Anpassbare und Flexible Gewebte Hitzeschilde für Gasturbinenmotorbauteile
Anmelder: Collins Engine Nozzles, Inc. 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4015911
- Aktenzeichen
- EP21215709
- Anmeldetag
- 17. Dezember 2021
- Veröffentlichung
- 8. November 2023
- Erteilung
- 8. November 2023
- Rechtsraum
- EP
- IPC
- F23R3/28
Abstract
A heat shielded assembly includes a fuel structure (106) of a combustor of a gas turbine engine and a woven heat shield (110) at least partially conformally surrounding the fuel structure and spaced from an exterior of the fuel structure by a distance where it surrounds the fuel structure. The fuel structure is configured to deliver fuel to the combustor. The woven heat shield comprises a first set of strands (112), a second set of strands (114) interwoven with the first set of strands, and a weave pattern comprising the first set of strands and the second set of strands. Each strand of the first set of strands extends in a first direction, each strand of the second set of strands extends in a second direction transverse to the first direction, and the first set of strands and the second set of strands are not attached where they intersect in the weave pattern.
Anmelder
- Firma
- Collins Engine Nozzles, Inc.
- Land
- 🇺🇸 USA
US-amerikanisches Unternehmen der Collins Aerospace (RTX-Konzern), spezialisiert auf Kraftstoffdüsen und Einspritzsysteme für Flugzeugtriebwerke und Gasturbinen.
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