Air cycle machine bypass duct
US-2024229810-A1 · Jul 11, 2024 · US
US9487299B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9487299-B2 |
| Application number | US-201213599840-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 30, 2012 |
| Priority date | Aug 30, 2011 |
| Publication date | Nov 8, 2016 |
| Grant date | Nov 8, 2016 |
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A reconfigurable vent system in fluid communication with an air chiller to deliver chill air to one or more galley food and beverage storage compartments in parallel is reconfigurable to operate in either of an air-through or an air-over orientation. The reconfigurable vent system comprises a vent in fluid communication with the air chiller via a duct and configured to provide the chill air to the one or more galley food and beverage storage compartments. The vent directs the chill air substantially toward the interior of the one or more galley food and beverage storage compartments in the air-through orientation at a first angle, and the vent directs the chill air substantially around the one or more galley food and beverage storage compartments in the air-over orientation at a second angle different from the first angle.
Opening claim text (preview).
What is claimed is: 1. A reconfigurable aircraft galley chiller vent system comprising: a first duct in fluid communication with an aircraft galley chiller and configured to receive chill air from the aircraft galley chiller; a first vent in fluid communication with the first duct and configured to provide the chill air to one or more galley food and beverage storage compartments which receive the chill air in parallel with one another, the first vent comprising: a first housing; and a chilled air outlet assembly removably fastened to the first housing, the chilled air outlet assembly configurable into an air-through orientation as well as being configurable into an air-over orientation by rotating the chilled air outlet assembly such that an interior side of the chilled air outlet assembly remains facing an interior side of the first housing, the chilled air outlet assembly including a vent panel having one or more vent openings through which air flows and a closed panel through which no air flows or less air flows in comparison with the vent panel, an edge of the closed panel is adjacent to an edge of the vent panel; wherein when the chilled air outlet assembly of the first vent is configured in the air-through orientation, the vent panel is installed at a first position of the first housing while the closed panel is installed at a second position of the first housing distinct from and adjacent to the first position such that the first vent directs the chill air substantially toward an interior of the one or more galley food and beverage storage compartments at a first angle, wherein when the chilled air outlet assembly of the first vent is configured in the air-over orientation, the vent panel is installed at the second position of the first housing while the closed panel is installed at the first position of the first housing such that the first vent directs the chill air around the one or more galley food and beverage storage compartments at a second angle different from the first angle, wherein the first angle and the second angle are relative to a horizontal plane between the first vent and the one or more galley food and beverage storage compartments, and wherein the closed panel is disposed at a third angle, the third angle being relative to a plane of the vent panel and being the absolute value of a difference between the first angle and the second angle. 2. The reconfigurable aircraft galley chiller vent system of claim 1 , wherein the chilled air outlet assembly further comprises one or more fans installed adjacent to the one or more vent openings and configured to cause air to flow through the one or more vent openings outward from the first vent. 3. The reconfigurable aircraft galley chiller vent system of claim 1 , further comprising: a second duct in fluid communication with the aircraft galley chiller and configured to provide return air to the aircraft galley chiller; a second vent in fluid communication with the second duct and configured to receive the return air from the one or more galley food and beverage storage compartments, the one or more galley food and beverage storage compartments providing the return air to the second vent in parallel with one another, the second vent comprising: a second housing; and a return air inlet assembly removably fastened to the second housing, the return air inlet assembly configurable into an air-through orientation as well as being configurable into an air-over orientation by rotating the return air inlet assembly such that an interior side of the return air inlet assembly remains facing an interior side of the second housing, the return air inlet assembly including a vent panel having one or more vent openings through which air flows and a closed panel through which no air flows or less air flows in comparison with the vent panel, an edge of the closed panel of the return air inlet assembly is adjacent to an edge of the vent panel of the return air inlet assembly, wherein when the return air inlet assembly of the second vent is configured in the air-through orientation, the vent panel of the return air inlet assembly is installed at a first position of the second housing while the closed panel of the return air inlet assembly is installed at a second position of the second housing distinct from and adjacent to the first position of the second housing such that the second vent receives the return air substantially from the interior of the one or more galley food and beverage storage compartments at a fourth angle, wherein when the return air inlet assembly of the second vent is configured in the air-over orientation, the vent panel of the return air inlet assembly is installed at the second position of the second housing while the closed panel of the return air inlet assembly is installed at the first position of the second housing such that the second vent receives the return air from around the one or more galley food and beverage storage compartments at a fifth angle different from the fourth angle, wherein the fourth angle and the fifth angle are relative to a horizontal plane between the second vent and the one or more galley food and beverage storage compartments, and wherein the closed panel of the return air inlet assembly is disposed at a sixth angle, the sixth angle being relative to a plane of the vent panel of the return air inlet assembly and, being the absolute value of a difference between the fourth angle and the fifth angle. 4. The reconfigurable aircraft galley chiller vent system of claim 3 , wherein the return air inlet assembly further comprises one or more fans installed adjacent to the one or more vent openings and configured to cause air to flow through the one or more vent openings inward to the second vent. 5. The reconfigurable aircraft galley chiller vent system of claim 1 , wherein each of the one or more galley food and beverage storage compartments comprises a trolley that moves the respective galley food and beverage storage compartment toward the first vent to establish fluid communication between the first vent and the food and beverage storage compartment, and away from the first vent to disconnect fluid communication between the first vent and the food and beverage storage compartment. 6. The reconfigurable aircraft galley chiller vent system of claim 1 , wherein the aircraft galley chiller includes: a rectangular case encasing components of a vapor cycle system, the case comprising two main surfaces having a larger surface area than four remaining surfaces of the case, a condenser, a compressor, and an evaporator, wherein the condenser, compressor, and evaporator operate as part of the vapor cycle system to provide chill air to the first duct. 7. The reconfigurable aircraft galley chiller vent system of claim 1 , wherein the aircraft galley chiller is remotely mounted from the one or more galley food and beverage storage compartments, the aircraft galley chiller comprising: a condenser, a compressor, and an evaporator, wherein the condenser, compressor, and evaporator operate as part of a vapor cycle system to provide chill air to the first duct via one or more remote chill air ducts. 8. The reconfigurable aircraft galley chiller vent system of claim 1 , wherein the aircraft galley chiller includes: a liquid to air heat exchanger coupled with a supplemental liquid cooling system that comprises a remote chiller that chills liquid coolant that flows through the liquid to air heat exchanger; and a fan that causes air to flow through the liquid to air heat exchanger to be chilled, wherein the chilled air is provided to the first duct as the chill air. 9. A method of reconfiguring a vent system including a duct in fluid
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