4.7 Article

Thermomechanical design rules for photovoltaic modules

Journal

PROGRESS IN PHOTOVOLTAICS
Volume -, Issue -, Pages -

Publisher

WILEY
DOI: 10.1002/pip.3624

Keywords

design rules; digital prototyping; FEM simulation; PV modules; stress

Funding

  1. Stiftung Begabtenforderung Cusanuswerk
  2. Cusanuswerk in Bonn, Germany

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This paper presents a set of thermomechanical design rules to support and accelerate future PV module developments. The design rules are derived from a comprehensive parameter sensitivity study using finite element method simulations. The study reveals the critical interactions within a PV module and emphasizes the importance of the encapsulant's mechanical properties. A set of 15 thermomechanical design rules are derived, covering various aspects including the encapsulant, solar cells, and module size. The concept of specific thermal expansion stiffness is introduced as a measure of the material's thermomechanical performance.
We present a set of thermomechanical design rules to support and accelerate future (PV) module developments. The design rules are derived from a comprehensive parameter sensitivity study of different PV module layers and material properties by finite element method simulations. We develop a three dimensional finite element method (FEM) model, which models the PV module geometry in detail from busbar and ribbons up to the frame including the adhesive. The FEM simulation covers soldering, lamination, and mechanical load at various temperatures. The FEM model is validated by mechanical load tests on three 60-cell PV modules. Here, for the first time, stress within a solar cell is measured directly using stress sensors integrated in solar cells (SenSoCells (R)). The results show good accordance with the simulations. The parameter sensitivity study reveals that there are two critical interactions within a PV module: (1) between ribbon and solar cell and (2) between front/back cover and interconnected solar cells. Here, the encapsulant plays a crucial role in how the single layers interact with each other. Therefore, its mechanical properties are essential, and four design rules are derived regarding the encapsulant. Also four design rules concern front and back sides, and three address the solar cells. Finally, two design rules each deal with module size and frame, respectively. Altogether we derive a set of 15 thermomechanical design rules. As a rule of thumb of how well a bill of material will work from a thermomechanical point of view, we introduce the concept of specific thermal expansion stiffness E alpha=E center dot alpha center dot Aj center dot h$$ {\hat{E}}_{\alpha }=E\cdotp \alpha \cdotp {A}_{\mathrm{j}}\cdotp h $$ as the product of Young's modulus E$$ E $$, coefficient of thermal expansion alpha$$ \alpha $$, joint area Aj$$ {A}_{\mathrm{j}} $$, and materials height h$$ h $$. The difference between two materials is a measure of how much thermal strain one material can induce in another. A strong difference means that the material with the larger value will induce thermal strain in the other.

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