This application is based on and claims the priority under 35 U.S.C. §119 of German Patent Application 102 29 799.1, filed on Jul. 3, 2002, the entire disclosure of which is incorporated herein by reference.
The invention relates to a method and apparatus for processing and re-using of gray water for the flushing of toilets, particularly in vacuum toilet systems used in aircraft to optimize the use of available water.
Commercial aircraft currently carry fresh water for the flushing of vacuum operated toilets in these aircraft. Moreover, the lavatory basins also use freshwater which, by its use in the handwash basin becomes so called “gray water”. Thus, in the passenger lavatories substantial quantities or volumes of gray water are produced, which conventionally are not used for any further purpose. The inventors have discovered that following a simple treatment or processing of this gray water it would be quite suitable for use as toilet flushing water.
In view of the foregoing it is the aim of the invention to achieve the following objects singly or in combination:
According to the invention there is provided a method for processing and reusing gray water for flushing a toilet, comprising the following steps:
According to the invention there is further provided an apparatus for processing and reusing gray water, said apparatus comprising:
The accompanying
The block diagram of
The gray water after passing through the coarse filter 3 and the fine filter 4 is collected in the processing tank or treatment chamber 5 for a further treatment by an anodic oxidizer 9 controlled by a central control unit 7.
The treatment chamber 5 in which the gray water is collected, is equipped with an overflow 6 that leads into a gray water collecting conduit 19. The excess gray water taken up by the overflow 6 is either used in a tank cleaning system for cleaning a wastewater collecting tank 20B, including a gray water collecting tank or container 19A located near the wastewater collectinp tank 20B, a pressure increasing pump and at least one spray nozzle (not shown). Alternatively, any excess processed water can be fed to a discharge or drainage mast for discharge outside the aircraft body.
The treatment chamber or processing tank 5 is also equipped with preferably at least two water level sensors LIS21 and LIS22 which provide their sensor signals to the central processing unit 7 which processes the sensor signals to form control signals. If the water content, or rather the treated water content in the treatment chamber or processing tank 5 reaches the low level sensed by the sensor LIS22, the respective signal is processed to provide a control signal for the controller 1A of the faucet 1 to thereby replenish the water in the treatment tank 5 with fresh water from the fresh water source 18. This replenishing takes place automatically through the lavatory basin 2 and is preferably performed when the respective toilet is unoccupied. For this purpose a toilet door switch 15 and an infrared sensor 16 are used to provide their respective signals to the central processing unit 7, which in turn provides a control signal through an electrical connection 1D to the faucet 1. The automatic replenishing is disabled when the toilet is occupied so as not to startle a user when the faucet would open automatically. The replenishing is stopped when the water level in the tank 5 reaches the position of the upper or maximum level sensor LIS21.
It is also possible to preset, in the central processing unit 7, a defined temperature range for the water passing through the faucet 1. The heater 1B is controlled appropriately by the central processing unit 7 so as to maintain the temperature of the water in the defined temperature range.
The flushing of a toilet bowl 11 is initiated by a flushing or rinsing button 14 that also delivers its signal to the central processing unit 7 for starting a motor M that drives a pump 8 for increasing the pressure of the water coming from the tank 5 through a conduit 8A. The pressure is increased until an excess pressure valve 13, operable by the central control unit 7 through a solenoid 13A, opens, to supply flushing water through the nozzles 12 into the toilet bowl 11 for rinsing the toilet bowl. The control unit 7 provides a time interval following the operation of the button 14. At the end of this time interval the motor M is switched off again. Simultaneously, the central control unit 7 energizes a vacuum toilet flushing system or suction device 10 also for a defined time interval, whereby any blackwater containing feces or the like is sucked into the vacuum wastewater system 20 which is equipped with a separate wastewater conduit 20A. According to the invention the fresh water supply conduit 18A, the gray water collecting conduit 19 and the wastewater conduit 20A are entirely separate from each other. In other words, there is no direct connection between these conduits 18A, 19 and 20A.
The control, closed loop control, and monitoring of the above described replenishing operation, pumping operation, and flushing operation and the power supply to the pump, valves and vacuum flushing system 10 is performed by the central control unit 7 which in turn communicates with other system components in the aircraft through a so-called CANBUS 17, also referred to as a communication area network.
As described herein, water is replenished into the processing tank 5 from the faucet 1 through the lavatory basin 2. This can be carried out in different ways, for example as follows. The water replenishment may involve detecting at least one filling level in the processing tank 5 as a minimum filling level with the sensor LIS22, producing a control signal as a minimum level control signal from the sensor LIS22 for controlling the fresh water supply faucet 1 of the lavatory basin 2 for replenishing water in the processing tank 5 to a medium filling level from the fresh water supply faucet 1. Alternatively the water replenishment may involve sensing a plurality of filling levels including a high filling level with the sensor LIS21 and a low filling level with the sensor LIS22 in the processing tank 5 to produce respective high filling level and low filling level control signals for controlling the fresh water supply through the faucet 1 and the lavatory basin 2 so that a larger fresh water volume is supplied into the processing tank 5 through the faucet 1 and lavatory basin 2 in response to the low filling level signal and a smaller fresh water volume is supplied into the processing tank 5 through the faucet 1 and lavatory basin 2 in response to the high filling level control signal. Also, the water discharge or withdrawal from the processing tank 5 may involve sensing a plurality of filling levels including a maximum filling level with the sensor LIS21 and a minimum filling level with the sensor LIS22 in the processing tank 5 to produce respective higher and lower filling level control signals for controlling the withdrawal of processed water from the processing tank 5 so that more processed water is withdrawn from the processing tank 5 in response to the higher filling level control signal and less processed water is withdrawn from the processing tank 5 in response to the lower filling level control signal.
Instead of using a rotary pump, the pump 8 could be a piston cylinder pump 80 shown schematically in
Advantages of the invention are seen in that the use of fresh water is noticeably reduced, whereby it is now possible to use smaller freshwater tanks in an aircraft, thereby reducing the required fresh water volume with the added benefit of reducing the starting weight of the aircraft, which in turn positively influences the payload or the fuel consumption.
Yet another advantage is seen in that the anodic oxidizing of the gray water as taught by the invention obviates the use of a so-called recharge liquid which is a disinfectant that is mixed into the gray water or wastewater so that the wastewater tank does not require a separate disinfection. Again, obviating the need for a disinfection agent reduces the starting weight of the aircraft with the same positive effects regarding the payload and the fuel consumption as mentioned above.
Another advantage is seen that by not using the so-called disinfecting agent no water is produced that requires a special handling of the respective wastewater on the ground when servicing an aircraft which is conventionally rather expensive. By using the anodically oxidized gray water as taught by the invention as a toilet rinsing water, the resulting wastewater can be discharged directly into sewage treatment plants on the ground. Furthermore, the anodically oxidized rinsing water acts as a preventive agent against the formation of a so-called biofilm in toilets and respective wastewater conduits.
A further advantage is seen in that the present system can work with noticeably higher rinsing pressures than are conventionally possible. This has a positive influence since less water can be used for the toilet flushing, while even better cleaning results are achieved.
The control of all toilet facilities and their respective components takes place by a single control unit 7. The connection to other aircraft systems is possible through the above mentioned simple so-called CANBUS 17, which is available in the aircraft anyway and thus no further efforts and expenses are necessary for an individual wiring system.
Although the invention has been described with reference to specific example embodiments, it will be appreciated that it is intended to cover all modifications and equivalents within the scope of the appended claims. It should also be understood that the present disclosure includes all possible combinations of any individual features recited in any of the appended claims.
Number | Date | Country | Kind |
---|---|---|---|
102 99 799 | Jul 2002 | DE | national |
Number | Name | Date | Kind |
---|---|---|---|
3318449 | Jennings et al. | May 1967 | A |
3774246 | Beer | Nov 1973 | A |
3939499 | Roberts | Feb 1976 | A |
4713525 | Eastep | Dec 1987 | A |
5035011 | Rozenblatt et al. | Jul 1991 | A |
5106493 | McIntosh | Apr 1992 | A |
5147532 | Leek, Jr. | Sep 1992 | A |
5245711 | Oldfelt et al. | Sep 1993 | A |
5421040 | Oldfelt | Jun 1995 | A |
5454936 | Ask et al. | Oct 1995 | A |
5611088 | Almon | Mar 1997 | A |
6143185 | Tracy et al. | Nov 2000 | A |
6319390 | Kono et al. | Nov 2001 | B1 |
6463956 | Walker | Oct 2002 | B1 |
20040031761 | Wunsche et al. | Feb 2004 | A1 |
20040133968 | Hoehne et al. | Jul 2004 | A1 |
20050126927 | Lindauer et al. | Jun 2005 | A1 |
Number | Date | Country |
---|---|---|
3500130 | Jul 1986 | DE |
G8717458 | Apr 1989 | DE |
3809888 | Oct 1989 | DE |
3901320 | Jun 1990 | DE |
4328014 | Jan 1994 | DE |
G9410633 | Sep 1994 | DE |
G 94 17 730 | Feb 1995 | DE |
4429201 | Feb 1996 | DE |
296 18 711 | Feb 1997 | DE |
197 17 579 | Oct 1998 | DE |
0 653 520 | May 1995 | EP |
06273171 | Sep 1994 | JP |
Number | Date | Country | |
---|---|---|---|
20040045910 A1 | Mar 2004 | US |