PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Investigations of the temperature distribution in the exhaust system of an aircraft piston engine

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Ultralight aviation is based on piston engines requiring both performance and reliability. An important aspect is also the requirements for the installation of such an engine on an airframe, especially its heat emission. This is firstly because of the need to ensure proper engine cooling and secondly because composite elements of the airframe skin are not exposed to excessive overheating. For this purpose, bench tests of the temperature distribution of the exhaust system of ROTAX 912 engine were carried out. Measurements were taken at 6 points of the exhaust system, where the temperature of the exhaust gases and exhaust pipes were measured. The tests covered a wide range of engine operation. The paper presents the temperature distribution at selected points in relation to the engine speed and load.
Czasopismo
Rocznik
Strony
12--18
Opis fizyczny
Bibliogr. 9 poz., fot. kolor., wykr.
Twórcy
  • Faculty of Mechanical Engineering, Lublin University of Technology
  • Faculty of Mechanical Engineering, Lublin University of Technology
  • Faculty of Mechanical Engineering, Lublin University of Technology
Bibliografia
  • [1] CZARNIGOWSKI, J., SKIBA, K. Electric energy balance of the ROTAX 912 with fuel injection. Journal of KONES Powertrain and Transport. 2017, 24(1). DOI: 10.5604/01.3001.0010.2834.
  • [2] KANG, G.-W., HU, Y., LI, Y.-D., JIANG, W.-H. Parameters matching of ultralight electric aircraft propulsion system. Hangkong Dongli Xuebao/Journal of Aerospace Power. 2013, 28(12), 2641-2646. www.scopus.com/inward/record.uri?eid=2-s2.0-84891890860&partnerID=40&md5= b9e3dab95eb862a2441425fefd7848bc
  • [3] STOCKHOLM, J.G. Applications in thermoelectricity. Materials Today: Proceedings. 2018, 5(4), 1, 10257-10276, DOI:10.1016/j.matpr.2017.12.273.
  • [4] TOMAŽIČ, J., TOMAŽIČ, T., ŽEMVA, A. Battery-cell balancing in electric-powered ultralight aircraft [Napetostno izenačevanje akumulatorjev v ultralahkih letalih na električni pogon]. Elektrotehniski Vestnik/Electrotechnical Review. 2010, 77(4), 188-193, www.scopus.com/inward/record.uri?eid=2-s2.0-79551613076&partnerID=40&md5= 6d7e93c2b8b848245c2bde2a25aa311e
  • [5] ZHU, Q., FORSYTH, A., TODD, R. Investigation of hybrid electric aircraft operation on battery degradation. 2018 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference. ESARSITEC 2018, art. 8607617, 2019. www.scopus.com/inward/record.uri?eid=2-s2.0-85062082639&doi=10.1109%2fESA RSITEC.2018.8607617&partnerID=40&md5=67fc1d4b18d 7bb37a139a17c9d0d0d7e
  • [6] 2015 General Aviation Statistical Databook & 2016 Industry Outlook General Aviation Manufacturers Association.
  • [7] European Aviation Safety Agency. Certification Specifications for Very Light Aeroplanes CS-VLA. ED Decision 2009/003/R.
  • [8] Light Aircraft Global Market Growth, CAGR, Trend Status and Forecast 2018- 2025. ReportHive 2018.
  • [9] Regulatory Options for the European Light Aircraft (ELA1) Phase 3 FINAL REPORT”. november 2010 EASA.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-800e1745-b848-43fa-9de4-bfc5cbeaa5c7
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.