Vacuum toilet system

• US 3,995,328 A
• Filed: 12/13/1974
• Issued: 12/07/1976
• Est. Priority Date: 12/13/1974
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Kristoffersen, Bjorn R., Carolan, Raymond J.
• Primary Examiner(s): Haroian, Harry N.
• Application Number:
  US05/532,569
• Time in Patent Office: 725 Days
• Field of Search: 4/1, 4/10, 4/11, 4/12, 4/69, 4/76, 4/77, 4/78, 4/79, 4/80, 4/89, 4/90, 4/115, 4/216, 210/167, 210/152
• US Class Current: 4/316
• CPC Class Codes: B64D 11/02 Toilet fittings of general application A47K
• CPC Class Codes: E03D 5/016 with recirculation of bowl-cleaning fluid
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A vacuum flush waste diposal system for aircraft; wherein the required vacuum is acquired at altitude through the differential pressure between the aircraft cabin pressure and the ambient pressure above approximately 15,000 feet. When the aircraft is below this altitude or on the ground, the vacuum is provided by a blower. For flushing the toilet bowl, a timing device is initially actuated and functions: to introduce a recirculated flush fluid into a flush ring in the upper portion of the toilet bowl; and to open a drain in the lower portion of the toilet bowl, leading to the vacuum waste line; whereby, the waste and flush water are rapidly propelled through the waste line towards a centrally located holding tank, by the differential pressure acting upon it. Once in the holding tank, the waste fluid is filtered out for further use as the recirculated flush fluid.

The holding tank is positioned within the fuselage of the aircraft and has a vertically oriented filter screen separating the tank longitudinally into a fore and aft compartment, so that the acceleration forces of take-off and the deceleration forces of braking upon landing causes the fluid to slosh fore and aft through the filter screen to aid in the filtration process.

The toilet bowl incorporates integral air slots around the periphery of the toilet bowl so that there is no possibility of inadvertant injury to the user that could be caused by the sudden application of vacuum pressure to a seated occupant.

Claims

1. A vacuum flush waste disposal system for an aircraft having a pressurized passenger compartment, said system comprising:

a receptacle mounted within the pressurized passenger compartment for receiving waste;

said receptacle having an outlet from which the waste is to be extracted;

a tank for holding the waste;

a first valve means connected to said receptacle outlet;

a waste conduit interconnecting said tank with said first valve means;

a recovery system contained within the tank for producing filtered liquid;

a liquid pressure pump connected to the tank for withdrawing and pressurizing the filtered liquid;

spray means mounted within the upper portion of the receptacle for cleaning the inner surface thereof;

a second valve means operatively connected to said spray means for controlling the flow of liquid therefrom;

a flush fluid conduit connecting the liquid pressure pump with said second valve means;

means for venting the tank to ambient air pressure so as to induce a pressure differential between the tank and said first valve means, above a predetermined altitude;

an air suction pump connected to the tank for producing a predetermined vacuum pressure in the tank when the aircraft is below said predetermined altitude;

manually actuated means having an automatic cycle of operation;

connected to both said first and second valve means, for automatically opening and then closing each of said valve means after a predetermined interval of time;

thereby releasing pressurized filtered liquid through the spray means, into the receptacle and subjecting the receptacle outlet to a suction pressure corresponding to the predetermined minimum pressure differential between the tank and the pressurized passenger compartment for removal of the waste from the receptacle and for flowing the received waste through said conduit into the waste holding tank; and

said receptacle incorporating suction-break means for preventing the application of a suction force to an occupant.

2. The vacuum flush waste disposal system as set forth in claim 1, wherein:

said suction-break means comprises air vents in the upper portion of said receptacle for admitting air to the interior of the receptacle at a location other than the normal waste receiving opening, in order to prevent the possibility of injury to the user, by the vacuum force applied during the flushing cycle, in the event that the user sits down in direct contact with the receptacle, with a normally used seat in an up position, and sealingly engages the top peripheral edge of the receptacle.

3. The vacuum flush waste disposal system as set forth in claim 1 further comprising:

an overflow sensor mounted to the receptacle and connected to the manually actuated means for automatically actuating said first valve means to prevent overflow of the receptacle.

4. The vacuum flush waste disposal system as set forth in claim 1 wherein:

the bottom surface of said tank slopes to a low point from which a constant fluid pick-up is provided for the liquid pressure pump during in-flight attitude changes of the aircraft.

5. The vacuum waste disposal flush system as set forth in claim 1 wherein said recovery system comprises:

a screen filter positioned within said tank so as to divide said tank into a waste receiving compartment and a filtered liquid compartment for providing flushing fluid.

6. The vacuum waste disposal flush system as set forth in claim 5, wherein:

the filtered liquid is withdrawn from the tank through outlets located in the bottom thereof and recirculated to the waste receiving compartment for continuously removing sediments and thereby preventing solids from building up such as paper mache from tiny pulp particles and clogging the system.

7. The vacuum flush waste disposal system as set forth in claim 5 wherein:

a filter cake is formed by the accumulated entrapment of paper particles by the screen filter for producing a finer particle filtration of the withdrawn liquid as the size of the filter cake is increased.

8. The vacuum flush waste disposal system as set forth in claim 5 further comprising:

a deflector mounted adjacent to the waste conduit opening into the waste receiving compartment of the tank for directing the incoming waste against the filter to wash along the screen and aid in keeping it from clogging up.

9. The vacuum flush waste disposal system as set forth in claim 5 wherein:

said tank is mounted within the fuselage of the aircraft such that the waste receiving compartment and the filtered liquid compartment are aligned longitudinally with respect to the fuselage of the aircraft; and

said screen filter is positioned, in said tank, transversely between said longitudinally aligned waste receiving compartment and filtered liquid compartment.

10. The vacuum flush waste disposal system as set forth in claim 9 wherein:

said waste receiving compartment and said filtered liquid compartment are arranged such that the liquid contained in the waste receiving compartment is caused to seep through the screen filter due to the liquid head created by the angle of inclination of the tank when the aircraft is at a relatively high angle-of-attack as at take-off and during climb-out.

11. A vacuum powered toilet flush system for an aircraft having a pressurized passenger compartment, said system comprising:

a tank centrally located within the fuselage of the aircraft and positioned outside of the pressurized passenger compartment, for holding waste;

a recovery system contained within the tank for producing filtered flushing fluid;

a pressure system and a storage system interconnected to the tank for recovering and storing the filtered flushing fluid under pressure;

means for venting the tank to ambient air, for providing vacuum thereto above a predetermined altitude;

a vacuum blower connected to the tank for producing a predetermined vacuum pressure in the tank when the aircraft is below said predetermined altitude;

a toilet bowl mounted within the pressurized passenger compartment for receiving waste;

said toilet bowl having an outlet in the bottom thereof from which waste is to be extracted;

a first valve means connected to said toilet bowl outlet;

a waste line interconnecting said tank with said first valve means;

a toilet bowl spray ring mounted within the upper portion of the toilet bowl for cleaning the inner surface thereof;

a second valve means operatively connected to said spray ring;

a flush fluid line connecting the pressurized flush fluid storage system with said second valve means;

actuator means connected to the first and second valve means;

a toilet flush trip handle and timer mechanism operatively connected to said actuator means for controlling the actuation cycle of said first and second valve means for the admittance of flush fluid through the spray ring and vacuum pressure removal of waste from the toilet bowl to the waste holding tank; and

said toilet bowl incorporating suction-break means for preventing the application of a suction force to an occupant.

12. The vacuum powered toilet flush system as set forth in claim 11, wherein:

said suction-break means comprises air vents in the upper portion of said toilet bowl for admitting air to the interior of the toilet bowl at a location other than the normal toilet bowl waste receiving opening, in order to prevent the possibility of injury to the user, by the vacuum force applied during the flushing cycle, in the event that the user sits down in direct contact with the bowl, with a normally used seat in an up position, and sealingly engages the top peripheral edge of the toilet bowl.

13. The vacuum powered toilet flush system as set forth in claim 11 further comprising:

an overflow sensor mounted to the toilet bowl and connected to the toilet flush timer for automatically actuating said first valve means to prevent overflow of the toilet bowl.

14. The vacuum powered toilet flush system as set forth in claim 11 further comprising:

a sump located in the bottom of the tank for providing a constant fluid pick-up to the pressure system and storage system during in-flight attitude changes of the aircraft.

15. The vacuum powered toilet flush system as set forth in claim 11 wherein said recovery system comprises:

a screen filter positioned within said tank so as to divide said tank into a waste receiving compartment and a filtered liquid compartment for providing flushing fluid.

16. The vacuum powered toilet flush system as set forth in claim 15, wherein:

the filtered flushing fluid is withdrawn from the tank through outlets located in the bottom thereof and recirculated to the waste receiving compartment for continuously removing sediments and thereby preventing solids from building up, such as paper mache from tiny pulp particles and clogging the system.

17. The vacuum powered toilet flush system as set forth in claim 15 wherein:

a filter cake is formed by the accumulated entrapment of paper particles by the screen filter for producing a finer particle filtration of the withdrawn liquid as the size of the filter cake is increased.

18. The vacuum powered toilet flush system as set forth in claim 15 further comprising:

a deflector mounted adjacent to the waste line opening into the waste receiving compartment of the tank for directing the incoming waste against the filter to wash along the screen and aid in keeping it from clogging up.

19. The vacuum powered toilet flush system as set forth in claim 15 wherein:

said tank is mounted within the fuselage of the aircraft such that the waste receiving compartment and the filtered liquid compartment are aligned longitudinally with respect to the fuselage of the aircraft; and

said screen filter is positioned, in said tank, transversely between said longitudinally aligned waste receiving compartment and filtered liquid compartment.

20. The vacuum powered toilet flush system as set forth in claim 19 wherein:

said waste receiving compartment and said filtered liquid compartment are arranged such that the liquid contained in the waste receiving compartment is caused to seep through the screen filter due to the liquid head created by the angle of inclination of the tank when the aircraft is at a relatively high angle-of-attack as at take-off and during climb-out.

21. A vacuum powered toilet flush system for an aircraft having a pressurized passenger compartment, said system comprising:

a toilet bowl mounted within the pressurized passenger compartment for receiving waste;

said toilet bowl having an outlet from which the waste is to be extracted;

a tank for holding the waste;

a filter positioned with the tank so as to divide the tank into a waste receiving compartment and a filtered liquid compartment;

a waste conduit interconnecting the outlet of the toilet bowl with the waste receiving compartment of the tank;

means for venting the tank to ambient air pressure so as to induce a pressure differential between the tank and the toilet bowl outlet in the pressurized passenger compartment above a predetermined altitude;

a vacuum pump connected to the tank and operated in response to ambient air pressure below a predetermined altitude for producing a predetermined minimum pressure differential between the tank and the toilet bowl;

a liquid pressure pump connected to the filtered liquid compartment of the tank for withdrawing and pressurizing the filtered liquid;

a spray ring mounted within the upper portion of the toilet bowl and connected to the liquid pressure pump for ejecting the pressurized filtered liquid against the inner surface of the toilet bowl to cleanse it;

a spray ring valve connected to the spray ring for controlling the flow of liquid from the toilet spray ring;

a toilet bowl outlet valve connected to the toilet bowl outlet and normally retained in a closed position until opened to evacuate the toilet bowl;

manually actuated means having an automatic cycle of operation, connected to both the spray ring valve and the toilet bowl outlet valve, for automatically opening and then closing each of said valves after a predetermined interval of time;

thereby releasing the pressurized filtered liquid into the toilet bowl and subjecting the waste matter to a pressure differential corresponding to the predetermined minimum pressure differential between the tank and the pressurized passenger compartment for flowing the waste through conduits into the waste receiving compartment of the tank; and

said toilet bowl incorporating suction-break means for preventing the application of a suction force to an occupant.

22. The vacuum powered toilet flush system as set forth in claim 21, wherein:

said suction-break means comprises air vents in the upper portion of said toilet bowl for admitting air to the interior of the toilet bowl at a location other than the normal toilet bowl waste receiving opening, in order to prevent the possibility of injury to the user, by the vacuum force applied during the flushing cycle, in the event that the user sits down in direct contact with the bowl, with a normally used seat in an up position, and sealingly engages the top peripheral edge of the toilet bowl.

23. The vacuum powered toilet flush system as set forth in claim 21 further comprising:

an overflow sensor mounted to the toilet bowl and connected to the manually actuated means for automatically actuating the toilet bowl outlet valve to prevent overflow of the toilet bowl.

24. The vacuum powered toilet flush system as set forth in claim 21 further comprising:

a sump located in the bottom of the waste receiving compartment of the tank for providing a constant fluid pick-up to the liquid pressure pump during in-flight attitude changes of the aircraft.

25. The vacuum powered toilet flush system as set forth in claim 21 wherein:

flushing fluid is withdrawn from the filtered liquid compartment through outlets located in the bottom thereof and recirculated to the waste receiving compartment for continuously removing sediments and thereby preventing solids from building up, such as paper mache from tiny pulp particles and clogging the system.

26. The vacuum powered toilet flush system as set forth in claim 21 wherein:

said filter screen provides a matrix for the accumulated entrapment of paper particles to form a filter cake for producing a finer particle filtration of the withdrawn liquid as the size of the filter cake is increased.

27. The vacuum powered toilet flush system as set forth in claim 21 further comprising:

a deflector mounted adjacent to the waste conduit opening into the waste receiving compartment of the tank for directing the incoming waste against the filter to wash along the screen and aid in keeping it from clogging up.

28. The vacuum powered toilet flush system as set forth in claim 21 wherein:

said tank is mounted within the fuselage of the aircraft such that the waste receiving compartment and the filtered liquid compartment are aligned longitudinally with respect to the fuselage of the aircraft; and

said screen filter is positioned, in said tank, transversely between said longitudinally aligned waste receiving compartment and filtered liquid compartment.

29. The vacuum powered toilet flush system as set forth in claim 28 wherein:

said waste receiving compartment and said filtered liquid compartment are arranged such that the liquid contained in the waste receiving compartment is caused to seep through the screen filter due to the liquid head created by the angle of inclination of the tank when the aircraft is at a relatively high angle-of-attack as at take-off and during climb-out.