Stützring mit Hitzeschild für Gehäuseflansche
Anmelder: Raytheon Technologies Corporation, United Technologies Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3569818
- Aktenzeichen
- EP19174592
- Anmeldetag
- 15. Mai 2019
- Veröffentlichung
- 7. April 2021
- Erteilung
- 7. April 2021
- Rechtsraum
- EP
- IPC
- F01D5/18F01D9/04F01D25/14F01D25/24
Abstract
A heat shield vane support (300) may have a structure including at least one of a cylindrical (330) and a frustoconical (332) portion with an outboard diameter (308) and an inboard diameter (306) extending about an axis (301) and extending axially between a forward face (302) and an aft face (304) and may comprise a flange (310) extending circumferentially about the aft face (304) radially inward from the inboard diameter (306), a plurality of anti-rotation features (314) distributed circumferentially about the inboard diameter (306) extending radially inward from the inboard diameter (306) and extending axially with respect to the cylindrical structure between a forward edge (313) and an aft edge (315) defining a length L, and a plurality of teeth (312) distributed circumferentially about the forward face (302) and extending axially from the forward face (302).
Anmelder
- Firmen
- Raytheon Technologies Corporation
United Technologies Corporation - Land
- 🇺🇸 USA
US-amerikanischer Luft- und Raumfahrt- sowie Verteidigungskonzern, entstanden aus Raytheon und United Technologies. Entwickelt und fertigt Triebwerke, Avionik, Radarsysteme, Raketen- und Verteidigungstechnik für zivile und militärische Kunden.
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