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000826737 0247_ $$2Handle$$a2128/13650
000826737 0247_ $$2ISSN$$a1866-1793
000826737 020__ $$a978-3-95806-201-6
000826737 037__ $$aFZJ-2017-00955
000826737 041__ $$aGerman
000826737 1001_ $$0P:(DE-Juel1)157996$$aKoch, Denise Silke$$b0$$eCorresponding author$$gfemale$$ufzj
000826737 245__ $$aEntwicklung selbstheilender Wärmedämmschichten$$f- 2016-07-07
000826737 260__ $$aJülich$$bForschungszentrum Jülich GmbH Zentralbibliothek, Verlag$$c2016
000826737 300__ $$aX, 120 S.
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000826737 3367_ $$02$$2EndNote$$aThesis
000826737 3367_ $$0PUB:(DE-HGF)11$$2PUB:(DE-HGF)$$aDissertation / PhD Thesis$$bphd$$mphd$$s1485432077_32145
000826737 3367_ $$2DRIVER$$adoctoralThesis
000826737 4900_ $$aSchriften des Forschungszentrums Jülich Reihe Energie & Umwelt / Energy & Environment$$v355
000826737 502__ $$aUniversität Bochum, Diss., 2016$$bDr.$$cUniversität Bochum$$d2016
000826737 520__ $$aThe presented work is dealing with the manufacturing of self-healing thermal barrier coatings by atmospheric plasma spraying that are applicable in high temperature processes with thermal loading. The turbine blades of gas turbines for example, experience thermal stresses that are induced into the thermal barrier coatings and can cause crack development. After a certain time these cracks grow and lead to a spallation of the coating. By this, the turbine blade would not be protected any more. With the integration of a self-healing process, the time between maintenances can be extended to save operational costs. The basic idea to realize such self-healing coatings is the integration of MoSi$_{2}$ as self-healing particles. The oxidation of MoSi$_{2}$ leads to the formation of SiO$_{2}$ that can infiltrate cracks and seals them. This can prevent the spallation of the coating. The presented work was performed within a project named SAMBA (self-healing thermal barrier coatings) that was funded by the European Union. The first step in the production of a self-healing thermal barrier coating was the integration of MoSi$_{2}$ particles into a coating. Yttria stabilized zirconia (YSZ) was used as coating matrix since this is the state of the art material. Due to a decomposition of the MoSi$_{2}$ when spraying it at conditions that are needed to produce coatings made out of YSZ, the manufacturing of a homogeneous mixed coating of YSZ and MoSi$_{2}$ from a powder mixture of both materials was not possible. This problem was solved by using a second injection point located at a distance from the plasma-torch-exit. Nevertheless the coatings made out of YSZ and pure MoSi$_{2}$ were not suitable to work as a self-healing thermal barrier coating due to the fact that the oxidation of MoSi$_{2}$ was not controlled. The volume expansion caused by the formation of SiO$_{2}$ induces stresses into the coating that lead to a failure and the spallation of the coating. The second step in the development was to encapsulate the MoSi$_{2}$ particles with Al$_{2}$O$_{3}$, as this encapsulation was supposed to work as a protection against a premature oxidation of the MoSi$_{2}$. As the spraying process leads to a deformation of the particles during deposition on the substrate, a pre-encapsulation of the powder would be destroyed. Because of this, the encapsulation has to be formed in-situ within the coating. Several coatings were produced using Al doped MoSi$_{2}$ to integrate it into the YSZ coatings. These coatings were heat treated and by this several requirements were determined that need to be fulfilled in order to enable the self-healing process. Coatings that have been produced using spraying parameters, that enable the fulfillment of these requirements, and these coatings resulted in an improvement of the lifetime of the coatings compared to standard YSZ coatings. Within the SAMBA project further analysis and investigations will be performed to be able to judge on the self-healing abilities of coatings produced by the procedures described in this work.
000826737 536__ $$0G:(DE-HGF)POF3-113$$a113 - Methods and Concepts for Material Development (POF3-113)$$cPOF3-113$$fPOF III$$x0
000826737 536__ $$0G:(DE-Juel1)HITEC-20170406$$aHITEC - Helmholtz Interdisciplinary Doctoral Training in Energy and Climate Research (HITEC) (HITEC-20170406)$$cHITEC-20170406$$x1
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000826737 9141_ $$y2016
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