Results 31 to 40 of about 34,020 (251)

Selection Methodology of an Electric Actuator for Nose Landing Gear of a Light Weight Aircraft

open access: yesApplied Sciences, 2020
Landing gear system of an aircraft enables it to take off and land with safety and comfort. Because of the horizontal and vertical velocity of aircraft, upon landing, the complete aircraft undergoes different forcing functions in the form of the impact ...
Taimur Ali Shams   +5 more
doaj   +1 more source

Analysis of Catapult-Assisted Takeoff of Carrier-Based Aircraft Based on Finite Element Method and Multibody Dynamics Coupling Method

open access: yesAerospace, 2023
Catapult-assisted takeoff is the initiation of flight missions for carrier-based aircrafts. Ensuring the safety of aircrafts during catapult-assisted takeoff requires a thorough analysis of their motion characteristics.
Haoyuan Shao   +5 more
doaj   +1 more source

Calculation of steering system parameters of a military training aircraft [PDF]

open access: yesINCAS Bulletin, 2022
The mechanical-hydraulic steering system of a military training aircraft is a technical problem for specialized engineers and it must be investigated and solved in a scientific manner using theoretical knowledge, calculus programs such as Mathcad, and ...
Bogdan Adrian NICOLIN, Ilie NICOLIN
doaj   +1 more source

Research on Ground Tie-down Characteristics of Typical-layout Civil Aircraft

open access: yesHangkong gongcheng jinzhan, 2022
The aircraft is impacted by severe weather on parking apron,and the aerodynamic research of parking is important for parking safety.In order to analyze the aerodynamic difference of typical-layout civil aircraft induced by ground cross-wind,and determine
BAI Feng, WANG Qizhi
doaj   +1 more source

Shock and harmonic response analysis of UAV nose landing gear system with air damper

open access: yesCogent Engineering, 2021
This research presents a response analysis of a UAV nose landing gear system equipped with an air damper under shock and harmonic excitation. The study begins with dynamic modeling of the UAV landing gear system.
Lovely Son   +4 more
doaj   +1 more source

Keandalan Komponen Nose Wheel Assy pada Pesawat Cessna

open access: yesQuantum Teknika, 2023
Maintenance is taken to maintain the reliability of the components that support overall nurse performance. One of them is the landing gear which functions for all aircraft movements on the ground including taking off, landing, taxing and parking, and ...
Sri Mulyani, Istyawan Priyahapsara
doaj   +1 more source

Simulation analysis on semi-active control drop dynamics of whole aircraft landing gear

open access: yesHangkong gongcheng jinzhan, 2023
The application of semi-active control technology on landing gear is mostly limited to single or magnetorheological landing gear. The research on the whole aircraft is more valuable for the practical application of semi-active control.
REN Panting, XU Feng
doaj   +1 more source

Noise Characterization of a Full-Scale Nose Landing Gear [PDF]

open access: yesJournal of Aircraft, 2018
This paper presents experimental results from a nose landing-gear test campaign. A highly detailed model of the nose section of a 90-seat configuration green regional aircraft concept was built and...
Gareth J. Bennett   +2 more
openaire   +3 more sources

Optimization of laser texture geometry and resulting functionality of nickel aluminium bronze for landing gear applications

open access: yesInternational Journal of Lightweight Materials and Manufacture, 2021
Nickel-aluminium bronze (NAB) is adopted in certain crucial applications such as nut threads of actuator screw assembly in nose landing gear, which forms the critical weakest link for landing gear operation.
A. Bharatish   +5 more
doaj   +1 more source

A bifurcation study to guide the design of a landing gear with a combined uplock/downlock mechanism [PDF]

open access: yes, 2014
This paper discusses the insights that a bifurcation analysis can provide when designing mechanisms. A model, in the form of a set of coupled steady-state equations, can be derived to describe the mechanism.
Knowles, James A C   +3 more
core   +3 more sources

Home - About - Disclaimer - Privacy