Aircraft environmental control system
AssigneeHamilton Sundstrand Corporation
InventorsYonghua Zhu, Catherine Thibaud
Life of this patent
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Abstract
An aircraft environmental control system includes means for mixing and conditioning bleed air from a bleed air input and recirculation air from an aircraft interior to provide mixed, conditioned air to the aircraft interior. The system also includes a first contaminant removal device and a second contaminant removal device arranged in a path of at least part of the recirculation air, prior to the means for mixing and conditioning, and a valve (SV1) arranged to alternate flow of recirculation air through the first and second contaminant removal devices.
Claims4
An aircraft environmental control system, comprising:
- means for mixing and conditioning bleed air from a bleed air input and recirculation air from an aircraft interior to provide mixed, conditioned air to the aircraft interior;
- a first contaminant removal device and a second contaminant removal device arranged in a path of at least part of the recirculation air, prior to the means for mixing and conditioning;
- a first split valve (SV1) arranged to alternate flow of recirculation air through the first and second contaminant removal devices;
- means for passing conditioned regeneration air through the contaminant removal devices to desorb the one or more contaminants for purging from the system;
- a second split valve (SV2) for alternately passing the conditioned regeneration air through the first and second contaminant removal devices, the valves being arranged such that when recirculation air flows passing through one of the first and second contaminant removal devices, conditioned regeneration air flows passing through the other of the contamination removal devices;
- and
- an energy storage device configured to recover energy from the conditioned regeneration air passing therethrough after it has passed through the contamination removal device for desorption.
A method of providing conditioned air to an aircraft interior comprising:
- mixing and conditioning bleed air and recirculation air from the aircraft to provide mixed conditioned air to the aircraft interior;
- removing one or more contaminants from the recirculation air, prior to mixing, by passing the recirculation air through one of two contaminant removal devices and alternating the flow of recirculation air from passing through one of the contaminant removal devices to passing through the other contaminant removal device;
- regenerating contaminant removing material of the contaminant removal devices by passing conditioned regeneration air through the devices to desorb the contaminant adsorbed by the devices, wherein the first device is regenerated while recirculation air passes through the second device and vice versa;
- and
- storing energy from the regeneration air after it has passed through the contaminant removal device to desorb the contaminant.
Dependencies are inferred from the claim text.