Issues during assembly new type of electric brake prototype and initial tests of individual components

• Autorzy: Grygorcewicz P.

Identyfikatory

DOI

10.5604/01.3001.0012.4335

• Języki publikacji: EN

Abstrakty

EN

In this article, the author focused on the two main issues. Firstly, the assembly phase of the new type of electric brake prototype was described and secondly author introduced the initial tests of individual components. The assembly phase of the new prototype of the electric brake was very significant. In this stage, the parts were fitted and mounted. The new functionality of new type prototype was checked and the designing was verified. If there were some mounting problems this was proper time to correct the dimensions and exchange parts. Sometimes the materials or even or heat treatment of some part were exchanged. In that kind of prototype, it was really important to check electric parts like motors during the load. The most important issue was to find the best solution. The motors weight should have been as small as possible and the nominal torque should have been enough for normal working of prototype. In the initial tests of individual components, the real parameters were tested and possibility of using the parts was checked too. During designing phase, the parameters were defined and the tests results gave the answers for the possibility of real working on the object. The most important parameters there were the motors parameters and the possibility of mechanism force transmission.

Słowa kluczowe

EN

assembly; electric brake; prototype; mounting; new designing

• 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: 2018
• Tom: Vol. 25, No. 3
• Strony: 213--218
• Opis fizyczny: Bibliogr. 4 poz., rys.

Twórcy

autor

Grygorcewicz P.

• Institute of Aviation Krakowska Av. 110/114, 02-256 Warszawa, 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., Skorupka, Z., Wybrane zagadnienia projektowania hamulców, Autobusy, 3, 2013.
• [3] Grygorcewicz, P., Skorupka, Z., Badanie laboratoryjne hamulców ciernych w laboratorium badań podwozi lotniczych, TTS Technika Transportu Szynowego, 2013.
• [4] Skorupka, Z., Kajka, R., Kowalski, W., Armoured vehicles brakes tests, Journal of KONES, 2011.

Uwagi

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