CA1103071A - Method of forming a socket weld - Google Patents

Method of forming a socket weld

Info

Publication number
CA1103071A
CA1103071A CA329,851A CA329851A CA1103071A CA 1103071 A CA1103071 A CA 1103071A CA 329851 A CA329851 A CA 329851A CA 1103071 A CA1103071 A CA 1103071A
Authority
CA
Canada
Prior art keywords
tubular element
recess
seat
socket
weld
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
Application number
CA329,851A
Other languages
French (fr)
Inventor
James E. Reardon
Pembroke O. Leach
Vernon W. Camp
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.)
Combustion Engineering Inc
Original Assignee
Combustion Engineering Inc
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 Combustion Engineering Inc filed Critical Combustion Engineering Inc
Priority to CA329,851A priority Critical patent/CA1103071A/en
Application granted granted Critical
Publication of CA1103071A publication Critical patent/CA1103071A/en
Expired legal-status Critical Current

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Abstract

Improved Method of Forming a Socket Weld Abstract An improved method of forming a socket weld connection between a tubular element and a vessel, of the type wherein a recess having a diameter slightly greater than the diameter of the tubular element is bored into the surface of the vessel, the tubular element is inserted into the recess so as to contact the seat thereof and welding heat is applied externally around the circumference of the tubular element at the intersection of the tubular element with the surface of the vessel. The improvement comprises tapering the seat of the recess from its outer circumference inward at a downward angle with respect to the horizontal of at least 10° and not more than 15°.

Description

3C) 7~

Description Improved Method of Forming a Socket_Weld Technical Field The invention relates to a method of forming a socket weld connection between a tubular element such as a pipe, a nipple or a nozzle and a second element such as another pipe, a drum, a header or a tube sheet.
When welding a tubular element such as a pipe, nipple or nozzle to a second element such as another tube, a boiler drum or a header or a tube sheet of a heat exchanger, a socket weld is often used where~n the end of the tubular element is inserted into a recess, termed a socket, in the surface of the second element. To properly align the tubular element prior to weld;ng, it is desirable to bring the end of the tubular element in contact with the seat of the socket.
However, a structure of this type is considerably stressed when the weld is made and tens;onsare produced in the weld seam which may cause cracking of the seam when the weld contracts as it cools. For this reason, contact of the end of the pipe with socket set ;s usually avolded by back~ng-off the tubular element away from the socket set such that a gap of approximately one and one-half millimeters is maintained between the end of the tubular element and the socket seat.
By doing this, the end of the tubular element is free to move axially downward as the weld contracts thereby relieving stresses in the weld seam which could otherwise cause cracking of the seam. Unfortunately, backing the tubular element away from the socket seat is a cumbersome operation which can also result in inaccurate positioning of the tubular element.

1~3(~71 Backqround Art The prior art, U.S. Patent No. 3,003,601, provided for a socket weld connection between a tubular element and a second element wherein a portion of the end of the tubular element was maintained in contact with the seat of a flat bottom socket in the surface of the second element during the welding process without causing crack-ing of the resultant weld seam. According to this prior art, the end face of the tubular element must be machined to provide a relatively thin rim extending from the end of the tubular element. The tubular element is inserted into the socket such that the relatively thin rim extending from the end of the tubular element contacts the flat seat of the socket, a gap thereby being established between the end of the tubular element and the socket seat into which the relatively thin rim is free to deform upon shrinking of the weld.
Disclosure of Invention According to the present invention there is provided an improved method of forming a socket weld connection between a tubular element and a vessel, of the type wherein a recess having a diameter slight~y greater than the diameter of the tubular element is bored into the surface of the vessel, the tubular element is inserted into the recess so as to contact the seat thereof and welding heat is applied externally around the circumference of the tubular element at the intersection of the tubular element with the surface of the vessel. The improvement compr;ses tapering the seat of the recess from its outer circumference inward at a downward angle with respect to the horizontal of at least 10 and not more than 15.
The improved method of the present invention possesses the advantage that the end face of the tubular element need not be machined to produce a relatively thin rim extending therefrom. Thus a very time consuming step is eliminated in favor of the simple operation of tapering the socket seat as the socket is bored into the second element.
Another advantage of the present invention is that the flat end face of the tubular element is permitted to contact the seat of the recess thereby ensuring accurate positioning of the tubular element within the recess, while at the same time providing a gap `` l~G3~71 between the end face of the tubular element and the seat of the recess so that the tubular element may deform upon shrinking of the structure after the weld has been made without causing excessive stresses and cracking within the weld connection. Contact between the end face of the tubular element and the seat of the socket is limited to a line contact along the outer circumference of the end of the tubular ele-ment. This limited contact has been shown to be sufficient to ensure accurate positioning of the tube, but not great enough to offer sufficient resistance to deformation to induce excessive stresses within the weld seam as the weld shr;nks upon cooling.

Brief Description of the Drawing These and further features and advanta~es of the invention become evident in the description of the following embodiment shown in the drawing attached wherein:
Figure 1 is a sectional side elevation view of a tube socket welded to another tube with a fillet weld in accordance with the method of the present invention; and Figure 2 is a sectional side elevation view of a tubular element welded to a vessel with a single-J groove weld in accordance with the method of the present invention.

Best Mode for Carryin~ Out the Invention Referring to the drawings, a tubular element 10 is shown welded to a second element 20, such as another tube as shown in Figure 1 or a vessel such as a drum or header as shown in Figure 2.
A recess is bored into the surface of the second element, and the end face 50 of the tubular element 10 is inserted therein. The recess may comprise a number of known shapes such as the simple annular socket 30 of Figure 1 or the more elaborate socket 32 of Figure 2 wherein a weld groove, such as a single-J pipe weld groove, is embodied in the socket itself. It is desirable to insert the tubular element 10 all the way into the recess 30, 32 until the end face 50 of tubular element 10 is in contact with the seat 40 of the socket so that proper and accurate positioning of the tubular element can be assured.
In accordan~e with the invention, the seat 40 of the socket 30, 32 is tapered from its outer circumference inward at a downward ' .. . ............... . ~:
.

3C~71 angle with respect to the horizontal of at least 10. Although any taper of an angle greater than 10 ensures that sufficient space is available for the end face of the tubular element to deform without causing excessive stresses in the weld seam, it is preferred that the angle of the taper be limited to not more than 15 in order to avoid removing unnecessary large amounts of metal from the second element which could locally adversely affect the structural integrity of the second element.
In forming the weld, welding metal is deposited externally around the circumference of the tubular element 10 at the intersec-tion of the tubular element 10 with element 20 to form a weld seam 60 therebetween. As the weld seam 60 cools and contracts, the outer circumferential portion of the end face 50 of the tubular element 70 is free to deform inward and downward into the gap between the end face 50 of the tubular element 10 and the tapered seat 40 of the socket. Because the tubular element 10 is free to deform, stresses do not develop within the weld seam 60 upon contraction and the weld seam 60 is not subject to cracking. The gap 45 between the end face 50 of the tubular element 10 and the tapered seat 40 of the socket is essential for allowing the desired deformation necessary to produce the socket weld connection of the present invention.

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Claims (2)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE PROPERTY
OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A method of forming a socket weld connection between a tubular element and a second element, wherein a recess having a diameter slightly greater than the diameter of the tubular element is bored into the surface of the second element, the tubular ele-ment is inserted into the recess so as to contact the seat there-of, and welding metal is deposited externally around the circum-ference of the tubular element at the intersection of the tubular element with the second element, characterized by the improvement of: tapering the seat of the recess from its outer circumference inward at a downward angle with respect to the horizontal of at least 10° and not more than l5°.
2. A method according to Claim 1, further characterized by tapering the seat of the recess from its outer circumference inward at a downward angle with respect to the horizontal of substantially 10°.
CA329,851A 1979-06-15 1979-06-15 Method of forming a socket weld Expired CA1103071A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA329,851A CA1103071A (en) 1979-06-15 1979-06-15 Method of forming a socket weld

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA329,851A CA1103071A (en) 1979-06-15 1979-06-15 Method of forming a socket weld

Publications (1)

Publication Number Publication Date
CA1103071A true CA1103071A (en) 1981-06-16

Family

ID=4114463

Family Applications (1)

Application Number Title Priority Date Filing Date
CA329,851A Expired CA1103071A (en) 1979-06-15 1979-06-15 Method of forming a socket weld

Country Status (1)

Country Link
CA (1) CA1103071A (en)

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