# US 12,006,951 B2 · Turbo-machine arrangement > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,006,951 B2 - Document ID: US12006951B2 - Status: Granted - Kind: B2 - Application number: 17/861,748 - Filed: 2022-07-11 - Published: 2023-01-19 - Granted: 2024-06-11 - Earliest claimed: 2021-07-14 - Assignees: MAN Energy Solutions SE - Applicants: MAN Energy Solutions SE - Inventors: Dirk Büche; Janine Sutter - Web page: https://patentgrep.com/patent/US12006951B2 ## CPC - F04D 17/122: {the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors} - F04D 29/5806: {Cooling the drive system} - F04D 25/06: the pump being electrically driven (F04D25/08 takes precedence) - F04D 29/056: Bearings - F04D 29/5826: {Cooling at least part of the working fluid in a heat exchanger} - F04D 29/584: {cooling or heating the machine (F04D29/5846, F04D29/5853 take precedence)} - F04D 29/5846: {cooling by injection} - F05D 2260/601: using an ejector or a jet pump - F04D: NON-POSITIVE-DISPLACEMENT PUMPS (engine fuel-injection pumps F02M; ion pumps H01J41/12; electrodynamic pumps H02K44/02) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS ## Abstract A turbo-machine arrangement having a compressor section comprising a compressor shaft, an electric machine having a shaft, the compressor shaft is coaxial to the shaft. The compressor shaft is coupled to the electric machine shaft. The electric machine and compressor section are arranged in a common housing and mounted via bearings. The housing having a supply line via which uncompressed working medium is supplied, a discharge line, via which compressed working medium is discharged, and an ejector, supplied via a first connection with working medium at a first pressure level for drawing in working medium at a lower second pressure level via a second connection. A mixture formed in the ejector is supplied to the electric machine and/or another assembly to be cooled via a third connection. ## Claims ### Claim 1 A turbo-machine arrangement, comprising: at least one single or multi-stage compressor section configured to increase a pressure of a working medium, wherein the at least one single or multi-stage compressor section comprises a compressor shaft; an electric machine having a shaft; wherein the respective compressor shaft runs coaxially to the shaft of the electric machine; wherein the respective compressor shaft is coupled to the shaft of the electric machine; a common hermetically sealed single or multi-part housing in which the electric machine and the at least one single or multi-stage compressor section is are arranged and mounted in the housing via bearings such that the at least one single or multi-stage compressor section, the electric machine, and the bearings are altogether washed about by the working medium; a supply line configured to supply uncompressed working medium to the turbo-machine arrangement; a discharge line configured to discharge working medium compressed by the turbo-machine arrangement; and at least one ejector, supplied via a first line or a first connection with working medium at a first pressure level as propellant to draw in working medium at a lower second pressure level via a second line or a second connection, wherein a mixture formed in the at least one ejector of the working medium at the first pressure level and the working medium at the second pressure level is supplied as cooling medium to the electric machine and/or to at least one other assembly to be cooled via a third line or a third connection, wherein the first line or the first connection is arranged directly between the at least one ejector and the common hermetically sealed single or multi-part housing and the third line or the third connection is arranged directly between the at least one ejector and the common hermetically sealed single or multi-part housing. ### Claim 2 (depends on 1) The turbo-machine arrangement according to claim 1, wherein the at least one ejector is supplied via the first line or the first connection with at least partially compressed working medium as propellant for drawing in uncompressed working medium via the second line or the second connection, and wherein the mixture formed in the at least one ejector of the at least partially compressed working medium and of the uncompressed working medium is supplied to the electric machine and/or to the at least one other assembly to be cooled via the third line or the third connection as the cooling medium. ### Claim 3 (depends on 1) The turbo-machine arrangement according to claim 1, wherein the at least one ejector is coupled via the first line or the first connection to: the compressor section or one of the multi-stage compressor sections or to the discharge line of the turbo-machine arrangement or to a first leakage point of the turbo-machine arrangement. ### Claim 4 (depends on 1) The turbo-machine arrangement according to claim 1, wherein the at least one ejector is coupled via the second line or the second connection to: the supply line of the turbo-machine arrangement or to the compressor section or one of the multi-stage compressor sections or a second leakage point of the turbo-machine arrangement or a return line of the turbo-machine arrangement for the cooling medium conducted via or through the electric machine and/or the at least one other assembly to be cooled. ### Claim 5 (depends on 1) The turbo-machine arrangement according to claim 1, wherein the at least one ejector is coupled via the third line or the third connection to the electric machine and/or to the at least one other assembly to be cooled. ### Claim 6 (depends on 1) The turbo-machine arrangement according to claim 1, wherein a return line for the cooling medium conducted via or through the electric machine and/or the at least one other assembly to be cooled is coupled to the second line leading to the at least one ejector or the second connection of the at least one ejector. ### Claim 7 (depends on 1) The turbo-machine arrangement according to claim 1, wherein a single compressor section having at least one compressor stage is arranged on a side of the electric machine coaxially to the same. ### Claim 8 (depends on 1) The turbo-machine arrangement according to claim 1, wherein two compressor sections each with at least one compressor stage which, on sides of the electric machine located opposite one another, are each arranged co-axially to the same. ### Claim 9 A turbo-machine arrangement, comprising: at least one single or multi-stage compressor section configured to increase a pressure of a working medium, wherein the at least one single or multi-stage compressor section comprises a compressor shaft; an electric machine having a shaft; wherein the respective compressor shaft runs coaxially to the shaft of the electric machine; wherein the respective compressor shaft is coupled to the shaft of the electric machine; a common hermetically sealed single or multi-part housing in which the electric machine and the at least one single or multi-stage compressor section is arranged and mounted in the housing via bearings such that the at least one single or multi-stage compressor section, the electric machine, and the bearings are altogether washed about by the working medium; a supply line configured to supply uncompressed working medium to the turbo-machine arrangement; a discharge line configured to discharge working medium compressed by the turbo-machine arrangement; and at least one ejector, supplied via a first line or a first connection with working medium at a first pressure level as propellant to draw in working medium at a lower second pressure level via a second line or a second connection, wherein a mixture formed in the at least one ejector of the working medium at the first pressure level and the working medium at the second pressure level is supplied as cooling medium to the electric machine and/or to at least one other assembly to be cooled via a third line or a third connection, wherein a return line for the cooling medium conducted via or through the electric machine and/or the at least one other assembly to be cooled is coupled to the supply line of the turbo-machine arrangement such that an opening point of the return line of the cooling medium into the supply line of the turbo-machine arrangement, seen in a through-flow direction of the supply line, lies downstream of a branch-off point of the second line or of the second connection of the supply line of the turbo-machine arrangement. ### Claim 10 (depends on 9) The turbo-machine arrangement according to claim 9, wherein a heat exchanger or cooler is integrated in the return line.