Spannungsentlastungskompressormantel-Kompressionsringe

EP4148281 Art B1 13. August 2025

Anmelder: Hamilton Sundstrand Corporation 🇺🇸

Details

Veröffentlichungs-Nr.
EP4148281
Aktenzeichen
EP22194864
Anmeldetag
9. September 2022
Veröffentlichung
13. August 2025
Erteilung
13. August 2025
Rechtsraum
EP
IPC
F04D29/02F04D29/28
Offizieller Volltext

Abstract

A compressor assembly (300) includes a compressor (144) including a central shaft (210) including an external surface (214), a shroud (220) extending circumferentially around the central shaft. The shroud including a radially inward surface (224) and radially outward surface (222) located opposite the radially inward surface. The external surface of the central shaft and the radially inward surface of the shroud are in a facing spaced relationship forming a core flow path (C) therebetween. The compressor also includes a plurality of blades (125) extending from the central shaft to the shroud. The compressor assembly also includes a compression ring (400) extending circumferentially around the shroud, the compression ring being in an interference fit with the shroud. The compression ring is configured to apply a radially inward compressive force (F1) along one or more portions of the radially outward surface of the shroud, the radially inward compressive is configured to compress the shroud and the plurality of blades into the central shaft.

Anmelder

Firma
Hamilton Sundstrand Corporation
Land
🇺🇸 USA
🇺🇸 Hamilton Sundstrand

US-amerikanisches Unternehmen der Luft- und Raumfahrtindustrie, das Flugzeugsysteme wie Umweltkontroll-, Energie- und Antriebssysteme entwickelt; heute Teil von Collins Aerospace innerhalb von RTX.

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