Title:
INERTING SYSTEM FOR AN AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2009/141400
Kind Code:
A4
Abstract:
The invention relates to an inerting system for an aircraft, comprising at least one air separation module provided with at least one air inlet, a first air outlet and a second air outlet. Said air separation module is designed in such a manner that an incoming air flow is divided into a first air flow and a second air flow. The first airflow is enriched with oxygen in relation to the incoming air flow and is removed by the first air outlet and the second air flow is enriched with nitrogen in relation to the incoming air flow and is removed by the second air outlet. The claimed inerting system is characterised in relation to known inerting systems in that the air inlet can be connected to an air removal point in an air preparation system and that the inerting system is designed to guide the first air flow into a cabin that is to be climatised.
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Inventors:
CREMERS JOERG (DE)
KRICKE KLAUS-DIETER (DE)
SCHUMACHER CHRISTIAN (DE)
KRICKE KLAUS-DIETER (DE)
SCHUMACHER CHRISTIAN (DE)
Application Number:
PCT/EP2009/056180
Publication Date:
July 15, 2010
Filing Date:
May 20, 2009
Export Citation:
Assignee:
AIRBUS OPERATIONS GMBH (DE)
CREMERS JOERG (DE)
KRICKE KLAUS-DIETER (DE)
SCHUMACHER CHRISTIAN (DE)
CREMERS JOERG (DE)
KRICKE KLAUS-DIETER (DE)
SCHUMACHER CHRISTIAN (DE)
International Classes:
B64D13/00; B64D37/32
Attorney, Agent or Firm:
MAIWALD PATENTANWALTS GMBH (KorbinianElisenho, Elisenstr. 3 Munich, DE)
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