收藏切换
Tightening Force Monitoring Method of Structures by a Smart Fiber Bolt Under High Temperature Circumstance
收藏切换
PDF
Zeli WANG1, Gang FAN2, Yuning WANG3
Missiles and Space Vehicles | 2026, (3) : 101 - 106
Less
收藏切换
Missiles and Space Vehicles | 2026, (3): 101-106
Environment and Test
Tightening Force Monitoring Method of Structures by a Smart Fiber Bolt Under High Temperature Circumstance
Full
Zeli WANG1, Gang FAN2, Yuning WANG3
Affiliations
  • 1.Beijing Institute of Structure and Environment Engineering, Beijing, 100076
  • 2.Science and Technology on Space Physics Laboratory, Beijing, 100076
  • 3.Aerospace Research Institute of Materials & Processing Technology, Beijing, 100076
Published: 2026-06-25 doi: 10.7654/j.issn.2097-1974.20260313
Outline
收藏切换

A novel smart bolt combined with fiber EFPI/FBG micro-structures is presented to monitor the state of tightening force of a bolted aerospace structure under high temperature circumstance. In this smart fiber bolt, the fiber EFPI micro-structure is applied to obtain the length variation in the direct of bolt axis under the effect of tightening force. And the fiber Bragg grating micro-structure is applied to obtain the bolt temperature. With the parameters obtained by the fiber EFPI/FBG micro-structures, the tightening force can be obtained through the approach presented. Test samples which are 50mm long M8 bolts combined with fiber EFPI/FBG micro-structures are made and tested by a universal testing machine with a heating chamber. The test results show that the smart fiber bolt presented can be used to obtain maximum 10kN tightening force under the temperature of 500 degree centigrade with maximum relative error 3.1%. This smart fiber bolt can be used to monitor the state of structure connection under high temperature circumstance.

smart bolt  /  tightening force  /  high temperature structure  /  fiber optical sensing  /  state monitor
Zeli WANG, Gang FAN, Yuning WANG. Tightening Force Monitoring Method of Structures by a Smart Fiber Bolt Under High Temperature Circumstance[J]. Missiles and Space Vehicles, 2026 , (3) : 101 -106 . DOI: 10.7654/j.issn.2097-1974.20260313
Year 2026 volume Issue 3
PDF
186
84
Cite this Article
BibTeX
Article Info
doi: 10.7654/j.issn.2097-1974.20260313
  • Receive Date:2025-03-11
  • Online Date:2026-07-22
  • Published:2026-06-25
Article Data
Affiliations
History
  • Received:2025-03-11
  • Revised:2025-04-28
Affiliations
    1.Beijing Institute of Structure and Environment Engineering, Beijing, 100076
    2.Science and Technology on Space Physics Laboratory, Beijing, 100076
    3.Aerospace Research Institute of Materials & Processing Technology, Beijing, 100076
References
Share
https://castjournals.cast.org.cn/joweb/ddyht/EN/10.7654/j.issn.2097-1974.20260313
Share to
QR

Scan QR to access full text

Cite this article
BibTeX
Citations
表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
关闭全屏
  • BibTeX
  • EndNote
  • RefWorks
  • TxT