METHOD AND SYSTEM FOR MANAGEMENT OF GREY WATER IN AN AIRCRAFT
This invention relates to a method of draining grey water contained in a water holding tank of a system for management of grey water in aircraft toilets. According to the invention, the method consists of draining the grey water through an undulating diaphragm pump comprising an inlet conduit connected to the said holding tank; the pump diaphragm is able to undulate, by way of actuating means, between two flanges for draining the said grey water present in the holding tank through the inlet conduit of the pump to a discharge conduit of the pump.
1 . A method of draining grey water contained in a holding tank of a system for management of grey water in aircraft toilets, comprising: draining the grey water through an undulating diaphragm pump comprising an inlet conduit connected to the holding tank, the pump diaphragm being able to undulate between two flanges for draining the said grey water present in the holding tank through the inlet conduit of the pump to a discharge conduit of the pump.
2 . A system for management of grey water in aircraft toilets, comprising a washbasin, a water supply valve of the said basin, a grey water drainage system of the washbasin connected to a holding tank, which is equipped with a filter, and a bowl connected to the holding tank, and a main grey water tank, the bowl and the holding tank being connected to the said main tank by conduits, wherein the system comprises an undulating diaphragm pump having an inlet conduit connected to the holding tank and a discharge conduit connected to the bowl, the pump diaphragm being adapted to undulate, by way of actuating means, between two flanges for draining the said grey water present in the holding tank through the inlet conduit of the pump to the discharge conduit of the pump in order to supply grey water to the bowl.
3 . The system for management of grey water according to claim 2 , wherein the actuating means of the diaphragm pump consist of an electromagnetic linear actuator and damping means that define the stroke of the electromagnetic actuator.
4 . The system for management of grey water according to claim 2 , wherein the pump has a cylindrical case, defining a cylindrical chamber into which the inlet conduit and the coaxial discharge conduit open; the undulating diaphragm comprises a central aperture that extends directly in line with the discharge conduit.
5 . The system for management of grey water according to claim 4 , wherein the inlet conduit of the diaphragm pump extends radially in relation to the pump case.
6 . The system for management of grey water according to claim 4 , wherein the inlet conduit of the diaphragm pump extends from the opposite side of the discharge conduit, coaxially in relation to the latter.
7 . The system for management of grey water according to claim 4 , wherein the inlet conduit of the diaphragm pump is in the form of multiple vents created in the cylindrical pump case for connecting the cylindrical chamber and the external components of the pump.
8 . The system for management of grey water according to claim 2 , wherein the inlet conduit and/or the discharge conduit of the diaphragm pump contains at least one filter.
9 . The system for management of grey water according to claim 2 , wherein the diaphragm pump comprises at least one sensor, such as a pressure sensor and/or a temperature sensor and/or a grey water sensor.
10 . A system for management of grey water in aircraft toilets, comprising: a diaphragm pump having an inlet conduit connected to a holding tank and a discharge conduit connected to a bowl, the diaphragm pump being selectively undulated between two flanges for draining grey water present in the holding tank through the inlet conduit to the discharge conduit of the diaphragm pump to supply grey water to the bowl.
11 . The system for management of grey water according to claim 10 further comprising an electromagnetic linear actuator and wherein the diaphragm pump is undulated by the electromagnetic linear actuator.