Brown Richard E, Baumel Julian J, Klemm Robert D
Department of Anatomy and Physiology, College of Veterinary Medicine, Kansas State University, Manhattan, Kansas 66506.
Burke Museum, Division of Birds, University of Washington, Seattle, Washington 98195.
J Morphol. 1995 Jul;225(1):91-105. doi: 10.1002/jmor.1052250108.
The supporting elements of the avian propatagium were examined in intact birds and as isolated components, using static force-length measurements, calculated models, and airflow observations. The propatagial surface supported between Lig. propatagiale (LP) and brachium-antebrachium is equally resistant to distortion over the range of wing extension used in flight. The lengths LP assumes in flight occur across a nearly linear, low-stiffness portion of the force-length curve of its extensible pars elastica. In an artificial airflow, intact wings automatically extend; their degree of extension is roughly correlated with the airflow velocity. Comparisons between geometric models of the wing and the passive force-length properties of LPs suggest that the stress along LP blances the drag forces acting to extend the elbow. The mechanical properties (stiffness) of the LP vary and appear to be tuned for flight-type characteristics, e.g., changes in wing extension during flight and drag. Lig. limitants cubiti and LP combine to limit elbow extension at its maximum, a safety device in flight preventing hyperextension of the elbow and reduction of the propatagium's cambered flight surface. Calculations using muscle and ligament lengths suggest that M. deltoideus, pars propatagialis, via its insertions onto both the propatagial ligaments, controls and coordinates propatagial deployment, leading edge tenseness, and elbow/wing extension across the range of wing extensions used in flight. The propatagial ligaments and M. deltoideus, pars propatagialis, along with skeleto-ligamentous elbow/carpus apparatus, are integral components of the wing's extension control mechanism. © 1995 Wiley-Liss, Inc.
利用静力-长度测量、计算模型和气流观察,对完整鸟类以及作为分离组件的鸟类前翼膜的支撑元件进行了研究。在前翼膜韧带(LP)和肱部-前臂之间支撑的前翼膜表面,在飞行中使用的翼展范围内对变形具有同等抗性。LP在飞行中所呈现的长度出现在其可伸展弹性部分的力-长度曲线的近乎线性、低刚度部分。在人工气流中,完整的翅膀会自动伸展;其伸展程度大致与气流速度相关。对翅膀几何模型与LP的被动力-长度特性之间的比较表明,沿LP的应力平衡了作用于伸展肘部的阻力。LP的力学特性(刚度)各不相同,且似乎是根据飞行类型特征进行调整的,例如飞行过程中翼展的变化和阻力。尺骨限制韧带和LP共同作用,在最大程度上限制肘部伸展,这是飞行中的一种安全装置,可防止肘部过度伸展以及前翼膜弯曲飞行表面的减小。使用肌肉和韧带长度进行的计算表明,三角肌前翼膜部通过其在两个前翼膜韧带上的附着点,控制并协调前翼膜的展开、前缘张力以及在飞行中使用的翼展范围内的肘部/翅膀伸展。前翼膜韧带和三角肌前翼膜部,连同骨骼-韧带肘部/腕部装置,是翅膀伸展控制机制的组成部分。© 1995威利-利斯公司。