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四翼恐龙小盗龙不同后翼翼型的滑翔模型测试

Model tests of gliding with different hindwing configurations in the four-winged dromaeosaurid Microraptor gui.

机构信息

Department of Ecology & Evolutionary Biology, University of Kansas, Lawrence, KS 66045-7534, USA.

出版信息

Proc Natl Acad Sci U S A. 2010 Feb 16;107(7):2972-6. doi: 10.1073/pnas.0911852107. Epub 2010 Jan 25.

Abstract

Fossils of the remarkable dromaeosaurid Microraptor gui and relatives clearly show well-developed flight feathers on the hind limbs as well as the front limbs. No modern vertebrate has hind limbs functioning as independent, fully developed wings; so, lacking a living example, little agreement exists on the functional morphology or likely flight configuration of the hindwing. Using a detailed reconstruction based on the actual skeleton of one individual, cast in the round, we developed light-weight, three-dimensional physical models and performed glide tests with anatomically reasonable hindwing configurations. Models were tested with hindwings abducted and extended laterally, as well as with a previously described biplane configuration. Although the hip joint requires the hindwing to have at least 20 degrees of negative dihedral (anhedral), all configurations were quite stable gliders. Glide angles ranged from 3 degrees to 21 degrees with a mean estimated equilibrium angle of 13.7 degrees, giving a lift to drag ratio of 4.1:1 and a lift coefficient of 0.64. The abducted hindwing model's equilibrium glide speed corresponds to a glide speed in the living animal of 10.6 m x s(-1). Although the biplane model glided almost as well as the other models, it was structurally deficient and required an unlikely weight distribution (very heavy head) for stable gliding. Our model with laterally abducted hindwings represents a biologically and aerodynamically reasonable configuration for this four-winged gliding animal. M. gui's feathered hindwings, although effective for gliding, would have seriously hampered terrestrial locomotion.

摘要

小盗龙属及其近亲的化石清晰地显示出后肢和前肢都有发育良好的飞行羽毛。现代脊椎动物中没有后肢作为独立的、完全发育的翅膀的;因此,由于缺乏活体样本,对于后翼翼的功能形态或可能的飞行形态,意见分歧不大。我们根据一个个体的实际骨架进行了详细的重建,制作了轻便的三维物理模型,并对解剖学上合理的后翼翼构型进行了滑翔测试。模型的后翼进行了外展和侧向伸展的测试,以及之前描述的双翼面构型的测试。尽管髋关节要求后翼至少有 20 度的负迎角(下反角),但所有的构型都非常稳定的滑翔器。滑翔角度从 3 度到 21 度不等,平均估计平衡角为 13.7 度,升力与阻力比为 4.1:1,升力系数为 0.64。外展后翼模型的平衡滑翔速度对应于活体动物的滑翔速度为 10.6 米/秒。虽然双翼面模型的滑翔效果几乎与其他模型一样,但它在结构上存在缺陷,需要一个不太可能的重量分布(很重的头部)才能稳定滑翔。我们的模型具有侧向外展的后翼,代表了这种四翼滑翔动物的生物和空气动力学上合理的构型。小盗龙的羽毛后翼虽然对滑翔很有效,但会严重阻碍陆地运动。

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