Title:
SYSTEM FOR INERTING AND METHOD FOR GENERATING INERTING GAS IN AIRCRAFT, OPERATING WITHOUT COLLECTING OUTSIDE AIR
Document Type and Number:
Japanese Patent JP2018177208
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide an inerting system for aircraft that can generate a low-temperature inerting gas without the need to collect outside air.SOLUTION: An inerting system 1 includes a gas circuit comprising successively at least one air inlet 2, a compressor 3 and an air separation module 7. The air separation module 7 includes an outlet 8 for oxygen-enriched gas and an outlet 9 for an inerting gas. The air separation module 7 includes gas permeation membranes resistant to a temperature greater than or equal to 100°C, preferably greater than or equal to 140°C, and the inerting gas outlet 9 is connected to a turbine 10 for releasing pressure and cooling the inerting gas.SELECTED DRAWING: Figure 1
Inventors:
PIERRICK MAILHET
FREDERIC TONG-YETTE
FREDERIC TONG-YETTE
Application Number:
JP2018066076A
Publication Date:
November 15, 2018
Filing Date:
March 29, 2018
Export Citation:
Assignee:
ZODIAC AEROTECHNICS
International Classes:
B64D37/32; B01D53/22; B64D25/00
Domestic Patent References:
| JP2012096195A | 2012-05-24 | |||
| JP2003291894A | 2003-10-15 |
Foreign References:
| US20080060523A1 | 2008-03-13 |
Attorney, Agent or Firm:
Asamura patent office