7 results on '"Domin, Jarosław"'
Search Results
2. Docking unmanned multi-rotor platform for the diagnostic of building structures strengthened with fiber-reinforced polymer overlays.
- Author
-
Czyba, Roman, Domin, Jarosław, and Górski, Marcin
- Subjects
- *
FIBER-reinforced plastics , *AUTOMATIC control systems , *BUILDING design & construction , *STRUCTURAL health monitoring , *EARTH stations - Abstract
External fiber-reinforced polymer overlays have become the most popular method of building structures' strengthening on a global scale. Since no widely used and reliable methods for diagnosing the connection of overlays with the strengthened surface have been developed so far, developing such a method with the entire system, enabling easy and reliable use, has become a vital need of the construction sector. The paper presents an original infrared-based diagnostic module placed on a drone, enabling docking under the structure and conducting precise, uninterrupted diagnostics. The article describes the solutions and configuration of the automatic drone control system and the diagnostic module in all phases of its operation. The embedded measurement and control system has a multi-level structure distributed between the onboard automation system and the ground control station. Laboratory and field tests have shown that the road viaduct solution accurately reproduces joint damage, enabling the assessment of the structure's safety. • A thermography-based device for diagnosing the quality of the bond of FRP strengthening with a concrete surface was constructed. • The diagnostic module was placed on a flying platform in order to perform tests on hard-to-reach structures. • The proposed unmanned multi-rotor platform is equipped with a system that allows docking under the structure for testing and precise graphical data collection. • By creating a unique docking platform, automated processes for flight, approach to structure, docking, measurement and departure have been developed. • Laboratory and field tests show that the road viaduct solution accurately maps bond damage, enabling the estimation of load capacity of strengthened structural elements. [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
- View/download PDF
3. Conception of the throttle-return valve for the magnetorheological fluid.
- Author
-
PILCH, ZBIGNIEW and DOMIN, JAROSŁAW
- Subjects
- *
MAGNETORHEOLOGICAL fluids , *SMART materials , *HYDROCARBONS , *MAGNETIC flux , *TENSILE strength - Abstract
The paper presents the concept of the throttle-return valve dedicated for magne-torheological fluid. Basic properties of the magnetorheological fluid, valve conception and field calculations were presented. [ABSTRACT FROM AUTHOR]
- Published
- 2018
- Full Text
- View/download PDF
4. Two module electromagnetic launcher with pneumatic assist.
- Author
-
Kluszczynski, K. and Domin, Jarosław
- Subjects
- *
ELECTROMAGNETIC launchers , *PNEUMATICS , *RAILGUNS , *ELECTRIC resistance , *DIFFERENTIAL equations , *MATHEMATICAL models - Abstract
Purpose – The purpose of this paper is to present a new concept of a multi-module electromagnetic launcher with pneumatic assist. The authors focus on the problem of modelling a two-module electromagnetic launcher consisting of a coil-gun (module C) and a rail-gun (module R), as well as on the key problem of determining their position-dependent parameters, i.e. the resistances and inductances of discharging electrical circuits connected with the both modules. Special attention is paid to the possibility of influencing the missile’s flight via basic controller variation of the initial voltage values across the terminals of the capacitor batteries supplying current to both modules C and R. Design/methodology/approach – Analysis of the electromagnetic launcher has been based on the circuit-field approach. Differential equations describing movement of the missile have been drawn from circuit theory. The Finite Element Method and the Comsol Multiphysic program were used to determine position-dependent parameters in module C. It is worth emphasising that the effect of saturation (resulting from B-H curve for ferromagnetic part of the considered magnetic circuit) was taken into account. The influence of the initial missile speed adjusted in a pneumatic assist unit on the missile’s velocity was also considered and illustrated by appropriate simulations (the Matlab program). Findings – In analysing the flight of a missile along coil-gun and rail-gun modules, it is necessary to distinguish between three specific stages of the moveable element: the “fall in” stage, the “drive through” stage and the “fall out” stage. One of the most important findings is that during modelling, it is necessary to take into account of all the three above-mentioned stages of missile movement and, in particular, the “fall in” stage. It was shown both by computer simulations and laboratory investigations that this stage plays an important role in determining the time curves of decaying currents in discharging electrical circuits of both module C and module R. Research limitations/implications – The main difficulties are related to determining the influence of air drag force upon missile movement (especially in module C), as well as identifying an accurate value for contact resistances and friction force between the rails and the missile in module R. Practical implications – Hybrid construction employing propelling units of different characters should be treated as a promising and challenging trend in developing launcher structure. One of the most significant advantages of such a solution is the possibility of influencing missile velocity during its flight. Social implications – Since the first device was successfully completed in 1920 the continuous rise in the interest on electromagnetic launchers has been observed. As far as their social and technical impact is concerned, one of the most promising fields of interest seem to be launchers of satellites, high-pressure compressors, simulators modelling collisions between meteoroids and the surface of the earth and electromagnetic guns on board war ships. Originality/value – The novel concept in developing the construction of launchers presented in this paper has been to integrate propelling modules of different characteristics and to create a new multi-module constructional-compact whole. The designed and constructed prototype consists of three modules: a pneumatic drive unit and two electromagnetic drive units that have different principles of operation. The original methodology leading to the creation of its effective mathematical model (focusing on determination of position-depended parameters) was presented and verified in an experimental way. [ABSTRACT FROM AUTHOR]
- Published
- 2015
- Full Text
- View/download PDF
5. Influence Of The Reinforcement On The Destruction Image Of The Composites Panels After Applying Impact Load.
- Author
-
Sławski, Sebastian, Szymiczek, Małgorzata, and Domin, Jarosław
- Subjects
- *
STRUCTURAL panels , *COMPOSITE materials , *IMPACT (Mechanics) , *MECHANICAL loads , *EPOXY resins - Abstract
This article presents result of the researches regarding puncture resistance of the multi-layer composite with reinforcement made of aramid fibers and epoxy matrix. Resin has been mixed with curing agents with different viscosity and amine number (Aradur 3486 and Aradur 3487) and aliphatic polyanine (Aradur 3405). Authors compare results of that researches with result of researches concerning on puncture resistance of epoxy – carbon multi-layer material. Part of the tested samples were subjected to ageing process in thermal shocks conditions (-20/+130˚C - with 105 min holding in each temperature and 30 min on temperature change). Puncture resistance researches were performer with different values of penetrators kinetic energy. A steel cylinder ended with a cone (opening angle 60°) with the mass of 55g have been used as a penetrator. Experiment have been performed on hybrid electromagnetic launcher with pneumatic support. Comparison of the anti-penetration properties have been done based on cavity diameter at the sample created in result of penetrator impact. [ABSTRACT FROM AUTHOR]
- Published
- 2019
- Full Text
- View/download PDF
6. Application of the DIC Technique to Remote Control of the Hydraulic Load System.
- Author
-
Jasiński, Radosław, Stebel, Krzysztof, and Domin, Jarosław
- Subjects
- *
HYDRAULIC control systems , *ELECTRONIC speckle pattern interferometry , *ELECTRICAL engineering , *DIGITAL image correlation , *CONCRETE beams , *COMPUTER engineering , *BENDING moment - Abstract
Displacements or deformations of materials or structures are measured with linear variable differential transducers (LVDT), fibre optic sensors, laser sensors, and confocal sensor systems, while strains are measured with electro-resistant tensometers or wire strain gauges. Measurements significantly limited to a point or a small area are the obvious disadvantage of these measurements. Such disadvantages are eliminated by performing measurements with optical techniques, such as digital image correlation (DIC) or electronic speckle pattern interferometry (ESPI). Many devices applied to optical measurements only record test results and do not cooperate with the system that exerts and controls load. This paper describes the procedure for preparing a test stand involving the Digital Image Correlation system ARAMIS 6M for remote-controlled loading. The existing hydraulic power pack (ZWICK-ROELL) was adapted by installing the modern NI cRIO-9022 controller operating under its own software developed within the LABVIEW system. The application of the DIC techniques to directly control load on the real structure is the unquestionable innovation of the described solution. This led to the elimination of errors caused by the test stand susceptibility and more precise relations between load and displacements/strains which have not been possible using the previous solutions. This project is a synergistic and successful combination of civil engineering, computer science, automatic control engineering and electrical engineering that provides a new solution class. The prepared stand was tested using two two-span, statically non-determinable reinforced concrete beams loaded under different conditions (force or displacement). The method of load application was demonstrated to affect the redistribution of bending moments. The conducted tests confirmed the suitability of the applied technique for the remote controlling and recording of test results. Regardless of the load control method (with force or displacement), convergent results were obtained for the redistribution of bending moments. Force-controlled rotation of the beam section over the support was over 50% greater than rotation of the second beam controlled with an increase in the displacement. [ABSTRACT FROM AUTHOR]
- Published
- 2020
- Full Text
- View/download PDF
7. Low Velocity Impact Response and Tensile Strength of Epoxy Composites with Different Reinforcing Materials.
- Author
-
Sławski, Sebastian, Szymiczek, Małgorzata, Kaczmarczyk, Jarosław, Domin, Jarosław, and Świtoński, Eugeniusz
- Subjects
- *
TENSILE strength , *IMPACT response , *EPOXY resins , *ARAMID fibers , *TENSILE tests - Abstract
This paper presents the results of research concerning multilayered epoxy composites reinforced with different materials. The strength of multilayered composites depends, to a large extent, on the reinforcing material. The authors decided to compare the low velocity impact response and perform tensile strength tests on several composites, to ascertain the mechanical properties of the prepared composites. Five different reinforcing materials were provided for the research (two fabrics made from aramid fibers, two fabrics made from carbon fibers and one fabric made from polyethylene fibers). The composites were manufactured by the vacuum supported hand laminating method. The low velocity impact response tests were conducted with the use of a pneumatic launcher. Three strikers with different geometry (conical striker, hemispherical striker and ogival striker) were used. A comparison of the resulting damage to the composites after the impact of the strikers was based on the images obtained using an optical microscope; tensile tests were also performed. The experimental investigation showed significant differences in the mechanical properties of the composites, depending on the applied reinforcing material. It was found that, as a result of the impacts, less damage occurred in the composites which were characterized by a lower Young's modulus and a higher tensile strength. [ABSTRACT FROM AUTHOR]
- Published
- 2020
- Full Text
- View/download PDF
Catalog
Discovery Service for Jio Institute Digital Library
For full access to our library's resources, please sign in.