Multi-mode Motion Analysis of Sideward Opening Aircraft Doors Based on Position and Orientation Characteristic Theory

Wu Borui; Hang Lubin; Peng Jiyou; Huang Xiaobo; Wu Yang; Qiu Xudong

doi:10.16578/j.issn.1004.2539.2022.10.014

您当前的位置：

首页 >

文章列表页 >

Multi-mode Motion Analysis of Sideward Opening Aircraft Doors Based on Position and Orientation Characteristic Theory

Test·Analysis | 更新时间：2022-11-05

- Multi-mode Motion Analysis of Sideward Opening Aircraft Doors Based on Position and Orientation Characteristic Theory
- Journal of Mechanical Transmission Vol. 46, Issue 10, Pages: 93-98(2022)
- 作者机构：
  
  1.上海工程技术大学机械与汽车工程学院，上海 201620
  2.上海市大型构件智能制造机器人技术协同创新中心，上海 201620
  3.上海飞机设计研究院，上海 201210
- 作者简介：
- 基金信息：
- DOI：10.16578/j.issn.1004.2539.2022.10.014
  CLC：
扫描看全文
吴柏锐,杭鲁滨,彭继友等.基于方位特征集的飞机侧开式登机舱门开启机构变模式运动分析[J].机械传动,2022,46(10):93-98.

Wu Borui,Hang Lubin,Peng Jiyou,et al.Multi-mode Motion Analysis of Sideward Opening Aircraft Doors Based on Position and Orientation Characteristic Theory[J].Journal of Mechanical Transmission,2022,46(10):93-98.
吴柏锐,杭鲁滨,彭继友等.基于方位特征集的飞机侧开式登机舱门开启机构变模式运动分析[J].机械传动,2022,46(10):93-98. DOI： 10.16578/j.issn.1004.2539.2022.10.014.

Wu Borui,Hang Lubin,Peng Jiyou,et al.Multi-mode Motion Analysis of Sideward Opening Aircraft Doors Based on Position and Orientation Characteristic Theory[J].Journal of Mechanical Transmission,2022,46(10):93-98. DOI： 10.16578/j.issn.1004.2539.2022.10.014.

摘要

登机舱门作为大型客机的一个重要部件，其运动状态和运动模式分析对于舱门功能和运动链设计至关重要。从机器人机构拓扑综合视角，首次提出将某型侧开式登机舱门开启运动机构抽象为2条SS支路与1条, $◇ (R / / R / / R / / R) ⊥ R / / R$ ,http://html.publish.founderss.cn/rc-pub/api/common/picture?pictureId=36500686&type=,http://html.publish.founderss.cn/rc-pub/api/common/picture?pictureId=36500682&type=,33.35866928,3.47133350,支路构成的并联机构，进行了舱门及其开启机构运动关联性研究。基于并联机构方位特征集（POC）理论，分析了侧开式登机舱门开启机构拓扑尺度约束类型特征，揭示了舱门机构提升和旋转运动过程具有1个自由度且选取不同独立元素的两种运动模式，进一步发现舱门运动模式切换的几何约束条件为：铰链臂机构转动副间距与平行杆机构杆长在水平面投影尺寸相等。结合挡块限位的舱门驱动保证几何约束条件恒定，提升了舱门模式切换的确定性及开启过程的稳定性。基于方位特征集进行的侧开式登机舱门开启过程研究为飞机舱门设计提供了新思路。

Abstract

As an important part of large passenger aircraft, the analysis of motion state and motion mode of passenger doors is very important for the design of door function and motion mechanism. From the viewpoint of topological synthesis of robot mechanism, it is proposed for the first time to abstract the opening motion mechanism of a certain type of the sideward opening aircraft door into a parallel mechanism composed of two SS branches and one , $◇ (R / / R / / R / / R) ⊥ R / / R$ ,http://html.publish.founderss.cn/rc-pub/api/common/picture?pictureId=36500696&type=,http://html.publish.founderss.cn/rc-pub/api/common/picture?pictureId=36500689&type=,33.35866928,3.47133350, branch, and research on the overall motion correlation of the sideward opening aircraft door and its opening mechanism is conducted. Based on the position and orientation characteristic (POC) theory, the topological dimension constraint type characteristics of the sideward opening aircraft door mechanism is analyzed. It reveals that the door mechanism possesses two kinds of motion modes with one degree of freedom and different number of non-independent elements during the lifting and rotating processes. The study finds that the geometric constraint condition of the sideward opening aircraft door motion mode switching is that the rotation pair spacing of hinge arm mechanism is equal to the projection size of the parallel link mechanism length on the horizontal plane. The aircraft door drive combined with limiting stopper ensures the constant geometric constraint conditions, improves the accuracy of door mode switching and the stability of the opening process. Research on the opening process of the sideward opening aircraft door based on POC theory provides a new idea for aircraft door design.

关键词

方位特征集侧开式登机舱门运动模式铰链臂机构平行杆机构

Keywords

Position and orientation characteristicsSideward opening aircraft doorMotion modeHinge arm mechanismParallel link mechanism

references

姚雄华，邓军锋，冯蕴雯.运输类飞机舱门设计［M］.北京：国防工业出版社，2017：354-364.

YAO Xionghua，DENG Junfeng，FENG Yunwen.The doors design of transport airplane［M］.Beijing：National Defense Industry Press，2017：354-364.

TIMOTHY J B，ARTHUR G E.Design of entrance door mechanism for sabreliner jet aircraft［J］.ASME.DETC-CIE96，Volume 2B：24th Biennial Mechanisms Conference，V02BT02A038，1996：18-22.

吴事兵.门梯合一式登机门开闭锁机构分析与应用［J］.机械科学与技术，2017，36（S1）：8-12.

WU Shibing.Analysis and application of opening and closing mechanism on door-stairs passenger door［J］.Mechanical Science and Technology for Aerospace Engineering，2017，36（S1）：8-12.

阎志鹏.波音飞机舱门机构分析［J］.中国民航学院学报（综合版），1988（3）：26-30.

YAN Zhipeng.Troubleshooting the abnormal operation of B737 passenger door［J］.Journal of Civil Aviation University of China，1988（3）：26-30.

BEINER L.Variable-geometry motion control of an aircraft door［J］.Journal of Mechanical Design，1999，121（2）：195-199.

叶梯.客机侧开式登机门优化设计与分析［D］.南京：南京航空航天大学，2018：7-32.

YE Ti.Optimal design and analysis of a side opening passenger door used for airliner［D］.Nanjing：Nanjing University of Aeronautics and Astronautics，2018：7-32.

黄振庭.客机舱门机构参数优化设计［D］.北京：清华大学，2011：22-47.

HUANG Zhenting.Parameter optimization of hatch mechanism for airliner［D］.Beijing：Tsinghua University，2011：22-47.

许清清.大型客机应急门运动机构仿真技术研究［D］.南京：南京航空航天大学，2012：17-30.

XU Qingqing.Research on simulation technique of aircraft emergency door motion mechanism［D］.Nanjing：Nanjing University of Aeronautics and Astronautics，2012：17-30.

袁修起.民用飞机舱门导向槽优化设计［J］.科技视界，2016（11）：278.

YUAN Xiuqi.Optimization design of door guiding device of aircraft door［J］.Science & Technology Vision，2016（11）：278.

袁修起.民用飞机舱门连杆支架优化研究［J］.民用飞机设计与研究，2014（2）：27-30.

YUAN Xiuqi.Study on optimization of connecting link support of aircraft door［J］.Civil Aircraft Design & Research，2014（2）：27-30.

杨小军.民用飞机舱门提升原理分析研究［J］.山东工业技术，2017（19）：275-276.

YANG Xiaojun.Principle analysis of aircraft door lifting［J］.Journal of Shandong Industrial Technology，2017（19）：275-276.

陈勇.波音737客舱门机械故障原因分析与排除［J］.航空维修与工程，2011（3）：60-62.

CHEN Yong.Troubleshooting the abnormal operation of B737 passenger door［J］.Aviation Maintenance & Engineering，2011（3）：60-62.

KONG X W.A variable-DOF single-loop 7R spatial mechanism with five motion modes［J］.Mechanisms and Machine Theory，2018：120（2）：239-249.

YANG T L，LIU A X，JIN Q，et al.Position and orientation characteristic equation for topological design of robot mechanisms［J］.Journal of Mechanical and Design，2009，131（2）：021001.

LEE C C，HERVE J M.Bricard one-DoF motion and its mechanical generation［J］.Mechanism and Machine Theory，2014，77：35-49.

YANG T L，LIU A X，SHEN H P，et al.On the correctness and strictness of the position and orientation characteristic equation for topological structure design of robot mechanisms［J］.Journal of Mechanisms and Robotics，2013，5（2）：021009.

LOPEZ-CUSTIDIO P，DAI J S.Design of a variable-mobility linkage using the bohemian dome［J］.Journal of Mechanical Design，2019，141（9）：092303.

张凤格.民用客机旅客登机门铰链臂结构设计研究［J］.民用飞机设计与研究，2010（3）：18-23.

ZHANG Fengge.Hinge structure design and research for civil aircraft passenger door［J］.Civil Aircraft Design & Research，2010（3）：18-23.

杨廷力.机器人机构拓扑结构设计［M］.北京：科学出版社，2004：75-80.

YANG Tingli.Theory and application of robot mechanism topology［M］.Beijing：Science Press，2004：75-80.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Multi-mode Motion Opening Mechanism Design for Aircraft Door Based on the Bricard Mechanism

Related Author

No data

Related Institution

No data

⁰