초록 ▼

A method is provided for compressing a gas in a single cycle and in a single cylinder to a pressure of at least 17.2 Mpa with a compression ratio of at least about five to one. The method further comprises dissipating heat from the cylinder during the compression stroke whereby the gas is discharged

A method is provided for compressing a gas in a single cycle and in a single cylinder to a pressure of at least 17.2 Mpa with a compression ratio of at least about five to one. The method further comprises dissipating heat from the cylinder during the compression stroke whereby the gas is discharged with a temperature significantly less than isentropic. The apparatus comprises a hollow cylinder and a reciprocable free-floating piston disposed therein. The piston divides the cylinder into: (a) a compression chamber within which a gas can be introduced, compressed, and discharged; and, (b) a drive chamber, into which a hydraulic fluid can be introduced and removed for actuating the piston. The apparatus further comprises a piston stroke length to piston diameter ratio of at least seven to one. For operating the apparatus with a compression ratio of at least five to one, an outlet pressure of at least 17.2 Mpa, and a gas discharge temperature significantly less than isentropic, the apparatus can further comprise a variable displacement hydraulic pump for controlling piston velocity, an electronic controller for maintaining an average piston velocity that is less than 0.5 feet per second, and a heat dissipator for dissipating heat from the cylinder.

대표청구항 ▼

What is claimed is: 1. A method of compressing a gas in a hydraulically driven reciprocating piston compressor that comprises a cylinder; a free floating piston disposed within said cylinder between a first closed end and a second closed end; a compression chamber defined by a volume within said cy

What is claimed is: 1. A method of compressing a gas in a hydraulically driven reciprocating piston compressor that comprises a cylinder; a free floating piston disposed within said cylinder between a first closed end and a second closed end; a compression chamber defined by a volume within said cylinder between said first closed end and said piston; and a drive chamber defined by a volume within said cylinder between said second closed end and said piston; said method comprising: (a) in an intake stroke, supplying said gas to said compression chamber; removing said hydraulic fluid from said drive chamber, whereby said gas supplied to said compression chamber is at a higher pressure than said hydraulic fluid within said drive chamber, causing said piston to move to reduce the volume of said drive chamber and increase the volume of said compression chamber until said compression chamber has expanded to a desired volume and is filled with said gas; and (b) in a compression stroke, supplying said hydraulic fluid to said drive chamber whereby said hydraulic fluid within said drive chamber is at a higher pressure than said gas within said compression chamber, causing said piston to move to increase the volume of said drive chamber and reduce the volume of said compression chamber thereby increasing the pressure of said gas held within said compression chamber; discharging said gas from said compression chamber when the pressure of said gas is increased in a single cycle to a pressure of at least 2500 psi (17.2 MPa), which is at least five times greater than the pressure of the gas supplied to said compression chamber; employing a piston stroke length to piston diameter ratio of more than even to one; and dissipating heat from said cylinder during said compression stroke whereby said gas is discharged from said compression chamber with a temperature significantly less than isentropic. 2. The method of claim 1 further comprising employing a cylinder with a piston stroke length to piston diameter ratio of between ten to one and one hundred to one. 3. The method of claim 1 further maintaining an average piston velocity that is less than or equal to 1.5 feet per second (0.46 meters per second). 4. The method of claim 1 further comprising transferring heat from said cylinder to said ambient environment through a heat dissipator. 5. The method of claim 4 wherein said heat dissipator comprises a cooling jacket disposed around said cylinder and directing a coolant to flow through said cooling jacket. 6. The method of claim 5 wherein coolant flows through said cooling jacket with a velocity that ensures there are no stagnant pockets within said cooling jacket. 7. The method of claim 5 further comprising supplying said gas to an engine and supplying said coolant from an engine coolant reservoir, but from a circuit that is independent from engine cooling circuits. 8. The method of claim 5 wherein said heat dissipator comprises a plurality of fins protruding from said cylinder and said heat dissipator operates by conducting heat from said cylinder to said plurality of fins which provides a greater surface area for transferring heat to the ambient environment. 9. The method of claim 8 further comprising blowing air through said plurality of fins to increase heat dissipation. 10. The method of claim 1 further comprising controlling when said piston reverses direction by sensing when said piston is proximate to an end of said cylinder. 11. The method of claim 1 further comprising controlling piston velocity during said compression stroke whereby said piston travels with at a first velocity during a first portion of the compression stroke and with a second velocity during a second portion of the compression stroke, wherein said second portion follows sequentially after said first portion and said second velocity is lower than said first velocity. 12. The method of claim 11 further comprising changing from said first portion of said compression stroke to said second portion of said compression stroke when gas pressure within said compression chamber exceeds a predetermined set point. 13. The method of claim 11 further comprising controlling piston velocity during a discharge portion of said compression stroke that occurs after said second portion of said compression stroke when gas is being discharged from said compression chamber, wherein piston velocity during said discharge portion is kept substantially constant. 14. The method of claim 13 wherein said piston velocity during said discharge portion of said compression stoke is equal to or less than piston velocity during said second portion of said compression stroke. 15. The method of claim 1 further comprising controlling piston velocity to follow a predetermined speed profile. 16. The method of claim 15 further comprising selecting said predetermined speed profile in response to a measured operating parameter. 17. The method of claim 16 wherein said in measured operating parameters include at least one of desired mass flow rate, inlet gas pressure, desired gas discharge pressure, and desired compression ratio. 18. The method of claim 15 further comprising selecting said predetermined speed profile from a plurality of predetermined speed profiles to control piston velocity at different times during a compression stroke, wherein said speed profiles control piston velocity to be highest near the beginning of the said compression stroke with piston velocity gradually declining to a lower velocity before stopping at the end of the compression stroke, the difference between said plurality of predetermined speed profiles can be the piston velocity at different times and/or the rate that piston velocity changes during the compression stroke, wherein of said plurality of predetermined speed profiles, said selected predetermined speed profile maximizes thermodynamic efficiency of compression for the desired mass flow rate and compression ratio. 19. The method of claim 1 further comprising gradually reducing piston velocity during a compression stroke, until said gas is being discharged from said compression chamber, and then maintaining a substantially constant piston velocity for the remainder of said compression stroke. 20. The method of claim 1 further comprising supplying a substantially constant amount of power to a hydraulic pump during a compression stroke, whereby piston velocity decreases as gas pressure within said compression chamber increases.