Komponente mit erosionsfester Schicht
Anmelder: Rolls-Royce plc 🇬🇧
Details
- Veröffentlichungs-Nr.
- EP2508712
- Aktenzeichen
- EP12159280
- Anmeldetag
- 13. März 2012
- Veröffentlichung
- 10. Mai 2017
- Rechtsraum
- EP
- IPC
- F01D5/28B29C70/22
Abstract
A composite component such as a blade or vane of a gas turbine engine comprises a body 2 and an erosion-resistant layer 4. The body 2 comprises a fibre reinforcement in a resin matrix, and the erosion-resistant layer 4 comprises a 3-D woven fabric element which is also resin-impregnated. The woven fabric element is made from a thermoplastics material such as PEEK, and may be thicker at the leading edge 6 of the component than at pressure and suction surfaces 8, 10. The component may be manufactured in a laying-up process in which the woven fabric element of the erosion-resistant layer 4 is placed in a mould with the resin-impregnated fibre reinforcement of the body 2 so that the resin of the body 2 migrates into the woven fabric element of the erosion-resistant layer 4.
Anmelder
- Firma
- Rolls-Royce plc
- Land
- 🇬🇧 Großbritannien
Britisches Unternehmen mit Sitz in Derby, das Flugzeugtriebwerke sowie Antriebssysteme für Luftfahrt, Marine und Energieerzeugung entwickelt und herstellt.
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