DAMAGE FROM CREVICE CORROSION IN AIRCRAFT DESIGNS AND THEIR DETECTION
Abstract
Presented examples of destruction of aircraft designs due to corrosion of metals under conditions of fatigue loading. It is shown that slit corrosion, which is an increase in corrosion in crevice and gaps between two metals, as well as in places of untight contact of metal with a nonmetallic material resistant to corrosion, leads to the appearance of corrosion products in the joints of the skin with the power suite, which supports it , which can lead to the swelling of some elements of the joint relative to other elements and provoke the tearing off of the heads of rivets with the further development of fatigue cracks and the destruction of aircraft structures. Shown, that visual inspection is not always effective for the detection of corrosion damage, and sometimes impossible, for example, in closed internal structures. New developments in the field of sensors and equipment for the detection of corrosive substances and corrosion damage are presented. Among them is information on the sensor (organic-ceramic composite) containing the conducting complex. When the composite is exposed to water liquids, its conductivity is lost. When the composite dries, the sensor reaches its initial values of resistance. Information is provided on the optical sensor for detecting corrosion in the construction of the airframe. This sensor is based on the remote detection of aluminum ions formed during corrosion. The development of a multi-parameter integrated sensor for assessing the structural integrity of aluminum alloys, the recording of the concentration of chloride ions, the release of hydrogen, changes in humidity and degradation of the material is presented. Information is provided on fluorescence-based optical sensors used to detect specific ions such as aluminum, indicating the beginning of corrosion of an aluminum alloy. Information is provided on the development of advanced digital X-ray methods for the detection of corrosion in the design of aircraft. The conclusion is made on the necessity of combining visual control and control with the use of means and methods for detecting corrosive substances and corrosion damage.
Keywords
Full Text:
PDF (Українська)References
Електронний ресурс. URL: http://www.corrosiondoctors.org/Aircraft/Aircraft.htm
J.F. Wildey II, "Aging Aircraft", Materials Performance, March 1990, pp.80-85.
Електронний ресурс.URL: https://sfw.so/1149033220-aloha-airlines-243-neveroyatnaya-posadkapovrezhdennogo-samoleta.html
Електронний ресурс. URL: http://www.corrosion-doctors.org/Formscrevice/pillowing2.htm
Aircraft Accident Report-Aloha Airlines, Flight 243, Boeing 737-200, N73711,near Maui, Hawaii, April 28,1988. Report Date: June 14,1989/National Transportation Safety Board Bureau of Accident investigation, Washington, D.C. 20594 – 262 pages
Електронний ресурс. URL: http://www.corrosion-doctors.org/Formscrevice/pillowing1.htm
Електронний ресурс. URL: https://en.wikipedia.org/wiki/Lockheed_CP-140_Aurora
Електронний ресурс. URL: http://www.corrosion-doctors.org/Formscrevice/rivets.htm
Електронний ресурс. URL: http://www.corrosion-doctors.org/Formscrevice/rivets2.htm
Eлектронний ресурс. URL: https://www.aviationpros.com/home/article/10381745/spotting-treating-and-preventing-corrosion
Sensors and Actuators B: Chemical Journal. Homepage www.elsevier.com/locate/snb. Liquid detection in confined aircraft structures based on lyotropic percolation thresholds/Helge Pfeiffera’*, Peter Heerb, Ioannis Pitropakisa, Gregory Pykaa, Greet Kerckhofsa, Maria Patitsaa, Martine Weversa - Katholieke Universiteit Leuven, Department of Metallurgy and Materials Engineering (MTM)
Hindawi Publishing Corporation International Journal of Aerospace Engineering Volume 2012, Article ID 684024, 11 pages doi:10.1155/2012/684024 Research Articl: Corrosion Sensor Development for Condition-Based Maintenance of Aircraft / Gino Rinaldi,1 Trisha Huber,2 Heather McIntosh,3 Les Lebrun,3 Heping Ding,3 and John Weber3. NRC Institute for Aerospace Research, National Research Council Canada, Institute for Microstructural Sciences, National Research Council Canada
Contents lists available at SciVerse ScienceDirect. Sensors and Actuators B: Chemical journal homepage www.elsevier.com/locate/snb. Optical sensors for corrosion detection in airframes/P.G. Venancioa b c, R.A. Cottisd, R. Narayanaswamye, J.C.S. Fernandesb c * a OGMA, Industrie Aeronautica de Portugal, 2615-173 Alverca, Portugal b Department of Chemical Engineering, Instituto Superior Tecnico, TULisbon, 1049-001 Lisboa, Portugal c ICEMS, Instituto Superior Tecnico, 1049-001 Lisbon, Portugal d Corrosion and Protection Centre, The University of Manchester, Manchester M13 9PL, United Kingdom e Centre for Instrumentation and Analytical Science, University of Manchester, Manchester M60 1QD, United Kingdom. Article history: Received 23 July 2012. Available online 22 March 2013
Nondestructive Testing and Evaluation, 2015. Enhanced radiographic imaging of defects in aircraft structure materials with the dehazing method/Effat Yahaghia*, Amir Movafeghib, Nooreddin Mohmmadzadehb - aDepartment of Physics, Imam Khomeini International University, Ghazvin, Iran; bNuclear Safety and Radiological Protection Department, Nuclear Science and Technology Research Institute, Tehran, Iran.
DOI: https://doi.org/10.32620/oikit.2019.83.10
Refbacks
- There are currently no refbacks.