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Fatigue Crack Propagation Estimation Based on Direct Strain Measurement during a Full-Scale Fatigue Test [PDF]

open access: yesSensors, 2022
Military aircraft are subjected to variable loads, which are the main cause of initiation and propagation of cracks in the most stressed locations of the airframe. The aim of a Full-Scale Fatigue Test (FSFT) is to represent actual load conditions in such
Piotr Reymer   +2 more
doaj   +2 more sources

Fatigue Design Evaluation of Railway Bogie with Full-Scale Fatigue Test [PDF]

open access: yesAdvances in Materials Science and Engineering, 2017
The bogie frame of a railway is an important structural member for the support of vehicle loading. In general, more than 25 years’ durability is necessary.
Jung-Won Seo   +4 more
doaj   +2 more sources

Mi-24 Helicopter Full Scale Fatigue Test Concept

open access: yesFatigue of Aircraft Structures, 2019
This paper presents a general concept of the Full Scale Fatigue Test of the Mi-24 helicopter including the test layout and load distribution, as well as describes the milestones to be achieved.
Reymer Piotr   +9 more
doaj   +2 more sources

Assessment model for multivariable fatigue performance of EA4T axles containing defects [PDF]

open access: yesScientific Reports
This study employed a combined experimental and theoretical approach to investigate the influence of foreign object damage (FOD) on the fatigue limit of surface-strengthened EA4T axles.
Yan Luo   +4 more
doaj   +2 more sources

Research on Development and Test Analysis of Full-Scale Fatigue Test System of X65 Submarine Pipeline [PDF]

open access: yesE3S Web of Conferences, 2021
The fatigue performance of welded joints of submarine pipelines is directly related to the safety and economic benefits of welded structures. Considering the limitations of fatigue calculation, anti-fatigue design and small-scale fatigue test in the ...
Hu Yanhua   +4 more
doaj   +1 more source

Application research on 5G technology in fatigue test of full-scale aircraft

open access: yesHangkong gongcheng jinzhan, 2023
With the development of aircraft demand, and emerging of new material and new process, the test and validation technology of aircraft structure strength will also face new challenges.
LIU Bing, ZHANG Jianfeng, MU Bin
doaj   +1 more source

Multi-joint and Large Load Wing Load Processing Method

open access: yesHangkong gongcheng jinzhan, 2020
For test piece lacking the right outer wing portion, the many and complicated butt joints, and the large test load, will bring great difficulty to the application of the wing load. Therefore the independent loading clamp is designed for the three sets of
WANG Xintao, XIA Long, LIU Xingke
doaj   +1 more source

Overview of the development of full-scale fatigue test technology for fighter

open access: yesHangkong gongcheng jinzhan, 2023
Structural strength is a key concern in fighter′s design and development. Fatigue strength of an aircraft determines important indicators such as safety, durability and reliability of the aircraft.
PEI Lianjie   +4 more
doaj   +1 more source

Improved resonance method for fatigue test of full-scale wind turbine blades

open access: yesAIP Advances, 2022
To further reduce the power of exciter in the common fatigue testing methods and increase the testing frequency to decrease the fatigue testing time, this paper proposes an improved fatigue testing method—Tug Fatigue Testing system (TFTs). The advantages
Aiguo Zhou   +3 more
doaj   +1 more source

Application of Concurrent Test Management Technique in Full Civil Aircraft Fatigue Test

open access: yesHangkong gongcheng jinzhan, 2019
Full aircraft structure fatigue test, as a part of civil aircraft structure airworthiness verification test, is the most complicated, the most expensive and the most time-consuming.
Xia Feng, Mu Shanshan
doaj   +1 more source

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