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Warianty tytułu
Porównanie aktuatorów hydraulicznych i elektrycznych wykorzystywanych w lotnictwie
Języki publikacji
Abstrakty
The paper presents electrical and hydraulic actuators. The main features of both types have been discussed. The efficiency, control loops and reliability were compared. Application of actuators was presented.
Omówiono najważniejsze cechy obu rozwiązań. Porównano sprawność, opisano sposoby sterowania oraz niezawodność. Podano przykłady wykorzystania elementów w maszynach lotniczych.
Czasopismo
Rocznik
Tom
Strony
27--32
Opis fizyczny
Bibliogr. 7 poz., rys., tab.
Twórcy
autor
- INSA Toulouse. France
Bibliografia
- [l] Maré J-C.: From Douglas DC3 to Airbus A380 - seventy years of innovation in aeraspace hydraulics, Proceedings of the 4th Internationales Fluidtechnisches Kolloquium, Dresden 2004.
- [2] Maré J-C.: The recent developments in aeraspace hydraulics, focussing on the new Airbus A380, Invited opening session of the 19th International Conference on Hydraulics and Pneumatics, Prag 2006.
- [3] Dee G., Vanthuyne T., Alexandre P.: An electrical thrust vector control system with dynamic force feedback, Proceedings of the third international conference on Recent Advances n Aerospace Actuation Systems and Components, Toulouse 2007.
- [4] Johanssonn B., Andersson J. and Krus P.: Thermal modeling of an electrohydrostatic actuation system, Proceedings of the first International Conference on Recent Advances in Aerospace Actuation Systems and Components, Toulouse 2001.
- [5] Maré J-C. and Moulaire P.: Expert rules for the design of position control of electrohydraulic actuators, Proceedings of the 6th Scandinavian International Conference on Fluid Power, Tampere 1999.
- [6] Biedermann O., Bildstein M.; Development, Qualification and Verification of the A380 Spoiler EBHA, Proceedings of the second International Conference on Recent Advances in Aerospace Actuation Systems and Components, Toulouse 2004.
- [7] DorkeI A., Biedermann O., Wennmacher G.; Theoretical validation and experimental verification of the electrically assisted hydraulic actuator concept, Proceedings of the third International Conference on Recent Advances in Aerospace Actuation Systems and Components, Toulouse 2007.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BWM4-0012-0009