Home Up Search                                                        

 

See 5 YouTube Video's of Key Website Points

.

Up Purchase Gas Saver TIP of the MONTH Improve Quality How GSS Works About Company Weld Safely PRODUCT INDEX Payback Estimates Production Results Flow Rate Limiter Orifice Flow Control Training Purchase Lean Manufacturing Go Green Weld School Video Overview Sales Literature Other Weld Info More GSS Info Services Overview Car Buffs Specials Contact Us Site Index

 

This Page Presents Welding 4130 Chrome Moly (Chromoly) Math, and Other Information About Welding 4130:

Click for BASIC 4130 WELDING DETAILS

Click for TECHNICAL & METALLURGICAL DETAILS

Click for WELDING HEAT TREATED 4130 CHROME MOLY

Click for METALLURGICAL DEFINITIONS

Click for WELDING A BETTER STEEL;  HY 130

Click for DEFINING "EFFECTIVE HEAT INPUT"

 

 

Detailed Review of GSS

 

 

Stop Wasting Shielding Gas!!

 

Improve Weld Start Quality

 

See YouTube Videos About Our

Patented MIG Shielding

"Gas Saver System" (GSS)

 

Just Click on Picture

 

 

Short Overview of GSS-

90 Seconds

 

What Users Say About GSS

 

Welding Race Cars

 

Math Used to Generate 4130 Information.

The Information Below;
bullet Provides the math equations that estimate the theoretical cooling rates for TIG welds in thin wall 4130 tubes.
bulletThe cooling rate equations were obtained from the Welding Handbook, Volume 1, 9th Edition, page 100.
bulletBoth thick and thin plate equations were developed by Professor C.A.  Adams et al.
 
The data is presented in a way so one can see the numbers from each part of the equation. As the thickness was increased so was the heat input.  A TIG process efficiency of 0.5 (50%) was used which is higher than the sited Welding Handbook reference but errors on the side of predicting a slower cooling rate. The thin plate equation is for two dimensional heat flow and may be OK for a butt weld but a Tee fillet weld will have faster cooling rate. Therefore despite trying to error on the side of predicting slower cooling rates, they are all around the 1/4 in Jominy bar location. The exact cooling rate will be somewhat dependent on the diameter of the tube as well. However I would expect that perhaps 1/2 way around the joint the cooling rate would be similar to that predicted. As the complete circular weld is made the last part will have a preheat from the weld start. However if a brittle structure is formed in any area and a crack forms, that is sufficient to be a problem.
Equation Elements and Values
bullet

Rc = Cooling rate at weld centerline; deg F/min

bullet

k = Thermal Conductivity of metal; BTU/min in deg F

bullet

p = Density of metal; lb/in3

bullet

C = Specific Heat of metal; BTU/ (lb deg F)

bullet

h = thickness of metal; in

bullet

Hnet = Net heat input; BTU/in [V*I / ipm*.057*process efficiency]

bullet

Tc = Temperature which cooling rate is calculated; deg F

bullet

To = Initial plate temperature; deg F

 

Welding Cooling Equations from pp 100 Welding Handbook Volume 1, 9th Edition

Thick Plate Equation =Rc =-[2*3.1416*k(Tc-To)2] / Hnet
Thin Plate Equation = Rc = 2*3.1416*kpC (h/Hnet)2(Tc-To)3

Calculate estimated cooling rate @ 1100 deg F for thin wall 4130 tube welds:

 

Tube = .040 in wall; V (volts) = 10; I (amps) = 70; travel = 12 ipm

Using thin plate equation:

bullet-2*3.1416*0.024*0.29*0.11= -.00481
bulletHnet = 1.66
bullet(h/Hnet)2 = 0.000579
bullet(Tc-To)3 = 1.07*109
bullet Rc = -2981 deg F / min = - 50 deg F / sec
Tube = .0625 in wall; V (volts) = 10; I (amps) = 90; travel = 11 ipm

Using thin plate equation:

bullet-2*3.1416*0.024*0.29*0.11= -.00481
bulletHnet = 2.33
bullet(h/Hnet)2 = 0.000718
bullet(Tc-To)3 = 1.07*109
bullet Rc = -3700 deg F / min = - 62 deg F / sec
Tube = .093 in wall; V (volts) = 10; I (amps) = 110; travel = 9 ipm

Using thin plate equation:

bullet-2*3.1416*0.024*0.29*0.11= -.00481
bulletHnet = 3.48
bullet(h/Hnet)2 = 0.000713
bullet(Tc-To)3 = 1.07*109
bullet Rc = -3671 deg F / min = - 61 deg F / sec
REFERENCES USED;
bulletUS Steel Atlas of Isothermal Transformation Diagrams
bulletRepublic Alloy steels
bulletR. A. Grange and Kiefer; "Transformation of Austenite on Continuous Cooling and Relation to Transformation at Constant Temperature."
bulletWalter Crafts and John Lamont; "Hardenability and Steel Selection."
bulletAWS Welding Handbook; Volume 1, 9th Addition
If a Search Engine Found This Page 1st- - - We'd Suggest a Visit to The Basic Welding 4130 Page; Then Return.  Click Here

This page presents the equations that support the data in the 4130 Technical Details page.

 

ONE PAGE SUMMARY

PURCHASE PRODUCT

 

 

FREE Corvette Accessory Installation Info

 

 

.

Check Out Welding Math Site

 

 

This Page Presents Welding 4130 Math, for Other Information:

Click for BASIC 4130 WELDING DETAILS

Click for TECHNICAL & METALLURGICAL DETAILS

Click for  EQUATIONS defining weld cooling rate in tubing

Click for WELDING HEAT TREATED 4130 CHROME MOLY

Click for METALLURGICAL DEFINITIONS

Click for WELDING A BETTER STEEL;  HY 130

 

"WARNING: "Weld Safely"

 
Save over $1000 per year per welder and improve weld starts with Payback measured in weeks!!
* US Patent  # 6,610,957;  "Welding Shielding Gas Saver Device" August 26, 2003,  Patent Pending in other countries.   The "Flow Rate Limiter" device is
 covered by 2008 US patent #7,462,709.  Other site material may be covered under our 2006 US Patents # 7,015,412 or # 7,019,248 .
Questions?   Send E-mail TechSupport@NetWelding.com
Last modified: 02/03/10

Copyright © 1999-2009 WA Technology TM; GSS TM.  All rights reserved.