IP Library Granted Patent US 7,335,853
Granted Patent B2
US 7,335,853 · App. 11/388,701 · Granted Feb 26, 2008

Method for orbital welding using a pulsed current

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Quick Facts
Patent No.
US 7,335,853
App. No.
11/388,701
Granted
Feb 26, 2008
Kind
B2
Abstract

A method for the orbital welding of tubular elements held in abutment comprising the steps of striking an arc at a strike point with an orbital welder between an electrode and a seam formed by a first tubular element and a second tubular element, held in abutment within a fixture; initiating an orbit of said electrode around an abutment of said first tubular element and said second tubular element; adjusting the current of said arc in a pulsed manner from a maximum current to a minimum current at a set frequency, combination of said maximum current and said minimum current forming an average current; decreasing said average current in a generally continuous manner as said orbit of said electrode progresses from said strike point, the rate of decrease of said maximum current having a generally inverse relationship to the rate of increase in temperature experienced by said tubular elements.

Claims (35)

1. A method for the orbital welding of tubular elements held in abutment comprising the steps of:

a) striking an arc at a strike point with an orbital welder between an electrode and a seam formed by a first tubular element and a second tubular element held in abutment within a fixture, said first tubular element having a wall, said second tubular element having a wall;

b) initiating an orbit of said electrode around an abutment of said first tubular element and said second tubular element;

c) adjusting the current of said arc in a pulsed manner from a maximum current to a minimum current at a set frequency;

d) decreasing said maximum current in a generally continuous manner as said orbit of said electrode progresses from said strike point, the rate of decrease of said maximum current having a generally inverse relationship to the rate of increase in temperature experienced by said tubular elements;

wherein an average current is generally decreasing continuously over time;

and wherein said minimum current is held generally constant;

and wherein an average temperature of said tubular elements is maintained within a predetermined range;

and wherein a resulting weld bead is fully penetrated through said walls of said first tubular element and said second tubular element.

2. The method of claim 1 further comprising the steps of:

decreasing rapidly said average current in a generally continuous manner at the conclusion of at least a first orbit of said electrode around said seam formed between said first tubular element and said second tubular element;

disengaging said arc.

3. A method for the orbital welding of tubular elements held in abutment comprising the steps of:

a) striking an arc at a strike point with an orbital welder between an electrode and a seam formed by a first tubular element and a second tubular element, held in abutment within a fixture, said first tubular element having a wall, said second tubular element having a wall;

b) initiating an orbit of said electrode around an abutment of said first tubular element and said second tubular element;

c) adjusting the current of said arc in a pulsed manner from a maximum current to a minimum current at a set frequency;

d) decreasing said maximum current in a generally continuous manner as said orbit of said electrode progresses from said strike point, the rate of decrease of said maximum current having a generally inverse relationship to the rate of increase in temperature experienced by said tubular elements;

e) decreasing said minimum current in a generally continuous manner as said orbit of said electrode progresses from said strike point, the rate of decrease of said maximum current having a generally inverse relationship to the rate of increase in temperature experienced by said tubular elements;

wherein an average current is generally decreasing continuously over time;

and wherein said minimum current is held generally constant;

and wherein an average temperature of said tubular elements is maintained within a predetermined range;

and wherein a resulting weld bead is fully penetrated through said walls of said first tubular element and said second tubular element.

4. The method of claim 3 further comprising the steps of:

decreasing rapidly said average current in a generally continuous manner at the conclusion of at least a first orbit of said electrode around said seam formed between said first tubular element and said second tubular element;

disengaging said arc.

5. A method for the orbital welding of tubular elements held in abutment comprising the steps of:

a) striking an arc at a strike point with an orbital welder between an electrode and a seam formed by a first tubular element and a second tubular element, held in abutment within a fixture, said first tubular element having a wall, said second tubular element having a wall;

b) initiating an orbit of said electrode around an abutment of said first tubular element and said second tubular element;

c) adjusting the current of said arc in a pulsed manner from a maximum current to a minimum current at a set frequency, combination of said maximum current and said minimum current forming an average current;

d) decreasing said average current in a generally continuous manner as said orbit of said electrode progresses from said strike point, the rate of decrease of said maximum current having a generally inverse relationship to the rate of increase in temperature experienced by said tubular elements;

wherein an average temperature of said tubular elements is maintained within a predetermined range;

and wherein a resulting weld bead is fully penetrated through said walls of said first tubular element and said second tubular element.

6. The method of claim 5 further comprising the steps of:

decreasing rapidly said average current in a generally continuous manner at the conclusion of at least a first orbit of said electrode around said seam formed between said first tubular element and said second tubular element;

disengaging said arc.

Assignments (7)
RELEASE OF SECURITY INTEREST Recorded Dec 22, 2016
From: PNC BANK
To: ARC MACHINES, INC.; ORBITAL ACQUISITION CORP.
Reel/Frame 040745/0767 →
PATENT SECURITY AGREEMENT Recorded Apr 5, 2012
From: ARC MACHINES, INC. AND ORBITAL ACQUISITION CORP.
To: PNC BANK, NATIONAL ASSOCIATION, AS AGENT
Reel/Frame 027995/0348 →
PATENT ASSIGNMENT Recorded Apr 4, 2012
From: MCGUSHION, KEVIN
To: ORBITAL ACQUISITION CORP.
Reel/Frame 027987/0854 →
RELEASE OF ASSIGNMENT FOR SECURITY OF PATENTS Recorded Apr 4, 2012
From: BANK OF AMERICA, N.A., AS SUCCESSOR BY MERGER TO MERRILL LYNCH COMMERCIAL FINANCE CORP.
To: ORBITAL ACQUISITION CORP.
Reel/Frame 027986/0705 →
SECURITY AGREEMENT Recorded Jul 14, 2008
From: ORBITAL ACQUISITION CORP.
To: PRAESIDIAN II SPV 1, LP, AS AGENT
Reel/Frame 021217/0921 →
SECURITY AGREEMENT Recorded Jul 11, 2008
From: ORBITAL ACQUISITION CORP.
To: MERRILL LYNCH COMMERCIAL FINANCE CORP., AS ADMINISTRATIVE AGENT
Reel/Frame 021217/0680 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 10, 2008
From: MCGUSHION, KEVIN
To: ORBITAL ACQUISITION CORP.
Reel/Frame 021217/0310 →
Continuity (2)
Provisional Application 6066541000 · Mar 25, 2005
Related Publication 20060213893A1 · Sep 28, 2006