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Behrendt, Thomas and Hackemann, Stefan and Mechnich, Peter and Shi, Yuan and Hönig, Sandrine and Hofmann, Severin and Koch, Dietmar (2017) Development and Test of Oxide/Oxide Ceramic Matrix Composites Combustor Liner Demonstrators for Aero-engines. Journal of Engineering for Gas Turbines and Power, 139 (3), GTP-16. American Society of Mechanical Engineers (ASME). doi: 10.1115/1.4034515. ISSN 0742-4795.
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Official URL: http://gasturbinespower.asmedigitalcollection.asme.org/article.aspx?articleID=2546912
Abstract
Ceramic matrix composites (CMC) offer the potential of increased service temperatures and are thus an interesting alternative to conventional combustor alloys. Tubular combustor liner demonstrators made of an oxide/oxide CMC were developed for a lean combustor in a future aero-engine in the medium thrust range and tested at engine conditions. During the design various aspects like protective coating, thermo-mechanical design, development of a failure model for the CMC as well as design and test of an attachment system were taken into account. The tests of the two liners were conducted at conditions up to 80% take-off. A new protective coating was tested successfully with a coating thickness of up to t=1 mm. Different inspection criteria were derived in order to detect crack initiation at an early stage for a validation of the failure model. With the help of detailed pre- and post-test computer tomography scans to account for the micro structure of the CMC the findings of the failure model were in reasonable agreement with the test results.
| Item URL in elib: | https://elib.dlr.de/106667/ | ||||||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||||||
| Title: | Development and Test of Oxide/Oxide Ceramic Matrix Composites Combustor Liner Demonstrators for Aero-engines | ||||||||||||||||||||||||
| Authors: |
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| Date: | 1 March 2017 | ||||||||||||||||||||||||
| Journal or Publication Title: | Journal of Engineering for Gas Turbines and Power | ||||||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||||||
| Volume: | 139 | ||||||||||||||||||||||||
| DOI: | 10.1115/1.4034515 | ||||||||||||||||||||||||
| Page Range: | GTP-16 | ||||||||||||||||||||||||
| Publisher: | American Society of Mechanical Engineers (ASME) | ||||||||||||||||||||||||
| ISSN: | 0742-4795 | ||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||
| Keywords: | Ceramic matrix composites, protective coating, combustor liner design, attachment system, combustor testing, computer tomography, failure model | ||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||
| HGF - Program Themes: | propulsion systems | ||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||
| DLR - Program: | L ER - Engine Research | ||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Combustion Chamber Technologies (old) | ||||||||||||||||||||||||
| Location: | Köln-Porz , Stuttgart | ||||||||||||||||||||||||
| Institutes and Institutions: | Institute of Propulsion Technology > Combustor Institute of Structures and Design > Ceramic Composite Structures Institute of Materials Research > Structural and Functional ceramics Institute of Materials Research > Experimental and Numerical Methods | ||||||||||||||||||||||||
| Deposited By: | Behrendt, Dr.-Ing. Thomas | ||||||||||||||||||||||||
| Deposited On: | 02 Nov 2016 09:56 | ||||||||||||||||||||||||
| Last Modified: | 28 Mar 2023 23:46 |
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- Development and Test of Oxide/Oxide Ceramic Matrix Composites Combustor Liner Demonstrators for Aero-engines. (deposited 02 Nov 2016 09:56) [Currently Displayed]
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