Patent · US Active

Main engine start by means of an aircraft air conditioning system

US8844296B2 · kind B2 · utility

5Cited by
8References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 7, 2013
Grant dateSep 30, 2014
Priority date
Expiry dateMar 7, 2033

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2013/0696
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An air conditioning system in an aircraft is provided. The system comprises at least one air cycle air-conditioning pack with a compressor comprising a bleed air outlet and with a compressed-air line connected to the bleed air connection, which compressed-air line is connectable to a starter turbine for a main engine. With the use of air from a compressor of an air conditioning pack it is not necessary to switch off the air conditioning pack; bleed air removal from the auxiliary power units becomes obsolete; and, since there is no unnecessary discharge of compressed air from a bleed air system, noise pollution on the ground is reduced.

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