Design Method for Pressurised and Non-Pressurised Tail Cargo Door’s Fairings Compartment in Transport Category Aircraft

• Autorzy: Grebenikov Oleksandr , Humennyi Andrii , Loginov Vasyl , Dveirin Olexandr , Konyshev Dmytro

Identyfikatory

DOI

10.2478/tar-2023-0017

• Języki publikacji: EN

Abstrakty

EN

The method for determining the main parameters of the tail cargo doors of transport category aircrafts is developed. A methodology for the ascertainment of these parameters has been described. An example based on an existing transport aircraft is considered. Gathered were information pertaining to the necessary design, operational and regulatory parameters and requirements of the international regulatory organisations Federal Aviation regulations (FAR), Certification Specification (CS) and Aviation Regulations (AR). The principle of determining the dimensions of the cargo compartment, cargo floor and the hitting platforms, in the form of a ramp with a pressure door and ladders, is presented based on the initial data. Considering the described loading and unloading, as well as landing, operations, the dependence of the ramp length on the length of the cargo floor is ascertained. A method for designing a cargo door fairings in the transport category aircraft fuselage tail part is presented. The main features of the fairings compartment have been determined, together with those of its main components and their varieties, depending on the scheme of the cargo door. Information is provided on the fairings compartment structural elements parameters selection.

Słowa kluczowe

EN

fairings compartment; pressurised fairing; middle fairing; side flap; drove; fairing rotation axis; closed position locks

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Transactions on Aerospace Research
• Rocznik: 2023
• Tom: Nr 3 (272)
• Strony: 55--71
• Opis fizyczny: Bibliogr. 16 poz., rys., tab.

Twórcy

autor

Grebenikov Oleksandr

• National Aerospace University “Kharkiv Aviation Institute”, 17 Chkalov Str., 61070 Kharkiv, Ukraine

• https://orcid.org/0000-0002-1509-0665

autor

Humennyi Andrii

• National Aerospace University “Kharkiv Aviation Institute”, 17 Chkalov Str., 61070 Kharkiv, Ukraine

• https://orcid.org/0000-0003-1020-6304

autor

Loginov Vasyl

• National Aerospace University “Kharkiv Aviation Institute”, 17 Chkalov Str., 61070 Kharkiv, Ukraine

• https://orcid.org/0000-0003-4915-7407

autor

Dveirin Olexandr

• ANTONOV Company, 1 Akademika Tupoleva Str., Gostomel, 03062 Kyiv, Ukraine

• https://orcid.org/0000-0002-5231-1033

autor

Konyshev Dmytro

• ANTONOV Company, 1 Akademika Tupoleva Str., Gostomel, 03062 Kyiv, Ukraine

• https://orcid.org/0000-0002-4537-532X

Bibliografia

• [1] Kiva, D.S. and Grebenikov, A.G. Scientific Foundations of the Transport Category Aircraft Integrated Design, Part 2. SC “Antonov”, National Aerospace University “KhAI” (2014).
• [2] Lepyakhov, Y.S. Fuselage Geometric Shape Construction. ASTC “Antonov” (2012): p. 135.
• [3] Balabuev, P.V., Bychkov, S.A., Grebenikov, A.G., et al. Airplanes with Gas Turbine Engines General Design Fundamentals: Textbook: In 2 Hours, Part 1. National Aerospace University “KhAI” (2003): p. 368.
• [4] Mak, M. Airworthiness Standards for Transport Category Aircraft (AP-25) (1994): 322 p. 6.
• [5] Katyrev, I.Y., Neimark, M.S., Sheinin, V.M., et al. Design of Civil Aircraft: Theories and Methods. In: Novozhilova, G.V. (eds). Mashinostroenie, Moskov (1991): p. 534.
• [6] Dveirin, A.Z., Kostyuk, V.A., Rabichev, A.I., Balun, A.V., and Konyshev, D.S. Transport Category Aircraft Cargo Doors Types Systematization and Classification According to the Main Design Features. In: Open Information and Computer Integrated Technologies: Collection of Articles. Scientific. tr. National Aerospace University them. NOT. Zhukovsky “KhAI”. Kharkov, No. 70 (2015): pp. 33-53.
• [7] Bychkov, S.A., Dveirin, A.Z., Kostyuk, V.A., Balun, A.V., Rabichev, A.I., Konyshev, D.S., and Dolgikh, V.S. “Method of Constructing a Mathematical Model of the Transport Aircraft Fuselage Tail Section Theory.” In: Open Information and Computer Integrated Technologies: Collection of Articles. Scientific. tr. National Aerospace University them. NOT. Zhukovsky “KhAI”. - Kharkiv, No. 78 (2017): pp. 5-17.
• [8] Boiler, C. “Structural Health Management of Ageing Aircraft and other Infrastructure.” [Electronic resource]: Monograph on Structural Health Monitoring, Institute of Smart Structures and Systems (ISSS) (2002): p. 35. Available at: https://www.osti.gov/servlets/purl/1120418 (Accessed on 27 October 2020).
• [9] Cavallini, G. and Lazzeri, R. “A Probabilistic Approach to Fatigue Risk Assessment in Aerospace Components.” Engineering Fracture Mechanics Vol. 74 No. 18 (2007): pp. 2964-2970.
• [10] Certification Specifications and Acceptable Means of Compliance for Normal-Category Aeroplanes CS-23. EASA (2017): p. 982.
• [11] Certification Specifications and Acceptable Means of Compliance for Large Aeroplanes CS-25. EASA (2020): p. 1162.
• [12] Hendricks, W.R. “The Aloha Airlines Accident - A New Era for Aging Aircraft.” In: Atluri, S.N., Sampath, S.G., and Tong, P. (eds). Structural Integrity of aging Airplanes. Springer-Verlag, Heidelberg (1991): pp. 153-166. (Springer Series in Computational Mechanics).
• [13] Joint Service Specification Guide for Aircraft Structures (JSSG-2006). Department of Defense USA (1998): p. 497.
• [14] Torenbeek E. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes. John Wiley and Sons, Chichester (2013): p. 410.
• [15] Raymer, D.P. Aircraft Design: A Conceptual Approach. 6th ed. AIAA education Series, California (2018): p. 918.
• [16] AC 25.783-1A - Fuselage Doors and Hatches. U.S. Department of Transportation, Federal Aviation Administration.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2024).