A study of loosening and fatigue of bolted joints under transverse vibration

Shinji Hashimura, Darrell F. Socie

Research output: Contribution to journalConference article

7 Citations (Scopus)

Abstract

Bolt loosening fatigue tests under small transverse vibrations have been performed to understand the behavior in the long life region. The current study is focused on the loosening-fatigue mechanism and on the estimation of nominal stress at the root of the first thread caused by transverse vibration. Results show that if a bolt has loosened within 103∼104 vibration cycles, damage such as crack nucleation at the root of the first thread is not observed, and loosening is due to bolt rotation. However, if loosening does not occur until approximately 105∼106 cycles, then a crack is observed at the root of the first thread in the all experiments. Loosening occurs due to loss of bolt stiffness caused by crack nucleation and propagation which then leads to bolt rotation. Results also show that the initial clamping force above a threshold level does not significantly influence the loosening-fatigue life of a bolted joint. The amplitude of the transverse vibration force is the most significant influence on the loosening-fatigue life.

Original languageEnglish
JournalSAE Technical Papers
DOIs
Publication statusPublished - 2005 Jan 1
Externally publishedYes
Event2005 SAE World Congress - Detroit, MI, United States
Duration: 2005 Apr 112005 Apr 14

Fingerprint

Bolted joints
Bolts
Fatigue of materials
Cracks
Nucleation
Crack propagation
Stiffness
Experiments

ASJC Scopus subject areas

  • Automotive Engineering
  • Safety, Risk, Reliability and Quality
  • Pollution
  • Industrial and Manufacturing Engineering

Cite this

A study of loosening and fatigue of bolted joints under transverse vibration. / Hashimura, Shinji; Socie, Darrell F.

In: SAE Technical Papers, 01.01.2005.

Research output: Contribution to journalConference article

@article{3bac4a1a0dae424e8596ea3ba3bd5ec7,
title = "A study of loosening and fatigue of bolted joints under transverse vibration",
abstract = "Bolt loosening fatigue tests under small transverse vibrations have been performed to understand the behavior in the long life region. The current study is focused on the loosening-fatigue mechanism and on the estimation of nominal stress at the root of the first thread caused by transverse vibration. Results show that if a bolt has loosened within 103∼104 vibration cycles, damage such as crack nucleation at the root of the first thread is not observed, and loosening is due to bolt rotation. However, if loosening does not occur until approximately 105∼106 cycles, then a crack is observed at the root of the first thread in the all experiments. Loosening occurs due to loss of bolt stiffness caused by crack nucleation and propagation which then leads to bolt rotation. Results also show that the initial clamping force above a threshold level does not significantly influence the loosening-fatigue life of a bolted joint. The amplitude of the transverse vibration force is the most significant influence on the loosening-fatigue life.",
author = "Shinji Hashimura and Socie, {Darrell F.}",
year = "2005",
month = "1",
day = "1",
doi = "10.4271/2005-01-1320",
language = "English",
journal = "SAE Technical Papers",
issn = "0148-7191",
publisher = "SAE International",

}

TY - JOUR

T1 - A study of loosening and fatigue of bolted joints under transverse vibration

AU - Hashimura, Shinji

AU - Socie, Darrell F.

PY - 2005/1/1

Y1 - 2005/1/1

N2 - Bolt loosening fatigue tests under small transverse vibrations have been performed to understand the behavior in the long life region. The current study is focused on the loosening-fatigue mechanism and on the estimation of nominal stress at the root of the first thread caused by transverse vibration. Results show that if a bolt has loosened within 103∼104 vibration cycles, damage such as crack nucleation at the root of the first thread is not observed, and loosening is due to bolt rotation. However, if loosening does not occur until approximately 105∼106 cycles, then a crack is observed at the root of the first thread in the all experiments. Loosening occurs due to loss of bolt stiffness caused by crack nucleation and propagation which then leads to bolt rotation. Results also show that the initial clamping force above a threshold level does not significantly influence the loosening-fatigue life of a bolted joint. The amplitude of the transverse vibration force is the most significant influence on the loosening-fatigue life.

AB - Bolt loosening fatigue tests under small transverse vibrations have been performed to understand the behavior in the long life region. The current study is focused on the loosening-fatigue mechanism and on the estimation of nominal stress at the root of the first thread caused by transverse vibration. Results show that if a bolt has loosened within 103∼104 vibration cycles, damage such as crack nucleation at the root of the first thread is not observed, and loosening is due to bolt rotation. However, if loosening does not occur until approximately 105∼106 cycles, then a crack is observed at the root of the first thread in the all experiments. Loosening occurs due to loss of bolt stiffness caused by crack nucleation and propagation which then leads to bolt rotation. Results also show that the initial clamping force above a threshold level does not significantly influence the loosening-fatigue life of a bolted joint. The amplitude of the transverse vibration force is the most significant influence on the loosening-fatigue life.

UR - http://www.scopus.com/inward/record.url?scp=85072452418&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=85072452418&partnerID=8YFLogxK

U2 - 10.4271/2005-01-1320

DO - 10.4271/2005-01-1320

M3 - Conference article

AN - SCOPUS:85072452418

JO - SAE Technical Papers

JF - SAE Technical Papers

SN - 0148-7191

ER -