Gasturbinenmotor mit Statorsegmenten
Anmelder: RTX Corporation, Raytheon Technologies Corporation, United Technologies Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3611347
- Aktenzeichen
- EP19191795
- Anmeldetag
- 14. August 2019
- Veröffentlichung
- 11. Oktober 2023
- Erteilung
- 11. Oktober 2023
- Rechtsraum
- EP
- IPC
- F01D9/04F01D25/24
Abstract
A gas turbine engine (20) includes a case assembly (60) and a stator segment (62). The case assembly defines a first slot (70) having a first surface (80) and a second surface (82). The stator segment includes a shroud body (100) axially extends between a first body end (110) and a second body end (112). A first flange (120) extends into the first slot. The first flange has a first flange first side (130), a first flange second side (132), a first flange first surface (134) and a first flange second surface (136) each circumferentially extending between the first flange first side and the first flange second side. A first portion (140) of the first flange first surface engages the first surface. A second portion (142) of the first flange first surface engages the first surface. A third portion (144) of the first flange first surface is spaced apart from the first surface.
Anmelder
- Firmen
- RTX Corporation
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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