Analysis of electric - drive applicability in mechanical brake for the commuter class airplane

• Autorzy: Grygorcewicz P.
• Języki publikacji: EN

Abstrakty

EN

This article presents selected issues related to the design methodology of the electric brakes during the construction process as well as other factors which are important in the design process. It is a very important issue due to affect on the airplane and automotive brake design. Nowadays when new solution of brakes is being designed there is a need to take into account various factors influencing the design such as: weight, compatibility and flexibility of use in various aircraft, reliability and durability, ease of installation and maintenance, low-cost operation and low cost components, braking efficiency, short braking distance. All of these factors are taken into account when designing a prototype of the electric brake as well as economical factor of the design. It is also necessary to verify the design during its creation using experimental and laboratory test data from other similar designs. The aim of the paper is to discuss design process from the very beginning (i.e. by comparing features of the electric brakes with other types of brakes in order to show advantages and disadvantages of chosen solution) to the creation of a working demonstrator in future. Author of the paper in his electric brake design bases on the experience of the Warsaw’s Institute of Aviation Landing Gear Department.

Słowa kluczowe

EN

transport; airplanes; brakes; landing gear; construction process

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2013
• Tom: Vol. 20, No. 2
• Strony: 143--148
• Opis fizyczny: Bibliogr. 9 poz., rys.

Twórcy

autor

Grygorcewicz P.

• Institute of Aviation, Landing Gear Department Krakowska Av. 110/114, 02-256 Warsaw, Poland tel.: [phone]

Bibliografia

• [1] Dietrich, M., Podstawy konstrukcji maszyn, WNT, Warszawa 1999.
• [2] Jachimowicz J., Metoda elementów skończonych, Wykłady, 2012.
• [3] Beitz, G. P. W., Nauka konstruowania, WNT, Warszawa 1984.
• [4] Currey, N. S., Aircraft Landing Gear Design Principles and Practices, Washington AIAA 1988.
• [5] Lewitowicz, J., Uncertainty and Dependability of the risk model applicable to operation of aircrafts, KONBiN, 1, 2010.
• [6] Lewitowicz, J., Kustoń, K., Podstawy eksploatacji statków powietrznych, ITWL, Warszawa 2003.
• [7] Czajgucki, J. Z., Filozoficzno-naukowo-dysertacyjne problemy modelowania i symulacji relacji niezawodnościowych w wieloaspektowych systemach, 2010.
• [8] http://www.safranmbd.com/wheels-and-brakes-176/
• [9] http://www.flightglobal.com/blogs/runway-girl/2008/10/photos-allelectric-braking-sys.html.