7 Papers
36 Citations
Kui Xu is an academic researcher from Nanjing University of Aeronautics and Astronautics. The author has contributed to research in topics: Bearing (mechanical) & Landing gear. The author has an hindex of 3, co-authored 7 publications.
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Papers
Patent
Plane type ejection launch carrier-borne aircraft front undercarriage static force test loading apparatus
Xiaohui Wei,Yan Xiaofeng,Wang Yong,Hong Nie,Chen Kaifan,Kui Xu +5 more
- 26 Feb 2014
TL;DR: In this paper, a plane type ejection launch carrier-borne aircraft front undercarriage static force test loading apparatus is provided, which consists of a plane-type test bench rack, an under-carriage, a lateral load load loading device, a course load loading and a mooring load loading.
21
Patent
Front undercarriage static force test loading device for frame-type catapult-assisted take-off shipboard aircraft
Xiaohui Wei,Yan Xiaofeng,Hong Nie,Chen Kaifan,Kui Xu,Li Lirong +5 more
- 26 Feb 2014
TL;DR: In this article, a front undercarriage static force test loading device for a frame-type catapult-assisted take-off shipboard aircraft is presented, which is designed to realize ejection application and load trapping, vertical, course, lateral, ejection and trapping load loadings of the aircraft are accomplished on the test stand.
10
Research on the Performance of an Aircraft Landing Gear Hook Lock Based on Bifurcation Analysis
TL;DR: Although the dynamic results can hardly explain the jump phenomenon of the lock mechanism at the moment of locking or unlocking, the bifurcation point of the static results suggests the occurrence of a stability change in the lock mechanisms at the moments of jumping, thereby explaining the jumping mechanism of theLock mechanism.
7
Design and Analysis of High-Speed Unmanned Aerial Vehicle Ground Directional Rectifying Control System
TL;DR: In this article, the full nonlinear equations of an unmanned aerial vehicle ground taxiing mathematical dynamic model are built based on a type of UAV data in LMS Virtual, where the flexible landing gear model is considered to make the aircraft ground motion more accurate.
5
Kinematic Singularity and Bifurcation Analysis of Sidestay Landing Gear Locking Mechanisms
TL;DR: Investigating the synchronous locking performance of the dual-sidestay landing gear based on the singularity and bifurcation theory reveals that the lock links must reach the lower overcenter singular point to fully lock the landing gear, and the singular point is sensitive to structural parameters.