The design resource of the airframe structure is assigned in the number of generalized typical flights or flight hours for all aircraft of the park. Both in the design and in the operational phases, the parameters of typical flight profiles serve as initial data for substantiating the design, accumulated or residual resources of the structural elements. An analysis of the load conditions of the transport category airplanes shows that even airplanes of the same type can have a completely different operating history. The projected typical flight profiles do not always correspond to the actual tasks performed by a particular aircraft. In addition, the operator does not have an explicit definition of the concept of a generalized type of flight....
The following article presents the research conducted under a complex structure integrity program fo...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
The thesis deals with the calculation and evaluation of the flight characteristics of the aeroplane ...
The paper has been intended to discuss the question of optimization of fatigue life of the PZL-130 O...
The subject of research in the paper is the process of forming a criterion base to evaluate the effe...
One of the problems becoming increasingly important in the exploitation process of each technical ob...
The doctoral thesis deals with reliability (dependability) analyses of operation and testing data of...
The reliable evaluation of operational loads plays a major role in the type and scope of mainte-nanc...
The subject of the article is a method for evaluating the effectiveness of modifications of transpor...
There the ample statistics of load factors has been generalized; the dependences of variables of dis...
Bakalářská práce se zaměřuje na nákladní leteckou dopravu. Zabývá se stručnou historií, vlastnostmi ...
The aim of thesis is to acquaint with the development of aircraft technology, to evaluate the operat...
Ukraine is an aviation state that has a full cycle of development and serial production of aircraft,...
The relevance of this study is predetermined by the improvement to the fuel efficiency of an aircraf...
This paper presents the method of evaluation of a technical object as immersed in a logistic system ...
The following article presents the research conducted under a complex structure integrity program fo...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
The thesis deals with the calculation and evaluation of the flight characteristics of the aeroplane ...
The paper has been intended to discuss the question of optimization of fatigue life of the PZL-130 O...
The subject of research in the paper is the process of forming a criterion base to evaluate the effe...
One of the problems becoming increasingly important in the exploitation process of each technical ob...
The doctoral thesis deals with reliability (dependability) analyses of operation and testing data of...
The reliable evaluation of operational loads plays a major role in the type and scope of mainte-nanc...
The subject of the article is a method for evaluating the effectiveness of modifications of transpor...
There the ample statistics of load factors has been generalized; the dependences of variables of dis...
Bakalářská práce se zaměřuje na nákladní leteckou dopravu. Zabývá se stručnou historií, vlastnostmi ...
The aim of thesis is to acquaint with the development of aircraft technology, to evaluate the operat...
Ukraine is an aviation state that has a full cycle of development and serial production of aircraft,...
The relevance of this study is predetermined by the improvement to the fuel efficiency of an aircraf...
This paper presents the method of evaluation of a technical object as immersed in a logistic system ...
The following article presents the research conducted under a complex structure integrity program fo...
In accordance with the airworthiness standards, the aircraft structure must be operationally surviva...
The thesis deals with the calculation and evaluation of the flight characteristics of the aeroplane ...