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Figure 5: Illustration of a finite element mesh used for this study.
        Figure 4: Illustration of the geometric parameters for lid and stiffener
        configurations; deformations were exaggerated for clarity. Anchoring outside of   Our model adds the loads condition over the induced “as-
        the package is also considered to evaluate extended fiber length.  assembled” fiber bends. From the assembled condition,
                                                             the  load  cases  start  with one of the following: 1) thermo-
          A nonlinear finite element model is used to evaluate the   mechanical loading over a wide range of temperatures, from
        above-mentioned strategies on a selected module geometry   deep cold environments (-40°C), to 250°C solder reflow for
        for various fiber layouts inside the package. The mechanical   surface-mount technology (SMT) compatibility and  ball  grid
        stresses and strains in the assembly are calculated with   array  (BGA)  attached  co-package; or 2) the retention forces
        a nonlinear algorithm to take into account the complex   that ribbons must withstand when pulled. Our goal is to ensure
        phenomena that occur under the various loading conditions   that the fiber bending, and implied stresses are below the
        that were used. First, the contact element between different   expected limits for these conditions. Table 1 details the loading
        parts of the module is modeled and activated due to thermally-
        induced warpage. Second, the instability inherent because of
        the high slenderness ratio of the optical fibers is taken into
        account by using a large displacement methodology. Therefore,
        fiber  buckling  under  compressive  efforts  is  accurately
        represented in the finite element model.
          The last significant nonlinear phenomenon captured by the
        model is the material properties’ dependence on temperature.
        In the temperature range considered in the present study,
        some materials undergo glass transition, which induces a
        sudden variation in the thermal expansion coefficient and
        elastic modulus. A pseudo-rheological strategy specifically
        developed for modeling the glass transition, described in [8],
        is used. The analysis also includes the effect of the assembly
        process to correctly track  the stresses in the module because
        the fiber ribbons are placed and positioned using interference-  Table 1: Simulation loading conditions.
        based fabrication. Once the adhesives are properly cured, the
        module is cooled down to room temperature. The interference   conditions, which are also illustrated in Figure 6. The fiber
        fabrication, curing and subsequent cooling induce bending   stresses and curvature are extracted as performance criteria
        in the fibers, which influences stress and how the fibers will   to understand key parameters influencing how the fibers are
        deform under thermal and mechanical loading. The model   loaded within the module. Also, the fiber needs to conserve
        described above captures all these effects in the simulation,   the radius of curvature above a certain threshold, and there are
        and a linear superposition of both the module assembly stress   limits to the anchoring force of the fibers, as more specifically
        and the applied load cases stress conditions, such as ribbons   the pistoning forces along the fiber in the V-groove need to be
        pull/twist and thermal cycling, is performed. A uniform   limited below certain thresholds to guarantee robustness.
        temperature is varied over time for the entire model from the   A first mathematical analysis was used to evaluate the
        assembly using a large-displacement condition, and a nonlinear   optimal anchoring distance of the strain relief of the ribbon
        approach is used to account for the contact between parts and   pigtails with regards to photonic die. The radii and force on
        the geometric instability effects such as buckling.  the fibers were calculated for various lengths. The differential
          Figure 5 shows an example of a second-order finite element   equations for the fiber in a simplified 2D case were solved, and
        mesh used for the analysis of the module’s stresses. The   Figure 7 presents the variation of fiber forces and radii for a
        adhesives’ behavior when undergoing the glass transition   range of fiber lengths. The forces on the fiber at the PIC die
        is considered in the model and the modulated stiffness with   are calculated and compared to our experimental limits. These
        regards to the temperature excursion is described in [8].   forces come from the thermal strain induced by environmental


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