Claims
- 1. A system for generating electricity comprising a power generating device and, operatively connected thereto, a fluid lubricated rotary positive displacement compressor system, wherein:(a) said fluid lubricated rotary positive displacement system is comprised of a rotary positive displacement compressor, wherein said rotary positive displacement compressor has a discharge pressure of from about 20 to about 950 pounds per square inch gauge, a pressure ratio per stage of from about 1.1 to about 30, and a flow capacity of from about 5 to about 3,000 standard cubic feet per minute; and (b) said fluid lubricated rotary positive displacement system is comprised of a receiving tank connected to said rotary positive displacement compressor, means for feeding gas at a pressure of from about 0.2 to about 400 pounds per square inch gauge to said rotary positive displacement compressor, means for feeding liquid to said receiving tank, means for cooling a mixture of said gas and said liquid, means for separating said mixture of said gas and said liquid, and means for feeding said liquid to said rotary positive displacement compressor.
- 2. The system as recited in claim 1, wherein said rotary positive displacement compressor is a guided rotor compressor.
- 3. The system as recited in claim 2, wherein said guided rotor compressor is comprised of a housing comprising a curved inner surface with a profile equidistant from a trochoidal curve, an eccentric mounted on a shaft disposed within said housing, a first rotor mounted on said eccentric shaft which is comprised of a first side, a second side, and a third side, a first partial bore disposed at the intersection of said first side and said second side, a second partial bore disposed at the intersection of said second side and said third side, a third partial bore disposed at the intersection of said third side and said first side, a first roller disposed and rotatably mounted within said first partial bore, a second roller disposed and rotatably mounted within said second partial bore, and a third roller disposed and rotatably mounted within said third partial bore, wherein:(a) said rotor is comprised of a front face, a back face, said first side, said second side, and said third side, wherein: 1. a first opening is formed between and communicates between said front face and said first side, 2. a second opening is formed between and communicates between said back face and said first side, wherein each of said first opening and said second opening is substantially equidistant and symmetrical between said first partial bore and said second partial bore, 3. a third opening is formed between and communicates between said front face and said second side, 4. a fourth opening is formed between and communicates between said back face and said second side, wherein each of said third opening and said fourth opening is substantially equidistant and symmetrical between said second partial bore and said third partial bore, 5. a fifth opening is formed between and communicates between said front face and said third side, and 6. A sixth opening is formed between and communicates between said back face and said third side, wherein each of said fifth opening and said sixth opening is substantially equidistant and symmetrical between said third partial bore and said first partial bore. (b) each of said first partial bore, said second partial bore, and said third partial bore is comprised of a centerpoint which, as said rotary device rotates, moves along said trochoidal curve; (c) each of said first opening, said second opening, said third opening, said fourth opening, said fifth opening, and said sixth opening has a substantially U-shaped cross-sectional shape defined by a first linear side, a second linear side, and an arcuate section joining said first linear side and said second linear side, wherein: 1. said first linear side and said second linear side are disposed with respect to each other at an angle of less than ninety degrees; and 2. said substantially U-shaped cross-sectional shape has a depth which is at least equal to its width; (d) the diameter of said first roller is equal to the diameter of said second roller, and the diameter of said second roller is equal to the diameter of said third roller; (e) the widths of each of said first opening, said second opening, said third opening, said fourth opening, said fifth opening, and said sixth opening are substantially the same, and the width of each of said openings is less than the diameter of said first roller; and (f) each of said first side, said second side, and said third side has substantially the same geometry and size and is a composite shape comprised of a first section and a second section, wherein said first section has a shape which is different from that of said second section.
- 4. The system as recited in claim 2, wherein said compressor is an oil lubricated compressor.
- 5. The system as recited in claim 3, wherein each of said first roller, said second roller, and said third roller is a solid roller.
- 6. The system as recited in claim 3, wherein each of said first roller, said second roller, and said third roller is a hollow roller.
- 7. The system as recited in claim 4, wherein said power generating device is a microturbine.
- 8. The system as recited in claim 1, wherein said power generating device is a microturbine.
- 9. The system as recited in claim 7, wherein said compressor has a pressure ratio for each of its stages of from about 1.5 to about 6.
- 10. The system as recited in claim 4, wherein said power generating device is a fuel cell.
- 11. The system as recited in claim 4, wherein said power generating device is a reciprocating internal combustion engine.
- 12. The system as recited in claim 4, wherein said power generating device is a reciprocating external combustion engine.
- 13. The system as recited in claim 1, further comprising an electric motor operatively connected to said rotary positive displacement compressor.
- 14. The system as recited in claim 7, wherein said microturbine is a Brayton cycle system.
- 15. The system as recited in claim 8, wherein said microturibne is a Brayton cycle system.
- 16. The system as recited in claim 13, wherein wherein said Brayton cycle system is comprised of a compressor, a turbine, a combustor with a plurality of gaseous fuel nozzles and a plurality of air inlets, and a permanent magnet motor generator.
- 17. The system as recited in claim 15, wherein said system for generating electricity is comprised of means for transmitting heat produced by said microturbine to a boiler.
CROSS-REFERENCE TO RELATED PATENT APPLICATION
This application is a continuation-in-part of applicant's copending patent application U.S. Ser. No. 09/775,292, filed on Feb. 1, 2001, which was a continuation-in-part of applicant's copending patent application U.S. Ser. No. 09/672,804, filed Sep. 28, 2000, which was a continuation-in-part of patent application U.S. Ser. No. 09/536,332, filed on Mar. 24, 2000, now U.S. Pat. No. 6,266,952, which was a continuation-in-part of patent application U.S. Ser. No. 09/416,291, filed on Oct. 14, 1999, now abandoned, which was a continuation-in-part of patent application U.S. Ser. No. 09/396,034, filed Sep. 15, 1999, now U.S. Pat. No. 6,301,898, which in turn was a continuation-in-part of patent application U.S. Ser. No. 09/181,307, filed on Oct. 28, 1998, now abandoned.
This application is also a continuation-in-part of applicant's patent application U.S. Ser. No. 09/441,312, filed on Nov. 16, 1999, now U.S. Pat. No. 6,213,744.
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