Authored by: Edited by
"Joint Decisions," MACHINE DESIGN, April 1, 2005 "How Tight is Right?" MACHINE DESIGN, August 23, 2001 |

Measuring torque when installing threaded fasteners is the best indicator of future joint performance, right? Actually, bolt tension is a better performance indicator, but measuring torque is far easier to do.

Download this article in .PDF format This file type includes high resolution graphics and schematics when applicable. |

Bolt tension is created when a bolt elongates during tightening, producing the clamp load that prevents movement between joint members. Such movement is arguably the most common cause of structural joint failures. The relationship between applied torque and the tension created is described by the relationship:

*T = K × D × F*

where *T* = torque, *K* = nut factor, sometimes called the friction factor, *D* = bolt diameter, and *F* = bolt tension generated during tightening. This expression is often called the short-form equation.

**The nut factor**

The nut factor, *K*, consolidates all factors that affect clamp load, many of which are difficult to quantify without mechanical testing. The nut factor is, in reality, a fudge factor, not derived from engineering principles, but arrived at experimentally to make the short-form equation valid.

Various torque-tension tests call for controlled tensioning of a threaded fastener while monitoring both torque and tension. At a specified torque or tension, the known values for *T*, *D*, and *F* are inserted into the short-form equation to permit solving for *K*.

Many engineers use a single value of *K* across a variety of threaded-fastener diameters and geometries. This approach is valid to some extent, because an experimentally determined nut factor is by definition independent of fastener diameter. But to truly understand the factors involved, it is helpful to compare the short-form equation with a torque-tension relationship derived from engineering principles.

Several of these equations are common, especially in designs that are primarily used in the E.U. Each produces similar results and takes the general form:

*T = F × X*

M_{A} = F_{V} × [(0.159 × P) + (0.578 × d_{2} × μ_{ }G) + (D_{Km} × μ_{K} / 2)]T = F × [0.5 × (P + 1.154 × π × μ_{th} × d_{2})/( – 1.154 × μ_{ th} × P / d_{2}) + (μ_{b} × (D_{o} + d_{h})/4)]The following table defines each variable and shows that, although the long-form equations appear unrelated, they are actually different forms of the same equation and yield similar results. Each term calculates a length which, when multiplied by the force generated by bolt tension, generates a moment or torque. They represent reaction torques resisting the input torque and must sum to equal that input torque. The term containing the variable P is the clamp load on thread pitch’s inclined plane. The second term — involving μ, or _{G}μ — is resisting torque caused by thread friction, and the last — using _{th}μ, _{n}μ, or _{K}μ — is a similar resisting torque generated by friction between the nut or head face and mating surface. The value of each term indicates the relative influence of each of these friction factors._{b}For example, applying the Motosh equation to an M12-1.75 angehead screw with friction coefficients μ equal to 0.15, shows that each additional 1,000 N of tension produces 0.28 N-m of reaction torque from clamp load on the thread pitch, 0.93 N-m of reaction torque from thread friction, and 1.35 N-m of reaction torque from friction under the nut. Total torque is then 2.56 N-m. These values break out to 10.9%, 36.3%, and 52.8%, respectively, of the total torque, confirming the commonly heard assertion that only 10 to 15% of the input torque goes toward stretching the bolt._{n} |

where *X* represents a series of terms detailing fastener geometry and friction coefficients. These relationships are often referred to as long-form equations. (Three of the most widely used long-form equations are discussed in the sidebar, *The long way*.)

To understand how the nut factor compares to the terms in the long-form equations, let’s consider the so-called Motosh equation:

*T _{in} = F_{P} × [(P/2 ) + (μ_{t} × r_{t}/cos ) + (μ_{n} × r_{n})]* where

*T*= input torque,

_{in}*F*= fastener preload,

_{P}*P*= thread pitch,

*μ*= friction coefficient in the threads,

_{t}*r*= effective radius of thread contact,

_{t}*μ*= half angle of the thread form (30° for UN and ISO threads),

*μ*= friction coefficient under the nut or head, and

_{n}*r*= effective radius of head contact.

_{n}The equation is essentially three terms, each of which represents a reaction torque. The three reaction torques must sum to equal the input torque. These elements, both dimensional and frictional, contribute in varying degrees to determining the torque-tension relationship, the purpose of calculating nut factor.

**The impact of variables**

So how do design decisions influence the nut factor that defines the torque-tension relationship? Specifically, engineers may wonder how valid a nut factor determined from a torquetension test on one type of fastener is for other fastener geometries.

The short-form equation is structured so that the fastener diameter, *D*, is separate from the nut factor, *K*. This implies that a nut factor derived from torque-tension tests on one fastener diameter can be used to calculate the torque-tension relationship for fasteners with a different diameter.

Like the nut factor itself, however, this approach is only an approximation. The accuracy of using a nominal fastener diameter, *D*, to apply a constant nut factor across a range of fastener sizes depends on the extent to which fastener diameter affects reaction torque.

Because some variables that affect bolted-joint design have more of an impact than others, it makes sense to examine them individually.

Clearance-hole diameter, for instance, is directly tied to nominal diameter. The long-form equations calculate that swapping a close-diametrical-clearance hole with one 10% larger leads to a 2% reduction in bolt tension for a given torque. Enlarging the fastener-head bearing diameter by 35%, say by replacing a standard hex-head fastener with a hex-flange-head, cuts bolt tension by 8% for a given torque.

Both bearing diameter and hole clearance generally scale linearly with bolt diameter, so their relative importance remains the same over a range of fastener diameters. However, different head styles or clearances change the reaction torque from underhead friction because the contact radius changes.

Doubling the thread friction coefficient on its own, say by changing the finish or removing lubricant, reduces bolt tension by 28% for a given torque. Engineers should note that the thread and underhead friction coefficients are often assumed to be equal for convenience in test setups and calculations. ISO 16047 estimates that this assumption can lead to errors of 1 to 2%.

Thread pitch tends to be more independent of nominal diameter than the other variables. Increasing just thread pitch by 40% cuts tension 5% for a given torque. However, the reaction-torque term containing the thread pitch, *P — P/2 π *— does not contain a friction coefficient. Therefore, as fastener diameter and, consequently, friction increase, the relative importance of thread pitch falls.

Motosh | D _{IN}/V_{DI} | ISO 16047 | Description |

T_{in} | M_{A} | T | Input torque |

F_{P} | F_{V} | F | Fastener preload or tension |

P | P | P | Thread pitch |

r_{n} | D_{Km}/2 | (D_{o} + d_{h})/4 | Effective radius of head contact |

μ_{n} | μ_{K} | μ_{b} | Coefficient of friction under head |

μ_{t}. | μ_{G} | μ_{th} | Coefficient of friction in threads |

r_{t} | d_{2}/2 | d_{2}/2 | Effective radius of thread contact (half the thread-pitch diameter) |

β | Half-angle of thread form (30° for UN and ISO threads) |

There is a maximum deviation of 4.2% between the results of the short and long-form equations for standard- pitch, metric, hex-head-cap screws with constant and equal coefficients of friction. As friction coefficients increase, there’s less error in assuming the nut factor varies directly with nominal diameter because the impact of thread pitch, the most independent variable, falls.

So, if all else is held constant, it’s reasonable to apply a nut factor calculated at one fastener diameter across a range of fastener sizes. For best results, engineers should base testing on the weighted mean diameter of the fasteners for which the nut factor will be used.

Many engineers find it expedient to apply a single nut factor across even greater fastener ranges, such as those with different head styles or clearance diameters. Applying the nut factor to joints where geometric variables other than nominal diameters are changing causes the short-form-equation results to differ from the long-form results by up to 15%.

**Long or short?**

So given all the discussion about which variables impact the nut factor and when it is reasonable to use a constant nut factor across a range of fasteners, it may seem as if the longform equations get engineers closer to the “right” answer thanks to their fundamental correctness. However, long-form equations, even when derived from engineering principles, use assumptions and approximations that may make them no more correct than an equation using an experimentally derived nut factor.

The potential errors in both types of equations pale compared to the variations in real-world joints. Bench-top torque-tension testing shows approximately 10% variations within samples even when all fasteners and bearing materials are the same. According to both short and longform equations, there should be no variation at all. Friction coefficients seem to vary from sample to sample.

The situation is even worse in production-representative joints. One in-joint torque-tension test with bolt tension measured in real time using ultrasonic pulse-echo techniques revealed variations inherent in how components fit together. A six-bolt pattern magnified the effects of imperfect contact between bolts and the bearing surface and produced a 60% sample-to-sample variation because both geometric and friction variables were changing over the sample set.

The bottom line is that neither the nut factor nor the long-form equation’s friction coefficients can be reliably established using reference tables. Only testing accurately determines friction conditions. As we have seen, these are too sensitive to component and assembly variation to be determined by analysis alone.

Testing reliably converts input torque to induced tension, letting engineers determine mean friction coefficients or nut factors and the distributions about those means. Tests may also help engineers identify inherent shortcomings in joints that need to be revised to make them more reliable.