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ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI

Year 2017, Volume: 6 Issue: 2, 700 - 709, 31.07.2017
https://doi.org/10.28948/ngumuh.341863

Abstract

   Bu
çalışmada; orta menzilli bir uçağın (Airbus 320) uçuş rotası tırmanma, düz uçuş
ve alçalma olarak üç safhaya ayrılarak uçağın dinamik yörünge profili
oluşturulmuştur. Her bir uçuş safhası için BADA (Base of Aircraft Database)
verileri kullanılarak matematiksel yakıt modeli geliştirilmiştir. Aynı orta
menzilli uçağın, iki farklı tarifeli uçuş rotasına ait uçuş bilgileri analiz
edilmiştir. Bu kapsamda planlanan uçuş mesafesi ve gerçek uçuş mesafesi
arasındaki fark hesaplanmış ve bu farkın maksimum (fmax), minimum (fmin)  ve ortalama (fort) değerlerine
karşılık gelen rotalar için yakıt tüketim hesabı tüm uçuş safhaları için
hesaplanarak elde edilen yakıt tüketimi, farklı rotalardaki aynı tip uçak için
karşılaştırılmıştır.

References

  • [1] CAO, Y., KOTEGAWA, T., SUN, D., DELAURENTIS, D., POST, J., “Evaluation of Continuous Descent Approach as a Standard Terminal Airspace Operation”, Ninth USA/Europe Air Traffic Management Research and Development Seminar, Berlin, Germany, 2011.
  • [2] PINKERTON, S., “Arrival Procedures-From Standard to Tailored Arrivals”, LAX /Community Noise Roundable, Recap of the Regular Meeting, 2013.
  • [3] SAHIN, O., USANMAZ, O., “A New Standard Instrument Arrival: The Point Merge System”, Aircraft Engineering and Aerospace Technology: An International Journal, 85, 136–143, 2013.
  • [4] SAHIN, O., “Etkileşimli Havaalanları için Geliş Yolu Önerisi”, Havacılık ve Uzay Teknolojileri Dergisi, 8, 19-26, 2015.
  • [5] ROBINSON J.E., KAMGARPOUR, M., “Benefits of Continuous Descent Operations in High-Density Terminal Airspace Under Scheduling Constraints”, 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, Fort Worth, Texas, 2010.
  • [6] TURGUT, E.T., USANMAZ, O., CANARSLANLAR, A.O., SAHIN, O., “Energy and Emission Assessments of Continuous Descent Approach”, Aircraft Engineering and Aerospace Technology: An International Journal, 82, 32–38, 2010.
  • [7] SAHIN, O., TURAN, O., “Evaluation of Aircraft Descent Profile”, Energy Procedia, 95, 308-313, 2016.
  • [8] COLLINS, B., “Estimation of Aircraft Fuel Consumption,” Journal of Aircraft, 19, 969–975, 1982.
  • [9] TRANI, A., WING-HO, F., SCHILLING, G., BAIK, H., SESHADRI, A., “A Neural Network Model to Estimate Aircraft Fuel Consumption”, 4th AIAA Aviation Technology, Integration and Operations (ATIO) Forum, Chicago, USA, 20–22, 2004.
  • [10] PATTERSON, J., NOEL, G., SENZIG, D., ROOF, C., AND FLEMING, G., “Analysis of ICAO Departure Profile Using Real-Time Cockpit Flight Data Recorder Information,” Transportation Research Board 87th Annual Meeting, 1823-1840, 2008.
  • [11] SENZIG, D.A., FLEMING G.G., “Modeling of Terminal Area Airplane Fuel Consumption”, Journal of Aircraft, 46, 1089-1093, 2009.
  • [12] https://www.faa.gov/about/office_org/headquarters_offices/apl/research/models/sage/media/FAA-EE-2005-03_SAGE-Validation.pdf (erişim tarihi 12.10.2016).
  • [13] LEE, J., WAITZ, I., KIM, B., FLEMING, G., MAURICE, L., HOLSCLAW, C., “System for Assessing Aviation’s Global Emissions (SAGE), Part 2:Uncertainty Assessment”, Transportation Research Part D: Transport and Environment, 12, 381–395, 2007.
  • [14] HILL, P., and PETERSEN, C., Mechanics and Thermodynamics of Propulsion, (2nd ed.), Addison-Wesley, Reading, MA, 1992.
  • [15] http://flightaware.com/ (erişim tarihi 07.10.2016).

MODELING OF FUEL CONSUMPTION FOR A MEDIUM RANGE AIRCRAFT

Year 2017, Volume: 6 Issue: 2, 700 - 709, 31.07.2017
https://doi.org/10.28948/ngumuh.341863

Abstract

   In this
study, the flight path for a medium-range aircraft (A320) is analyzed in three
phases as climb, cruise, descent and a dynamic trajectory flight is performed.
A mathematical fuel consumption model based on Base of Aircraft Database (BADA)
for each flight phase is developed. Flight path data belong to two different
scheduled flight operations are examined. The deviation of actual flight
distance from scheduled ones are calculated, then the fuel consumption models
are improved for routes corresponding to maximum (fmax), minimum (fmin)
and average (fort) value of deviations. The fuel consumption is
calculated for these specific routes. Finally, the fuel consumption is compared
for medium range aircraft flying different routes.

References

  • [1] CAO, Y., KOTEGAWA, T., SUN, D., DELAURENTIS, D., POST, J., “Evaluation of Continuous Descent Approach as a Standard Terminal Airspace Operation”, Ninth USA/Europe Air Traffic Management Research and Development Seminar, Berlin, Germany, 2011.
  • [2] PINKERTON, S., “Arrival Procedures-From Standard to Tailored Arrivals”, LAX /Community Noise Roundable, Recap of the Regular Meeting, 2013.
  • [3] SAHIN, O., USANMAZ, O., “A New Standard Instrument Arrival: The Point Merge System”, Aircraft Engineering and Aerospace Technology: An International Journal, 85, 136–143, 2013.
  • [4] SAHIN, O., “Etkileşimli Havaalanları için Geliş Yolu Önerisi”, Havacılık ve Uzay Teknolojileri Dergisi, 8, 19-26, 2015.
  • [5] ROBINSON J.E., KAMGARPOUR, M., “Benefits of Continuous Descent Operations in High-Density Terminal Airspace Under Scheduling Constraints”, 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, Fort Worth, Texas, 2010.
  • [6] TURGUT, E.T., USANMAZ, O., CANARSLANLAR, A.O., SAHIN, O., “Energy and Emission Assessments of Continuous Descent Approach”, Aircraft Engineering and Aerospace Technology: An International Journal, 82, 32–38, 2010.
  • [7] SAHIN, O., TURAN, O., “Evaluation of Aircraft Descent Profile”, Energy Procedia, 95, 308-313, 2016.
  • [8] COLLINS, B., “Estimation of Aircraft Fuel Consumption,” Journal of Aircraft, 19, 969–975, 1982.
  • [9] TRANI, A., WING-HO, F., SCHILLING, G., BAIK, H., SESHADRI, A., “A Neural Network Model to Estimate Aircraft Fuel Consumption”, 4th AIAA Aviation Technology, Integration and Operations (ATIO) Forum, Chicago, USA, 20–22, 2004.
  • [10] PATTERSON, J., NOEL, G., SENZIG, D., ROOF, C., AND FLEMING, G., “Analysis of ICAO Departure Profile Using Real-Time Cockpit Flight Data Recorder Information,” Transportation Research Board 87th Annual Meeting, 1823-1840, 2008.
  • [11] SENZIG, D.A., FLEMING G.G., “Modeling of Terminal Area Airplane Fuel Consumption”, Journal of Aircraft, 46, 1089-1093, 2009.
  • [12] https://www.faa.gov/about/office_org/headquarters_offices/apl/research/models/sage/media/FAA-EE-2005-03_SAGE-Validation.pdf (erişim tarihi 12.10.2016).
  • [13] LEE, J., WAITZ, I., KIM, B., FLEMING, G., MAURICE, L., HOLSCLAW, C., “System for Assessing Aviation’s Global Emissions (SAGE), Part 2:Uncertainty Assessment”, Transportation Research Part D: Transport and Environment, 12, 381–395, 2007.
  • [14] HILL, P., and PETERSEN, C., Mechanics and Thermodynamics of Propulsion, (2nd ed.), Addison-Wesley, Reading, MA, 1992.
  • [15] http://flightaware.com/ (erişim tarihi 07.10.2016).
There are 15 citations in total.

Details

Subjects Mechanical Engineering
Journal Section Mechanical Engineering
Authors

Özlem Şahin 0000-0002-9632-5533

Charkaz Aghayeva This is me 0000-0003-0507-9785

Publication Date July 31, 2017
Submission Date November 24, 2016
Acceptance Date April 5, 2017
Published in Issue Year 2017 Volume: 6 Issue: 2

Cite

APA Şahin, Ö., & Aghayeva, C. (2017). ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi, 6(2), 700-709. https://doi.org/10.28948/ngumuh.341863
AMA Şahin Ö, Aghayeva C. ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI. NOHU J. Eng. Sci. July 2017;6(2):700-709. doi:10.28948/ngumuh.341863
Chicago Şahin, Özlem, and Charkaz Aghayeva. “ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI”. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi 6, no. 2 (July 2017): 700-709. https://doi.org/10.28948/ngumuh.341863.
EndNote Şahin Ö, Aghayeva C (July 1, 2017) ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi 6 2 700–709.
IEEE Ö. Şahin and C. Aghayeva, “ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI”, NOHU J. Eng. Sci., vol. 6, no. 2, pp. 700–709, 2017, doi: 10.28948/ngumuh.341863.
ISNAD Şahin, Özlem - Aghayeva, Charkaz. “ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI”. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi 6/2 (July 2017), 700-709. https://doi.org/10.28948/ngumuh.341863.
JAMA Şahin Ö, Aghayeva C. ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI. NOHU J. Eng. Sci. 2017;6:700–709.
MLA Şahin, Özlem and Charkaz Aghayeva. “ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI”. Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi, vol. 6, no. 2, 2017, pp. 700-9, doi:10.28948/ngumuh.341863.
Vancouver Şahin Ö, Aghayeva C. ORTA MENZİLLİ BİR UÇAK İÇİN YAKIT MODELİNİN OLUŞTURULMASI. NOHU J. Eng. Sci. 2017;6(2):700-9.

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