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Number of results: 11
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Abstract

The development of air transport affects elements of the aviation fuel market. In recent years an increase in both the number of passengers and the number of passenger operations has been observed. This phenomenon also concerns passengers and the number of operations served by Polish airports which translates into more and more fuel consumption in Poland. The authors of the study tried to approximate the characteristics of aviation fuels used in various types of aircrafts. The most important of them, from the perspective of the Polish aviation sector, include Jet. This type of fuel plays a key role in civil aviation. In the article, the enterprises operating in the analyzed sector were also reviewed. The empirical part of the article is devoted, in turn, to the analysis of changes in air passenger transport in Poland and changes in Jet fuel prices on the Polish fuel markets. The conducted research shows that the dynamics of changes in the number of passengers, as well as the number of passenger operations at Polish airports were characterized by an upward trend, and the increase in the number of passengers was driven not only by a larger number of available flights, but also by such factors as: increasing the capacity of aircraft and increasing the fill rate for seats. The authors have also attempted to examine the strength of dependence between the number of passengers deciding to use Polish airports and Jet fuel prices, which in recent years have undergone significant fluctuations. For this purpose, the value of Pearson’s linear correlation coefficient was used and the analyzed period covered the years 2011–2017. The data on passenger traffic used in the study came mainly from periodic reports prepared by the Civil Aviation Office (ULC).

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Authors and Affiliations

Justyna Muweis
Bartosz Łamasz
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Abstract

Embedded software and dedicated hardware are vital elements of the modern world, from personal electronics to transportation, from communication to aerospace, from military to gaming, from medical systems to banking. Combinations of even minor hardware or software defects in a complex system may lead to violation of safety with or even without evident system failure. a major problem that the computing profession faces is the lack of a universal approach to unite the dissimilar viewpoints presented by computer science, with its discrete and mathematical underpinnings, and by computer engineering, which focuses on building real systems and considering spatial and material constraints of space, energy, and time. Modern embedded systems include both viewpoints: microprocessors running software and programmable electronic hardware created with an extensive use of software. The gap between science and engineering approaches is clearly visible in engineering education. This survey paper focuses on exploring the commonalities between building software and building hardware in an attempt to establish a new framework for rejuvenating computing education, specifically software engineering for dependable systems. We present here a perspective on software/hardware relationship, aviation system certification, role of software engineering education, and future directions in computing.

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Authors and Affiliations

A.J. Kornecki
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Abstract

The social and political transformations Russia underwent in the 20th century were also reflected in the sphere of imagery. This also refers to the imagery of movement and means of transport. The process of linking the imagery of means of transportation with the political doctrine in force is mostly visible in the period of Soviet rule, in particular in the interwar period when the foundations of this rule were laid. Then, aviation was to become one of the strongly ideologized means of transport. The ideologization process occurred at various levels, starting from onomastic procedures through advertising and linking aviation and Soviet rule within artistic and literary conceptualisations. In Soviet culture, an aeroplane or a rocket were not merely means of transport but the means by which the expansion of communist ideology globally was supposed to be facilitated.

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Authors and Affiliations

Roman Bobryk
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Abstract

This work presents a numerical simulation of aviation structure joined by friction stir welding, FSW, process. The numerical simulation of aviation structure joined by FSW was created. The simulation uses thermomechanical coupled formulation. Th model required creation of finite elements representing sheets, stiffeners and welds, definition of material models and boundary conditions. The thermal model took into account heat conduction and convection assigned to appropriate elements of the structure. Time functions were applied to the description of a heat source movement. The numerical model included the stage of welding and the stage of releasing clamps. The output of the simulation are residual stresses and deformations occurring in the panel. Parameters of the global model (the panel model) were selected based on the local model (the single joint model), the experimental verification of the local model using the single joint and the geometry of the panel joints.

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Authors and Affiliations

P. Lacki
K. Adamus
J. Winowiecka
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Abstract

Aviation testing is intrinsically connected with rotary telemetry, which enables engineers to measure and verify parameters of high-speed aircraft engines components during laboratory testing. The main purpose of this article is to propose new design concept of smart telemetry module for temperature measurements, which could be easily adapted to various demands of high-speed rotary components tests and is more handful, functional and affordable than other solutions on the market. The result of the work is a telemetry system in form of light weight, PCB-based, wireless powered, smart transducer. Article presents state of art analysis, design and manufacturing steps, test results and conclusions.
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Authors and Affiliations

Tomasz Kabala
1
Jerzy Weremczuk
2

  1. Łukasiewicz Research Network – Institute of Aviation, Poland
  2. Faculty of Electronics and InformationTechnology, Warsaw University of Technology, Poland
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Abstract

One of the little described problems in hydrostatic drives is the fast changing runs in the hydraulic line of this drive affecting the nature of the formation and intensity of pressure pulsation and flow rate occurring in the drive. Pressure pulsation and flow rate are the cause of unstable operation of servos, delays in the control system and other harmful phenomena. The article presents a flow model in a hydrostatic drive line based on fluid continuity equations (mass conservation), maintaining the amount of Navier-Stokes motion in the direction of flow (x axis), energy conservation (liquid state). The movement of liquids in a hydrostatic line is described by partial differential equations of the hyperbolic type, so modeling takes into account the wave phenomena occurring in the line. The hydrostatic line was treated as a cross with two inputs and two outputs, characterized by a specific transmittance matrix. The product approximation was used to solve the wave equations. An example of the use of general equations is presented for the analysis of a miniaturized hydrostatic drive line fed from a constant pressure source and terminated by a servo mechanism.

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Authors and Affiliations

L. Ułanowicz
G. Jastrzębski
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Abstract

The aim of the article is to determine the main factors responsible for development of Podkarpackie Voivodeship in the last 15 years and to answer the question whether they were suffi ciently strong impulse to divert the region from its development model. The main method used for identifying the factors that determine the development of the region was individual, in-depth interviews with the main actors on the regional scene, supported by desk research analysis (of the voivodeship’s strategic and operational documents) and statistical data analysis (Central Statistical Office and Eurostat). The research highlights the importance of the immobile and intangible development factors – a high quality of strategic thinking of local and especially regional authorities and consistent implementation of development policies, a high level of social capital, extensive networks and the ability to co-operate – which have helped to eliminate the limitations resulting from the weakness of other factors.

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Authors and Affiliations

Anna Dąbrowska
Jacek Szlachta
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Abstract

Coordinate Measurement Machines (CMMs) have been extensively used in inspecting mechanical parts with higher accuracy. In order to enhance the efficiency and precision of the measurement of aviation engine blades, a sampling method of profile measurement of aviation engine blade based on the firefly algorithm is researched. Then, by comparing with the equal arc-length sampling algorithm (EAS) and the equi-parametric sampling algorithm (EPS) in one simulation, the proposed sampling algorithm shows its better sampling quality than the other two algorithms. Finally, the effectiveness of the algorithm is verified by an experimental example of blade profile. Both simulated and experimental results show that the method proposed in this paper can ensure the measurement accuracy by measuring a smaller number of points.

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Authors and Affiliations

Zhi Huang
Liao Zhao
Kai Li
Hongyan Wang
Tao Zhou
ORCID: ORCID
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Abstract

This document provides a simplified solution to the problem of calculation of laser hazard distances defined in the Advisory Circular 70-1B by the U.S. Federal Aviation Administration regarding atmospheric attenuation (assuming its constant value) and measurement uncertainties. The calculation approaches and examples presented in this document do not specify the procedure that should be followed in the case of atmospheric attenuation, nor do they take into account the uncertainties associated with the measured parameters. The analysis presented in the article complements to some extent AC 70-1B and can be used by those who need such a simplified solution regarding illumination of landing or taking off aircrafts. The article presents a sample analysis for a typical laser pointer, where the necessary parameters of the laser beam along with the appropriate uncertainties were determined in accordance with the methods accredited by the Polish Centre for Accreditation while the appropriate laser hazard distances were calculated taking into account different atmospheric attenuation coefficients.
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Authors and Affiliations

Jarosław Młyńczak
1

  1. Military University of Technology, Institute of Optoelectronics, Gen. S. Kaliskiego 2, 00-908 Warszawa, Poland
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Abstract

Research of semiotic aspects Lithuanian military air navigation charts was based on the semantic, graphic and information load analysis. The aim of semantic analysis was to determine how the conventional cartographical symbols, used in air navigation charts, correspond with carto-linguistic and carto-semiotic requirements. The analysis of all the markings was performed complex and collected by questionnaire were interviewed various respondents: pilots, cartographers and other chart users. The researches seek two aims: evaluate information and graphical load of military air navigation charts. Information load evaluated to calculate all objects and phenomenon, which was in 25 cm² of map. Charts analysis showed that in low flight charts (LFC) average information load are 4 – 5 times richer than in the operational maps. Map signs optimization on LFC has to be managed very carefully, choosing signs that can reduce the load of information and helps for the information transfer process. Graphical load of maps evaluated of aeronautical maps is not great (5 – 12%) and does not require reduction the information load and generalization of charts. Air navigation charts analysis pointed that not all air navigation sings correspond carto-semiotic requirements and must be improved. The authors suggested some new sings for military air navigation chart, which are simpler, equivalent to human psychophysical perception criteria, creates faster communication and less load on the chart.
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Authors and Affiliations

Donatas Ovodas
Algimantas Česnulevičius
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Abstract

This article seeks to answer the question of how international criminal law (ICL), the 1971 Montreal Convention, and international humanitarian law (IHL) influenced the proceedings in the MH-17 case, with particular emphasis on the Dutch Prosecutors’ line of reasoning in proceedings before the District Court in The Hague (DCiTH), as well as on the judgments that the DCiTH delivered on 17 November 2022. Notably, the analysis below aims to establish whether, by refusing to grant combatant status to the defendants, the District Court acted within the limits permissible under international law, even though this Court admitted that at the moment of the MH-17’s downing, the nature of the conflict in Eastern Ukraine was an international, not a non-international, one. In conclusion, the article argues that, firstly, even though the DCiTH’s interpretation of the IHL is not free of certain flaws, the Court’s line of reasoning and the sentences it delivered are a pragmatic attempt to bridge the gap between the proper administration of justice and the efficiency of criminal proceedings in a case where an airplane downing takes place during an international armed conflict. Secondly, although most recently the European Court on Human Rights (ECtHR) took note of the MH-17 judgments, for the reasons explained in this article the scope of their potential impact on the further development of international and domestic jurisprudence is uncertain, and remains to be seen.
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Authors and Affiliations

Aleksander Gubrynowicz
1
ORCID: ORCID

  1. Faculty of Law and Administration, University of Warsaw

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