Wszystkie pola: Coordinate Measuring Technique - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Automated measurement of bevel gears of the aircraft gearbox using GOM
Autorzy:: Marciniec, A.
Budzik, G.
Dziubek, T.
Powiązania:: https://bibliotekanauki.pl/articles/247190.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: gear
aircraft gearbox
coordinate measuring technique
Opis:: Manufacture of aircraft gearbox elements requires control of gear geometric parameters at different stages of technological process. Acceleration and automation of measurement process can affect the duration of the finished item production. In case of measurement of gear wheels using modern technologies based on numerical machines, measurement process is based on processing of numerical data obtained by measurement using coordinate measuring machines. The goal of this paper is to present the opportunity to automate the measurement process of bevel gears, using coordinated optical scanner ATOS by GOM, equipped with a turntable. Using coordinate measuring technique, you can specify a set of methods and procedures for the designation of the complex dimensions of physical objects and transform them into a computer program space of coordinate measuring devices. The topics included in the article are intended to show the capabilities of the device used to improve the measurement process and shorten its time, and hence, lower its costs. Another thing described in the paper is the impact of measurement performance in automatic mode on the quality of performance - the numerical image of scanned surface, from the standpoint of accuracy and number of collected data points in the shortest time. The article includes an analysis of conditions related to the measurement works, such as the process of preparing the model and measurement equipment and data processing capacity. The result of the work will be presented methodology for automated scanning measurements of bevel Sears.
Źródło:: Journal of KONES; 2011, 18, 4; 259-264
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Automated measurement of bevel gears of the aircraft gearbox using GOM
Autorzy:: Marciniec, A.
Budzik, G.
Dziubek, T.
Powiązania:: https://bibliotekanauki.pl/articles/242283.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: gear
aircraft gearbox
coordinate measuring technique
Opis:: Manufacture of aircraft gearbox elements requires control of gear geometric parameters at different stages of technological process. Acceleration and automation of measurement process can affect the duration of the finished item production. In case of measurement of gear wheels using modern technologies based on numerical machines, measurement process is based on processing of numerical data obtained by measurement using coordinate measuring machines. The goal of this paper is to present the opportunity to automate the measurement process of bevel gears, using coordinated optical scanner ATOS by GOM, equipped with a turntable. Using coordinate measuring technique, you can specify a set of methods and procedures for the designation of the complex dimensions of physical objects and transform them into a computer program space of coordinate measuring devices. The topics included in the article are intended to show the capabilities of the device used to improve the measurement process and shorten its time, and hence, lower its costs. Another thing described in the paper is the impact of measurement performance in automatic mode on the quality of performance - the numerical image of scanned surface, from the standpoint of accuracy and number of collected data points in the shortest time. The article includes an analysis of conditions related to the measurement works, such as the process ofpreparing the model and measurement equipment and data processing capacity. The result of the work will be presented methodology for automated scanning measurements of bevel Sears.
Źródło:: Journal of KONES; 2011, 18, 2; 287-292
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Analysis of dimensional accuracy of blade of aircraft engine using a coordinate measuring machine
Autorzy:: Budzik, G
Kubiak, Krzysztof
Zaborniak, M.
Przeszłowski, Ł.
Dziubek, T.
Cygan, M.
Tutak, M.
Matysiak, H
Powiązania:: https://bibliotekanauki.pl/articles/244267.pdf
Data publikacji:: 2014
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: aircraft engines turbine blades
optical measurements
coordinate measuring technique
Opis:: Technological process of aircraft engine turbine blades requires control of blade geometric parameters. Innovation technologies for measurement of aircraft engine turbine blades are based on coordinate numerical machines – measurement process is based on processing of numerical data obtained by measurement using coordinate measuring machines. The paper presents the opportunity of analysis of dimensional accuracy of aircraft engine turbine blades measurements using coordinate measuring machine (CMM). Coordinate measuring machine allows specifying full methodology for designation of complex dimensions of physical objects (blade of aircraft engine) and transforming them into a computer program space of coordinate measuring devices. Presented paper includes capabilities of device used in the study to improve the measurement process and blades geometry analysis in the technological and economical aspects. Another issue described in the paper is impact of measurement performance in automatic mode on the quality of performance – the numerical model of geometry, from the standpoint of accuracy and number of collected data points in time. Measurements using a coordinate measuring machine are among the most accurate methods of measuring. The paper includes an analysis of conditions related to the measurement works, such as the process of preparing the model, measurement equipment and data processing capacity. As the result, methodology of (CMM) measurements of aircraft engine turbine blades will be presented.
Źródło:: Journal of KONES; 2014, 21, 2; 33-37
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: Optical measurement of aircraft engine turbine blades
Autorzy:: Budzik, G.
Kubiak, K.
Rokicki, P.
Dziubek, T.
Nowotnik, A.
Matysiak, H.
Cygan, R.
Tutak, M.
Boś, P.
Powiązania:: https://bibliotekanauki.pl/articles/247470.pdf
Data publikacji:: 2013
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: aircraft engines turbine blades
optical measurements
coordinate measuring technique
Opis:: Manufacturing of aircraft engine turbine blades requires control of blade geometric parameters at different stages of technological process. Acceleration and automation of measurement process can affect the duration of the finished item production. Modern technologies for measurement of aircraft engine turbine blades are based on numerical machines - measurement process is based on processing of numerical data obtained by measurement using coordinate measuring machines. The paper presents the opportunity of automation of aircraft engine turbine blades measurements using scanner ATOS II Triple Scan with blue light source technology. Coordinate measuring technique allows to specify full methodology for designation of complex dimensions of physical objects and transform them into a computer program space of coordinate measuring devices. Presented paper includes capabilities of device used in the study to improve the measurement process in the technological and economical aspects. Another issue described in the paper is impact of measurement performance in automatic mode on the quality of performance – the numerical model of surface, from the standpoint of accuracy and number of collected data points in time. The paper includes an analysis of conditions related to the measurement works, such as the process of preparing the model, measurement equipment and data processing capacity. As the result methodology for automated scanning measurements of aircraft engine turbine blades will be presented.
Źródło:: Journal of KONES; 2013, 20, 2; 21-26
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: The determination of accuracy of test gear wheel for aeronautical dual - power path gear before heat treatment
Autorzy:: Dziubek, T.
Budzik, G.
Kozik, B.
Sobolewski, B.
Powiązania:: https://bibliotekanauki.pl/articles/241821.pdf
Data publikacji:: 2013
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: gear
aircraft gearbox
coordinate measuring technique
dual-power path gear
Opis:: Manufacture of aircraft gearbox elements requires control of gear geometric parameters at different stages of technological process. In case of measurement of gear wheels using modern technologies based on numerical machines, measurement process is based on processing of numerical data obtained by measurement using coordinate measuring machines. The goal of this paper is to present the measurement process of gears, using coordinated optical scanner ATOS II TripleScan by GOM, equipped with a turntable. The aim of this study is to develop and execute the analysis accuracy of the geometry of the gear of aeronautical dual-power path gear after the roughing operation using optical coordinate measuring methods. Executed research will enable the detection of errors occurring in the machining process and to determine the value of founded the machining allowance finishing in relation to the CAD model. Using coordinate measuring technique, one can specify a set of methods and procedures for the designation of the complex dimensions of physical objects and transform them into a computer program space of coordinate measuring devices. On this basis, it is possible to determine the accuracy of the gear wheel as the workpiece prior to heat treatment. The results will be the basis to determine the effect of heat treatment on changes in the geometry of the gear and the benchmark for determining the correctness of the finishing.
Źródło:: Journal of KONES; 2013, 20, 2; 83-90
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 6.

Tytuł:: The determination of accuracy of the demonstrator of aeronautic bevel gearbox, accomplished by selected rapid prototyping techniques using an optical scanner Atos II Triple Scan
Autorzy:: Marciniec, A.
Budzik, G.
Dziubek, T.
Sobolewski, B.
Zaborniak, M.
Powiązania:: https://bibliotekanauki.pl/articles/247540.pdf
Data publikacji:: 2014
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: bevel gear
aircraft gearbox
optical scanner
coordinate measuring technique
rapid prototyping
gear modelling
Opis:: Designing and manufacturing of aeronautic bevel gearboxes is a complicated and time-consuming process because of complex kinematics of the machining process as well as numbers of manufacturing methods. Machine manufacturers usually provide algorithms used in manufacture process. This requires substantial financial resources and, in consequence, it increases the costs of production. Using other commonly available calculation algorithm requires a lot of studies to verify whether the proposed gearbox works correctly. In order to reduce the manufacturing costs of prototypes, it is possible to use Rapid Prototyping methods. Using both Rapid Prototyping techniques and coordinate optical measurements enables to verify the correctness of assumptions made in the initial stage of product designing. This approach reduces significantly both prototyping time and manufacturing costs. In order to ensure the effectiveness of prototyping process, it is essential to provide the accuracy of manufactured prototypes. That is the reason why it is necessary to determine manufacturing methods that will ensure the highest geometric accuracy. The study presents the modelling and manufacturing process of aeronautic bevel gear of demonstrator taking into consideration the accuracy of selected Rapid Prototyping methods. The gear modelling is based on machining simulation method conducted in Autodesk Inventor. The measurement results are shown in displacement maps obtained with an optical scanner Atos II Triple Scan and universal GOM Inspect Professional software, which determines the prototype accuracy in relation to 3D-CAD models.
Źródło:: Journal of KONES; 2014, 21, 3; 205-209
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 7.

Tytuł:: The determination of accuracy of testing gear wheel for aeronautical dual-power path gear after heat treatment
Określenie dokładności testowego koła zębatego lotniczej przekładni dwudrożnej po obróbce cieplnej
Autorzy:: Dziubek, T.
Powiązania:: https://bibliotekanauki.pl/articles/327472.pdf
Data publikacji:: 2015
Wydawca:: Polska Akademia Nauk. Polskie Towarzystwo Diagnostyki Technicznej PAN
Tematy:: error detection
gear
diagnostics
aircraft gearbox
coordinate measuring technique
wykrywanie błędów
koło zębate
diagnostyka
przekładnia lotnicza
współrzędnościowa technika pomiarowa
Opis:: Manufacture of aircraft gearbox elements requires control of gear geometric parameters at different stages of technological process. The aim of this study is to present develop and execute the analysis accuracy of the geometry of the gear of aeronautical dual-power path gear after the roughing operation using coordinated optical scanner ATOS II Triple Scan. Research was carried out in order to detect errors occurring in the machining process and to determine the value of founded the machining allowance finishing in relation to the CAD model. On this basis, it is possible to determine the accuracy of the gear wheel as the workpiece after heat treatment. The results will be the basis to determine the effect of heat treatment on changes in the geometry of the gear and the benchmark for determining the correctness of the finishing.
Produkcja elementów przekładni lotniczych wymaga kontroli parametrów geometrycznych kół zębatych na różnych etapach procesu technologicznego. Celem niniejszej pracy jest przedstawienie opracowania i wykonania analizy dokładności geometrii koła przekładni dwudrożnej po obróbce zgrubnej przy użyciu współrzędnościowego skanera optycznego ATOS II Triple Scan. Badania przeprowadzono w celu wykrycia błędów powstałych w procesie obróbki skrawaniem oraz określenia wartości założonych naddatków na obróbkę wykańczającą w odniesieniu do modelu CAD. Na tej podstawie możliwe jest określenie dokładności wykonania koła zębatego, jako półwyrobu po obróbce cieplnej. Otrzymane wyniki będą podstawą do określenia wpływu obróbki cieplnej na zmiany geometrii koła zębatego ze wzorcem odniesienia dla określenia poprawności wykonania obróbki wykańczającej.
Źródło:: Diagnostyka; 2015, 16, 2; 61-66
1641-6414
2449-5220
Pojawia się w:: Diagnostyka
Dostawca treści:: Biblioteka Nauki

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