Results from laboratory tests of new electric brake prototype

• Autorzy: Grygorcewicz Paweł

Identyfikatory

DOI

10.2478/kones-2019-0056

• Języki publikacji: EN

Abstrakty

EN

The main idea of this article was to compare the results of new design electric brake to the older version of hydraulic brake in laboratory tests. The energy of braking should be very similar due to the same mass of the airplane. That is why the laboratory tests of both brakes were took place in the same stand. Of course, the parameters were similar but not at all. The main idea was to create the solution, which could be used in vehicle like airplane. The electric brakes could replace traditional hydraulic brake solution. The results could be interesting for every researcher who is interested in brakes. Other important idea of this article was to describe the tests of new electric brake prototype. The purpose of the tests was to check designing of electric brakes. The electric brake prototype should ensure sufficient efficiency, safety, reliability and durability during braking, which is required in certification processes and is particularly important when researching innovative solutions. It was really important to verify the design and check the parameters. Of course, there is really important to remember that in every new type of the prototype solutions there are many pros and cons, which are typical only for considered design. Nowadays every electric brake design is different because there is a lot of new concept.

Słowa kluczowe

EN

laboratory testing; electric brake; braking 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: 2019
• Tom: Vol. 26, No. 3
• Strony: 47--52
• Opis fizyczny: Bibliogr. 4 poz., rys.

Twórcy

autor

Grygorcewicz Paweł

• Łukasiewicz Research Network – Institute of Aviation Krakowska Av. 110/114, 02-256 Warsaw, Poland tel.: [phone] ext. 657, fax: [phone]

Bibliografia

• [1] Currey, N. S., Aircraft Landing Gear Design Principles and Practices, Washington AIAA, 1988.
• [2] Grygorcewicz, P. Paprzycki, I., Stanowisko i wytyczne do badań ABS w samolotach, Logistyka, 2015.
• [3] Grygorcewicz, P., Issues During Assembly New Type of Electric Brake Prototype and Initial Tests of Individual Components, Journal of KONES, Vo. 25, No. 3, pp. 213-218, 2018.
• [4] Grygorcewicz, P., Skorupka, Z., Badanie laboratoryjne hamulców ciernych w laboratorium badań podwozi lotniczych, TTS Technika Transportu Szynowego, 2013.

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).