Waste Heat Recovery Systems Having Magnetic Liquid Seals

• US 20150330261A1
• Filed: 05/08/2015
• Published: 11/19/2015
• Est. Priority Date: 05/15/2014
• Status: Abandoned Application

• Current Assignee: Echogen Power Systems, LLC
• Original Assignee: Echogen Power Systems, LLC
• Inventors: Held, Timothy
• Application Number:
  US14/707,041
• Publication Number:
  US 20150330261A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F01D 11/003 by packing rings; Mechanical seals
• CPC Class Codes: F01D 25/183 Sealing means
• CPC Class Codes: F01K 23/10 with exhaust fluid of one cycle heating the fluid in another cycle F01K17/025 takes precedence
• CPC Class Codes: F01K 25/103 Carbon dioxide F01K25/065 takes precedence
• CPC Class Codes: F02G 5/02 Profiting from waste heat of exhaust gases
• CPC Class Codes: F05D 2240/55 Seals
• CPC Class Codes: F16J 15/004 forming of recuperation chamber for the leaking fluid
• CPC Class Codes: F16J 15/43 kept in sealing position by magnetic force
• CPC Class Codes: Y02E 10/10 Geothermal energy
• CPC Class Codes: Y02E 10/46 Conversion of thermal power into mechanical power, e.g. Rankine, Stirling or solar thermal engines

Abstract

A system including a seal cartridge is provided. The seal cartridge includes a housing defining a passageway that receives a driveshaft. A dry gas seal is circumferentially disposed about the passageway within the housing at a first axial location along the housing. A magnetic liquid seal is circumferentially disposed about the passageway within the housing at a second axial location along the housing. A fluid leakage cavity is formed between the dry gas seal at the first axial location and the magnetic liquid seal at the second axial location. An extraction port is disposed in the housing and enables recovery of a leaked fluid from the fluid leakage cavity.

Claims

1. A heat engine system, comprising:

a working fluid circuit having a high pressure side and a low pressure side and being configured to flow a working fluid therethrough, wherein at least a portion of the working fluid comprises supercritical carbon dioxide; and

a turbopump coupled to the working fluid circuit and comprising;

a pump portion;

a drive turbine coupled to the pump portion, fluidly coupled to and disposed between the high pressure side and the low pressure side, and configured to convert a pressure drop in the working fluid to mechanical energy;

a driveshaft coupled to the drive turbine and the pump portion and configured to drive the pump portion with the mechanical energy to enable the pump portion to circulate the working fluid through the working fluid circuit, wherein the driveshaft is at least partially contained within a housing;

a dry gas seal circumferentially disposed about the driveshaft between the driveshaft and the housing at a first axial location along the driveshaft;

a magnetic liquid seal circumferentially disposed about the driveshaft between the driveshaft and the housing at a second axial location along the driveshaft, wherein a fluid leakage cavity is formed between the dry gas seal at the first axial location and the magnetic liquid seal at the second axial location; and

an extraction port disposed in the housing and configured to enable recovery of a leaked fluid from the fluid leakage cavity.

2. The heat engine system of claim 1, further comprising a lube oil system disposed at a third axial location along the driveshaft, wherein the magnetic liquid seal is configured to seal off the fluid leakage cavity from the lube oil system.

3. The heat engine system of claim 1, further comprising a leak recapture system fluidly coupled to the extraction port and comprising a compressor configured to compress the leaked fluid.

4. The heat engine system of claim 3, wherein the leak recapture system further comprises a leak recapture storage vessel configured to receive the compressed leaked fluid from the compressor for storage.

5. The heat engine system of claim 3, wherein the compressor is fluidly coupled to the working fluid circuit and configured to provide the compressed leaked fluid to the working fluid circuit.

6. The heat engine system of claim 1, wherein the magnetic liquid seal comprises a magnet, a first pole piece, a second pole piece, a magnetically permeable shaft, and a ferrofluid, and wherein the ferrofluid is configured to form a sealing ring about the magnetically permeable shaft in a gap formed between the magnetically permeable shaft and the first and second pole pieces.

7. The heat engine system of claim 1, comprising a cooling system fluidly coupled to the working fluid circuit and the magnetic liquid seal and configured to provide the working fluid in a supercritical state to the magnetic liquid seal to cool the magnetic liquid seal.

8. A heat engine system, comprising:

a working fluid circuit having a high pressure side and a low pressure side and being configured to flow a working fluid therethrough, wherein at least a portion of the working fluid circuit contains the working fluid in a supercritical state;

a turbopump fluidly coupled to the working fluid circuit between the low pressure side and the high pressure side, and being configured to circulate the working fluid within the working fluid circuit; and

a magnetic liquid seal disposed in the turbopump and comprising a ferrofluid and a magnet configured to maintain the ferrofluid in a ring shape to seal a fluid leakage cavity of the turbopump from a lube oil system of the turbopump.

9. The heat engine system of claim 8, wherein the turbopump comprises a drive turbine configured to generate mechanical energy, a pump portion, and a driveshaft coupled to the drive turbine and the pump portion and configured to drive the pump portion with the mechanical energy to enable the pump portion to circulate the working fluid through the working fluid circuit.

10. The heat engine system of claim 9, wherein the turbopump comprises a dry gas seal circumferentially disposed about the driveshaft, and the fluid leakage cavity is axially disposed between the dry gas seal and the magnetic liquid seal along the driveshaft.

11. The heat engine system of claim 8, wherein the turbopump comprises an extraction port disposed therein and configured to enable recovery of a leaked fluid from the fluid leakage cavity.

12. The heat engine system of claim 11, further comprising a leak recapture compressor configured to receive the leaked fluid from the extraction port and to compress the leaked fluid.

13. The heat engine system of claim 8, further comprising a cooling system fluidly coupled to the working fluid circuit and the magnetic liquid seal and configured to transfer the working fluid from the working fluid circuit to the magnetic liquid seal to cool the magnetic liquid seal.

14. A heat engine system, comprising:

a working fluid circuit having a high pressure side and a low pressure side and being configured to flow a working fluid therethrough, wherein the working fluid is in a supercritical state in at least a portion of working fluid circuit;

a turbopump coupled to the working fluid circuit and comprising a pump portion and a drive turbine coupled to the pump portion via a driveshaft, wherein the driveshaft is at least partially contained within a housing;

a dry gas seal circumferentially disposed about the driveshaft between the driveshaft and the housing at a first axial location along the driveshaft;

a magnetic liquid seal circumferentially disposed about the driveshaft between the driveshaft and the housing at a second axial location along the driveshaft, wherein a fluid leakage cavity is formed between the dry gas seal at the first axial location and the magnetic liquid seal at the second axial location; and

a cooling system fluidly coupled to the working fluid circuit and the magnetic liquid seal and configured to transfer the working fluid from the working fluid circuit to the magnetic liquid seal to cool the magnetic liquid seal.

15. The heat engine system of claim 14, further comprising an extraction port disposed in the housing and configured to enable recovery of a leaked fluid from the fluid leakage cavity.

16. The heat engine system of claim 15, further comprising a leak recapture compressor configured to receive the leaked fluid from the extraction port and to compress the leaked fluid.

17. The heat engine system of claim 15, further comprising a condenser configured to receive the leaked fluid from the extraction port and to condense the leaked fluid.

18. The heat engine system of claim 14, further comprising a lube oil system disposed at a third axial location along the driveshaft, wherein the magnetic liquid seal is configured to seal the fluid leakage cavity from the lube oil system.

19. The heat engine system of claim 14, wherein the magnetic liquid seal comprises a magnet, a first pole piece, a second pole piece, a magnetically permeable shaft, and a ferrofluid, and wherein the ferrofluid is configured to form a sealing ring about the magnetically permeable shaft in a gap formed between the magnetically permeable shaft and the first and second pole pieces.

20. The heat engine system of claim 14, wherein the working fluid comprises supercritical carbon dioxide.

21. A heat engine system, comprising:

a working fluid circuit having a high pressure side and a low pressure side and being configured to flow a working fluid therethrough, wherein at least a portion of the working fluid comprises supercritical carbon dioxide;

a heat exchanger configured to be fluidly coupled to and in thermal communication with the working fluid in the high pressure side of the working fluid circuit, wherein the heat exchanger is configured to transfer thermal energy from a heat source stream to the working fluid in the high pressure side;

a power turbine fluidly coupled to and disposed between the high pressure side and the low pressure side of the working fluid circuit and configured to convert a pressure drop in the working fluid to mechanical energy;

a driveshaft coupled to the power turbine and configured to drive a device with the mechanical energy, wherein the driveshaft is at least partially contained within a housing;

a dry gas seal circumferentially disposed about the driveshaft between the driveshaft and the housing at a first axial location along the driveshaft;

a magnetic liquid seal circumferentially disposed about the driveshaft between the driveshaft and the housing at a second axial location along the driveshaft, wherein a fluid leakage cavity is formed between the dry gas seal at the first axial location and the magnetic liquid seal at the second axial location; and

an extraction port disposed in the housing and configured to enable recovery of a leaked fluid from the fluid leakage cavity.

22. The heat engine system of claim 21, further comprising a leak recapture system fluidly coupled to the extraction port and comprising a compressor configured to compress the leaked fluid.

23. The heat engine system of claim 22, wherein the leak recapture system further comprises a leak recapture storage vessel configured to receive and store the compressed leaked fluid from the compressor.

24. The heat engine system of claim 22, wherein the compressor is fluidly coupled to the working fluid circuit and configured to provide the compressed leaked fluid to the working fluid circuit.

25. A system, comprising:

a seal cartridge, comprising;

a housing defining a passageway configured to receive a driveshaft;

a dry gas seal circumferentially disposed about the passageway within the housing at a first axial location along the housing;

a magnetic liquid seal circumferentially disposed about the passageway within the housing at a second axial location along the housing, wherein a fluid leakage cavity is formed between the dry gas seal at the first axial location and the magnetic liquid seal at the second axial location; and

an extraction port disposed in the housing and configured to enable recovery of a leaked fluid from the fluid leakage cavity.

26. The system of claim 25, wherein the seal cartridge is configured to be disposed in a gas compressor, a power turbine, or a turbopump.