Roymech engineering encyclopedia

Bolt Preload – Joint Stiffness, Tightening Torque and Clamp Force


Bolt preload is the initial tensile force introduced into a fastener during tightening. The corresponding compressive force clamps the joint members together and is fundamental to the performance of most highly loaded bolted joints.

Need help selecting a bolt, screw or threaded fastener? See the Fastener Selection Guide for guidance on fastener types, threads, strength classes, loading, preload, tightening, thread engagement, locking, studs and anchors.

This page provides engineering methods for estimating bolt preload, bolt and joint stiffness, the distribution of external separating loads, thermal effects, tightening torque and methods of establishing or measuring bolt tension.

Important: Bolt preload calculations can become complex for critical joints. Fatigue, joint settlement and embedding, eccentric loading, gasket behaviour, temperature, tightening scatter, friction, relaxation and load introduction can all affect the actual bolt load. The methods below are useful engineering reference methods but should not replace the applicable design standard or a detailed joint analysis where failure is safety-critical.

See also: Fastener Engineering Tables and Design Data.

Page sections:
Bolt preload | Bolt stiffness | Joint stiffness | External load distribution | Thermal effects | Tightening torque | Combined stress | Preload methods | Preload accuracy

Nomenclature

Symbol Description Typical Units
Ab Effective bolt cross-sectional area mm2 or m2
At Bolt tensile stress area mm2 or m2
d Nominal bolt diameter mm or m
Fp Initial bolt preload N
Fe External separating load applied to the joint N
ΔFb Increase in bolt load caused by external load N
ΔFj Reduction in joint clamping force caused by external load N
Fb Total tensile force in bolt N
kb Bolt stiffness N/mm or N/m
kj Effective stiffness of clamped joint members N/mm or N/m
C Bolt load fraction or joint stiffness factor dimensionless
E Young's modulus N/mm2 or N/m2
L Effective length mm or m
δ Elastic deflection mm or m
T Tightening torque N·m
K Nut factor used in simplified torque-preload equation dimensionless
μ Thread coefficient of friction dimensionless
μc Bearing-face coefficient of friction dimensionless
α Coefficient of thermal expansion when used in thermal equations K-1
ΔT Temperature change K or °C

Bolt Preload

A tightened bolt is stretched elastically while the joint members are compressed. The tensile force in the bolt and the compressive clamping force in the joint are approximately equal and opposite before an external load is applied.

Bolt preload and joint stiffness diagram showing bolt tension and joint compression

A sufficiently high and controlled preload is generally desirable because it helps maintain joint contact, reduces the alternating component of bolt stress under fluctuating external loads, improves resistance to loosening and can prevent relative movement between the joint faces.

However, preload must remain within the permissible capacity of the fastener, threads and joint. Excessive preload can cause bolt yielding, thread stripping, bearing damage or damage to the clamped components.

Preload Relative to Proof Load

The original RoyMech guidance used a preload of approximately 80% of bolt proof load as a typical value. This is a useful traditional engineering reference point for some non-critical steel bolted joints, but it is not a universal preload requirement.

Fp ≈ 0.8 Fproof
Legacy / preliminary guidance: The 80% proof-load value is retained from the original RoyMech engineering notes. The appropriate target preload depends on the fastener system, joint design, tightening method, preload scatter, required clamp load and applicable design standard. Do not automatically specify 80% of proof load for every bolted joint.

Bolt Stiffness

Within the elastic range, a bolt behaves approximately as a tension spring. For a uniform section:

δ = FL EA

Therefore the axial stiffness is:

k = F δ = EA L

A real bolt normally consists of several sections having different cross-sectional areas. The unthreaded shank, threaded portion and the elastic contribution of the head and engaged threads can therefore be treated as springs connected in series.

1 kb = ∑ i Li Ei Ai

For sections of the same material:

1 kb = 1 E ∑ i Li Ai

The original RoyMech method allows approximately for elasticity in the bolt head and engaged nut/thread region by using effective lengths:

Lse = Ls + 0.4 ds Lte = Lt + 0.4 dr

where Ls is the shank length, Lt is the threaded length within the effective bolt spring, ds is the shank diameter and dr is the thread root diameter.

Bolt stiffness model showing effective shank and threaded lengths

Engineering approximation: The 0.4d effective-length corrections are retained from the original RoyMech method. More detailed bolted-joint models may use different effective head and thread lengths.

Clamped Joint Stiffness

Determining the stiffness of the clamped members is generally more difficult than determining bolt stiffness because the compressive load spreads through the material beneath the bolt head, nut and washers.

For a simple uniform compressed section:

kj = EA L

For several joint components in series:

1 kj = ∑ i Li Ei Ai

The original RoyMech notes use a rough preliminary approximation in which the compressed region is treated as an annulus having an outside diameter of approximately 2.5 times the bolt diameter and an inside diameter approximately equal to the bolt diameter.

Legacy preliminary approximation: The 2.5d annulus is retained as useful historical RoyMech guidance for rough calculations. Actual joint stiffness depends strongly on joint geometry, washer and bearing-face diameter, plate thickness, hole size, material properties and the spread of compression through the members. For a detailed calculation see Joint Stiffness.

External Load Distribution Between Bolt and Joint

When an external tensile force tends to separate a preloaded joint, the whole external load is not normally added directly to the existing bolt preload.

Before joint separation, part of the external load increases bolt tension and the remainder reduces compression in the clamped members.

Bolt and joint stiffness diagram showing external load distribution

Define the bolt load fraction:

C = kb kb + kj

The increase in bolt load caused by an external separating load Fe is:

Δ Fb = C Fe

The corresponding reduction in joint compression is:

Δ Fj = ( 1 − C ) Fe

The total bolt force while the joint remains closed is therefore:

Fb = Fp + C Fe

The remaining joint compression is:

Fj = Fp − ( 1 − C ) Fe

Joint Separation Load

Separation begins when the remaining compressive force in the joint reaches zero:

Fj = 0

Therefore the idealised external separation load is:

Fe,sep = Fp 1 − C
Why preload improves fatigue performance: If the bolt is relatively compliant and the clamped joint is relatively stiff, C is small. Only a small proportion of a fluctuating external load then appears as a fluctuating tensile load in the bolt while the joint remains clamped. This is the engineering principle behind RoyMech's original observation that longer, relatively slender bolts can provide favourable fatigue behaviour in suitably designed joints.

Thermal Effects on Bolt Preload

If the bolt and clamped components have similar coefficients of thermal expansion and experience approximately the same temperature change, thermal effects on preload may be small.

If their coefficients of thermal expansion or temperatures differ, differential expansion can increase or decrease bolt preload.

For an idealised bolt and joint having the same effective length L and uniform temperature change ΔT:

Δ Lj = αj L Δ T Δ Lb = αb L Δ T

The differential free expansion is:

Δ Ldiff = ( αj − αb ) L Δ T

The equivalent stiffness of the bolt and joint acting in series is:

keq = kb kj kb + kj

For this simple model, the change in bolt preload is:

Δ FT = keq ( αj − αb ) L Δ T

and:

Fp,hot = Fp + Δ FT
Simplified thermal model: Real joints may have different effective bolt and joint lengths, non-uniform temperature distributions, gaskets, creep, relaxation and temperature- dependent material properties. Those effects require a more detailed analysis.

Setting Preload by Tightening Torque

The most widely used approximate relationship between tightening torque and bolt preload is:

T = K Fp d

where:

  • T = tightening torque;
  • K = empirical nut factor;
  • Fp = desired preload;
  • d = nominal bolt diameter.

Legacy Nut-Factor Reference Values

The following values are retained from the original RoyMech page as indicative historical engineering values.

Steel Thread / Surface Condition Indicative K
As received – stainless on mild or alloy steel 0.30
As received – mild or alloy steel on similar material 0.20
Cadmium plated 0.16
Molybdenum-disulphide grease 0.14
PTFE lubrication 0.12
Legacy / indicative data: These K values are retained because they are useful for understanding the magnitude of lubrication and surface-condition effects. They should not be used as guaranteed values for a particular fastener system. Actual torque/clamp-force behaviour depends on the fastener finish, lubricant, coating, bearing surface, thread condition, tightening speed and manufacturing variation. Use measured or supplier-qualified data where preload accuracy is important.

Example – Simplified Torque Estimate

For:

  • Target preload Fp = 20 kN
  • Nominal diameter d = 10 mm = 0.010 m
  • Nut factor K = 0.20
T = 0.20 × 20000 × 0.010 = 40 N · m

This is an estimate, not a guarantee that tightening to 40 N·m will produce exactly 20 kN preload.

Thread and Bearing Friction Torque

A more detailed tightening model separates the torque required to advance the thread from the torque lost through friction in the thread and beneath the rotating nut or bolt head.

Bolt tightening torque equation including thread and collar friction

The original equation uses:

  • Fp = desired bolt preload;
  • p = thread pitch;
  • dm = mean thread diameter;
  • μ = coefficient of thread friction;
  • μc = coefficient of bearing-face or collar friction;
  • α = half included thread angle, 30° for ISO metric threads;
  • rc = effective collar friction radius.

Friction normally consumes most of the applied tightening torque. Consequently relatively small changes in thread or bearing-face friction can produce substantial changes in achieved preload.

This is the principal limitation of torque-controlled tightening.

Legacy Simplified Friction Equation

The original RoyMech page gives a further approximation for a standard 60° thread by assuming:

  • μc = μ;
  • dm ≈ 0.92d;
  • α = 30°;
  • rc ≈ 0.625d.

This reduces to:

T ≈ Fp ( 0.159 p + 1.156 μ d )
Legacy approximation: This expression is retained from the original RoyMech analysis as a useful engineering approximation. It assumes particular geometry and equal thread and bearing friction coefficients and should not be treated as a universal torque-preload equation.

Friction reference data are available on the Coefficient of Friction page.

Bolt Stress During Tightening

During torque tightening the bolt is subjected simultaneously to axial tension from the preload and torsion generated by thread friction. Consequently the stress state during tightening is more severe than that produced by axial preload alone.

Combined tensile and torsional stress equation for a tightened bolt

The original RoyMech expression uses:

  • F = bolt tensile force;
  • Tf = thread torque;
  • Ar = thread-root area;
  • dr = thread-root diameter.

For some calculations the tensile stress area At can be used with an equivalent stress diameter:

dt = 4 At π

See Screw Thread Stress Areas and Thread Stripping for tensile stress-area calculations.

Methods of Establishing Bolt Preload

There are several ways of establishing or measuring preload. Selection depends on the required accuracy, fastener size, access, joint geometry, number of fasteners and installation conditions.

Torque-Controlled Tightening

Torque-controlled tightening is convenient and inexpensive but the achieved preload is strongly affected by friction. Where accurate preload is required, the torque procedure should be based on representative torque/clamp-force testing or validated installation data.

Turn-of-Nut / Angle Tightening

After the joint has reached a defined snug condition, the nut or bolt is rotated through a specified additional angle. This controls fastener extension more directly than torque alone.

The required rotation depends on the bolting system, grip length and joint configuration. Compressible coatings, settlement and an inconsistent snug condition can affect the result.

Direct Tension Indicators

Direct tension indicators provide an indication of achieved bolt preload rather than relying solely on tightening torque. Structural DTI systems use specially formed washers whose projections compress as bolt tension increases.

The original RoyMech notes described checking the remaining gap using a feeler gauge. That remains useful historical information, but the installation and acceptance procedure should be taken from the specification applicable to the actual DTI system.

Bolt Elongation Measurement

If the effective bolt stiffness is known, preload can be inferred from measured elastic elongation:

Fp = kb δ

For a uniform bolt section this becomes:

Fp = E A δ L

Ultrasonic Measurement

Ultrasonic instruments can infer bolt extension from changes in acoustic time-of-flight. They are particularly useful where bolt tension must be measured without direct access to both ends of the fastener.

Accuracy depends on calibration, bolt material, geometry, temperature, surface condition and operator procedure.

Hydraulic Bolt Tensioning

A hydraulic tensioner applies a direct axial tensile force to the bolt. While the bolt is stretched, the nut is run down; hydraulic pressure is then released and part of the applied tension remains as bolt preload.

Hydraulic tensioning avoids the high torsional stress associated with torque tightening and is particularly useful for large studs and heavily loaded flange joints.

Allowance must be made for load transfer and preload loss when hydraulic pressure is released.

Multi-Jackbolt Tensioners

Multi-jackbolt tensioners use a number of smaller jackbolts around a main nut body. The individual jackbolts can be tightened using much lower torque than would be required to tighten a conventional large nut directly.

The original RoyMech page specifically identified Superbolt-type systems as a practical option for large bolts requiring otherwise very high tightening torques.

Strain Gauges and Instrumented Fasteners

Strain gauges, load-indicating bolts and other instrumented fasteners can provide direct or indirect measurement of bolt tension. These methods are useful where preload verification is more important than installation simplicity.

Thermal Tensioning

The original RoyMech notes also describe thermal tensioning. The bolt is heated, installed and the nut brought into position. Cooling contracts the bolt and generates tensile preload.

For a simple free thermal-strain approximation:

ε = σ E

and:

ε = α Δ T

giving:

Δ T = σ E α

This is an idealised relationship. In practice, heat transfer to the joint, temperature gradients, installation time, relaxation and uncertainty in the final grip condition make thermal preload control difficult.

Legacy Structural Bolting Information

Legacy standard information: The original RoyMech page referred to BS 4604 for high-strength friction-grip structural bolting and described torque, turn-of-nut and direct-tension measurement procedures. This material is retained below for engineers dealing with older structures, drawings and specifications. BS 4604 should not be used as the current specification for new structural bolting.

Under the historical BS 4604 approach, high-strength friction-grip bolts were installed to specified minimum tensions using methods including:

  • calibrated torque tightening;
  • part-turn / turn-of-nut tightening;
  • direct tension measurement.

The original RoyMech notes emphasised that torque-controlled results could show substantial variation even when a defined installation procedure was followed. They also noted the importance of establishing the correct snug condition before turn-of-nut tightening.

Those observations remain useful engineering principles even though the referenced structural-bolting standard is now legacy.

Current structural bolting: For new UK/European preloaded structural bolting, refer to the applicable parts of the BS EN 14399 series and the structural execution requirements applicable to the project. Direct tension indicators for HR/HV bolt and nut assemblies are covered by BS EN 14399-9:2018.

Indicative Bolt Preload Accuracy

The following figures are retained from the original RoyMech page. They are useful for comparing the approximate relative capability of different preload-setting methods, but they should not be interpreted as guaranteed accuracy limits.

Preload Method Original RoyMech Indicative Accuracy
Operator feel ±35%
Torque wrench ±25%
Angle tightening / turn-of-nut ±15%
Load-indicating washer ±10%
Measured bolt elongation ±5%
Hydraulic bolt tensioning approximately ±1% to ±10%
Strain gauges / ultrasonics approximately ±1%
Multi-jackbolt tensioner approximately ±5%
Legacy indicative data: These percentages are retained because they provide useful historical engineering guidance and relative comparison between methods. Actual uncertainty depends on equipment, calibration, installation procedure, fastener geometry, friction, operator technique and joint conditions. They are not guaranteed performance figures for modern equipment or installation procedures.

Preload Loss After Tightening

The preload immediately after tightening is not necessarily the preload that remains in service. Possible causes of preload loss include:

  • embedding and flattening of surface asperities;
  • joint settlement;
  • gasket relaxation;
  • creep of soft joint materials;
  • paint or coating compression;
  • temperature changes;
  • plastic deformation beneath the bolt head, nut or washer;
  • thread or bearing-surface yielding;
  • vibration and relative movement where the joint is inadequately clamped.

These effects should be considered where maintaining a minimum service clamp force is important.

Practical Bolt Preload Design Considerations

  • Establish the clamp force required to prevent separation, slip, leakage or other unacceptable joint behaviour.
  • Select a fastener and property class capable of providing the required preload with adequate margin.
  • Check bolt tensile stress, thread capacity and bearing stresses beneath the head, nut and washers.
  • Determine bolt and joint stiffness where external separating loads are significant.
  • Allow for preload scatter when specifying the target installation preload.
  • Account for settlement, embedding, gasket relaxation and other expected preload losses.
  • Consider fatigue using the fluctuating bolt load rather than simply applying the full fluctuating external joint load to the bolt.
  • Use controlled friction conditions when tightening by torque.
  • Where preload is critical, consider direct tension measurement, elongation measurement, hydraulic tensioning or another method less dependent on friction.

Torque / Clamp-Force Testing

ISO 16047:2005 with Amendment 1:2012 specifies conditions for torque/clamp-force testing of threaded fasteners and related parts. It provides a controlled test framework for determining torque and clamp-force characteristics rather than assuming a universal nut factor.

This is particularly relevant when a tightening torque is to be established for a specific fastener, coating and lubrication system.

Related RoyMech Bolt Preload Calculators

Use these calculators for bolt preload, tightening torque, proof load and clamp-force checks.

Calculator Use
Bolt Preload Calculator Estimate bolt preload and clamp force from tightening torque.
Bolt Tightening Torque Calculator Calculate tightening torque from target preload, diameter and nut factor.
Bolt Proof Load Calculator Calculate proof load and compare it with the proposed preload.
Washer Bearing Pressure Calculator Calculate bearing pressure beneath a washer, nut face or bolt head from clamp force.
Bolt Tensile Stress Calculator Calculate tensile stress from axial bolt load.
Bolted Joint and Fastener Calculators View all RoyMech bolt and fastener calculators.

Related Threaded Fastener References

External Engineering References

  1. ExcelCalcs – Detailed Bolted Joint Calculations – legacy spreadsheet-based bolted-joint calculation reference.
  2. Bolt Science – specialist technical information on bolted joints and fastener tightening.
  3. Superbolt – multi-jackbolt tensioning systems and technical information.
  4. Rotabolt – bolt tension monitoring systems.
  5. Futek Bolt Torque Calculator – external bolt torque calculation resource.
  6. SmartBolts – visual direct-tension-indicating fasteners.
  7. Applied Bolting – direct tension indicators and structural bolting information.
  8. SureBolt – ultrasonic bolt tension measurement information.
  9. MITCalc – engineering calculation software including bolted-joint calculations.
  10. University of Western Australia – Loads in an Elastic Bolted Assembly – detailed engineering notes on bolted-joint loading.

Standards References

  • ISO 16047:2005 + Amd 1:2012 – Fasteners – Torque/clamp force testing.
  • ISO 898-1:2013 – Mechanical properties of fasteners made of carbon steel and alloy steel – Part 1: Bolts, screws and studs with specified property classes.
  • BS EN 14399 series – High-strength structural bolting assemblies for preloading.
  • BS EN 14399-9:2018 – High-strength structural bolting assemblies for preloading – System HR or HV – Direct tension indicators for bolt and nut assemblies.
  • BS 4604 – legacy British Standard referenced by the original RoyMech page for high-strength friction-grip structural bolting. Retained here for historical engineering reference rather than current specification.

ISO 16047 remains the published ISO torque/clamp-force testing standard and includes Amendment 1:2012. For critical tightening specifications, use the applicable current standard together with fastener-manufacturer data and, where appropriate, testing of the actual fastener, lubricant and coating combination.





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