An environmental control system (ECS) includes an air cycle machine (ACM) subsystem that is in a heat exchange relationship with one or more liquid cycle subsystems. Compressed air which exits a compressor section of the ACM is communicated to a reheater and a condenser to further cool the water vapor bearing air by condensing and separating the water into a water extractor. Dehumidified air exits the extractor and is communicated to an air-liquid heat exchanger to absorb a first heat load. The heated dehumidified air recovers thermal energy from the air-liquid heat exchanger and is expanded over a first turbine. The expanded air is communicated through the condenser and reheater such that the expanded air absorbs thermal energy therefrom. The recovered thermal energy in the expanded air then used by a second turbine to increase its efficiency. The expanded air from the second turbine is placed in the thermal exchange with a second air-liquid heat exchanger to absorb a second heat load.
Cabin Air Temperature Control With Cooling Of Recirculated Air
Gregory Defrancesco - Simsbury CT Thomas Zywiak - Suffield CT
Assignee:
Hamilton Sundstrand - Windsor Locks CT
International Classification:
F25D 900
US Classification:
62401, 62172
Abstract:
A cabin air temperature control system includes cooling recirculated air. A first air circuit includes an intake that receives air from outside the cabin and then conditions the air to bring it closer to a desired cabin temperature before the air is introduced into the cabin. A second air circuit recirculates air from the cabin and then reintroduces it back into the cabin. The second circuit includes an air cooling assembly, comprising a heat exchanger, that is selectively used to cool the recirculated air before it is reintroduced into the cabin. A bypass flow arrangement is provided to selectively direct the recirculated air through the air cooling assembly or to simply recirculate it back into the cabin depending on the current temperature adjustment needs.
Louis J. Bruno - Ellington CT Thomas Zywiak - Suffield CT Harold W. Hipsky - Willington CT
Assignee:
Hamilton Sundstrand - Windsor Locks CT
International Classification:
F25D 900
US Classification:
62402, 62 86
Abstract:
An aircraft air conditioning air supply system is provided that includes a primary propulsion turbine engine having a bleed valve providing pressurized air. A ram air inlet provides ram air. A super charger includes a spool with at least two turbines mounted thereon driven by the pressurized air from the engine. At least one compressor is connected to the turbines, preferably mounted on the same spool as the turbines, and receives the ram air. The turbines drive the compressor and compresses the ram air for use by an air conditioning pack. The supercharger provides compressed air to an air conditioning pack that conditions the compressed air and distributes the refrigerated air throughout the aircraft. The number of turbines and compressors for the super charger is selected by matching the specific speeds of the compressors and turbines.
An inerting system provides air with reduced oxygen content by flowing and directing air through an air separation module. Optimal working pressure for the air separation module is obtained with two compressors. A first compressor elevates air from the aircraft cabin to a second pressure. The second pressure is at an intermediate level below the working pressure of the air separation module. A second compressor elevates air from the second pressure to the working pressure. The second compressor is driven by air that is exhausted through a turbine. The pressure difference between air at the working pressure and air required by the fuel distribution system is used to power the turbine and drive the second compressor.
Charles J. McColgan - West Granby CT, US Christopher G. Haddad - West Willington CT, US Thomas M. Zywiak - Suffield CT, US
Assignee:
Hamilton Sundstrand - Windsor Locks CT
International Classification:
B64D013/08
US Classification:
2441185, 236 13, 454261
Abstract:
A mixer includes a fresh air tube defining a passage having an inlet receiving conditioned air from an air conditioning pack. The fresh air tube includes an outlet providing mixed air to a cabin of the aircraft. An outer tube at least partially surrounds the fresh air tube and receives recirculated air from the cabin. Multiple holes in the fresh air tube fluidly connect the outer tube to the fresh air tube. The warm recirculation air surrounds the portion of the fresh air tube to heat it preventing ice from forming. The warm recirculation air entering the fresh air tube through the holes homogeneously mixes with the conditioned air from the pack to provide a uniform mixture of air within the fresh air tube, which further ensures the prevention of ice build up.
Air Cycle Air Conditioning With Adaptive Ram Heat Exchanger
An air conditioning pack for an aircraft provides primary and secondary heat exchangers arranged in a ram air duct. A third heat exchanger is arranged in the ram air duct and is fluidily connected to the primary and secondary heat exchangers. The overall or combined size of the primary, secondary, and third heat exchangers is less than that of the typical primary and secondary heat exchangers of the prior art. A combination of heat exchangers is used to provide cooling during worst case scenarios enabling efficient use of the overall heat exchangers configuration to provide the desired cooling capacity.
Aircraft Air Conditioning System Mixer With Corrugations
Charles J. McColgan - West Granby CT, US Christopher G. Haddad - West Willington CT, US Thomas M. Zywiak - Suffield CT, US
Assignee:
Hamilton Sundstrand - Windsor Locks CT
International Classification:
B64D013/08
US Classification:
2441185, 454 76
Abstract:
A mixer includes a fresh air tube defining a passage having an inlet receiving conditioned air from an air conditioning pack. The fresh air tube includes an outlet providing mixed air to a cabin of the aircraft. An outer tube at least partially surrounds the fresh air tube and receives recirculated air from the cabin. A circumferential corrugation in the fresh tube forms multiple lobes in the fresh air tube fluidly connect the outer tube to the fresh air tube. The warm recirculation air surrounds the portion of the fresh air tube to heat it preventing ice from forming. The warm recirculation air entering the fresh air tube through the lobes homogeneously mixes with the conditioned air from the pack to provide a uniform mixture of air within the fresh air tube, which further ensures the prevention of ice build up.
Thomas Zywiak - Suffield CT, US Louis J. Bruno - Ellington CT, US Diane Drew - Farmington CT, US Douglas L. Christians - Vernon CT, US
Assignee:
Hamilton Sundstrand - Windsor Locks CT
International Classification:
B60H 1/32
US Classification:
62199, 62244, 62506, 62DIG 5
Abstract:
A galley chiller system for an aircraft includes at least one condenser having a refrigerant fluid. The fluid within the condenser rejects heat to a first surrounding environment. To more efficiently use the condenser of the galley chiller system and reduce the requirement on other cooling systems within an aircraft, the condenser may reject its heat to a desired location using a heat exchanger. The galley chiller system includes at least one evaporator that receives fluid from the condenser. A first evaporator absorbs heat from a galley, which may include a bank of carts. The first evaporator is arranged in ducting that carries cooled air to the carts. A second evaporator may absorb heat from a cabin recirculation air duct of the aircraft cooling system. In this manner, the evaporators of the inventive galley chilling system cools not only the galley carts but also provides supplemental cooling to the aircraft cooling system thereby reducing its cooling requirements.