EP 3591237 B1 20210519 - STRUCTURAL MODULE FOR A COMPRESSOR OF A TURBOMACHINE
Title (en)
STRUCTURAL MODULE FOR A COMPRESSOR OF A TURBOMACHINE
Title (de)
STRUKTURBAUGRUPPE FÜR EINEN VERDICHTER EINER STRÖMUNGSMASCHINE
Title (fr)
MODULE STRUCTURAL POUR UN COMPRESSEUR D'UNE TURBOMACHINE
Publication
Application
Priority
DE 102018116062 A 20180703
Abstract (en)
[origin: US2020011346A1] A structural subassembly for a compressor of a turbomachine, which has a rotor having a plurality of blades, which extend radially in a flow path of the turbomachine, and a compressor casing, which forms a flow path boundary, which delimits the flow path through the turbomachine radially on the outside. In this subassembly, the compressor casing has casing structuring adjoining the rotor. It is envisaged that the compressor casing has a plurality of circumferential segments, which extend in the circumferential direction, wherein only one or only some of the circumferential segments forms or form casing structuring.
IPC 8 full level
F04D 29/52 (2006.01); F04D 29/68 (2006.01)
CPC (source: EP US)
F04D 29/526 (2013.01 - EP US); F04D 29/685 (2013.01 - EP US); F04D 27/0207 (2013.01 - US); F05D 2260/40311 (2013.01 - EP)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
EP 3591237 A1 20200108; EP 3591237 B1 20210519; DE 102018116062 A1 20200109; US 11131322 B2 20210928; US 2020011346 A1 20200109
DOCDB simple family (application)
EP 19181591 A 20190621; DE 102018116062 A 20180703; US 201916453193 A 20190626