Add to ORKGThis report describes the specific computational procedure system of aircrafts fatigue life monitoring. The proposed system Is based on operation monitoring of individual aircraft, which is equipped by a recording hardware unit and software processing. The fatigue damage of monitored sections of the aircraft construction has to be evaluated continuously by using this pre-programmed unit.Available from STL Prague, CZ / NTK - National Technical LibrarySIGLECZCzech Republi
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
Aircraft maintenance involves usage and/or damage detection of structures. Usage is asso-ci-ated wit...
In the aerospace industry one of the most important requirements in the aircraft design and operatio...
This report compiles the know-how system of the fatigue life monitoring of aircrafts. The proposed s...
Tato práce se zabývá nedestruktivní metodou kontroly únavy částí stroje, takzvané Structural Health ...
In this paper, some progress and achievements in aircraft integrity requirements, structural health ...
The paper has been intended to discuss the question of optimization of fatigue life of the PZL-130 O...
This report explains basic concepts and characteristics for description of fatigue properties of the...
This bachelor thesis deals with acceptable means of showing compliance with the FAR 23 regulation ba...
Material fatigue is the basic factor limiting aircraft's durability. It comes from the fact that cha...
Air Force Institute of Technology participates in the service life assessment programme SEWST. The a...
Individual aircraft life monitoring is required to ensure safety and economy of aircraft structure, ...
Development of an algorithm of fatigue life of structural components of road and rail vehicles as we...
Tato bakalářská práce se zabývá podrobným výkladem požadavků předpisu FAR 23 na experimentální a výp...
Abstract: Aero engine components are subject to considerable me-chanical and thermal loads. Some ext...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
Aircraft maintenance involves usage and/or damage detection of structures. Usage is asso-ci-ated wit...
In the aerospace industry one of the most important requirements in the aircraft design and operatio...
This report compiles the know-how system of the fatigue life monitoring of aircrafts. The proposed s...
Tato práce se zabývá nedestruktivní metodou kontroly únavy částí stroje, takzvané Structural Health ...
In this paper, some progress and achievements in aircraft integrity requirements, structural health ...
The paper has been intended to discuss the question of optimization of fatigue life of the PZL-130 O...
This report explains basic concepts and characteristics for description of fatigue properties of the...
This bachelor thesis deals with acceptable means of showing compliance with the FAR 23 regulation ba...
Material fatigue is the basic factor limiting aircraft's durability. It comes from the fact that cha...
Air Force Institute of Technology participates in the service life assessment programme SEWST. The a...
Individual aircraft life monitoring is required to ensure safety and economy of aircraft structure, ...
Development of an algorithm of fatigue life of structural components of road and rail vehicles as we...
Tato bakalářská práce se zabývá podrobným výkladem požadavků předpisu FAR 23 na experimentální a výp...
Abstract: Aero engine components are subject to considerable me-chanical and thermal loads. Some ext...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
Aircraft maintenance involves usage and/or damage detection of structures. Usage is asso-ci-ated wit...
In the aerospace industry one of the most important requirements in the aircraft design and operatio...