Self-loosening vs preload relaxation: which one is your joint?

A bolted joint loses clamp force in two different ways. In rotational self-loosening the nut backs off, driven by the internal off-torque M_self = F_V · P / 2π. In non-rotational preload loss the nut never moves and the clamped stack simply gets shorter, through embedment, coating creep, gasket relaxation, thermal ratcheting and fretting wear. Because a bolt is a very stiff spring, that costs an M16 joint 26,9 % of its preload for every 30 µm of stack shortening. Every locking device on the market addresses the first. None addresses the second.

How to tell which one you have

The witness mark is broken. The nut has visibly rotated.

→ Rotational self-loosening. Transverse slip has broken the friction grip and the stretched bolt has unwound itself. A wedge-locking washer, a thread-form nut or a threadlocker will help. Check first whether the preload was adequate: critical slip scales with clamp force, and an under-preloaded joint will loosen whatever you fit to it.

The witness marks line up perfectly. The joint is still loose, leaking or fretting.

→ Non-rotational preload loss. The clamped stack has shortened. No locking device on the market will change this, and re-torquing resets the clock without addressing the cause. Look at embedment, coating creep, gasket relaxation, thermal cycling and fretting wear.

Rotational self-loosening — the mechanism everyone knows

Junker (SAE 690055, 1969) established that transverse dynamic load is far more severe than axial, and that loosening requires relative slip at the thread flanks and at the bearing face. Once the bearing face slips, the friction vector — fixed in magnitude at µN — reorients into the transverse direction, and its circumferential component, the only thing resisting the internal off-torque, collapses toward zero.

The driving moment is M_self = F_V · P / 2π, which for a 70 kN M16 joint is 22,3 N·m — larger, on its own, than the prevailing torque most locking-nut standards require.

Pai & Hess (J. Sound Vib. 253(3), 2002) later showed loosening initiates at 46 to 66 % of the critical slip amplitude — from localised micro-slip, well below the threshold for the complete slip Junker described.

Non-rotational preload loss — the mechanism nothing addresses

Published magnitudes of non-rotational preload loss, by mechanism and source.
MechanismPreload lostWhenSource
Cyclic plastic ratcheting, first engaged threads10–40 %within 200 cyclesJiang, Zhang & Lee, ASME JMD 125(3), 2003
Embedment~10 %80 % on first load applicationVDI 2230 Sheet 1
Zinc coating creep~20 %service lifeFriction 10(3), 2022
Gasket relaxation, PTFE7–20 %service lifeFriction 10(3), 2022
Gasket relaxation, elastomer sheet55–65 %service lifeFriction 10(3), 2022
Thermal cycling 20 → 120 °C, low preload41 %first cycleEraliev et al., Adv. Mech. Eng. 13(8), 2021
Stress relaxation at 600 °C> 50 %Friction 10(3), 2022
Aluminium engine block at 240–260 °C100 %one week, removable by handJaglinski & Lakes, 2007
CFRP joint, embedment share of total loss26,9 %1 000 cycles, biaxialYang, An, Chen & Zou, 2023
Cryogenic flight joint, no re-torque> 40 %5-year extrapolationNASA JWST, ESMATS 2018

Why a small movement costs so much force

A bolt is a stiff spring. For an M16 joint with a 27,2 mm grip:

k_S = 793 kN/mm (bolt) · k_P = 3 012 kN/mm (members) · k_eq = 627 kN/mm

Preload lost to a stack shortening f_Z is F_Z = f_Z · k_eq. So 30 µm costs 18,8 kN, which is 26,9 % of a 70 kN preload. 150 µm costs the entire preload.

Residual clamp force against imposed stack shortening: a rigid stack reaches zero at 150 micrometres while ISOKLAMP retains 97 percent
Model-predicted. M16, k_S = 793 kN/mm, k_P = 3 012 kN/mm, F_V = 70,0 kN.
Residual clamp force against imposed stack shortening. Model-predicted, M16, F_V = 70,0 kN.
Stack shorteningRepresentative causeRigid stackBelleville stackISOKLAMP CFR
30 µmall-metal embedment, first load application73,1 %93,7 %99,4 %
80 µmplus zinc coating creep, first service months28,3 %83,3 %98,4 %
150 µmplus gasket relaxation and thermal ratcheting, one service year0,0 %68,7 %97,0 %

What the industry says about its own products

“Safety devices principally intended to resist rotational loosening and prevent loss of fasteners.”
— NASA-STD-5020, on locking features

That is an accurate description of the entire product category, and an admission. The industry has confused “the nut did not fall off” with “the joint still works.”

“Testing in accordance with this International Standard does not allow an absolute statement to be made on the locking behaviour of bolted assemblies under service loads.”
— ISO 16130:2015, scope

The standard tests are comparative bench tests at one amplitude, one frequency, one temperature. None of the four main ones — DIN 65151, DIN 25201-4, ISO 16130, NASM 1312-7 — measures non-rotational preload loss at all. NASM 1312-7 does not measure preload whatsoever; its criterion is rotation greater than 360°.

The two modes are causally linked

This is what makes the gap expensive. Non-rotational loss causes rotational loosening. Embedment and creep are precisely what drop the preload below the level at which friction grip prevents slip. Critical slip scales approximately with preload; drop the preload and you drop the slip threshold, and a joint that was stable becomes a joint that unwinds.

A rotational locking device fitted to a joint with an unmanaged relaxation problem is holding a nut onto a bolt that no longer clamps anything.

Glossary

clamp force F
The compressive force holding the clamped parts together, in newtons.
initial clamp force F_M
Clamp force immediately after tightening, before any relaxation.
pre-stressing force F_V
The target assembly preload; 70,0 kN for the M16 cl. 10.9 reference joint.
residual clamp force
Clamp force remaining after a defined number of load cycles.
relative clamp-force loss Y
Residual clamp force expressed as a fraction of F_V, per DIN 25201-4.
transverse displacement t_s
Imposed transverse amplitude in a Junker-type test, ±0,60 mm here.
load cycles N
Number of imposed transverse load cycles; the DIN 25201-4 criterion is read at N = 2 000.
embedment F_Z
Preload lost to plastic flattening of surface asperities in the stack.
load factor Φ
The share of an external axial load that is carried by the bolt rather than relieving the members.
prevailing torque
Torque required to run a locking nut down its thread with no clamp force present.
breakaway torque
Torque required to start loosening a tightened fastener.
self-loosening
Progressive rotational loss of preload under dynamic load, per Junker.
slackening
Loss of preload without rotation; the non-rotational mode.
micro-slip
Localised relative motion at part of the contact interface, below gross slip.
gross slip
Complete relative sliding across the whole bearing interface.
Junker curve
Residual clamp force plotted against load cycles in a transverse vibration test.