Results 11 to 20 of about 40,632 (210)

Generating Methods of Severe Load Spectra for Airplanes Based on Statistic Analysis in Flight Subjects

open access: yesHangkong gongcheng jinzhan, 2019
Nowadays, the mean load spectra is mostly used in fatigue test for aircraft, but it has the defects of long fatigue cycle. The severe load spectra is used instead, which can shorten the test time greatly. In order to meet the demand of full-scale fatigue
Zhang Jiajia, Jiang Zuguo, Feng Jianmin
doaj   +1 more source

Motion Synchronous Composite Decoupling with Fewer Sensors on Multichannel Hydraulic Force Control for Aircraft Structural Loading Test System

open access: yesSensors, 2018
The aircraft full-scale fatigue test is widely used in the modern aircraft industry for the safety of flight. Generally, the aircraft full-scale fatigue test is achieved by structural loading; multiple hydraulic actuators are used to apply load for force
Yaoxing Shang   +5 more
doaj   +1 more source

Full scale fatigue test of the Su-22 aircraft – Assumptions, process and preliminary conclusions [PDF]

open access: yesAIP Conference Proceedings, 2016
The following article describes the Full Scale Fatigue Test of the Su-22 UM3K fighter-bomber. The test was carried out due to the decision of the Polish Ministry of Defense to prolong the service life for this type of aircraft. Within the article authors present the main goals of the test as well as main assumptions and simplifications which had to be ...
Andrzej Leski   +4 more
openaire   +1 more source

STUDY ON FATIGUE SCATTER FACTOR OF AIRCRAFT STRUCTURE UNDER DURABILITY SEVERE LOAD SPECTRUM

open access: yesJixie qiangdu, 2021
Fatigue scatter factor is the reliability index of aircraft structure life,which is used to describe the reliability of analysis and test results.
WANG YongJun, LI Tang, DUI HongNa
doaj  

Remote Monitoring of Fatigue Cracks Growth in the Aircraft Structure Based on Active Piezosensor Network during the Full Scale Fatigue Test [PDF]

open access: yesKey Engineering Materials, 2013
One of the major issues from a structural integrity point of view of the aircraft structure is an appropriate health monitoring technology delivery for the damage tolerant philosophy. This paper presents a development of a system for fatigue crack growth monitoring and early damage detection in the PZL 130 ORLIK TC II turbo-prop military trainer aft ...
Krzysztof Dragan   +3 more
openaire   +1 more source

Selected Aspects Related to the Applied Loads Control During Fatigue Tests of a Metallic Airframe

open access: yesFatigue of Aircraft Structures, 2014
Service life of the PZL M28 is computed based on the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test objects are: (1) wing and ...
Brzęczek Józef   +2 more
doaj   +1 more source

Selected Aspects Related to Preparation of a Fatigue Test Plan of a Metallic Airframe

open access: yesFatigue of Aircraft Structures, 2014
Service life of the PZL M28 is computed based on the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test objects were: (1) wing and ...
Brzęczek Józef   +3 more
doaj   +1 more source

Introduction of an Individual Aircraft Tracking Program for the Polish SU-22

open access: yesFatigue of Aircraft Structures, 2017
The Su-22 fighter-bomber is a military aircraft used in the Polish Air Force (PLAF) since the mid 1980’s. By decision of the Ministry of National Defence Republic of Poland, the assumed service life for this type of aircraft was prolonged up to 3200 ...
Reymer Piotr   +4 more
doaj   +1 more source

The Definition of the Load Spectrum for SU-22 Fighter-Bomber Full Scale Fatigue Test

open access: yesFatigue of Aircraft Structures, 2015
The Su-22 fighter-bomber is a military aircraft used in the Polish Air Force since the mid 1980’s. By the decision of the Polish Ministry of Defense the predicted service life for this type of aircraft will be extended to 3200 flight hours.
Reymer Piotr   +3 more
doaj   +1 more source

Electrostatic Self‐Assembly Induced Nest‐Like MXene Networks on Fabric for Ultra‐Broadband Flexible Absorption

open access: yesAdvanced Science, EarlyView.
In this study, an electrostatically self‐assembled WPU‐MXene@FC flexible fabric constructs a “nest‐like” structure on fibers, building construct MXene multiple loss paths, achieving ultra‐wideband absorption of 25.3–1200 GHz in a thickness of 1.8 mm, while also exhibiting superhydrophobicity, acid and alkali resistance, and bending resistance ...
Min Luo   +7 more
wiley   +1 more source

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