Water walls for life support
09714183 ยท 2017-07-25
Assignee
Inventors
- Michael T. Flynn (Corte Madera, CA, US)
- Sherwin J. Gormly (Carson City, NV, US)
- Mona Hammoudeh (Alameda, CA, US)
- Tra-My Justine Richardson (Mountain View, CA, US)
Cpc classification
Y02A20/212
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y02A50/20
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B01D2259/4575
PERFORMING OPERATIONS; TRANSPORTING
C02F2201/009
CHEMISTRY; METALLURGY
B01D61/025
PERFORMING OPERATIONS; TRANSPORTING
C02F2201/001
CHEMISTRY; METALLURGY
C02F9/00
CHEMISTRY; METALLURGY
Y02A20/211
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B01D2311/08
PERFORMING OPERATIONS; TRANSPORTING
C02F2103/002
CHEMISTRY; METALLURGY
International classification
B01D61/00
PERFORMING OPERATIONS; TRANSPORTING
C02F9/00
CHEMISTRY; METALLURGY
B01D61/24
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method and associated system for processing waste gases, liquids and solids, produced by human activity, to separate (i) liquids suitable for processing to produce potable water, (ii) solids and liquids suitable for construction of walls suitable for enclosing a habitat volume and for radiation shielding, and (iii) other fluids and solids that are not suitable for processing. A forward osmosis process and a reverse osmosis process are sequentially combined to reduce fouling and to permit accumulation of different processable substances. The invention may be used for long term life support of human activity.
Claims
1. A method for processing waste liquids and waste solids aboard a spacecraft that is participating in space exploration and is subject to radiation in its space exploration activities, the method comprising: (i) providing a batch of a waste substance to be processed, comprising at least one of waste liquids and waste solids, in a first container having a semi-permeable first membrane on at least one surface of the first container, where the first membrane is impermeable to solids, does not pass liquids with high solute concentration, and does pass at least one selected liquid, comprising water, by forward osmosis action from the first container to a third container; (ii) providing a receiving liquid in the third container, where the at least one selected liquid in the first container has a positive osmotic pressure relative to the receiving liquid in the third container; (iii) allowing or causing at least a portion of the at least one selected liquid to move across the first membrane into the receiving liquid to provide, in the third container, a first mixture, comprising at least a portion of the at least one selected liquid and the receiving liquid; (iv) providing a reverse osmosis pump and a reverse osmosis membrane, connected together, and a second container; (v) allowing or causing at least a portion of the first mixture to be received by and to move through the reverse osmosis pump and, to move through the reverse osmosis membrane, and to be received in the second container, to provide a second mixture, comprising potable water, in the second container; (vi) for a time interval between first and second spaced apart times, terminating steps (i)-(v), removing from the first container a third mixture, comprising at least part of the waste solids and waste liquids that remain in the first container after at least a portion of the at least one selected liquid has moved across the first membrane, and applying the third mixture for at least one of habitat construction associated with, and radiation protection for, the spacecraft.
2. The method of claim 1, further comprising partly or fully deliquifying said third mixture before said third mixture is applied for at least one of said habitat construction and said radiation protection.
3. The method of claim 1, further comprising applying a disinfection process to said second mixture that is received by said second container from said reverse osmosis membrane system.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
DESCRIPTION OF THE INVENTION
(4) The invention comprises an assembly of membrane bags, initially packed as dry elements integrated into an inflatable or ridged habitat structure wall. After launch and deployment, the wall is initially filled with water and is maintained as a freshwater supply, thermal control mechanism and radiation shield. As the initial water supply is consumed, some of the depleted treatment bags are filled with wastewater and take on a dual role of active forward osmosis (FO) water treatment and water wall radiation shielding.
(5) When an FO element is exhausted or fouled, or stalled by presence of excessive waste side residuals, treatment ceases in that element, and the treatment element function is passed to the next bag in a sequence in the wall.
(6) Exhausted FO bag elements are drained, fluids are then mixed with feces, solid organic wastes, and/or advanced water treatment residuals, and are re-injected for sludge treatment, or simply cured in place to a stable solid. Exhausted bags now work as organic/solids composting digesters/driers. Anaerobic digestion will produce CO.sub.2 and CH.sub.4, which will be harvested, compressed and processed for use in O.sub.2 generation. Methanogenic composting will stabilize the bio-solids, producing humus. The bio-solids will then be dried using low-pressure ventilation of the bio-solids.
(7) Nitrogen-rich, urine-dominated brines, typical of a transit mission waste profile, are combined with thermally stabilized solids (charcoal and/or ash) and are aerobically treated to drive off ammonia and odor causing VOCs, to be dried to a sheet-rock like material in place, similar to gypsum. Once the humus or urine salts (sheet rock) are biologically stabilized, the bags become a permanent hydrocarbon/hydrated precipitate radiation shield and part of a habitat structure.
(8) Air treatment in a spacecraft traditionally includes the functions of thermal control, humidity control, CO.sub.2 control, and trace contaminates control. All of these functions can be accomplished to some extent by contacting cabin air with a water wall element constructed with a gas permeable membrane. This water wall element would be separate from the water/solids treatment wall element described previously.
(9) Humidity control is commonly accomplished in a spacecraft by the use of a condensing heat exchanger. A condensing heat exchanger operates by reducing the dew point of a gas such that water vapor condenses out of it and the resulting gas achieves a targeted relative humidity value as the gas leaves the exchanger. Membrane-based condensers can be used as condensing heat exchangers. These membrane condensers can be adapted to use the osmotic potential of salt water across a hydrophilic membrane to cause water vapor to condense.
(10) The approach used in the WW is driven by a combination of thermal and osmotic differences. Osmotic pressure differences are used to control latent energy and to condense water out of the atmosphere, while thermal control is used to control sensible energy and to maintain the cabin air at a specific temperature. In this process, water on one side of a membrane is maintained at a specified temperature, and the osmotic potential is adjusted to condense water out of the air, which is in contact with the other side of the membrane. The liquid water is then treated in a desalination system, which is returned to the water wall at the appropriate temperature and osmotic potential to repeat the process in a continuous cycle. The water removed in the desalination system is then processed to potable water standards.
(11) Carbon dioxide is sparingly soluble in water. However, once solubilized, CO.sub.2 can either be converted to carbonic acid (depending on the solution pH), adsorbed by liquid amines, by other liquid or by particulate adsorbent materials in solution, or consumed by organisms and converted to oxygen and biomass through photosynthesis or alkaline carbonate formation and other mineral or organic endpoints. Thus, a water/membrane gas contactor can be used to strip CO.sub.2 from cabin air as long as the carbonate ions are removed at a rate in proportion to the solubility restricted diffusion rate of CO.sub.2; this may require some pH control. The key to such a process is to provide enough gas/liquid contact area to compensate for the low solubility and diffusion limits of CO.sub.2 in water. The WW membrane provides an ideal construction for such an interface, because the inside surface area of the habitat is quite large.
(12) Levels of semi-volatile compounds in a spacecraft atmosphere can be controlled by contacting the atmosphere with liquid water. In such a construct, the maximum level of a given semi-volatile compound in the atmosphere can be calculated using the Henry's Law constant associated with the compound. If the liquid concentration of the compound is kept low, by processing the compound through a bioreactor, catalytic reactor or adsorbent bed, this non-equilibrium between the liquid phase and the gas phase will strip semi-volatile organics from the atmosphere. Some semi-volatiles with boiling points below that of water will not be completely removed so that a secondary biological or physical chemical system may be required.
(13) Removal or volatile organic carbon (VOC) may be accomplished by photo-catalysis. The inner liner of the inflatable habitat will be made of a woven silk material impregnated with titanium dioxide. Titanium dioxide is a photo-catalyst when illuminated by ultraviolet (UV) light, and when doped with nitrogen ions or tungsten trioxide TiO.sub.2 is also a visible light photo-catalyst. The inner walls of the habitat provide enough surface area to treat most volatile organics, even if conversion rates are low. The light source is the interior lighting of the habitat. The impact of day/night illumination on atmospheric VOC concentrations will have to be evaluated and there may be a need for supplemental biological or physical chemical VOC removal capability.
(14)
(15) The power module (PEM) 11 produces N.sub.2 as an output, which is received by an algae growth module 15. The algae growth (AG) module also receives N.sub.2 and clean water from the graywater/urine (GW/U) module 12, receives clean water, fertilizer and ammonium brine from the blackwater/solids (BW/S) module 16, and receives light or electromagnetic energy from an ambient light source. The algae growth (AG) module 15 produces N.sub.2, CO.sub.2 and O.sub.2 as outputs. The graywater/urine (GW/U) module 12 receives (non-clean) water from the air revitalization (AR) module 14 and NH.sub.3 brine from the blackwater/solids (BW/S) module 16 and condensate from other sources, and produces clean water, which is received by the algae growth (AG) module 15 and by the air revitalization (AR) module 14. The air revitalization module 14 receives clean water from the graywater/urine module 12 and from the humidity/thermal control module 13, receives CO.sub.2 and (alkaline) CO.sub.3 or another carbonate from other sources, and produces O.sub.2 and (non-clean) water as outputs. The humidity/thermal control module 13 receives humid air as an input from human activity and produces clean water as an output. The blackwater/solids (BW/S) module 16 receives blackwater, solids, and ammonium brine as inputs and produces (non-clean) water and fertilizer as outputs. Table 1 sets forth the inputs and outputs for each of the six modules. Here, HA in Table 1 refers to a module input that arises primarily from human activity.
(16) TABLE-US-00001 TABLE 1 Module Inputs and Outputs. Inputs. Outputs. PEM Cell Clean H.sub.2O (GW/U, N.sub.2 (AG) H/TC) H.sub.2O w. protons Organic fuel (BW/S) Algae Growth N.sub.2 (PEM, GW/U) N.sub.2 CO.sub.2 (AR) O.sub.2 Light (ambient) nutrition suppl. Fertilizer (BW/S) NH.sub.3 brine (BW/S) H.sub.2O (BW/S) Clean H2O (GW/U) Blackwater/Solids Black water (HA) Organic fuel (PEM) NH.sub.3 brine (AG) H2O (AG) Salts (HA) Fertilizer (AG) Humidity/Thermal Control Humid air clean H.sub.2O (AR, PEM) Air Revitalization (AR) Clean H.sub.2O (GW/U, (Alk)CO.sub.3 H/TC) CO.sub.2 (AR) O.sub.2 H.sub.2O (GW/U) H.sub.2O w. protons Graywater/Urine Gray water (HA) Clean H.sub.2O (AR, AG) Urine (HA) N.sub.2 (AG) Condensate (HA) NH3 brine (BW/S) H.sub.2O (AR)
(17) The functional flow diagram of
(18) A proton exchange medium (PEM) cell can use organic material, including waste, effluent and other residuals to generate electrical power. Some systems utilize a two-stage electrochemical process that first electrolyzes organics and water to supply H.sub.2 and O.sub.2 (stage 1). In stage 2, the O.sub.2 supplies oxygen for the crew, and the H.sub.2 is used to produce fuel, such as CH.sub.4.
(19) Table 2 illustrates a minimum number of bags with different functionalities that would be needed for one embodiment for estimated proportional sizing. The bags do not have uniform volume outputs, and a particular output of a bag may be allocated as an input for more than one bag having a different functionality.
(20) TABLE-US-00002 TABLE 2 Sizing of Water Wall Bags and Cells. Type of bag. No. of bags or cells. Algae growth (AG) 1 Blackwater/solids (BW/S) 5 Humidity/thermal control (H/TC) 6 Graywater/urine (GW/U) 10 Air revitalization (AR) 20 PEM 1
(21)
(22) When the solute is a salt, a portion of the solvent (initially part of the AW) that passes across the membrane 23 is received by an FO receiving liquid and by a desalinator, such as a reverse osmosis (RO) pump 24, which is connected to an RO membrane element 25 that provides a filtering action, passing low solute liquids LSL and holding or diverting fluids having a higher solute concentration. The LSL is subsequently collected in a second container 26 and is processed to convert a substantial portion to potable water and other useful liquids and gases.
(23) The AW solids and liquids are periodically removed from the container 21, dried or partly de-liquefied, and converted to habitat construction and/or to radiation protection material, for incorporation in one or more habitat walls. This de-liquefied material preferably includes some water and/or other low molecular weight liquids, which can serve as radiation protection material for the habitat structure. The habitat walls are movable and expandable to allow adjustment (e.g., increase) of the enclosed habitat volume used by the human participants and/or for implementing the project.
(24) An alternative approach uses a membrane-encased algae bioreactor segment of the water wall to strip CO.sub.2 and convert the substance into O.sub.2. Bio-air scrubbing has been used in industrial air pollution control, and more particularly for odor control for some time. Models for trace contaminant control can be constructed based on these industrial air pollution control systems. The technology of gas exchange membranes is well developed and can also be applied. Such a system could be very effective, but would likely require re-supply of nitrogen, because the amount of nitrogen available in the waste model is insufficient to support full CO.sub.2 conversion requirements. However, nitrogen is normally lost in the atmosphere due to spacecraft leakage and EVA, and re-supplying nitrogen as a fertilizer may offer benefits to re-supply when compared with tanked high-pressure gas.
(25) Anaerobic digestion will produce CO.sub.2 and CH.sub.4 gases, which can be harvested, compressed and processed for use in O.sub.2 generation. Ammonia and VOCs handling and control may be more flexible, depending on composition of the waste stream. Methanogenic composting will reduce the water content support diversion of this water, and stabilize the bio-solids.
(26) The WW approach supports and allows implementation of water recycling, air scrubbing and treatment, temperature control, humidity control, treatment and re-deployment of solids residuals that cannot be re-used for their original purpose, strengthening of the habitat walls, and provision of radiation shielding.
(27) Water bags may have pervaporation membranes oriented facing inward and can support removal of CO.sub.2 and trace organics from the ambient air.
(28) Air treatment in a spacecraft is traditionally includes the functions of thermal control, humidity control, CO.sub.2 control, and trace contaminant control. All of these functions can be accomplished to some extent by contacting cabin air with a water wall element constructed as a filter with a gas permeable membrane. The water wall element would be separate from the water/solids treatment wall element described in the preceding.
(29) Humidity control is commonly accomplished in a spacecraft by use of a condensing heat exchanger. A condensing heat exchanger operates by reducing the dew point of a gas so that water vapor condenses out of the gas, and the resulting gas achieves a targeted relative humidity as the gas leaves the exchanger. Membrane-based condensers can be used as condensing heat exchangers. These membrane condensers can be adapted to use the osmotic potential of salt water across a hydrophilic membrane to cause water vapor to condense.
(30) The approach used in the water wall relies on a combination of thermal and osmotic pressure differences. Osmotic pressure differences are used to control latent energy and to condense water out of the atmosphere. Thermal control is used to control sensible energy and to maintain the cabin air within a reasonable temperature range. In this process, water on one side of a membrane is maintained at a specified temperature and the osmotic potential is adjusted to condense water vapor out of the air that is in contact with the other side of the membrane. The liquid (mostly water) is then treated in a desalination system, which is returned to the water wall at the appropriate temperature and osmotic potential to repeat the process in a continuous sequence of cycles. The water removed in the desalination system is then treated to achieve potable water standards.
(31) Volatile organic carbon (VOC) removal may be accomplished by photo-catalysis. The inner liner of the inflatable habitat will be made of a woven silk material impregnated with titanium dioxide. Titanium dioxide is a photo-catalyst under ultraviolet (UV) light; when doped with nitrogen ions or tungsten trioxide TiO.sub.2 is also a visible light photo-catalyst. The inner walls of the habitat provide enough surface area to treat most volatile organics even if conversion rates are low. The light source is the interior lighting of the habitat. The impact of day/night illumination on atmospheric VOC concentrations will have to be evaluated and there may be a need for supplemental biological or physical chemical VOC removal capability.
(32) The FO process is adaptable and can be incorporated into the water wall bounding material that is used for inflatable structures. An FO bag would normally be packed as part of a flexible and inflatable habitat structure wall. The FO bag may be initially inflated with sterile saline water and initially maintained as part of a fresh water supply and radiation shield. As the initial water supply is consumed, the treatment bags are filled with waste water and serve a dual purpose, for active FO fluid treatment and for radiation shielding. Several different membrane materials are available to support forward osmosis, including cellulose tri-acetate.
(33)
(34) In a first mode of operation, for processing liquid and providing potable water, the valves 1, 4 and 5 are open and the valves 2, 3 and 6 are closed. The upstream region 30-1 of the FO bag 30 receives liquids from the graywater/blackwater processing tank 33 and/or from the solids processing tank 39. The downstream region 30-2 of the FO bag 30 contains a liquid(s) with solute and solvent, having a low osmotic potential (e.g., containing one or more salts, such as CaCO.sub.3 or MgCO.sub.3 or NaCl, relative to osmotic potential of the anticipated liquids received in the upstream region 30-1. A portion PL of the liquids, mostly water, in the upstream region 30-1 passes through the membrane 31 and into the downstream region 30-2. The liquids PL are received by the RO pump 35 and forcibly passed through the RO module 36 (optionally including an RO membrane), through the disinfectant module 37 (optional) and are collected in the potable water collector 38. Most of the remaining solutes in the liquids PL remain on the upstream side of the RO module 36.
(35) In a second mode of processing, which removes most of the residuals from the upstream region 30-1 associated with the FO bag 30, the valves 1 and 3 are closed and the valves 2, 4 and 5 are open. The remaining liquids in the upstream region 30-1 of the FO bag are circulated through the solids processing tank 37 and/or through the graywater/blackwater processing tank 33 to remove most of the residuals. After removals of most of these residuals, the remaining liquids, including some solutes and solvents, will circulate through the upstream region 30-1 of the FO bag 30 and may produce additional potable water.
(36) In a third mode of processing, to remove further solid waste, the valves 1, 2 and 5 are closed, valves 3 and 4 are open, and valve 6 may be open. The remaining liquids and solutes in the upstream region 30-1, which may be mostly solids, and some gases may be vented through the gas vent valve 6.
(37) In a fourth mode of processing, the valves the valves 3, 4 and 6 are open, valves 1, 2 and 5 are closed and the system acts to digest the solid waste (accumulated in the solids processing tank 39 and to vent the resulting gas produced by waste-digesting micro-organisms through the gas vent valve 6.