Compressor stage

Patent metadata

Field	Value
Publication number	US-10519975-B2
Application number	US-201415105041-A
Country	US
Kind code	B2
Filing date	Dec 16, 2014
Priority date	Dec 17, 2013
Publication date	Dec 31, 2019
Grant date	Dec 31, 2019

Abstract

Compressor stage with a stator-side intake connection piece via which medium which is to be compressed can be introduced into the compressor stage in the region of the compressor stage, with a stator-side inflow channel via which the medium to be compressed can be conveyed in direction of a rotor-side impeller proceeding from the intake connection piece, wherein the impeller has a radially inner hub, a radially outer cover disk and impeller blades extending between the hub and the cover disk, wherein a plus measuring point and a minus measuring point are provided at the compressor stage for measuring the effective pressure at the compressor stage, and wherein the minus measuring point is positioned upstream of the impeller outside of the stator-side inflow channel in an annular gap which branches off from the inflow channel.

First claim

The invention claimed is:

1. A compressor stage comprising:
a radial stator-side intake connection piece ( 33 ) configured to radially introduce a medium to be compressed into the compressor stage;
a rotor-side impeller ( 14 );
a stator-side inflow channel ( 11 ) having a circumferential extension and configured to convey the medium to be compressed in direction of the rotor-side impeller ( 14 ) proceeding from the intake connection piece, wherein the impeller ( 14 ) comprises a radially inner hub ( 16 ), a radially outer cover disk ( 17 ) and impeller blades ( 18 ) extending between the hub ( 16 ) and the cover disk ( 17 ); an annular gap ( 24 ) branching off from the inflow channel ( 11 );
a stator-side seal carrier ( 23 ) and a seal ( 22 );
a plus measuring point ( 31 ) and a minus measuring point ( 32 ) provided at the compressor stage for measuring the effective pressure at the compressor stage, the minus measuring point ( 32 ) positioned upstream of the impeller ( 14 ) outside of the stator-side inflow channel ( 11 ) in the annular gap ( 24 ); and
wherein the annular gap ( 24 ) extends radially outward over the entire circumferential extension of the inflow channel and is bounded adjacent to the impeller ( 14 ) by the stator-side seal carrier ( 23 ) which carries the seal ( 22 ) that cooperates with the cover disk ( 17 ) of the rotor-side impeller ( 14 ).

2. The compressor stage according to claim 1 , wherein the annular gap ( 24 ) is bounded opposite the impeller ( 14 ) by a stator-side housing ( 13 ).

3. The compressor stage according to claim 1 , wherein the annular gap ( 24 ) is formed as a chamber, and wherein the minus measuring point ( 32 ) is positioned in the chamber ( 28 ) of the annular gap ( 24 ).

4. The compressor stage according to claim 1 , additionally comprising a bore ( 25 ) leading to the minus measuring point ( 32 ) from radially outward for tapping an existing pressure level at the minus measuring point ( 32 ).

5. The compressor stage according to claim 1 , wherein the plus measuring point ( 31 ) is positioned in the region of the intake connection piece ( 33 ).

6. The compressor stage according to claim 1 , wherein the compressor stage is a radial compressor stage.

7. A compressor stage comprising:
a stator-side intake connection piece ( 33 ) for introducing a medium to be compressed into the compressor stage;
a rotor-side impeller ( 14 );
a stator-side inflow channel ( 11 ) for conveying the medium to be compressed in direction of the rotor-side impeller ( 14 ) proceeding from the intake connection piece, wherein the impeller ( 14 ) comprises a radially inner hub ( 16 ), a radially outer cover disk ( 17 ) and impeller blades ( 18 ) extending between the hub ( 16 ) and the cover disk ( 17 ); an annular gap ( 24 ) branching off from the inflow channel ( 11 );
a stator-side seal carrier ( 23 ) and a seal ( 22 );
a plus measuring point ( 31 ) and a minus measuring point ( 32 ) provided at the compressor stage for measuring the effective pressure at the compressor stage, the minus measuring point ( 32 ) positioned upstream of the impeller ( 14 ) outside of the stator-side inflow channel ( 11 ) in the annular gap ( 24 ); and
wherein the annular gap ( 24 ) is bounded adjacent to the impeller ( 14 ) by the stator-side seal carrier ( 23 ) which carries the seal ( 22 ) that cooperates with the cover disk ( 17 ) of the rotor-side impeller ( 14 ),
wherein the annular gap ( 24 ) branches off radially outward from the stator-side inflow channel ( 11 ) immediately upstream of the impeller ( 14 ).

8. A compressor stage comprising:
a stator-side intake connection piece ( 33 ) for introducing a medium to be compressed into the compressor stage;
a rotor-side impeller ( 14 );
a stator-side inflow channel ( 11 ) for conveying the medium to be compressed in direction of the rotor-side impeller ( 14 ) proceeding from the intake connection piece, wherein the impeller ( 14 ) comprises a radially inner hub ( 16 ), a radially outer cover disk ( 17 ) and impeller blades ( 18 ) extending between the hub ( 16 ) and the cover disk ( 17 ); an annular gap ( 24 ) branching off from the inflow channel ( 11 );
a stator-side seal carrier ( 23 ) and a seal ( 22 );
a plus measuring point ( 31 ) and a minus measuring point ( 32 ) provided at the compressor stage for measuring the effective pressure at the compressor stage, the minus measuring point ( 32 ) positioned upstream of the impeller ( 14 ) outside of the stator-side inflow channel ( 11 ) in the annular gap ( 24 ); and
wherein the annular gap ( 24 ) is bounded adjacent to the impeller ( 14 ) by the stator-side seal carrier ( 23 ) which carries the seal ( 22 ) that cooperates with the cover disk ( 17 ) of the rotor-side impeller ( 14 ) and opposite the impeller ( 14 ) by a stator-side housing ( 13 ),
wherein the annular gap ( 24 ) is bounded opposite the impeller ( 14 ) by a stator-side inlet star ( 27 ) which is fastened to the stator-side housing ( 13 ).

Assignees

• Man Diesel & Turbo Se
• Man Energy Solutions Se

Inventors

• Tiedtke Alf-Peter
• Wollnik Matthias

Classifications

• F05D2270/3011

  Inlet pressure · CPC title

• F05D2270/3015

  differential pressure · CPC title

• F04D29/4213 Primary

  suction ports · CPC title

• F04D27/00

  Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids · CPC title

• F04D29/162

  of a centrifugal flow wheel · CPC title