Jet aircraft data acquisition systems

• Autorzy: Rojewski A. , Bartoszewicz J.

Identyfikatory

DOI

10.5604/01.3001.0012.2486

• Języki publikacji: EN

Abstrakty

EN

The article presents systems, which record parameters of flight in modern aircraft F-16, which was delivered to Polish Airforce in 2006. With the current level of technical development of the aviation industry, data acquisition systems are an important element of all aircrafts. These systems are responsible for the flight safety, allow reading and storing the most important flight parameters, and combined with digital control and safety systems allow to counteract dangerous situations, which especially can happen often in the case of military aircraft such as the F-16 due to their combat purpose. Systems records basics parameters of plane and engine, as specific fuel consumption or height of flight provides video and audio recording, and aerial combat assistance. These systems record even failures of a braking system during landing. Thanks to modern technology, and devices like those described in this article, F-16 is one of the best fighters in the world. The amount of data provided by analogue and digital sensors is so large that it requires the partitioning of parameters and use of several basic recorders of the entire system is the unit called DAU, or Data Acquisition Unit, which records the most important flight parameters, such as flight time, engine speed, or altitude.

Słowa kluczowe

EN

aircraft; safety; jet engine; aviation

PL

samolot; bezpieczeństwo; silnik odrzutowy; lotnictwo

• 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. 1
• Strony: 333--338
• Opis fizyczny: Bibliogr. 7 poz., rys.

Twórcy

autor

Rojewski A.

• Poznan University of Technology, Chair of Thermal Engineering Piotrowo Street 30, 61-138 Poznan, Poland tel.: [phone]

autor

Bartoszewicz J.

• Poznan University of Technology, Chair of Thermal Engineering Piotrowo Street 30, 61-138 Poznan, Poland tel.: [phone]

Bibliografia

• [1] Bartoszewicz, J., Kłosowiak, R., Bogusławski, L., The analysis of the flow structure in a jet at variable geometry of the reverse chamber, International Journal of Heat and Mass Transfer, Vol. 55, 11, pp. 3239-3245, 2012.
• [2] GE Aviation, GE Aviation’s Data Aquisition System: the next generation data and recording system, Grand Rapids, https://www.geaviation.com/sites/default/files/DAS-datasheet.pdf.
• [3] Jójka, J., Ślefarski, R., Dimensionally reduced modeling of nitric oxide formation for premixed methane-air flames with ammonia content, Fuel, Vol. 217, pp. 98-105, 2018.
• [4] Satkowski, W., Gospodarka materiałami niebezpiecznymi w bazach lotnictwa wojskowego w zmiennych warunkach działania, rozprawa doktorska, Politechnika Poznańska, Poznan 2016.
• [5] Trelka, M., Monitorowanie uszkodzeń zespołu napędowego w zmiennych warunkach działania samolotu MiG-29, rozprawa doktorska, Politechnika Poznańska, Poznan 2016.
• [6] Urbaniak, R., Bartoszewicz, J., Kłosowiak, R., Main causes of NOx emissions by low-power boilers, Polish Journal of Enviromental Studies, Vol. 24, 5, pp. 2223-2230, 2015.
• [7] http://www.poznan.pl/mim/info/news/60-lecie-polskich-skrzydel-na-krzesinach,73293.html, access 12.10.2017

Uwagi

PL

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