Part of a gas turbine engine and method for the manufacturing the part
Research output: Intellectual Property › Patent application/Patent
Contributors
Abstract
The invention relates to a component of a gas turbine engine which has a fiber-composite material having a multiplicity of rovings, wherein at least one roving of the fiber-composite material along the spatial extent thereof has a variable cross section, at least two rovings have in each case a dissimilar cross section and/or the at least one roving follows a variable direction and the at least one roving is deposited by means of tailored fiber placement. The invention also relates to a method of a component.
Details
The invention relates to a component of a gas turbine engine which has a fiber-composite material having a multiplicity of rovings, wherein at least one roving of the fiber-composite material along the spatial extent thereof has a variable cross section, at least two rovings have in each case a dissimilar cross section and/or the at least one roving follows a variable direction and the at least one roving is deposited by means of tailored fiber placement. The invention also relates to a method of a component.
| Original language | English |
|---|---|
| IPC (International Patent Classification) | F01D 9/04 |
| Patent number | US 2023/0193770 |
| Filing date | 15 Dec 2022 |
| Country/Territory | United States of America |
| Priority date | 17 Dec 2021 |
| Priority number | DE102021214605 |
| Publication status | E-pub ahead of print - 22 Jun 2023 |
No renderer: customAssociatesEventsRenderPortal,dk.atira.pure.api.shared.model.researchoutput.Patent
External IDs
| ORCID | /0000-0003-1370-064X/work/142659458 |
|---|