Добірка наукової літератури з теми "Composite aircraft joints"
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Статті в журналах з теми "Composite aircraft joints"
Maier, Raluca. "Study on Increasing Performances of Hybrid Composite Through Pull Out Compression Test Assessement." Materiale Plastice 57, no. 1 (April 17, 2020): 329–35. http://dx.doi.org/10.37358/mp.20.1.5325.
Повний текст джерелаChowdhury, Nabil, Wing Kong Chiu, and John Wang. "Review on the Fatigue of Composite Hybrid Joints Used in Aircraft Structures." Advanced Materials Research 891-892 (March 2014): 1591–96. http://dx.doi.org/10.4028/www.scientific.net/amr.891-892.1591.
Повний текст джерелаFortier, Vincent, Jean-E. Brunel, and Louis L Lebel. "Fastening composite structures using braided thermoplastic composite rivets." Journal of Composite Materials 54, no. 6 (August 14, 2019): 801–12. http://dx.doi.org/10.1177/0021998319867375.
Повний текст джерелаRomano, Maria Grazia, Michele Guida, Francesco Marulo, Michela Giugliano Auricchio, and Salvatore Russo. "Characterization of Adhesives Bonding in Aircraft Structures." Materials 13, no. 21 (October 28, 2020): 4816. http://dx.doi.org/10.3390/ma13214816.
Повний текст джерелаRufin, Antonio C., and Robert L. Jochum. "Fatigue Analysis and Design of Composite-Metal Joints in Primary Aircraft Structures." Advanced Materials Research 891-892 (March 2014): 588–93. http://dx.doi.org/10.4028/www.scientific.net/amr.891-892.588.
Повний текст джерелаMcCarthy, Michael. "BOJCAS: bolted joints in composite aircraft structures." Air & Space Europe 3, no. 3-4 (May 2001): 139–42. http://dx.doi.org/10.1016/s1290-0958(01)90077-2.
Повний текст джерелаChernov, Andrey, Danil Fomin, Ivan Kondakov, Ivan Mareskin, and Alexander Shanygin. "Lightweight and reliable metal–composite joints based on harmonization of strength properties of joined parts." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 14 (May 24, 2018): 2663–72. http://dx.doi.org/10.1177/0954410018778797.
Повний текст джерелаBalinova, Yu A., D. V. Graschenkov, A. A. Shavnev, V. G. Babashov, A. S. Chaynikova, E. I. Kurbatkina, and A. N. Bolshakov. "High-temperature heat-shielding, ceramic and ceramic-metal composite materials for new-generation aviation equipment." Journal of «Almaz – Antey» Air and Defence Corporation, no. 2 (July 19, 2020): 83–92. http://dx.doi.org/10.38013/2542-0542-2020-2-83-92.
Повний текст джерелаJadee, Khudhayer J., and A. R. Othman. "Fiber Reinforced Composite Structure with Bolted Joint – A Review." Key Engineering Materials 471-472 (February 2011): 939–44. http://dx.doi.org/10.4028/www.scientific.net/kem.471-472.939.
Повний текст джерелаHart-Smith, L. J. "An Engineer'S Viewpoint on Design and Analysis of Aircraft Structural Joints." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 209, no. 2 (April 1995): 105–29. http://dx.doi.org/10.1243/pime_proc_1995_209_278_02.
Повний текст джерелаДисертації з теми "Composite aircraft joints"
Evans, Simon. "Characterisation of outgassing from carbon fibre composite aircraft joints subjected to lightning current." Thesis, Cardiff University, 2018. http://orca.cf.ac.uk/117887/.
Повний текст джерелаKapidzic, Zlatan. "Static and Fatigue Failure of Bolted Joints in Hybrid Composite-Aluminium Aircraft Structures." Doctoral thesis, Linköpings universitet, Mekanik och hållfasthetslära, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-122349.
Повний текст джерелаMarengo, Giovanni. "The use of unidirectional carbon fibre rods in high loaded joints for a composite large civil aircraft wing structure." Thesis, Cranfield University, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.393700.
Повний текст джерелаHarman, Alex Bruce Mechanical & Manufacturing Engineering Faculty of Engineering UNSW. "Optimisation and improvement of the design of scarf repairs to aircraft." Awarded by:University of New South Wales. School of Mechanical and Manufacturing Engineering, 2006. http://handle.unsw.edu.au/1959.4/26788.
Повний текст джерелаRenart, Canalias Jordi. "Desarrollo de un nuevo ensayo experimental para la evaluación de la calidad de uniones adhesivas entre componentes estructurales de composite para la indústria aeronáutica." Doctoral thesis, Universitat de Girona, 2010. http://hdl.handle.net/10803/296679.
Повний текст джерелаThe use of composite materials in the aircraft industry has been increasing in recent years due to their application in structural parts. To reduce the production costs of these components the join between skins and stiffeners is made by means of an adhesive. In order to guarantee that the bonded joint fulfils the structural requirements, experimental tests on specimens are done from the first development tasks and throughout the production stages. In the present work, an analysis of the experimental test methods to determine the quality of bonded joints has been performed - the quality of bonded joints depends on the quality of the surface preparation, the adhesive properties and the compatibility between the adhesive and the adherents. The work focuses on two objectives: the improvement of the double cantilever beam test, and the development of an alternative method of bonded joint characterization based on driving a wedge into the adhesive layer (Wedge Driven Test, WDT). In the double cantilever beam test, a mechanical fixture tool has been designed and a data reduction method for stick-slip crack propagation has been developed. On the other hand, the alternative test method such as the DCB, focuses on determining the fracture toughness in mode I of the adhesive joint, by means of introducing a wedge inside the specimen at a constant speed rate. To prove the sensitivity of the WDT to the quality of the adhesive joint, a series of testing campaigns has been performed over 4 adhesive joint configurations (combining 2 adhesives and 2 adherents). Moreover, deliberately produced bad surface preparations have been tested. From the test results, it has been observed that the driven wedge test exhibits an equivalent behaviour to the double cantilever beam test and has a similar level of sensitivity to the quality of the bonded joint.
Книги з теми "Composite aircraft joints"
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Critical joints in large composite primary aircraft structures. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.
Знайти повний текст джерелаCritical joints in large composite primary aircraft structures. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.
Знайти повний текст джерелаCritical joints in large composite primary aircraft structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаL, Sagui R., and Langley Research Center, eds. Critical joints in large composite primary aircraft structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаЧастини книг з теми "Composite aircraft joints"
Noeske, Michael, Welchy Leite Cavalcanti, Hauke Brüning, Bernd Mayer, Antonios Stamopoulos, Apostolos Chamos, Thomas Krousarlis, et al. "Introduction to Recent Advances in Quality Assessment for Adhesive Bonding Technology." In Adhesive Bonding of Aircraft Composite Structures, 1–50. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_1.
Повний текст джерелаTserpes, Konstantinos, Elli Moutsompegka, Mareike Schlag, Kai Brune, Christian Tornow, Ana Reguero Simón, and Romain Ecault. "Characterization of Pre-bond Contamination and Aging Effects for CFRP Bonded Joints Using Reference Laboratory Methods, Mechanical Tests, and Numerical Simulation." In Adhesive Bonding of Aircraft Composite Structures, 51–117. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_2.
Повний текст джерелаMalinowski, Paweł H., Tomasz Wandowski, Wiesław M. Ostachowicz, Maxime Sagnard, Laurent Berthe, Romain Ecault, Igor Solodov, Damien Segur, and Marc Kreutzbruck. "Extended Non-destructive Testing for the Bondline Quality Assessment of Aircraft Composite Structures." In Adhesive Bonding of Aircraft Composite Structures, 223–57. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_4.
Повний текст джерелаLeite Cavalcanti, Welchy, Elli Moutsompegka, Konstantinos Tserpes, Paweł H. Malinowski, Wiesław M. Ostachowicz, Romain Ecault, Neele Grundmann, et al. "Integrating Extended Non-destructive Testing in the Life Cycle Management of Bonded Products—Some Perspectives." In Adhesive Bonding of Aircraft Composite Structures, 331–50. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_6.
Повний текст джерелаVallejo, Nabil, L. A. Reyes, G. M. Hernández-Muñoz, and P. Zambrano-Robledo. "Parametric Effects in Hybrid Lap Joints of Composite Materials Used in Aircraft Structures." In Proceedings of the Symposium of Aeronautical and Aerospace Processes, Materials and Industrial Applications, 129–39. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-65611-3_12.
Повний текст джерелаFaisal, Nadimul, Ömer Necati Cora, Muhammed Latif Bekci, Romana Ewa Śliwa, Yehuda Sternberg, Shashank Pant, Richard Degenhardt, and Anil Prathuru. "Defect Types." In Structural Health Monitoring Damage Detection Systems for Aerospace, 15–72. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-72192-3_3.
Повний текст джерелаUeda, Y., H. Kuroki, T. Murooka, A. Tanaka, K. Miyazawa, I. Okumura, Y. Shigenari, K. Oikawa, and H. Morita. "Damage Tolerance Demonstration of Flange Joint for Aircraft Engine Composite Fan Case." In ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives, 207–18. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-1664-3_17.
Повний текст джерелаCHALKLEY, P., C. WANG, and A. BAKER. "Fatigue Testing of Generic Bonded Joints." In Advances in the Bonded Composite Repair of Metallic Aircraft Structure, 103–26. Elsevier, 2002. http://dx.doi.org/10.1016/b978-008042699-0/50007-3.
Повний текст джерелаMolent, Lorrie, and Rhys Jones. "The F111C Wing Pivot Fitting Repair and its Implications for the Design/Assessment of Bonded Joints and Composite Repairs." In Aircraft Sustainment and Repair, 511–43. Elsevier, 2018. http://dx.doi.org/10.1016/b978-0-08-100540-8.00010-8.
Повний текст джерелаMelhem, George Nadim. "Aerospace Fasteners: Use in Structural Applications." In Encyclopedia of Aluminum and Its Alloys. Boca Raton: CRC Press, 2019. http://dx.doi.org/10.1201/9781351045636-140000240.
Повний текст джерелаТези доповідей конференцій з теми "Composite aircraft joints"
Evans, S. J. "Fasteners: addressing the problem of sparking composite joints." In IET Seminar on Lightning Protection for Aircraft Components. Institution of Engineering and Technology, 2013. http://dx.doi.org/10.1049/ic.2013.0175.
Повний текст джерелаPLAKA, EVGENIA, BRETT BEDNARCYK, and MARIANNA MAIARÙ. "DESIGN OF ADHESIVELY BONDED COMPOSITE JOINTS USING A RAPID DESIGN TOOL." In Proceedings for the American Society for Composites-Thirty Seventh Technical Conference. Destech Publications, Inc., 2022. http://dx.doi.org/10.12783/asc37/36492.
Повний текст джерелаBazˇant, Zdeneˇk P., Jia-Liang Le, Ferhun C. Caner, and Qiang Yu. "Size Effect on Strength of Bi-Material Joints of Steel With Fiber-Polymer Composite." In ASME 2008 International Mechanical Engineering Congress and Exposition. ASMEDC, 2008. http://dx.doi.org/10.1115/imece2008-69229.
Повний текст джерелаMahmoud, Hassan A., Mostafa Shazly, Yehia Bahei-El-Din, and Emad El-Kashif. "Analysis of Composite Bolted Connection Joints Under Out of Plane Loading." In ASME 2020 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/imece2020-23303.
Повний текст джерелаCarr, Daniel, David Clark, Chris Stone, Manu Haddad, Simon Evans, Matthew Jenkins, and Matthew Cole. "Optical Techniques For the Analysis of Outgassing of Composite Aircraft Joints Under Lightning." In 2018 34th International Conference on Lightning Protection (ICLP). IEEE, 2018. http://dx.doi.org/10.1109/iclp.2018.8503423.
Повний текст джерелаYeh, P. C., P. Y. Chang, J. M. Yang, and D. Kordonowy. "The Effect of Damage on the Bonding Strength of Hybrid T-Joint Structures." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-85924.
Повний текст джерелаLIN, WENHUA, YEQING WANG, SPENCER LAMPKIN, SRIHARI GANESH PRASAD, OLESYA ZHUPANSKA, and BARRY DAVIDSON. "BOND STRENGTH DEGRADATION OF ADHESIVE- BONDED CFRP COMPOSITE LAP JOINTS AFTER LIGHTNING STRIKE." In Thirty-sixth Technical Conference. Destech Publications, Inc., 2021. http://dx.doi.org/10.12783/asc36/35742.
Повний текст джерелаBogdanovich, Alexander E., and Sergei P. Yushanov. "Failure Prediction of Bonded Joints of Composite Engineering Structures." In ASME 1998 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/imece1998-1199.
Повний текст джерелаGrimes, Glenn C. "Building Block Approach for Composite Aircraft Structure Prototypes: Allowables and Building Block Testing for DOD/NASA Vehicles." In ASME 1998 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/imece1998-0387.
Повний текст джерелаLee, David E., and H. Thomas Hahn. "Virtual Assembly Production Analysis of Composite Aircraft Structures." In ASME 1995 15th International Computers in Engineering Conference and the ASME 1995 9th Annual Engineering Database Symposium collocated with the ASME 1995 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/cie1995-0815.
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