IP Library Granted Patent US 10,105,639
Granted Patent B2
US 10,105,639 · App. 15/436,089 · Granted Oct 23, 2018

Inert gas generation system, and an aircraft fuel tank inerting system implementing said inert gas generation system

Inventor: Christophe Claris (Saint-Just-Saint-Rambert, FR)
Assignee: Zodiac Aerotechnics
B01D53/226B01D71/028B64D37/02B64D37/32B01D2053/221
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Quick Facts
Patent No.
US 10,105,639
App. No.
15/436,089
Granted
Oct 23, 2018
Kind
B2
Abstract

An inert gas generation system from a flow of air, notably for an inerting system for at least one aircraft fuel tank. The generation system includes an air circuit having an air inlet, an inert gas outlet, and a first and a second air separation module arranged in series on the air circuit to deplete oxygen within the air and to generate a nitrogen-enriched inert gas.

Claims (7)

1. An inert gas generation system from a flow of air, for an inerting system for at least one aircraft fuel tank, said generation system comprising an air circuit comprising an air inlet, an inert gas outlet, and a first and a second air separation module arranged in series on said air circuit to deplete oxygen within the air and to generate a nitrogen-enriched inert gas, characterized in that the air circuit comprises a first valve for selectively routing, upstream of the first module, a portion of the air flow directly to an inlet of the second module, and a second valve for selectively routing, downstream from the first module, the entire air flow directly to the inert gas outlet.

2. The generation system according to claim 1 , characterized in that the first valve and the second valve are arranged on the air circuit between the first module and the second module, the first valve being connected to the gas outlet by a first bypass circuit, and the second valve being connected to the air circuit upstream of the first module by a second bypass circuit.

3. The generation system according to claim 2 , characterized in that the first valve and the second valve are flow control valves.

4. The generation system according to claim 2 , characterized in that the first valve and the second valve are pressure control valves.

5. An inert gas generation system from a flow of air, for an inerting system for at least one aircraft fuel tank, said generation system comprising an air circuit comprising an air inlet, an inert gas outlet, and a first and a second air separation module arranged in series on said air circuit to deplete oxygen within the air and to generate a nitrogen-enriched inert gas,

characterized in that the first and second air separation module comprise zeolite membranes,

and further characterized in that the size of the zeolite membranes of the first module is different from the size of the zeolite membranes of the second module.

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 8, 2024
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 069124/0604 →
CORRECTIVE ASSIGNMENT TO CORRECT THE THE NAME OF RECEIVING PARTY, SAFRAN AEROTECHNICS SAS; PLEASE REMOVE 'SAS' FROM THE NAME PREVIOUSLY RECORDED ON REEL 055556 FRAME 0867. ASSIGNOR(S) HEREBY CONFIRMS THE SAFRAN AEROTECHNICS. Recorded May 25, 2022
From: ZODIAC AEROTECHNICS
To: SAFRAN AEROTECHNICS
Reel/Frame 060177/0282 →
CHANGE OF NAME Recorded Jan 26, 2021
From: ZODIAC AEROTECHNICS
To: SAFRAN AEROTECHNICS SAS
Reel/Frame 055556/0867 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 16, 2017
From: CLARIS, CHRISTOPHE
To: ZODIAC AEROTECHNICS
Reel/Frame 041598/0333 →
Priority Claims (1)
FR 16 51294 · Feb 18, 2016 · national
Continuity (1)
Related Publication 20170239615A1 · Aug 24, 2017