flame and cutting oxygen are projected by a double nozzle first positioned to project said sheets of preheat flame normal to the strip, and thereafter positioned to project said sheets Of cutting oxygen normal to the strip and against said preheated band.

6. Method of thermochemically severing thin flat metal strip, which comprises directing against one surface of the strip a row of oxy-fuel gas jets sufiiciently closely spaced to project a sheet of preheat flame extending the full width of the strip in a plane transverse to the strip to heat a narrow transverse band of the metal to oxygen ignition temperature, and thereafter directing against said band a row of cutting oxygen jets similarly spaced to project a sheet of cutting oxygen in a plane transverse to said strip but inclined thereto at an acute angle in a, longitudinal plane and intersecting the plane of the preheating flame at said band to pierce through the metal and sever the strip.

surface of the strip a sheet of oxy-fuel preheat flame extending transversely of the strip for the full width thereof to heat a narrow transverse band of the metal to the oxygen ignition temperature, means for thereafter directing a similar sheet of cutting oxygen against said band to .pierce through the metal and sever the strip."

and a support for holding said cutting oxygen sheet directing means stationary during the severing operation.

8. Apparatus for thermochemically severing thin flat metal strip into lengths, which comprises supports for holding said strip stationary during the severing operation, means for directing against one surface of the strip a plurality of longitudinally spaced rows of oxy-fuel jets transversely suificiently closely spaced to project a sheet of preheat flame extending for the full width of the strip to heat longitudinally spaced narrow transverse bands of the metal to oxygen ignition temperature, means for thereafter directing rows of cutting oxygen jets similarly directing means stationary during the severing operation.

9. Apparatus as claimed in claim 7 in which said jet directing means comprise a double nozzle provided with respective rows of passages in planes converging at the preheat band on the strip.

10. Apparatus as claimed in claim '7, in which said jet directing means comprise a double nozzle provided with respective rows of passages, and

a cooling chamber is provided between said rows ing operation, means for directing against one 35 surface of the strip a row of oxy-fuel gas jets sufiiciently closely spaced to project a sheet of preheat flame extending the full Width of the strip in a plane transverse to the strip to heat a narrow transverse band of the metal to oxygen ignition temperature, means for thereafter directing against said band a row of cutting oxygen jets similarly spaced to project a sheet of cutting oxygen in a plane transverse to said strip but inclined thereto at an acute angle in a, longitudinal plane and intersecting the plane of the preheating flame at said band to pierce through the metal and sever the strip and supports for holding said cutting oxygen jet row directing means v stationary during the severing operation.

ROGER S. BABCOCK.

REFERENCES CITED The following references are of record in the file of this patent:

UNITED STATES PATENTS Number Name Date 866,866 Jottrand Sept. 24, 1907 1,723,107 Wildeboer Aug. 6, 1929 2,202,130 Wagner May 28, 1940 2,204,756 Hasse et a1 June 18, 1940 2,290,295 Scheller July 21, 1942 2,302,164 Anderson Nov. 1'7, 1942 2,363,089 Scherl Nov. 21, 1944 FOREIGN PATENTS Number Country Date 586,116 France Dec. 22,1924 426,990 Germany Dec. 31, 1926