Pneumatic system for an aircraft
US-2015107261-A1 · Apr 23, 2015 · US
US9896216B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9896216-B2 |
| Application number | US-201615170457-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 1, 2016 |
| Priority date | Jun 1, 2016 |
| Publication date | Feb 20, 2018 |
| Grant date | Feb 20, 2018 |
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Official abstract text for this publication.
An environmental control system (ECS) includes a controller; and a mode selector in communication with the controller and configured to select at least one of a plurality of modes. The mode is based on one of: number of occupants in an environment; activity of the occupants in the environment; destination of the environment; and performance of an engine that moves the environment. The controller is configured to change an ECS load on the system based upon the selected mode.
Opening claim text (preview).
We claim: 1. A non-transitory computer-readable medium for an environmental control system (ECS) of a vehicle an aircraft comprising instructions stored thereon, that when executed on a processor, performing steps of: selecting at least one of a plurality of operating modes, wherein the at least one of the plurality of operating modes is based on a distance to a destination to be reached by an environment; changing, based on the selected at least one of the plurality of operating modes at least one of: a load on the ECS; a ventilation valve enabling flow into the environment; and an outflow valve enabling flow out of the environment. 2. The non-transitory computer-readable medium of claim 1 , wherein another operating mode is based on an occupancy of the environment and the occupancy is an occupancy number threshold. 3. The non-transitory computer-readable medium of claim 1 , wherein another operating mode is based on an occupancy of the environment and the occupancy is an occupancy activity threshold. 4. The non-transitory computer-readable medium of claim 1 , wherein the environment includes a first environment and a second environment. 5. The non-transitory computer-readable medium of claim 4 , wherein the ventilation valve is intermediate the first and second environments. 6. The non-transitory computer-readable medium of claim 4 , wherein the first environment is an aircraft cabin and the second environment is an aircraft cockpit.
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