Identyfikatory
Warianty tytułu
Języki publikacji
Abstrakty
The multirole F-16 is the most advanced aircraft in the Polish Air Forces. It has been equipped with the very modern, sophisticated and advanced turbofan engine F100-PW-229. Due to the fact, that there is only one engine, its reliability, durability, efficiency and performance are the crucial factors for the safety reasons. In the article author researched maintenance system of the F100 turbofan engines, to describe Engine Monitoring System features. Engine Monitoring System (EMS) is the key element in the engine prognostic and health monitoring. The EMS provides engine fault indicators to the pilots and technicians and with the engine performance trending affects the F-16 flight safety risk and enhanced engine maintenance management concept. The main goal of this article was to provide information on the F-16 Engine Monitoring System and its impact on the aircraft airworthiness and F-16 fleet readiness resulting from the engine reliability. It is also an introduction to the F-16 Engine Health Management concept.
Czasopismo
Rocznik
Tom
Strony
23--35
Opis fizyczny
Bibliogr. 12 poz., il. kolor., fot.
Twórcy
Bibliografia
- [1] Lockheed Martin STM 16-329PL (Poland Block 52) F100-PW-229 Power Plant.
- [2] F100 Pratt&Whitney F100 WUC, October 2018.
- [3] F100-PW-229 Periodic Engineering Excellence Reviev.
- [4] Lockheed Martin Aero Flight Safety, Operations and Maintenance, June 2018.
- [5] International Engine Management Program, October 2018.
- [6] Technical Manual T.O.00-20-1 Aerospace Equipment Maintenance Inspections, Documentation, Policies and procedures.
- [7] F100 Pratt&Whitney F100 WUC, October 2018.
- [8] Technical Manual General System Organizational Maintenance Power Plant Model F100-PW-229 Technical Order PL1F-16CJ-2-70GS-00-21.
- [9] Engine Management and Tracking System EMATS Maintenix
- [10] F100-PW-229 Engine Interactive Electronic Technical Manuals.
- [11] Technical Manual Maintenance Instructions Intermediate Level Introduction and General Information Aircraft Engine F100-PW-229 Technical Order 2J-F100-56-1.
- [12] Technical Manual Fault Isolation Organizational Maintenance Power Plant Model F100-PW-229 Technical Order PL1F-16CJ-2-70FI-00-21.
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-36cfb16f-3a12-465c-9dc6-2bb57b71f017