Thermo-mechanical design aspects for primary composite structures of large transport aircraft

Dieter Petersen; Raimund Rolfes; Rolf Zimmermann

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Thermo-mechanical design aspects for primary composite structures of large transport aircraft

机译：大型运输机主要复合结构的热机械设计方面

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Thermo-mechanical design aspects for primary carbon fibre reinforced plastics (CFRP) components, especially wings, of future large transport aircraft are discussed. Numerical simulations of the heating of a wing under intensive sun irradiation and of cooling during taxiing and take-off result in the recommendation of an appropriate design temperature. The study of flat stringer-stiffened panels reveals the influence of imperfections and boundary conditions on the buckling load under simultaneous thermal and mechanical loading.

机译：讨论了未来大型运输机的主要碳纤维增强塑料（CFRP）组件（尤其是机翼）的热机械设计方面。在强烈的阳光照射下，机翼的加热以及滑行和起飞过程中的冷却的数值模拟导致建议采用合适的设计温度。平板纵梁加劲板的研究揭示了缺陷和边界条件对同时受热和机械载荷的屈曲载荷的影响。

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来源
《Aerospace science and technology》 |2001年第2期|p.135-146|共12页
作者
Dieter Petersen; Raimund Rolfes; Rolf Zimmermann;
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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空、航天;
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1. A Two-Level Procedure for the Global Optimum Design of Composite Modular Structures-Application to the Design of an Aircraft Wing: Part 2: Numerical Aspects and Examples [J] . Montemurro M., Vincenti A., Vannucci P. Journal of Optimization Theory and Applications . 2012,第1期

机译：组合模块化结构全局优化设计的两级程序-在飞机机翼设计中的应用：第2部分：数值方面和示例
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4. ADHESIVELESS COMPOSITE STRUCTURES WITH CARBON FIBER PREPREGS FOR AIRCRAFT PRIMARY STRUCTURAL APPLICATIONS [C] . H.T.N. Gandy, R. Asmatulu ASME international mechanical engineering congress and exposition . 2013

机译：碳纤维预浸料无胶复合结构在飞机主要结构中的应用
5. The analysis of bonded repair solutions for primary composite aircraft structures [D] . Davies, Thomas Gethin 2013

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6. A study of laser surface treatment in bonded repair of composite aircraft structures [O] . Shaolong Li, Ting Sun, Chang Liu, 2018

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7. Design of Aircraft Structures - Structural Design of Carbon Fiber Composite Wing for the SARAS Civil Transport Aircraft [O] . Murthy Sridhara S 2010

机译：飞机结构设计-SARAS民用运输机碳纤维复合材料机翼的结构设计
8. Advanced composites structural concepts and materials technologies for primary aircraft structures: Design/manufacturing concept assessment [R] . Chu, Robert L., Bayha, Tom D., Davis, HU, 1992

机译：用于主要飞机结构的先进复合材料结构概念和材料技术：设计/制造概念评估

Thermo-mechanical design aspects for primary composite structures of large transport aircraft

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