Calculation method of distributed optical fiber-protective layer-pasting layer-substrate strain transfer
A technology of distributed optical fiber and protective layer, which is applied in the direction of using optical device to transmit sensing components, adopting optical device, converting sensor output, etc., can solve the problem that sensing optical fiber is not optical cable, etc., and achieve the effect of solving the problem of accurate mapping
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specific Embodiment approach 1
[0022] DETAILED DESCRIPTION figure 1 As shown, the present embodiment discloses a method of calculating a distributed optical fiber-protective layer-adhesive layer-matrix strain transmission, which includes the following steps:
[0023] Step 1: Determine the stiffness indicator of the fiber composite protective layer according to the distributed sensing cable section used, construct the shear relationship model of the core fiber and the composite protection layer, calculate the core fiber-composite protection layer strain transmission rate;
[0024] Step 2: Determine the thickness of the distributed sensing fiber optic cable to obtain the thickness and shear modulus of the distributed sensing fiber optic cable, calculate the composite protective layer-adhesive layer-matrix strain transmission rate based on delay theory;
[0025] Step 3: Depending on the site, the fiber-composite protective layer-adhesive layer-matrix model is established according to the on-site setting conditions...
specific Embodiment approach 2
[0027] DETAILED DESCRIPTION OF THE INVENTION 2: The present embodiment is a further description of the specific embodiments, and the calculation method of the core fiber-composite protection layer strain transmission rate is:
[0028] Step one by one: Taking the rigid layer (i.e., steel stranded pair) in the composite protection layer, the composite protective layer is divided into an inner protective layer-rigid layer-outer protective layer structure, and the layering determines the size and material parameters of each layer, The shear relationship model of the core fiber and the composite protection layer is shown in the formula (1),
[0029]
[0030] In r f To the core fiber axis to the core fiber - the radial distance of the inner protective layer interface, R i The radial distance of the core fiber axis to the internal protective layer - the radial distance of the rigid layer interface, τ f True stress at the core fiber - inner protective layer interface, ε f For the core f...
specific Embodiment approach 3
[0034] DETAILED DESCRIPTION OF THE INVENTION 3: The present embodiment is a further description of the specific embodiment, and the composite protective layer-adhesive layer-matrix strain transmission rate according to step b is:
[0035] Step 2: Determine the size and material properties of the sensing fiber optic cable adhesive layer, and construct a composite protective layer based on clarested theory based on the formula (3).
[0036]
[0037] In r s The radial distance of the core fiber axis to the rigid layer - the outer protective layer interface, R o The radial distance of the core optical fiber axis to the outer protective layer - the radial distance of the adhesive layer interface, R a The radial distance of the core fiber axis to the adhesive layer - the radial distance of the matrix interface, τ s Shear stress at the rigid layer - outer protective layer interface, ε s For the rigid layer, τ o,r For the outer protective layer, the shear stress of a side of the optical...
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