Distributed optical fiber-protective layer-adhesive layer-matrix strain transfer calculation method
A technology of distributed optical fiber and calculation method, which is applied in the direction of using optical devices to transmit sensing components, using optical devices, converting sensor outputs, etc., can solve the problem of sensing optical fibers not being optical cables.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
specific Embodiment approach 1
[0022] Specific implementation mode one: as figure 1 As shown, this embodiment discloses a calculation method for distributed optical fiber-protective layer-adhesive layer-substrate strain transfer, the method includes the following steps:
[0023] Step 1: Determine the stiffness index of the optical fiber composite protective layer according to the cross-sectional parameters of the distributed sensing optical cable, construct the shear relationship model between the core optical fiber and the composite protective layer, and calculate the strain transfer rate of the core optical fiber-composite protective layer;
[0024] Step 2: According to the field layout conditions of the distributed sensing optical cable, determine the thickness and shear modulus of the adhesive layer of the distributed sensing optical cable, and calculate the composite protective layer-adhesive layer-substrate strain transfer rate based on the shear lag theory;
[0025] Step 3: According to the field lay...
specific Embodiment approach 2
[0027] Embodiment 2: This embodiment is a further description of Embodiment 1. The calculation method of the core optical fiber-composite protective layer strain transfer rate described in step 1 is:
[0028] Step 11: taking the rigid layer (i.e. steel strand) in the composite protective layer as the boundary, divide the composite protective layer into inner protective layer-rigid layer-outer protective layer structure, determine the cross-sectional size and material parameters of each layer layer by layer, The shear relationship model between the core optical fiber and the composite protective layer is constructed as shown in formula (1),
[0029]
[0030] where r f is the radial distance from the core fiber axis to the core fiber-inner protective layer interface, r i is the radial distance from the core fiber axis to the inner protective layer-rigid layer interface, τ f is the shear stress at the core fiber-inner protective layer interface, ε f is the normal strain of ...
specific Embodiment approach 3
[0034] Specific embodiment three: This embodiment is a further description of specific embodiment one. The calculation method of the composite protective layer-adhesive layer-substrate strain transfer rate described in step two is:
[0035] Step 21: Determine the size and material properties of the adhesive layer of the sensing optical cable, and construct a composite protective layer-adhesive layer-substrate strain transfer model based on the shear lag theory according to formula (3),
[0036]
[0037] where r s is the radial distance from the core fiber axis to the rigid layer-outer protective layer interface, r o is the radial distance from the axis of the core fiber to the interface of the outer protective layer-paste layer, r a is the radial distance from the axis of the core fiber to the adhesive layer-substrate interface, τ s is the shear stress at the interface between the rigid layer and the outer protective layer, ε s is the normal strain of the rigid layer, τ ...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


