Superplastic forming

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Superplastic forming is an industrial process used for creating precise and complex components out of superplastic materials.

Contents

Process

The material is first heated up to promote superplasticity. For titanium alloys e.g. Ti 6Al 4V and some stainless steels this is around 900 °C (1,650 °F) and for aluminium alloys e.g. AA5083 it is between 450 and 520 °C. In this state the material becomes soft so processes that are usually used on plastics can be applied, such as: thermoforming, blow forming, and vacuum forming. [1] Inert gas pressure is applied on the superplastic sheet forcing it into a female die.

Advantages and disadvantages

The major advantage of this process is that it can form large and complex workpieces in one operation. The finished product has excellent precision and a fine surface finish. It also does not suffer from springback or residual stresses. Products can also be made larger to eliminate assemblies or reduce weight, which is critical in aerospace applications. [1] Lower strength required and less tooling costs. McDonnell Douglas utilized SPF design and production technology into the F-15 in the 1980s,[ citation needed ] while in Europe an example of application can be found in some Eurofighter Typhoon assemblies [2] [3] (e.g. engine bays panels, foreplanes, slats).

The largest disadvantage of the process is its slow forming rate. Cycle times vary from two minutes to two hours, therefore it is usually used in low volume production applications. [4] [1] Another disadvantage is the non-uniformity of the produced part thickness. [5] Several methods are used to improve the thickness uniformity of SPF parts. One is to apply a designed varying gas pressure profile instead of a constant pressure. [6] Another approach is to tailor the contact friction between the die surface and the superplastic sheet. [7]

See also

Related Research Articles

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Friction stir processing

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Diffusion bonding

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<span class="mw-page-title-main">Aluminium joining</span>

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Dissimilar friction stir welding

Dissimilar friction stir welding (DFSW) is the application of friction stir welding (FSW), invented in The Welding Institute (TWI) in 1991, to join different base metals including aluminum, copper, steel, titanium, magnesium and other materials. It is based on solid state welding that means there is no melting. DFSW is based on a frictional heat generated by a simple tool in order to soften the materials and stir them together using both tool rotational and tool traverse movements. In the beginning, it is mainly used for joining of aluminum base metals due to existence of solidification defects in joining them by fusion welding methods such as porosity along with thick Intermetallic compounds. DFSW is taken into account as an efficient method to join dissimilar materials in the last decade. There are many advantages for DFSW in compare with other welding methods including low-cost, user-friendly, and easy operation procedure resulting in enormous usages of friction stir welding for dissimilar joints. Welding tool, base materials, backing plate (fixture), and a milling machine are required materials and equipment for DFSW. On the other hand, other welding methods, such as Shielded Metal Arc Welding (SMAW) typically need highly professional operator as well as quite expensive equipment.

References

  1. 1 2 3 E. Degarmo, J. Black, and R. Kohser, Materials and Processes in Manufacturing (9th ed.), 2003, Wiley, ISBN   0-471-65653-4.
  2. Hoyle, Craig (May 2007). "Eurofighter production techniques boost BAE Systems". FlightGlobal.
  3. "Airbus Defence and Space Aerostructures presentation brochure" (PDF). Airbus Defence and Space Aerostructures. February 2021.
  4. Jarrar, Firas; Jafar, Reem; Tulupova, Olga; Enikeev, Farid; Al-Huniti, Naser (January 2016). "Constitutive Modeling for the Simulation of the Superplastic Forming of AA5083". Materials Science Forum. 838–839: 512–517. doi:10.4028/www.scientific.net/MSF.838-839.512. ISSN   1662-9752.
  5. F. Jarrar, M. Liewald, P. Schmid, and A. Fortanier, Superplastic Forming of Triangular Channels with Sharp Radii, Journal of Materials Engineering and Performance, 2014, 23(4), p 1313-1320.
  6. F.S. Jarrar, L.G. Hector Jr., M.K. Khraisheh, and K. Deshpande, Gas Pressure Profile Prediction from Variable Strain Rate Deformation Paths in AA5083 Bulge Forming, Journal of Materials Engineering and Performance, 2012, 21(11), p 2263–2273.
  7. 12. M.I. Albakri, F.S. Jarrar, and M.K. Khraisheh, Effects of Interfacial Friction Distribution on the Superplastic Forming of AA5083, Journal of Engineering Materials and Technology, 2011, 133, p 031008-031014.