Koshiyama Kenichiro, Nishimoto Keisuke, Ii Satoshi, Sera Toshihiro, Wada Shigeo
Graduate School of Engineering Science, Osaka University, Japan.
Graduate School of Engineering Science, Osaka University, Japan.
Clin Biomech (Bristol). 2019 Jun;66:32-39. doi: 10.1016/j.clinbiomech.2018.01.001. Epub 2018 Jan 20.
The pulmonary acinus is a dead-end microstructure that consists of ducts and alveoli. High-resolution micro-CT imaging has recently provided detailed anatomical information of a complete in vivo acinus, but relating its mechanical response with its detailed acinar structure remains challenging. This study aimed to investigate the mechanical response of acinar tissue in a whole acinus for static inflation using computational approaches.
We performed finite element analysis of a whole acinus for static inflation. The acinar structure model was generated based on micro-CT images of an intact acinus. A continuum mechanics model of the lung parenchyma was used for acinar tissue material model, and surface tension effects were explicitly included. An anisotropic mechanical field analysis based on a stretch tensor was combined with a curvature-based local structure analysis.
The airspace of the acinus exhibited nonspherical deformation as a result of the anisotropic deformation of acinar tissue. A strain hotspot occurred at the ridge-shaped region caused by a rod-like deformation of acinar tissue on the ridge. The local structure becomes bowl-shaped for inflation and, without surface tension effects, the surface of the bowl-shaped region primarily experiences isotropic deformation. Surface tension effects suppressed the increase in airspace volume and inner surface area, while facilitating anisotropic deformation on the alveolar surface.
In the lungs, the heterogeneous acinar structure and surface tension induce anisotropic deformation at the acinar and alveolar scales. Further research is needed on structural variation of acini, inter-acini connectivity, or dynamic behavior to understand multiscale lung mechanics.
肺腺泡是一种由导管和肺泡组成的盲端微观结构。高分辨率微型计算机断层扫描(micro-CT)成像最近提供了完整的体内腺泡的详细解剖信息,但将其力学响应与其详细的腺泡结构联系起来仍然具有挑战性。本研究旨在使用计算方法研究整个腺泡中腺泡组织在静态充气时的力学响应。
我们对整个腺泡进行静态充气的有限元分析。腺泡结构模型基于完整腺泡的micro-CT图像生成。肺实质的连续介质力学模型用于腺泡组织材料模型,并明确纳入表面张力效应。基于拉伸张量的各向异性力学场分析与基于曲率的局部结构分析相结合。
由于腺泡组织的各向异性变形,腺泡的气腔呈现非球形变形。在嵴状区域出现应变热点,这是由嵴上腺泡组织的棒状变形引起的。充气时局部结构变为碗状,并且在没有表面张力效应的情况下,碗状区域的表面主要经历各向同性变形。表面张力效应抑制了气腔体积和内表面积的增加,同时促进了肺泡表面的各向异性变形。
在肺中,异质性的腺泡结构和表面张力在腺泡和肺泡尺度上引起各向异性变形。需要进一步研究腺泡的结构变化、腺泡间连接或动态行为,以了解多尺度肺力学。