Aircraft air chiller with reduced profile

Patent metadata

Field	Value
Publication number	US-10021970-B2
Application number	US-201414502930-A
Country	US
Kind code	B2
Filing date	Sep 30, 2014
Priority date	Oct 1, 2013
Publication date	Jul 17, 2018
Grant date	Jul 17, 2018

Abstract

An improved aircraft air chiller unit particularly suited for an aircraft galley that requires refrigerated or cooled beverage/meal carts and/or chilled storage compartments. The chiller of the present invention takes the form of a line replaceable unit (“LRU”) and incorporates a liquid-cooled refrigerant vapor compression cycle, arranged in a housing with a vertical orientation. Because of the vertical orientation, ducting on the rear surface of the chiller is omitted, reducing the overall footprint.

First claim

We claim:

1. A liquid-cooled, vertically-oriented chiller adapted for cooling adjacent aircraft galley carts, comprising:
(a) a housing having a length and height that is greater than a width, and characterized by an absence of ducting exterior to the housing;
(b) a plurality of fans positioned in centered alignment in a top portion of the housing along at least a portion of the length of the housing and communicating with the exterior of the housing through openings in the top portion of the housing for drawing ambient air into the housing for chilling;
(c) an evaporator positioned in the housing and extending along at least a portion of the length of the housing directly below and in lengthwise alignment with the plurality of fans for receiving the ambient air drawn into the housing by the plurality of fans and discharging air chilled by contact with evaporator coils of the evaporator as the air moves past the evaporator coils from the fans above the evaporator to below the evaporator and out of a bottom portion of the housing to the adjacent galley carts;
(d) a vapor cycle refrigerant system positioned in the housing in circuit with the evaporator, the vapor cycle refrigerant system including a compressor, a heat exchanger, a condenser, a service block at least containing a filter/drier assembly, and an expansion valve, the vapor cycle refrigerant system configured to cycle warmed refrigerant from the evaporator to the condenser cooled by a coolant circuit such that the condenser is configured to cool and condense the refrigerant, wherein the condensed refrigerant is configured to pass through the service block and through the heat exchanger configured to exchange heat between the condensed refrigerant and vapor refrigerant passing through the heat exchanger from the evaporator such that heat exchanger is configured to superheat the vapor refrigerant before entering the compressor; and
(e) the coolant circuit including the condenser, a liquid reservoir, and a liquid pump for pumping coolant through the coolant circuit, wherein the chiller components of paragraphs (b), (c) and (d) are adapted to fit within the housing, and the compressor and condenser are positioned in the housing in a laterally offset, non-airflow interference position in relation to the fans and evaporator to maximize flow of chilled air into the top portion of the housing and out of the bottom portion of the housing,
wherein the heat exchanger is positioned below the evaporator and extends from the evaporator at an oblique angle towards the bottom portion of the housing.

2. A chiller according to claim 1 , and including a quick connect/disconnect coolant tubing connection upstream of the condenser and a quick connect/disconnect coolant tubing connection downstream of the liquid refrigerant pump.

3. A chiller according to claim 1 , wherein the housing is adapted to be positioned in a galley cart bay of an aircraft galley framework.

4. A chiller according to claim 1 , wherein a first quick connect/disconnect connection is coupled to a coolant tubing that delivers coolant from the condenser to an aircraft heat sink exterior of the housing, and a second quick connect/disconnect connection coupled to a coolant tubing that delivers coolant from the aircraft heat sink to the condenser.

5. A chiller according to claim 1 , in combination with an aircraft galley framework having a plurality of laterally-adjacent galley cart bays, at least one of which bays is adapted to receive the chiller.

6. A chiller according to claim 1 , wherein the superheated vapor refrigerant prevents refrigerant droplets from entering the compressor.

7. A liquid-cooled, vertically-oriented chiller adapted for cooling adjacent aircraft galley carts, comprising:
(a) a housing having a length and height that is greater than a width, and characterized by an absence of ducting exterior to the housing;
(b) a plurality of fans positioned in centered alignment in a top portion of the housing along at least a portion of the length of the housing and communicating with the exterior of the housing through openings in the top portion of the housing for drawing ambient air into the housing for chilling;
(c) an evaporator positioned in the housing and extending along at least a portion of the length of the housing directly below and in lengthwise alignment with the plurality of fans for receiving the ambient air drawn into the housing by the plurality of fans and discharging air chilled by contact with evaporator coils of the evaporator as the air moves past the evaporator coils from the fans above the evaporator to below the evaporator and out of a bottom portion of the housing to the adjacent galley carts;
(d) a vapor cycle refrigerant system positioned in the housing in circuit with the evaporator, the vapor cycle refrigerant system including a compressor, a heat exchanger, a condenser, a service block at least containing a filter/drier assembly, and an expansion valve, the vapor cycle refrigerant system configured to cycle warmed refrigerant from the evaporator to the condenser cooled by a coolant circuit such that the condenser is configured to cool and condense the refrigerant, wherein the condensed refrigerant is configured to pass through the service block and through the heat exchanger configured to exchange heat between the condensed refrigerant and vapor refrigerant passing through the heat exchanger from the evaporator such that heat exchanger is configured to superheat the vapor refrigerant before entering the compressor; and
(e) the coolant circuit including the condenser, a liquid reservoir, and a liquid pump for pumping coolant through the coolant circuit, wherein the chiller components of paragraphs (b), (c) and (d) are adapted to fit within the housing, and the compressor and condenser are positioned in the housing in a laterally offset, non-airflow interference position in relation to the fans and evaporator to maximize flow of chilled air into the top portion of the housing and out of the bottom portion of the housing,
wherein a first quick connect/disconnect connection is coupled to a coolant tubing that delivers coolant from the condenser to an aircraft heat sink exterior of the housing, and a second quick connect/disconnect connection coupled to a coolant tubing that delivers coolant from the aircraft heat sink to the condenser,
wherein the liquid-cooled, vertically-oriented chiller is in combination with an aircraft galley framework having a plurality of laterally-adjacent galley cart bays, at least one of which bays is adapted to receive the chiller,
wherein the heat exchanger is positioned below the evaporator and extends from the evaporator at an oblique angle towards the bottom portion of the housing.

Assignees

• Be Aerospace Inc

Inventors

• Lu Qiao
• Godecker William J
• Forbes James R

Classifications

• F25D17/067

  Evaporator fan units · CPC title

• F25D11/003

  Transport containers · CPC title

• B64D11/04 Primary

  Galleys · CPC title

• B64D2013/0629

  with subsystems for cooling food, catering or special loads · CPC title

• F25B1/005

  of the single unit type (F25B1/10 takes precedence) · CPC title