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喉部对中央气道振荡流的影响:一项模型研究。

Effect of the larynx on oscillatory flow in the central airways: a model study.

作者信息

Menon A S, Weber M E, Chang H K

出版信息

J Appl Physiol (1985). 1985 Jul;59(1):160-9. doi: 10.1152/jappl.1985.59.1.160.

Abstract

Measurements were made of the effect of the larynx on the oscillatory flow profiles in a 3:1 scale model of the human central airways. A fixed glottic aperture corresponding to the shape and size at midinspiration was used. Oscillatory airflows at peak Reynolds numbers, similar to those obtained during spontaneous breathing and panting, were studied. The flow distribution to the five lobar bronchi was maintained by distally placed linear resistors. A hot-wire anemometer probe was used to measure the local velocity along two perpendicular diameters at six stations distributed through the model. Near the proximal end of the trachea, the flat velocity profiles at the beginning of the flow cycle peaked at maximum flow because of the jet created by the glottic aperture. This peaked structure was conserved during the latter half of the inspiratory cycle. Close to the carina, the jet had almost dissipated and the entry conditions into the main bronchi corresponded to those in the absence of the laryngeal model. The effect of the glottic aperture on the mean velocity was not felt beyond the carina, and the characteristic skewed profiles seen in oscillatory flows, in the absence of the larynx, were present in the main and lobar bronchi.

摘要

对喉部对人体中央气道3:1比例模型中振荡流型的影响进行了测量。使用了一个对应于吸气中期形状和大小的固定声门孔径。研究了与自主呼吸和喘气时相似的峰值雷诺数下的振荡气流。通过在远端放置线性电阻器来维持流向五个叶支气管的流量分布。使用热线风速仪探头在模型中分布的六个站点沿着两条相互垂直的直径测量局部速度。在气管近端附近,由于声门孔径产生的射流,流动周期开始时的扁平速度剖面在最大流量时达到峰值。这种峰值结构在吸气周期的后半段得以保留。靠近隆突处,射流几乎消散,进入主支气管的入口条件与没有喉部模型时的情况相对应。声门孔径对平均速度的影响在隆突以外未被感觉到,并且在没有喉部的情况下振荡流中出现的特征性倾斜剖面在主支气管和叶支气管中也存在。

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