Creation of a SMART Layer prototype with fiber-optic sensors for monitoring the stress–strain state of structures fabricated from polymeric composite materials and an estimation of its technical characteristics

2021 ◽  
Vol 88 (4) ◽  
pp. 209
Author(s):  
G. S. Shipunov ◽  
M. A. Baranov ◽  
A. S. Nikiforov ◽  
A. A. Tikhonova ◽  
V. M. Osokin ◽  
...  
Keyword(s):  
Composite Materials ◽  
Strain State ◽  
Fiber Optic ◽  
Polymeric Composite ◽  
Fiber Optic Sensors ◽  
Stress Strain ◽  
Polymeric Composite Materials ◽  
Stress Strain State

scholarly journals Application of BIM-technologies during the construction and operation of buildings and structures

2021 ◽  
Vol 274 ◽  
pp. 06009
Author(s):  
Andrey Bogdanov ◽  
Vladislav Zaitsev ◽  
Karina Khalitova
Keyword(s):  
Decision Making ◽  
Life Cycle ◽  
Strain State ◽  
Fiber Optic ◽  
Fiber Optic Sensors ◽  
The State ◽  
Building Structure ◽  
Stress Strain ◽  
Stress Strain State ◽  
Incoming Information

The relevance of implementing BIM technologies at all stages of the building's life cycle from design to decision-making on its demolition is shown. Variants of the stress-strain state of buildings and structures are considered. An algorithm for analyzing incoming information and making decisions about major repairs, reconstruction, or demolition of an object is developed, depending on the values of parameters, their duration, and combinations obtained from sensors installed during their construction. The use of fiber-optic sensors for obtaining information and subsequent analysis of the state of the building structure and determining dangerous movements of its individual elements is proposed.

scholarly journals Fiber-optic sensors for monitoring the stress-strain state of construction objects

2019 ◽  
Vol 643 ◽  
pp. 012113
Author(s):  
E Badeeva ◽  
D Serebryakov ◽  
E Shachneva ◽  
A Badeev ◽  
T Murashkina
Keyword(s):  
Strain State ◽  
Fiber Optic ◽  
Fiber Optic Sensors ◽  
Stress Strain ◽  
Stress Strain State

Stress-Strain State Exploration of Stringer Made of Composite Materials Depending on Layers Stacking Structure

2018 ◽  
Vol 284 ◽  
pp. 71-76
Author(s):  
P.V. Solovyev ◽  
A.I. Gomzin ◽  
L.A. Ishbulatov ◽  
S.N. Galyshev ◽  
F.F. Musin
Keyword(s):  
Composite Materials ◽  
Cross Section ◽  
Strain State ◽  
Stress Strain ◽  
Stress Strain State ◽  
Airplane Wing ◽  
External Loads ◽  
Stacking Structure ◽  
Composite Carbon ◽  
Shaped Cross Section

In this article the results of stress-strain state investigation for composite airplane wing stringer with different layers stacking structures are presented. As an object of research, a stringer made of composite carbon with V-shaped cross-section is considered. Due to the stress-strain state analysis of various stringer structures, the most effective structure for stringer layers stacking is selected, both in the view of providing the most rigidity and optimal perception by the stringer the field of external loads, which are most typical for the conditions of its operation.

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