Integrated system for providing aircraft environmental control
US6817575B1 · kind B1 · utility
20Cited by
12References
12Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Sep 20, 2002 |
| Grant date | Nov 16, 2004 |
| Priority date | — |
| Expiry date | Sep 20, 2022 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D2013/0614
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The present invention relates to an integrated enviromental control system for an aircraft. The system uses bleed air from a propulsion engine to drive an air turbine which provides power to at least one aircraft component such as an aircraft mounted accessory drive. The system uses the bleed air exiting the air turbine as an air source for the cabin and/or flight deck enviromental control system.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.