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peen forming - Metal Improvement Company

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The majority of aircraft in production with aerodynamically<br />

formed aluminum alloy wingskins employ the <strong>peen</strong> <strong>forming</strong><br />

process.<br />

<strong>Metal</strong> <strong>Improvement</strong> <strong>Company</strong> has developed computer<br />

modeling techniques that allow feasibility studies of<br />

particular designs. The program takes three-dimensional<br />

engineering data and, based on the degree of compound<br />

curvature, calculates and illustrates the degree of <strong>peen</strong><br />

<strong>forming</strong> required. It also exports numerical data to define the<br />

Figure 10-4 Computer Modeling of<br />

<strong>peen</strong>ing that is required to obtain the curvatures. A<br />

significant advantage of these techniques is that MIC can<br />

Peen Forming Operation<br />

assist aircraft wing designers in the early stages of design. These techniques insure that the desired<br />

aerodynamic curvatures are met with economically beneficial manufacturing processes (Figure 10-4).<br />

C O N T O UR C O R R E C TION<br />

Shot <strong>peen</strong>ing utilizing <strong>peen</strong> <strong>forming</strong> techniques can be used to correct unfavorable geometry conditions.<br />

This is accomplished by shot <strong>peen</strong>ing selective locations of parts to utilize the surface loading from the<br />

induced compressive stress to restore the components to drawing requirements. Some examples are:<br />

• Driveshaft/crankshaft straightening<br />

• Roundness correction of ring shaped geometry<br />

• Aircraft wing stiffner adjustment<br />

• Welding distortion correction<br />

The <strong>peen</strong> <strong>forming</strong> process avoids the unfavorable tensile residual stresses produced by other straightening<br />

methods by inducing beneficial compressive residual stresses.<br />

W ORK H A R D E N I N G<br />

A number of materials and alloys have the potential to work harden through cold working. Shot <strong>peen</strong>ing<br />

can produce substantial increases in surface hardness for certain alloys of the following types of materials.<br />

• Stainless steel<br />

• Aluminum<br />

• Manganese stainless<br />

steels<br />

• Inconel<br />

• Stellite<br />

• Hastelloy<br />

This can be of particular value to<br />

parts that cannot be heat treated but<br />

require wear resistance on the<br />

surface. The following table<br />

illustrates examples of increases in<br />

surface hardness with shot <strong>peen</strong>ing.<br />

Material Before After Percent<br />

Shot Peen Shot Peen Increase<br />

Cartridge Brass 50 HRB 175 HRB 250<br />

304 Stainless 243 HV 423 HV 74<br />

316L Stainless 283 HV 398 HV 41<br />

Mn Stainless 23 HRC 55 HRC 139<br />

Inconel 625 300 HV 500 HV 67<br />

Stellite 42 HRC 54 HRC 29<br />

Hastalloy C 18 HRC 40 HRC 122 *<br />

Hastalloy C 25 HRC 45 HRC 80 **<br />

* Wrought condition ** Cast condition<br />

www.metalimprovement.com<br />

C H A P T E R T E N<br />

O THER APPL ICA T IONS<br />

35

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