Flap strut fairing system expluatation and critical path method use

• Autorzy: Zetliņa Sintija , Kleinhofs Martins

Identyfikatory

DOI

10.2478/tar-2024-0003

• Języki publikacji: EN

Abstrakty

EN

The flap strut fairing system is made of movable construction inside, but the outer skin is made of composite material. Each day, we can face an expensive repair for movable construction and outer skin as most of the aviation companies are dealing with mechanical issues that are not solved during a long period of time or somebody misses it due to human errors. In this abstract, we will look for options for easier and faster solutions to avoid the expensive operation process.

Słowa kluczowe

EN

composite materials; mechanical systems; cost-efficient

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Transactions on Aerospace Research
• Rocznik: 2024
• Tom: Nr 1 (274)
• Strony: 29--44
• Opis fizyczny: Bibliogr. 5 poz., rys., tab., wzory

Twórcy

autor

Zetliņa Sintija

• Institute of Aeronautics, Faculty of Mechanical Engineering, Transport and Aeronautics, Riga Technical University, 6A Kipsalas Street, Riga LV-1048, Latvia

• https://orcid.org/0000-0002-1732-5368

autor

Kleinhofs Martins

• Institute of Aeronautics, Faculty of Mechanical Engineering, Transport and Aeronautics, Riga Technical University, 6A Kipsalas Street, Riga LV-1048, Latvia

• https://orcid.org/0009-0007-8003-3601

Bibliografia

• [1] Summers HA. The application of the critical path method to aircraft maintenance [Thesis]. Vancouver: University of British Columbia; 1965. Available from: https://open.library.ubc.ca/media/stream/pdf/831/1.0102375/1
• [2] Kulkarni A., Yadav D., Nikraz H. Aircraft maintenance checks using critical chain project path. Aircr Eng Aerosp Technol. 2017;89(6):879-92. Available from: https://doi.org/10.1108/AEAT-10-2013-0186
• [3] Agyei W. Project planning and scheduling using PERT and CPM techniques with linear programming. Int J Sci Amp Technol Res. 2015;4(08):222-7. Available from: https://ethesisarchive.library.tu.ac.th/thesis/2020/TU_2020_6222040047_14097_13845.pdf
• [4] Paramonov Y., Kuznetsov A., Kleinhofs M. Reliabilty of fatigue-prone airframes and composite materials. Riga: Aviation Institute of Riga Technical University; 2011.122 p.
• [5] Airbus Portal Navigation URL. AIRBUS|Portals Login page. Available from: https://w3.airbus.com/1T40/search/Flap%20Track%203%20fairing%20seal%20replacement:AMM#HW_1

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa nr POPUL/SP/0154/2024/02 w ramach programu "Społeczna odpowiedzialność nauki II" - moduł: Popularyzacja nauki (2025)