Oren Liran, Dembinski Doug, Gutmark Ephraim, Khosla Sid
Department of Otolaryngology - Head and Neck Surgery, University of Cincinnati, Cincinnati, Ohio.
Department of Otolaryngology - Head and Neck Surgery, University of Cincinnati, Cincinnati, Ohio.
J Voice. 2014 May;28(3):297-304. doi: 10.1016/j.jvoice.2013.11.001. Epub 2014 Feb 1.
OBJECTIVES/HYPOTHESIS: Characterizing the vertical stiffness gradient that exists between the superior and inferior aspects of the medial surface of the vocal fold. Characterization of this stiffness gradient could elucidate the mechanism behind the divergent glottal shape observed during closing.
Basic science.
Indentation testing of the folds was done in a canine model. Stress-strain curves are generated using a customized load-cell and the differential Young's modulus is calculated as a function of strain.
Results from 11 larynges show that stress increases as a function of strain more rapidly in the inferior aspect of the fold. The calculations for local Young's modulus show that at high strain values, a stiffness gradient is formed between the superior and inferior aspects of the fold.
For small strain values, which are observed at low subglottal pressures, the stiffness of the tissue is similar in both the superior and inferior aspects of the vocal fold. Consequently, the lateral force that is applied by the glottal flow at both aspects results in almost identical displacements, yielding no divergence angle. Conversely, at higher strain values, which are measured in high subglottal pressure, the inferior aspect of the vocal fold is much stiffer than the superior edge; thus, any lateral force that is applied at both aspects will result in a much greater displacement of the superior edge, yielding a large divergence angle. The increased stiffness observed at the inferior edge could be due to the proximity of the conus elasticus.
目的/假设:描绘声带内侧表面上、下部分之间存在的垂直刚度梯度。对这种刚度梯度的表征可以阐明在闭合过程中观察到的声门形状发散背后的机制。
基础科学。
在犬类模型中对声带进行压痕测试。使用定制的测力传感器生成应力-应变曲线,并计算作为应变函数的微分杨氏模量。
来自11个喉部的结果表明,在声带的下部,应力随应变的增加更为迅速。局部杨氏模量的计算表明,在高应变值时,声带的上、下部分之间形成了刚度梯度。
对于在低声门下压力下观察到的小应变值,声带上下部分的组织刚度相似。因此,声门气流在两个部分施加的侧向力导致几乎相同的位移,不会产生发散角。相反,在高声门下压力下测量的较高应变值时,声带的下部比上边缘硬得多;因此,在两个部分施加的任何侧向力都会导致上边缘的位移大得多,从而产生大的发散角。在下边缘观察到的刚度增加可能是由于弹性圆锥的接近。