The present invention relates to a two-phase separator, and more particularly to two-phase separation, accumulation, and pumping that maximizes accumulating and pumping ability while minimizing power consumption.
Because of re-supply constraint in long duration missions, such as space missions, minimizing mass, volume and power are essential. Closed Advanced Life Support Systems (ALS), including Air Revitalization Subsystem, Water Revitalization Subsystem, etc., are desirable. In a typical Advanced Air Revitalization System, water is electrolyzed into oxygen (O2) and hydrogen (H2) in an oxygen generation subsystem. Water is also consumed in various hygiene needs, physiological loads and other life support functions. A typical Water Recovery System (WRS) will regenerate water from various wastewater streams.
One WRS system is a Sabatier System which is designed to recover water and does so via a reaction that produces water vapor mixed with gases (primarily methane and CO2). CO2 reacts with H2 and generates water and methane according to the following Sabatier reaction:
CO2+4H2→2H2O+CH4
The Sabatier system accomplishes this by utilizing hydrogen, carbon dioxide, and waste products from the life support system to produce water and methane.
The catalytic methanation reaction between CO2 and H2 is exothermic and self-sustainable. Water vapor generated from the Sabatier reactor can be recovered by passing the product gases through a condenser in which the water is condensed, yielding a two-phase flow (water in mostly gas stream). The recovered water is then recycled back into the life support system to provide oxygen; while the methane can be used for propulsion, or can be broken down further to recover the hydrogen. This technology is applicable not only to transit phases of exploration, but surface habitats as well as in-situ propellant production.
Accordingly, it is desirable to provide a compact and lightweight two-phase separator system which separates water from gas, accumulate the water, and pumps the water at higher pressure for downstream processing and use while minimizing power consumption.
The rotary phase separator system according to the present invention generally includes a rotary drum separator (RDS) and a motor assembly. The motor assembly drives a rotating assembly of the RDS in response to a controller which drives the RDS at two operation speeds. A low speed is used for separating and accumulating water from gas. A higher speed is used for pumping the water once the accumulator is full.
In operation, the two-phase flow (water in mostly gas stream) in input into an impeller shaft section of a hollow shaft through a two-phase inlet tap. The two-phase flow is centrifugally flung to the outer diameter of the impeller shaft section that moves the water radially outward while allowing the gas to communicate and collect within a central shaft section along an axis of rotation. The primary separating impeller provides ample flow area for the gas while maintaining small clearances to the central shaft section and thence to a gas outlet tube. A secondary separating impeller mounted within the hollow shaft facilitates separation capability and robustness to further minimize liquid (if present) injection into an inlet of the gas outlet tube.
The accumulating function is effectuated inside an accumulator section and an impeller pump section that form an annulus around the center hollow shaft. The water rotates at essentially shaft speed since it is fully enclosed by the accumulator section and the impeller pump section and has virtually no exposure to stationary walls. The “full” level of the accumulators is at the hollow shaft OD. The “empty” level of the accumulator section is at the accumulator OD. The smooth outside walls of the drums minimize power losses. A minimized diameter to length ratio also minimizes power losses. As the accumulator section and the impeller pump section fill with liquid, the gases therein are forced radially inward back into the hollow shaft toward the axis of rotation and through the shaft gas communication apertures and thence into the inlet of the gas outlet tube.
The pumping function is accomplished by the impeller pump section which is facilitated by the internal vanes between the impeller disks. Once the accumulation section is “full” the liquid is pumped through the tangential outlet located at the maximum diameter of the device to maximize both static and dynamic head.
The RDS operates on a two-speed schedule. At low speed, about 1000 rpm, the RDS creates enough of an artificial gravity field to effectively separate the gas and liquid phases. The gas port is always open when the Sabatier is in process mode generating water; therefore the vent gases flow through the RDS with very little pressure drop. Once the liquid level of the separator reaches the high end of the operating range (“full”), the controller increases the speed of the RDS to about 2000 rpm. At this speed, the pressure generated by the centrifugal and velocity forces of the liquid in the impeller shaft section of the rotating assembly is sufficient to overcome the system backpressure and the liquid empties from the RDS. The high speed condition is maintained for a sufficient length of time such that the liquid level drops to the low end of the operating range (“empty”).
The present invention therefore provides a compact and lightweight two-phase separator system which separates water from gas, accumulate the water, and pumps the water at higher pressure for downstream processing and use while minimizing power consumption.
The various features and advantages of this invention will become apparent to those skilled in the art from the following detailed description of the currently preferred embodiment. The drawings that accompany the detailed description can be briefly described as follows:
The rotary phase separator system 14 generally includes a rotary drum separator (RDS) 16 and a motor assembly 18. The motor assembly 18 drives the RDS 16 through a rotating assembly 20 (
The RDS preferably operates at two operation speeds. A low speed is used for separating and accumulating water from gas. A higher speed is used for pumping the water once the accumulator is full. It should be understood that other two-phase reduction systems will also benefit from the RDS 16 designed according to the present invention. The rotary phase separator system 14 provide for separation of methane gas and liquid water phases at about 10 psia, and pumping of the liquid to a water bus pressure of up to 18 psia. The rotary phase separator system 14 achieves this pumping at less than 100 Watts, and separation at less than 25 Watts.
Referring to
Referring to
The primary separating impeller 46 includes internal vanes 60 (
The secondary separating impeller 48 inside the hollow shaft 44 facilitates separation capability and robustness. This secondary separating impeller 48 includes internal passages 62 (
The hollow shaft 44 supports a stepped drum 50 (also illustrated in
The aspect ratio of the stepped drum 50 is preferably sized to minimize power for both the accumulating and pumping functions. The accumulator section 52 has a relatively small diameter to minimize power losses and uses axial length to accomplish volume for accumulation. The impeller pump section 54 of the drum has a larger diameter in order to achieve pumping head but has a small axial length in order to minimize power losses.
The impeller pump section 54 includes impeller disks 58 each having internal vanes 60 that facilitate the pumping function (also illustrated in
Preferably, a labyrinth type geometry seal 78 is located on outer diameter of the accumulator section 52 of stepped drum 50 to minimize the flow of a recirculation loop from high-pressure side of the pump (at the largest diameter) to the inlet side of the pump. It should be understood that various seal arrangements may be used with the present invention.
The hollow shaft 44 includes a multitude of shaft gas communication apertures 68 (also illustrated in
In operation, the two-phase flow (water in mostly gas stream) input into the impeller shaft section 72 of the hollow shaft through the two-phase inlet port 38. The two-phase flow is centrifugally flung to the outer diameter of the impeller shaft section 72 that moves the water radially outward through the liquid communication ports 70 while allowing the gas to communicate into the central shaft section 76. The primary separating impeller 46 provides ample flow area for the gas while maintaining relatively small clearance to the central shaft section 76 and thence to the inlet 64 of the gas outlet tube 56 to avoid liquid carryover. The secondary separating impeller 48 facilitates separation capability and robustness to further minimize liquid (if present) entry into the inlet 64 of the gas outlet tube 56.
The accumulating function is effectuated inside the accumulator section 52 and the impeller pump section 54 that create a stepped annulus around the center hollow shaft 44. The water rotates at essentially shaft speed since it is fully enclosed by the accumulator section 52 and the impeller pump section 54 and has virtually no exposure to stationary housing walls. The “full” level is at the OD of the hollow shaft 44. The “empty” level of the accumulator will be at the OD of the accumulator section 52. The smooth outside walls of the stepped drum 50 minimize power losses. A minimized diameter to length ratio also minimizes power losses. Notably, as the accumulator section 52 and the impeller pump section 54 fill with liquid, gases therein (if present) are forced toward the axis of rotation A and back into the hollow shaft 44 through the shaft gas communication apertures 68 and thence into the into the inlet 64 of the gas outlet tube 56.
The pumping function is accomplished by the impeller pump section 54 which is facilitated by the internal vanes 60 between the impeller disks 58. Once the accumulator section 52 is “full,” the liquid is pumped through the tangential outlet port 30 located at the maximum diameter of the impeller pump section 54 to maximize both static and dynamic head.
Preferably, the RDS 16 operates on a two-speed schedule. At low speed, about 1000 rpm, the RDS 16 creates enough of an artificial gravity field to effectively separate the gas and liquid phases. The gas outlet port 36 is open when the Sabatier is in process mode generating water; therefore the vent gases flow through the RDS 16 with very little pressure drop. Pressure port 32, the gas outlet port tap 36 and the radial port 34 (
It should be understood that relative positional terms such as “forward,” “aft,” “upper,” “lower,” “above,” “below,” and the like are with reference to the normal operational attitude of the vehicle and should not be considered otherwise limiting.
It should be understood that although a particular component arrangement is disclosed in the illustrated embodiment, other arrangements will benefit from the instant invention.
Although particular step sequences are shown, described, and claimed, it should be understood that steps may be performed in any order, separated or combined unless otherwise indicated and will still benefit from the present invention.
The foregoing description is exemplary rather than defined by the limitations within. Many modifications and variations of the present invention are possible in light of the above teachings. The preferred embodiments of this invention have been disclosed, however, one of ordinary skill in the art would recognize that certain modifications would come within the scope of this invention. It is, therefore, to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described. For that reason the following claims should be studied to determine the true scope and content of this invention.
This invention was made with government support under Contract No.: NSA898053 awarded by NASA. The government therefore has certain rights in this invention.
Number | Name | Date | Kind |
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5244479 | Dean, II et al. | Sep 1993 | A |
5693125 | Dean | Dec 1997 | A |
20030000184 | Dean | Jan 2003 | A1 |
Number | Date | Country |
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1531700 | Nov 1978 | GB |
Number | Date | Country | |
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20070256398 A1 | Nov 2007 | US |