System for cooling food in an airplane

• US 5,513,500 A
• Filed: 11/28/1994
• Issued: 05/07/1996
• Est. Priority Date: 11/26/1993
• Status: Expired due to Term

• Current Assignee: Daimlerchrysler North America Corporation (Mercedes-Benz Group AG)
• Original Assignee: Daimler-Benz AG (Mercedes-Benz Group AG)
• Inventors: Fischer, Juergen, Fischer, Heinz, Scherer, Thomas
• Primary Examiner(s): Tapolcai, William E.
• Application Number:
  US08/345,910
• Time in Patent Office: 526 Days
• Field of Search: 62/237, 62/239, 62/430, 62/435, 62/438
• US Class Current: 62/239
• CPC Class Codes: B64D 11/0007 Devices specially adapted for food or beverage distribution services
• CPC Class Codes: B64D 11/04 Galleys
• CPC Class Codes: B64D 13/00 Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space , or structural parts of the aircraft treatment rooms with artificial climate for medical purposes A61G10/02; respiratory apparatus in general A62B; for vehicles in general B60H
• CPC Class Codes: B64D 2013/0629 with subsystems for cooling food, catering or special loads
• CPC Class Codes: F25D 17/02 for circulating liquids, e.g. brine
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

A cooling system is provided for cooling food in an aircraft while the food is stored in known catering trolleys that are stowed at prescribed stowage locations, preferably for example at least one on-board galley (3A to 3E) within the aircraft cabin. The cooling system includes at least one central cooling plant (4) located below the cabin floor of the aircraft. Heat exchanger units (9A, 9B, 17A, 17B) are provided in the galleys (3A to 3E). A distribution conduit system, including a supply conduit (5) and a return conduit (6) as well as connector conduits (10A, 10B, 11A, 11B), couples the central cooling plant (4) with the respective heat exchangers (9A, 9B, 17A, 17B) arranged in the galleys (3A to 3E). Connector adapters are provided at various locations along the supply conduit (5) and the return conduit (6), and the connector conduits (10A, 10B, 11A, 11B) include quick connectors that are connectable to the adapters. The galleys may quickly and easily be repositioned as desired within the cabin to achieve different cabin layouts. The heat and noise of the cooling plant is removed from the cabin to an underfloor space, and a more efficient installation and reconfiguration of the system, as well as an overall space and weight saving, is achieved.

Claims

1. A cooling system for cooling food stored in portable storage containers that are stowed in stowage locations in two or more galleys within a passenger cabin of a pressurized aircraft, the aircraft having a fuselage enclosing the passenger cabin and a hold and a cabin floor arranged within said fuselage, said cooling system comprising at least one central cooling plant arranged in said aircraft below said cabin floor outside said passenger cabin, at least one heat exchanger arranged external to said storage containers at each of said stowage locations, a cooling medium, and a cooling medium distribution conduit system connecting said cooling plant with said heat exchangers, wherein said conduit system includes a supply conduit and a return conduit each connected with said cooling plant, and connector conduits connecting said heat exchangers with said supply and return conduits.

2. The cooling system of claim 1, comprising only one said cooling plant.

3. The cooling system of claim 1, wherein said supply and return conduits are arranged below said cabin floor and extend over substantially the entire length of said cabin.

4. The cooling system of claim 1, further comprising respective quick connectors provided on respective ones of said connector conduits and adapted to couple said respective connector conduit to one of said return and supply conduits at one of a plurality of coupling locations along said return conduit and said supply conduit, and comprising connector adapters provided at said plurality of coupling locations along said return conduit and said supply conduit, and wherein said quick connectors are adapted to couple said connector conduits to said adapters.

5. The cooling system of claim 1, wherein said cooling medium is a liquid coolant, and said conduits of said distribution conduit system are liquid coolant conduits.

6. The cooling system of claim 1, wherein said cooling medium is a vaporizable refrigerant, said supply conduit is a liquid refrigerant supply conduit, said return conduit is a vapor refrigerant return conduit, and said heat exchanger is an evaporator.

7. The cooling system of claim 1, wherein said distribution conduit system further comprises a pump adapted to convey said cooling medium through said distribution conduit system.

8. The cooling system of claim 1, wherein said cooling plant comprises a compression cooling plant.

9. The cooling system of claim 1, wherein said cooling plant comprises a fuselage skin heat exchanger arranged on said fuselage.

10. The cooling system of claim 1, wherein said cooling plant comprises a liquid/air heat exchanger adapted to be cooled by a primary cooling air flow, wherein said aircraft further includes air conditioning packs, and wherein said primary cooling air flow is a cooled air flow provided by said air conditioning packs.

11. The cooling system of claim 1, wherein said cooling plant comprises an adsorption cooling apparatus.

12. The cooling system of claim 6, wherein said cooling plant comprises an adsorption cooling apparatus.

13. The cooling system of claim 5, wherein said liquid coolant is a water/glycol mixture.

14. The cooling system of claim 4, wherein the number of said coupling locations along said conduits is greater than the number of said galleys, and wherein said quick connectors removably couple said connector conduits to said adapters to allow the flexible relocation of said galleys within said cabin.

15. The cooling system of claim 1, further comprising a respective closed-loop secondary cooling air circuit including air ducts arranged at each of said stowage locations and connecting said heat exchangers with said storage containers to circulate air respectively in a closed loop through one of said heat exchangers and through at least one of said storage containers.

16. The cooling system of claim 15, wherein said closed-loop secondary cooling air circuit further includes a blower to drive said circulation of air in said closed loop.

17. The cooling system of claim 1, wherein said heat exchangers are connected parallel to each other to said conduits.

18. The cooling system of claim 1, further comprising an air duct system connecting a plurality of said storage containers in parallel to each other to one of said heat exchangers to form a closed airflow loop through said heat exchanger, said air duct system and said plurality of said storage containers.

19. The cooling system of claim 1, wherein said portable storage containers are at no time connected hydraulically to said distribution conduit system.