Überschallverdichter und Verfahren zu seiner Montage

Details

Veröffentlichungs-Nr.

EP2466146

Aktenzeichen

EP11192277

Anmeldetag

7. Dezember 2011

Veröffentlichung

28. Juni 2017

Erteilung

28. Juni 2017

Rechtsraum

EP

IPC

F04D21/00F04D29/62F04D29/64F04D29/28F04D29/32

Abstract

A supersonic compressor (10) includes a fluid inlet (26), a fluid outlet (28), a fluid conduit (32) extending therebetween, and a supersonic compressor rotor (40) disposed within the fluid conduit. The rotor includes a rotor disk (48) that includes a substantially cylindrical body (50) extending between a radially inner (56) and outer surface (58) and a plurality of vanes (46) coupled to the body that extend radially outward from the rotor disk, adjacent vanes form a pair. The rotor disk further includes a shroud (200) extending about the rotor disk. The shroud is coupled to at least a portion of each of the plurality of vanes. The radially outer surface, the pair of adjacent vanes, and the shroud are oriented such that a fluid flow channel (80) is defined therebetween. The rotor disk also includes a plurality of adjacent supersonic compression ramps (98) positioned within the fluid flow channel.

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA

Fachgebiete