Designing process of landing gear in 3D CAD program

• Autorzy: Grygorcewicz P.

Identyfikatory

DOI

10.5604/12314005.1216474

• Języki publikacji: EN

Abstrakty

EN

This article presents selected issues related to the design methodology of the landing gear during the construction process. The 3D modelling of the landing gear nowadays is very popular method, which simplifies the process and reduces the costs of the prototype. The author used the designing program Solid Edge ST 7. The concepts and phases of designing will be shown in this elaboration. Readers can see the problems resolved by designers and this is showing the scale of designing challenges. The landing gear consist of many parts and every of this parts needs to be design to meet the requirements of construction. Only experienced designers can effort to design landing gear because they have to acquire specific knowledge. The aim of the paper is to discuss design process from the very beginning first steps to the final version of the landing gear. All of different factors like weight, durability, resistance of the weather are taken into account when designing a prototype of the landing gear 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 article also subscribes some methods, which help designer to find the proper solution. The presented landing gear was designed by Landing Gear Laboratory team Institute of Aviation.

Słowa kluczowe

EN

transport; airplanes; designing; main landing gear; CAD

• 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: 2016
• Tom: Vol. 23, No. 3
• Strony: 165--170
• Opis fizyczny: Bibliogr. 8 poz., rys.

Twórcy

autor

Grygorcewicz P.

• Institute of Aviation Transport and Energy Conversion, Transport Systems Krakowska Avenue 110/114, 02-256 Warsaw, Poland tel.: [phone]

Bibliografia

• [1] Beitz, G. P. W., Nauka konstruowania, WNT, Warszawa 1984.
• [2] Currey, N. S., Aircraft Landing Gear Design Principles and Practices, AIAA, Washington 1988.
• [3] Dietrich, M., Podstawy konstrukcji maszyn, WNT, Warszawa 1999.
• [4] Grygorcewicz, P., Analysis of electric –drive applicability in mechanical brake for the commuter class airplane, IL, Warszawa 2013.
• [5] Jachimowicz, J., Metoda elementów skończonych, Wykłady, 2012.
• [6] Lewitowicz, J., Uncertainty and Dependability of the risk model applicable to operation of aircrafts, KONBiN, 1, 2010.
• [7] Lewitowicz, J., Kustoń, K., Podstawy eksploatacji statków powietrznych, ITWL, Warszawa 2003.
• [8] Skorupka, Z., Tywoniuk, A., Wybrane zagadnienia konstrukcji podwozia do wiatrakowca I28, IL, Warszawa 2013.

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę.