Analysis of influence of legal requirements on the design of electronic ignition system for aviation piston engine

• Autorzy: Czarnigowski J. , Jakliński P.

Identyfikatory

DOI

10.5604/01.3001.0010.2801

• Języki publikacji: EN

Abstrakty

EN

The article is a review of European aviation regulations with respect to their impact on the design of a new electronic ignition system for aircraft engines. The analysis covers the EASA decision on certification specifications as well as recommended means of compliance and related standards on testing and designing electronic subassemblies and their programming. The analysis focuses on the following aspects: design requirements (system configuration), functional requirements (principles of operation), safety (fault tolerance), material requirements (with regard to corrosion and fire resistance of electronic components) and scope of tests for particular component. The analysis is illustrated by a case of a research and development project to design and implement an ignition system for a piston engine. The engine with its new ignition system was to be offered commercially as a product of a Polish aircraft engine manufacturer. The article is a review of European aviation regulations with respect to their impact on the design of a new electronic ignition system for aircraft engines. The analysis covers the EASA decision on certification specifications and their programming. It is illustrated by a case of a particular engine re-engineering project.

Słowa kluczowe

EN

transport; road transport; simulation; combustion engine; air pollution; environmental protection

PL

transport; transport drogowy; symulacja; silnik spalinowy; zanieczyszczenie powietrza; ochrona środowiska

• 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: 2017
• Tom: Vol. 24, No. 1
• Strony: 91--100
• Opis fizyczny: Bibliogr. 15 poz., rys.

Twórcy

autor

Czarnigowski J.

• Lublin University of Technology Department of Thermodynamics Fluid Mechanics and Aviation Propulsion Systems Nadbystrzycka 36, 20-618 Lublin, Poland tel.:+ 48 81 5384745, fax: + 48 81 5384749

autor

Jakliński P.

• Lublin University of Technology Department of Thermodynamics Fluid Mechanics and Aviation Propulsion Systems Nadbystrzycka 36, 20-618 Lublin, Poland tel.:+ 48 81 5384745, fax: + 48 81 5384749

Bibliografia

• [1] ICAO, Outlook for Air Transport to the Year 2025, Circular 313, AT/134, Montreal: International Civil Aviation Organization, 2007.
• [2] ACARE, Strategic Research & Innovation Agenda, Brussels: Advisory Council for Aeronautics Research, 2012.
• [3] ICAO, Convention on International Civil Aviation, Ninth Edition, Doc. 7300/9, Montreal: International Civil Aviation Organization, 2006.
• [4] Oster, C. V., Strong, J. S., Zorn, C. K., Analyzing aviation safety: problems, challenges, opportunities, Research in Transportation Economics, 43, 148-164, 2013.
• [5] EASA, Decision No. 2003/009/RM of the Executive Director of the European Aviation Safety Agency of 24 October 2003 on certification specifications, including airworthiness codes and acceptable means of compliance, for European Technical Standard Orders (CS-E), Cologne: European Aviation Safety Agency, with amendments, 2003.
• [6] RTCA, DO-160E Environmental Conditions and Test Procedures for Airborne Equipment, Radio Technical Commission for Aeronautics, Washington D.C. 2004.
• [7] RTCA, DO-178B Software Considerations in Airborne Systems and Equipment Certification, Radio Technical Commission for Aeronautics, Washington D.C. 1992.
• [8] RTCA, DO-254 Design Assurance Guidance for Airborne Electronic Hardware, Radio Technical Commission for Aeronautics, Washington D.C. 2000.
• [9] Polish Aviation Act, Ustawa z dnia 3 lipca 2002 r. Prawo lotnicze, t.j. Dz.U. 2013/1393, with amendments, 2013.
• [10] EASA, Commission Regulation (EC) No. 216/2008 of the European Parliament and of the Council of 20 February 2008 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency, and repealing Council Directive 91/670/EEC,Regulation (EC) No 1592/2002 and Directive 2004/36/EC, 2008 OJ L 79/1,
• [11] EASA, Commission Regulation (EC) No. 1702/2003 of 24 September 2003 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organizations, OJ L 243/6, 2003.
• [12] EASA, Commission Regulation (EC) No. 2042/2003 of 20 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks, OJ L 315/1, 2003.
• [13] Jakliński, P., Analysis of the dual control system operation during failure conditions, Eksploatacja i Niezawodność – Maintenance and Reliability, No. 3, Vol. 15, pp. 266-272, 2013.
• [14] Jakliński, P., Wendeker, M., Czarnigowski, J., Duk, M., Zyska, T., Klimkiewicz, J., The Comparison of the Operating Parameters in an Aircraft Radial Piston Engine Fuelled by 100LL and ES95 Gasoline, PTNSS-2009-SS1-C064 Combustion Engines Silniki Spalinowe No. 1, pp. 52-59, 2009.
• [15] Czarnigowski, J., Jakliński, P., Wendeker, M., Fuelling of aircraft radial piston engines by ES95 and 100LL gasoline, Fuel 89, 3568-3578, 2010.

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).