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Technological Level of CMC Components for Stationary Gas Turbines and Aero-Engines

Wehrel, Patrick (2022) Technological Level of CMC Components for Stationary Gas Turbines and Aero-Engines. DLR-Interner Bericht. DLR-IB-AT-KP-2022-32. 43 S.

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Item URL in elib:https://elib.dlr.de/186166/
Document Type:Monograph (DLR-Interner Bericht)
Title:Technological Level of CMC Components for Stationary Gas Turbines and Aero-Engines
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Wehrel, PatrickUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2022
Refereed publication:No
Open Access:Yes
Number of Pages:43
Status:Published
Keywords:Ceramic Matrix Composite, CMC, keramische Faserverbundwerkstoffe, Ceramic, Keramik, Turbine, Aero-Engine, Triebwerk, Gas Turbine, CMC Combustor, CMC Liner, CMC Shroud, CMC Vane, CMC Blade, CMC Nozzle, SiC/SiC, Ox/Ox, Environmental Barrier Coating, EBC
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Future Engines and Engine Integration
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine
Deposited By: Wehrel, Patrick
Deposited On:23 May 2022 14:53
Last Modified:13 Mar 2023 09:18

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  • Technological Level of CMC Components for Stationary Gas Turbines and Aero-Engines. (deposited 23 May 2022 14:53) [Currently Displayed]

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