Patent · US Active

Aircraft energy management system including engine fan discharge air boosted environmental control system

US9254920B2 · kind B2 · utility

20Cited by
11References
20Claims
0Family size

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Inventors

Key dates

Filing dateMay 30, 2012
Grant dateFeb 9, 2016
Priority date
Expiry dateNov 14, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft energy management system including a cabin air compressor adapted to be coupled to a source of fan discharge air at a first pressure during an inflight operating mode and adapted to be coupled to a ram intake air during a ground operating mode. The system further including an environmental control system mechanically coupled to a compressor exit of the cabin air compressor. The aircraft energy management system configured to provide a conditioned fluid flow to an aircraft cabin, cockpit or de-icing system.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.