Jet ejector system and method

1. A jet ejector method, comprising:

providing a primary jet ejector having a primary inlet stream;

coupling one or more secondary jet ejectors to the primary jet ejector such that all of the jet ejectors are in a cascaded arrangement;

bleeding off a portion of the primary inlet stream and directing the portion of the primary inlet stream to the secondary jet ejector that is closest to the primary jet ejector in the cascaded arrangement;

directing a motive fluid into the secondary jet ejector that is farthest from the primary jet ejector in the cascaded arrangement;

at each secondary jet ejector, receiving at least some of the portion of the primary inlet stream and at least some of the motive fluid to create respective mixtures within the secondary jet ejectors; and

at each secondary jet ejector, directing at least a portion of the respective mixture to adjacent jet ejectors in the cascaded arrangement.

2. The method of claim 1 , further comprising:

directing a portion of the mixture from the secondary jet ejector that is farthest from the primary jet ejector in the cascaded arrangement to a compressor; and

compressing the portion to produce the motive fluid.

3. The method of claim 2 , further comprising powering the compressor with a steam turbine.

4. The method of claim 3 , further comprising directing waste steam from the steam turbine to the primary jet ejector or one of the secondary jet ejectors.

5. The method of claim 2 , further comprising powering the compressor with a device selected from the group consisting of an engine and an electric motor.

6. The method of claim 2 , further comprising powering the compressor with a Brayton cycle engine.

7. The method of claim 1 , wherein providing the primary jet ejector comprises providing a plurality of primary jet ejectors in series with one another.

8. The method of claim 7 , further comprising providing each of the plurality of primary jet ejectors with a respective set of secondary jet ejectors.

9. The method of claim 8 , wherein at least some of the secondary jet ejectors of one of the plurality of primary jet ejectors serve as at least some of the secondary jet ejectors of another one of the plurality of primary jet ejectors.

10. The method of claim 8 , further comprising an equal number of stages of secondary jet ejectors in each respective set, and wherein the secondary jet ejectors comprising a particular stage are in series.

11. A jet ejector method, comprising:

providing a primary jet ejector having a primary inlet stream and an outlet stream;

coupling one or more secondary jet ejectors to the primary jet ejector such that all of the jet ejectors are in a cascaded arrangement;

bleeding off a portion of the outlet stream and directing the portion of the outlet stream to the secondary jet ejector that is closest to the primary jet ejector in the cascaded arrangement;

directing a motive fluid into the secondary jet ejector that is farthest from the primary jet ejector in the cascaded arrangement;

at each secondary jet ejector, receiving at least some of the portion of the outlet stream and at least some of the motive fluid to create respective mixtures within the secondary jet ejectors; and

at each secondary jet ejector, directing at least a portion of the respective mixture to adjacent jet ejectors in the cascaded arrangement.

12. The method of claim 11 , further comprising:

directing a portion of the mixture from the secondary jet ejector that is farthest from the primary jet ejector in the cascaded arrangement to a compressor; and

compressing the portion to produce the motive fluid.

13. The method of claim 12 , further comprising powering the compressor with a device selected from the group consisting of a steam turbine, an engine, and an electric motor.

14. The method of claim 11 , wherein providing the primary jet ejector comprises providing a plurality of primary jet ejectors in series with one another, the outlet stream associated with the last primary jet ejector in the series.

15. The method of claim 14 , wherein the secondary jet ejectors are associated with the last primary jet ejector in the series.

16. The method of claim 14 , further comprising providing each of the plurality of primary jet ejectors with a respective set of secondary jet ejectors.

17. The method of claim 16 , further comprising an equal number of stages of secondary jet ejectors in each respective set, and wherein the secondary jet ejectors comprising a particular stage are in series.

18. A jet ejector method, comprising:

providing a primary jet ejector having a primary inlet stream at a first pressure, a secondary inlet stream at a second pressure, and an outlet stream;

coupling one or more secondary jet ejectors to the primary jet ejector such that all of the jet ejectors are in a cascaded arrangement;

directing a motive fluid at a third pressure into the secondary jet ejector that is farthest from the primary jet ejector in the cascaded arrangement; and

causing a fluid flow comprised of at least some of the primary inlet stream and at least some of the motive fluid through each of the secondary jet ejectors such that the third pressure is larger than the second pressure and the second pressure is larger than the first pressure.

19. The method of claim 18 , wherein a compression ratio for each of the primary and secondary jet ejectors is no more than approximately three.

20. The method of claim 18 , wherein an area ratio for the primary jet ejector is selected from the group consisting of approximately three, approximately four, and approximately five.

21. A jet ejector, comprising:

a nozzle having a first stream flowing therethrough, the nozzle comprising an upstream portion, a downstream portion, and a throat disposed between the upstream portion and the downstream portion;

a plurality of sets of apertures located in a wall of the nozzle in the throat, the plurality of sets of apertures longitudinally spaced along the wall;

each of the plurality of sets of apertures having its apertures circumferentially located around the wall; and

a device operable to inject a motive fluid through the apertures and into the first stream.

22. The jet ejector of claim 21 , wherein the apertures comprise circumferential slots.

23. The jet ejector of claim 21 , wherein the motive fluid enters the first stream at an angle with respect to a flow direction of the first stream.

24. The jet ejector of claim 21 , wherein respective pressures of the motive fluid associated with respective ones of the plurality of sets of apertures are approximately equal.

25. The jet ejector of claim 21 , wherein respective pressures of the motive fluid associated with respective ones of the plurality of sets of apertures are approximately unequal.

26. The jet ejector of claim 25 , wherein the respective pressures of the motive fluid increase in a downstream direction.

27. The jet ejector of claim 21 , wherein the apertures comprise point sources.

28. The jet ejector of claim 27 , wherein each point source is coupled to a respective fan-shaped duct formed in the wall and defined by walls diverging in the downstream direction.

29. The jet ejector of claim 28 , wherein the fan-shaped ducts are NACA ducts.

30. The jet ejector of claim 21 , wherein the motive fluid is selected from the group consisting of a gas, a vapor, and a liquid.

31. A jet ejector, comprising:

a nozzle having a first stream flowing therethrough, the nozzle comprising an upstream portion, a downstream portion, and a throat disposed between the upstream portion and the downstream portion;

a plurality of apertures located in a wall of the nozzle in the throat, the plurality of apertures longitudinally spaced along the wall; and

a device operable to inject a motive liquid through the plurality of apertures and into the first stream and wherein respective pressures of the motive liquid associated with each of the plurality of apertures are approximately equal.

32. The jet ejector of claim 31 , wherein the apertures comprise nozzles.

33. The jet ejector of claim 31 , wherein the motive liquid enters the first stream at an angle with respect to a flow direction of the first stream.

34. The jet ejector of claim 31 , wherein respective pressures of the motive liquid associated with respective ones of the plurality of apertures are approximately unequal.

35. The jet ejector of claim 34 , wherein the respective pressures of the motive liquid increase in a downstream direction.

36. The jet ejector of claim 31 , wherein the apertures comprise passageways associated with one or more tubes coupled to the wall of the nozzle in the throat.

37. The jet ejector of claim 36 , wherein the motive liquid enters the first stream parallel with respect to a flow direction of the first stream.

38. The jet ejector of claim 36 , further comprising a plurality of receptacles coupled to the wall of the nozzle in the throat and associated with respective ones of the plurality of tubes in order to collect the motive fluid exiting therefrom.

39. A jet ejector method, comprising:

causing a first stream to flow through a nozzle; and

injecting a motive fluid into the first stream through a plurality of sets of apertures located in a wall of a throat of the nozzle, the plurality of sets of apertures longitudinally spaced along the wall of the throat, wherein the respective pressures of the motive fluid increase in a downstream direction.

40. The method of claim 39 , wherein the apertures are selected from the group consisting of circumferential slots, annular openings, and point sources.

41. The method of claim 39 , further comprising causing the motive fluid to enter the first stream at an angle with respect to a flow direction of the first stream.

42. The method of claim 39 , further comprising causing respective pressures of the motive fluid associated with respective ones of the plurality of sets of apertures to be approximately equal.

43. The method of claim 39 , further comprising causing respective pressures of the motive fluid associated with respective ones of the plurality of sets of apertures to be approximately unequal.

44. The method of claim 39 , wherein the motive fluid is selected from the group consisting of steam and liquid water.