IP Library Granted Patent US 9,272,786
Granted Patent B2
US 9,272,786 · App. 10/565,712 · Granted Mar 1, 2016

Circuit for supplying oxygen to aircraft passengers

Inventors: Jean-Michel Cazenave (Seyssins, FR); Jean Dehayes (Lumbin, FR); Didier Gaget (Sassenage, FR); Stéphane Lessi (Newark, DE); Nicolas Schmutz (Paris, FR)
Assignee: L'Air Liquide Société Anonyme Pour L'Étude Et L'Exploitation Des Procedes Georges Claude
B64D11/00B64D25/00A62B7/14B64D2231/02Y02T50/46Y10T137/6906
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Quick Facts
Patent No.
US 9,272,786
App. No.
10/565,712
Granted
Mar 1, 2016
Kind
B2
Abstract

The invention relates to a circuit for supplying oxygen to aircraft passengers. According to the invention, the line ( 5 ) used to supply pressurized oxygen to the passenger masks ( 6 ) comprises a motorized pressure regulator ( 8 ) which can be actuated in response to a pressure control signal ( 10 ) provided by an electronic control unit ( 9 ) according to a signal ( 11 ) that is representative of the cabin pressure ( 12 ).

Claims (10)

1. A circuit for supplying oxygen to aircraft passengers of an aircraft having a cabin in case of accidental cabin depressurization, comprising:

a pressurized oxygen tank;

a first line fluidly communicating with the tank for supplying oxygen to a plurality of aircraft passenger masks;

a first pressure sensor adapted to measure an absolute pressure in the cabin;

a servocontrolled pressure regulator;

an electronic control unit;

a second pressure sensor disposed in the first line downstream of the pressure regulator that is adapted to measure the pressure in the first line downstream of the pressure regulator, wherein the pressure regulator is adapted to regulate the pressure in the first line downstream of the pressure regulator by following a setpoint signal generated by the electronic control unit according to a cabin pressure signal received by the electronic control unit from the first pressure sensor and also according to a regulated pressure signal received by the electronic control unit from the second pressure sensor.

2. The circuit of claim 1 , further comprising a second line fluidly communicating between portions of the first line upstream of the pressure regulator and downstream of the second pressure sensor that bypasses the pressure regulator, the second line including a safety solenoid valve for short-circuiting the pressure regulator in case of failure of the pressure regulator.

3. The circuit of claim 1 , further comprising an oxygen therapy system fluidly communicating with the first line downstream of the second pressure sensor.

4. The circuit of claim 1 , further comprising a third line fluidly communicating with the tank for supplying oxygen to aircraft crew masks in the cabin.

Assignments (4)
CHANGE OF ADDRESS Recorded Oct 2, 2024
From: L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE
To: SAFRAN AEROSYSTEMS
Reel/Frame 069084/0460 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 16, 2024
From: L'AIR LIQUIDE, SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE
To: SAFRAN AEROSYSTEMS
Reel/Frame 068957/0421 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 28, 2009
From: DEHAYES, JEAN
To: L'AIR LIQUIDE SOCIETE ANONYME POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE
Reel/Frame 022743/0576 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 11, 2006
From: CAZENAVE, JEAN-MICHEL; DEHAYES, JEAN; GAGET, DIDIER; LESSI, STEPHANE; SCHMUTZ, NICOLAS
To: L'AIR LIQUIDE, SOCIETE ANONYME A DIRECTOIRE ET CONSEIL DE SURVEILLANCE POUR L'ETUDE ET L'EXPLOITATION DES PROCEDES GEORGES CLAUDE
Reel/Frame 018218/0631 →
Priority Claims (1)
FR 03 50394 · Aug 4, 2003 · national
Continuity (1)
Related Publication 20070144597A1 · Jun 28, 2007