Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Xingbo FANG"'
Publikováno v:
Aerospace, Vol 10, Iss 10, p 828 (2023)
The torsion spring of a carrier-based aircraft landing gear is a key component, which is normally manufactured out of AerMet100 ultra-high-strength steel. The takeoff and landing performance is greatly influenced by its bearing capacity and structura
Externí odkaz:
https://doaj.org/article/a81c0a5da1054355aa99453a9bbc1dc9
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
Double-cavity shock absorber with high-pressure piston is the core component of the nose landing gear of the carrier-based aircraft, and its fast-extension performance seriously affects the safety of the catapult-assisted takeoff. The design of a car
Externí odkaz:
https://doaj.org/article/15b70dcfe0fb4a7197c75bd357a81c8f
Publikováno v:
Aerospace, Vol 9, Iss 3, p 168 (2022)
Rapid launch is one of the key indicators of UAV swarm operations, and one of the key decisions that determines the ultimate success of launch system development is the choice of its product architecture. The high-definition design structure matrix (
Externí odkaz:
https://doaj.org/article/bc2d90c8e70b423284d527329c8eeafd
Publikováno v:
Applied Sciences, Vol 11, Iss 19, p 9037 (2021)
The catapult process of a carrier-based aircraft includes multiple links such as catapult tensioning, separation of the holding rod, dragging and running, separation of the catapult and drag shuttle, and free running. The connection relationships bet
Externí odkaz:
https://doaj.org/article/c63c30a9089e4fa7bdee401a5f920153
Publikováno v:
Applied Sciences, Vol 11, Iss 12, p 5445 (2021)
The aim of this paper is to obtain the strut friction–touchdown performance relation for designing the parameters involving the strut friction of the landing gear in a light aircraft. The numerical model of the landing gear is validated by drop tes
Externí odkaz:
https://doaj.org/article/e7436bda2cbe4a6f9379c7ffa3961173
Publikováno v:
Mechanics. 28:145-151
This study concentrates on the fatigue performance of ultra-high-strength steel Aermet100 under different loading rates. The standard specimen measured the static mechanical properties of Aermet100 steel, based on which the basic mechanical propertie
Publikováno v:
The Aeronautical Journal. 125:2200-2216
The capability of aircraft tyres to sustain landing impact loads is essential for flight landing safety. Hence, the development of a reliable experimental database is necessary to validate numerical models. The experimental data on aircraft tyre land
Publikováno v:
The Aeronautical Journal. 125:1083-1102
Carrier-based unmanned aerial aircraft (UAV) structure is subjected to severe tensile load during takeoff, especially the drawbar, which affects its fatigue performance and structural safety. However, the complex structural features pose great challe
Publikováno v:
Journal of Aerospace Engineering. 35
Publikováno v:
Applied Sciences
Volume 11
Issue 19
Applied Sciences, Vol 11, Iss 9037, p 9037 (2021)
Volume 11
Issue 19
Applied Sciences, Vol 11, Iss 9037, p 9037 (2021)
The catapult process of a carrier-based aircraft includes multiple links such as catapult tensioning, separation of the holding rod, dragging and running, separation of the catapult and drag shuttle, and free running. The connection relationships bet