Many variations of these formulas exist and are readily available online. These variations may often seem to be at odds with one another, but they are invariably the same formulas simplified or combined. What is presented here are the unsimplified formulas. All formulas use the following keys: • Lf = flat length of the sheet • BA = bend allowance • BD = bend deduction • R = inside bend radius • K = K-factor, which is t / T • T = material thickness • t = distance from inside face to the
neutral axis • A = bend angle in degrees (the angle through which the material is bent) The 'neutral axis' (also called the neutral line) is an imaginary profile that can be drawn through a cross-section of the workpiece that represents the locus where no
tensile or
compressive stress are present but
shear stresses are at their maximum. In the bend region, the material between the neutral line and the inside radius will be under compression during the bend while the material between the neutral line and the outside radius will be under tension during the bend. Its location in the material is a function of the forces used to form the part and the material yield and tensile strengths. This
theoretical definition also coincides with the geometric definition of the plane representing the unbent flat pattern shape within the cross-section of the bent part. Furthermore, the bend allowance (see below) in air bending depends primarily on the width of the opening of the bottom die. As a result, the bending process is more complicated than it appears to be at first sight. Both bend deduction and bend allowance represent the difference between the neutral line or unbent 'flat pattern' (the required length of the material prior to bending) and the formed bend. Subtracting them from the combined length of both flanges gives the flat pattern length. The question of which to use is determined by the dimensioning method used to define the flanges as shown in the two diagrams below. The flat pattern length is always shorter in length than the sum of all the flange length dimensions due to the
geometric transformation. This gives rise to the common perspective that that material is stretching during bending and the bend deduction and bend allowance are the distance that each bend stretches. While a helpful way to look at it, a careful examination of the formulas and stresses involved show this to be false. Most
3D Solid Modeling CAD software has sheet metal functions or add-ons that performs these calculations automatically.
Bend allowance The 'bend allowance' (BA) is the length of the arc of the neutral line between the tangent points of a bend in any material. Adding the length of each flange as dimensioned by B in the diagram to the BA gives the Flat Pattern length. This bend allowance formula is used to determine the flat pattern length when a bend is dimensioned from 1) the center of the radius, 2) a tangent point of the radius (B) or 3) the outside tangent point of the radius on an acute angle bend (C). When dimensioned to the outside tangent, the material thickness and bend radius are subtracted from it to find the dimension to the tangent point of the radius before adding in the bend allowance. The BA can be estimated using the following formula, which incorporates the empirical K-factor: :BA = A \left( \frac{\pi}{180} \right) \left( R + (K \times T \right))
Bend deduction The bend deduction BD is defined as the difference between the sum of the flange lengths (from the edge to the apex) and the initial flat length. The
outside set back (OSSB) is the length from the tangent point of the radius to the apex of the outside of the bend. The
bend deduction (BD) is twice the outside setback minus the bend allowance. BD is calculated using the following formula, where A is the angle in radians (=degrees*π/180): :BD = 2 \left(R + T \right) \tan{ \frac{A}{2}} - BA For bends at 90 degrees this formula can be simplified to: :BD = R \left(2 - A \right) + T \left(2 - KA \right)
K-factor K-factor is a ratio of the location of the neutral line to the material thickness as defined by t/T where t = location of the neutral line and T = material thickness. The K-factor formula does not take the forming stresses into account but is simply a geometric calculation of the location of the neutral line after the forces are applied and is thus the roll-up of all the unknown (error) factors for a given setup. The K-factor depends on many variables including the material, the type of bending operation (coining, bottoming, air-bending, etc.) the tools, etc. and is typically between 0.3 and 0.5. The following equation relates the K-factor to the bend allowance: : K = \frac{-R + \frac{BA}{\pi A / 180}}{T}. The following table is a "
rule of thumb". Actual results may vary remarkably. The following formula can be used in place of the table as a good
approximation of the K-factor for air bending: : K = \frac{\log \min\left(100, \frac{\max(20 R, T)}{T}\right)}{2 \log 100}. == Advantages and disadvantages ==