STRUCTURE SYNTHESIS OF SIX-BAR MECHANISMS FOR AIRCRAFT HIGH-LIFT SURFACES

被引：0

作者：

Wang, Anngwo ^{[1
]}

Yan, Hong-Sen ^{[2
]}

Kuo, Chin-Hsing ^{[3
]}

机构：

[1] MOOG Inc, Aircraft Grp, Torrance, CA 90501 USA

[2] Natl Cheng Kung Univ, Tainan 70101, Taiwan

[3] Natl Taiwan Univ Sci & Technol, Taipei 10607, Taiwan

来源：

PROCEEDINGS OF THE ASME INTERNATIONAL DESIGN ENGINEERING TECHNICAL CONFERENCES AND COMPUTERS AND INFORMATION IN ENGINEERING CONFERENCE 2012, VOL 4, PTS A AND B | 2012年

关键词：

D O I：

暂无

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

Slat/flap driven mechanisms are essential transmission components of high lift systems and may contain combinations of linkages, ball screws, cam tracks and gears. This paper is, therefore, devoted to the structural synthesis of the aircraft slats/flaps driven mechanisms with six links. Based on the concept of generalization and specialization of mechanisms, all feasible new design alternatives are systematically derived and summarized as a complete atlas listed in Appendix. The provided atlas is useful for designers when considering alternative topological structures of the slats/flaps driven mechanisms in the future.

引用

页码：541 / +

页数：3

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