Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel Test

Wind tunnel test is an important part of the development of the aircraft, and the aircraft position and attitude adjustment mechanism is an indispensable part of the test. An adjusting mechanism capable of achieving multi-path angle coupling output is proposed. Firstly, the implementation principle...

Full description

Saved in:
Bibliographic Details
Main Authors: Xiaoru Li, Juan Huang, Xinghui Li
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Transmission 2019-06-01
Series:Jixie chuandong
Subjects:
Online Access:http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2019.06.016
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1841548821462515712
author Xiaoru Li
Juan Huang
Xinghui Li
author_facet Xiaoru Li
Juan Huang
Xinghui Li
author_sort Xiaoru Li
collection DOAJ
description Wind tunnel test is an important part of the development of the aircraft, and the aircraft position and attitude adjustment mechanism is an indispensable part of the test. An adjusting mechanism capable of achieving multi-path angle coupling output is proposed. Firstly, the implementation principle of the mechanism is introduced. The kinematics equation derivation is performed. Combine with Matlab and set the aircraft under two kinds of motion conditions, the drive the displacement and velocity of mechanism are solved, and the spatial motion trajectory of the aircraft is calculated. On this basis, the drive extreme displacement is set. The boundary mapping method is used to analyze the workspace of the mechanism. The results show that the mechanism has a large workspace and could complete the adjustment of a wide range of aircraft path angles within the set of two extreme displacement. As a wind tunnel test adjustment mechanism has application prospects.
format Article
id doaj-art-47be4fcb635d4ecdbf328d2c9b6ed8a0
institution Kabale University
issn 1004-2539
language zho
publishDate 2019-06-01
publisher Editorial Office of Journal of Mechanical Transmission
record_format Article
series Jixie chuandong
spelling doaj-art-47be4fcb635d4ecdbf328d2c9b6ed8a02025-01-10T14:00:17ZzhoEditorial Office of Journal of Mechanical TransmissionJixie chuandong1004-25392019-06-0143879230641042Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel TestXiaoru LiJuan HuangXinghui LiWind tunnel test is an important part of the development of the aircraft, and the aircraft position and attitude adjustment mechanism is an indispensable part of the test. An adjusting mechanism capable of achieving multi-path angle coupling output is proposed. Firstly, the implementation principle of the mechanism is introduced. The kinematics equation derivation is performed. Combine with Matlab and set the aircraft under two kinds of motion conditions, the drive the displacement and velocity of mechanism are solved, and the spatial motion trajectory of the aircraft is calculated. On this basis, the drive extreme displacement is set. The boundary mapping method is used to analyze the workspace of the mechanism. The results show that the mechanism has a large workspace and could complete the adjustment of a wide range of aircraft path angles within the set of two extreme displacement. As a wind tunnel test adjustment mechanism has application prospects.http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2019.06.016Wind tunnel testParallel mechanismPath angleWorkspace
spellingShingle Xiaoru Li
Juan Huang
Xinghui Li
Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel Test
Jixie chuandong
Wind tunnel test
Parallel mechanism
Path angle
Workspace
title Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel Test
title_full Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel Test
title_fullStr Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel Test
title_full_unstemmed Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel Test
title_short Design and Workspace Analysis of Position and Attitude Adjustment Mechanism for a Wind Tunnel Test
title_sort design and workspace analysis of position and attitude adjustment mechanism for a wind tunnel test
topic Wind tunnel test
Parallel mechanism
Path angle
Workspace
url http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2019.06.016
work_keys_str_mv AT xiaoruli designandworkspaceanalysisofpositionandattitudeadjustmentmechanismforawindtunneltest
AT juanhuang designandworkspaceanalysisofpositionandattitudeadjustmentmechanismforawindtunneltest
AT xinghuili designandworkspaceanalysisofpositionandattitudeadjustmentmechanismforawindtunneltest