Cover of a turbomachine centrifugal compressor capable of being rigidly connected via the downstream side near to the upstream edge of same, and turbomachine comprising this cover
View Patent ↗A cover of a centrifugal compressor intended to be rigidly connected to a turbomachine housing, which includes a plurality of ports, is provided. The cover further includes a fastening device for fastening the cover to the housing. A portion of the fastening device is located upstream relative to the ports and can be accessed by a fastening tool through at least one of the ports of the cover. A turbomachine uses this cover to form a sealed space, in particular with a view to collecting air.
1. A cover for a centrifugal compressor which is intended to be fixed to a casing of a turbine engine, comprising an upstream edge and a downstream edge in the flow direction of the gases crossing the compressor, said cover comprising a plurality of openings and means for fixing to the casing,
wherein the fixing means are located upstream relative to the openings, said fixing means cooperating with clamping means, and the clamping means can be engaged by at least a straight portion of a fixing tool through at least one of said openings in the cover.
2. The centrifugal compressor cover according to claim 1 , wherein said openings are intended for an air offtake in the compressor.
3. The centrifugal compressor cover according to claim 1 , wherein said fixing means comprise an outer flange and fixing holes which pierce said flange, and the clamping means include a screw and a nut.
4. The centrifugal compressor cover according to claim 3 , wherein said outer flange forms a wall which completely surrounds said cover.
5. The centrifugal compressor cover according to claim 4 , configured such that each fixing hole can receive one clamping screw passing through at least one of said openings.
6. The centrifugal compressor cover according to claim 3 , wherein said outer flange extends close to the upstream edge of the cover.
7. The centrifugal compressor cover according to claim 3 , further comprising a downstream flange for holding against the casing of the turbine engine, which downstream flange is fastened to the outer wall of the cover between said openings and the downstream edge and forms a sealing means.
8. A turbine engine comprising a centrifugal compressor having a cover according to claim 3 , wherein a casing of the turbine engine is arranged so as to form a sealed connection with the upstream flange of the cover when the clamping means are clamped.
9. The turbine engine according to claim 8 , wherein the casing of the turbine engine is arranged so as to form, together with said cover, at least one closed space which recovers the air passing through the openings in the cover.
10. The turbine engine according to claim 9 , wherein at least some of the openings in the cover, and said at least one closed space, are designed to participate in an air offtake system.