IP Library Granted Patent US 9,649,514
Granted Patent B2
US 9,649,514 · App. 13/929,823 · Granted May 16, 2017

Chemical oxygen generator with bimetal reaction control

Inventors: Wolfgang Rittner (Ahrensbok, DE); Rüdiger Meckes (Berkenthin, DE); Günter Boomgaarden (Scharbeutz, DE); Marco Hollm (Rosdorf, DE)
Assignee: Zodiac Aerotechnics
A62B7/08A61M16/20A62B7/00A62B7/02A62B7/14A62B9/02A62B18/02A62B21/00B64D10/00B64D11/0015B64D11/00155B64D2231/00B64D2231/02G08B5/00G08B5/224G08B5/36
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Quick Facts
Patent No.
US 9,649,514
App. No.
13/929,823
Granted
May 16, 2017
Kind
B2
Abstract

The invention relates to a regulation device for a source of breathable gas, comprising a reaction medium adapted to perform an exothermic reaction for the production of breathable gas, the reaction medium surrounding an interior reaction volume having a breathable gas outlet. The invention further relates to a chemical oxygen generator system for the provision of breathable gas in an aircraft as well as to a method for regulating a source of breathable gas comprising the step of initiating an exothermic reaction of a reaction medium for the production of breathable gas, the reaction medium surrounding an interior reaction volume having a breathable gas outlet, wherein the breathable gas is flowing through the breathable gas outlet.

Claims (37)

1. A regulation device for a source of breathable gas, comprising:

a reaction medium comprising sodium chlorate having iron fillings, the reaction medium adapted to perform an exothermic reaction for production of oxygen, the reaction medium having an annular shape and surrounding an interior reaction volume having a reaction gas inlet and a first breathable gas outlet;

a flow regulator arranged at the first breathable gas outlet and adapted to regulate a flow of oxygen through the first breathable gas outlet depending at least on a temperature of the regulation device and to throttle the flow of oxygen through the first breathable gas outlet if the temperature of the regulation device is increased;

a rigid housing comprising a substantially tubular shape and comprising a second breathable gas outlet; and

an exterior volume arranged radially outwardly between the reaction medium and an annular wall of the housing, the exterior volume surrounding the reaction medium radially, wherein the regulation device is adapted to direct a flow of reaction gas through the exterior volume towards the reaction gas inlet of the interior reaction volume.

2. A regulation device according to claim 1 , wherein the flow regulator comprises a valve body actuated by a bimetal element.

3. A regulation device according to claim 1 , comprising:

a pressure relief valve adapted to release the oxygen from the housing if a predetermined pressure value is exceeded.

4. A regulation device according to claim 1 , wherein the flow regulator is adapted to regulate the flow of the oxygen through the first breathable gas outlet depending on an ambient temperature of an aircraft.

5. A regulation device according to claim 4 ,

wherein the flow regulator is adapted to throttle the flow of the oxygen through the first breathable gas outlet if the ambient temperature of the aircraft is increased.

6. Method for regulating a source of breathable gas, comprising the steps of:

a) initiating an exothermic reaction of a reaction medium comprising sodium chlorate having iron fillings for production of oxygen, the reaction medium having an annular shape and surrounding an interior reaction volume having a reaction gas inlet and a first breathable gas outlet, wherein the oxygen is flowing in a first direction through an exterior volume formed circumferentially around the reaction medium, from the exterior volume through the reaction gas inlet into the interior reaction volume, through the interior reaction volume in a second direction opposite the first direction and through the first breathable gas outlet, and

b) regulating a flow of the oxygen, which is flowing through the first breathable gas outlet, by a regulation device depending at least on a temperature of the regulation device.

7. Method according to claim 6 , wherein the regulating is achieved by a flow regulator comprising a valve body actuated by a bimetal.

8. Method according to claim 6 , comprising the step of:

directing a flow of reaction gas, which is flowing to a reaction gas inlet of the interior volume, through the exterior volume, the exterior volume being arranged between the reaction medium and a wall of a housing having a second breathable gas outlet.

9. Method according to claim 6 , comprising the step of:

regulating the flow of the oxygen through the first breathable gas outlet depending on an ambient temperature of an aircraft.

10. Method according to claim 9 , comprising the step of:

throttling the flow of the oxygen through the first breathable gas outlet if the temperature of the regulation device and/or the ambient temperature of the aircraft increases.

11. A regulation device according to claim 1 , wherein the flow regulator consists of a valve body actuated by a bimetal element.

12. A regulation device according to claim 2 , wherein the bimetal element is a bimetallic arm.

13. A regulation device according to claim 11 , wherein the bimetal element is a bimetallic arm.

14. A regulation device according to claim 3 , wherein the pressure relief valve is connected to a conduit adapted to direct the oxygen released by the pressure relief valve to an aircraft cabin.

15. A regulation device for a source of breathable gas, comprising:

a rigid housing comprising a substantially tubular shape that includes an exterior sidewall defining an inner cavity and a gas outlet in fluid communication with the inner cavity;

a reaction medium positioned within the inner cavity, the reaction medium defining an interior reaction volume having an inlet and an outlet, the reaction medium and housing defining an exterior reaction volume between the reaction medium and the exterior sidewall and in fluid communication with the interior reaction volume;

a flow regulator arranged between the outlet of the inner reaction volume and the gas outlet of the housing, the flow regulator adapted to selectively throttle a flow of the breathable gas from the outlet of the reaction medium to the gas outlet of the housing based on a temperature of the regulation device; and

an ignitor adapted to activate the reaction medium, wherein an activation of the reaction medium produces the breathable gas.

16. A regulation device according to claim 15 , wherein the housing further comprises an interior wall within the inner cavity, wherein the interior wall defines a first chamber and a second chamber within the inner cavity, wherein the reaction medium is positioned within the first chamber, and wherein the flow regulator is positioned within the second chamber.

17. A regulation device according to claim 16 , wherein the housing further comprises a support within the inner cavity, wherein the reaction medium is supported by the support within the inner cavity.

18. A regulation device according to claim 17 , wherein the interior wall defines an aperture in fluid communication with the outlet of the interior reaction volume, and wherein the flow regulator comprises:

a valve seat extending from the interior wall;

a valve body selectively movable through the valve seat; and

a bimetallic arm connected to the valve body, the bimetallic arm elastically deformable between a first state and a second state.

19. A regulation device according to claim 15 , wherein the housing further comprises an isolation layer at the exterior sidewall within the inner cavity.

Assignments (6)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE PREVIOUS RECORDED ASSIGNMENT PREVIOUSLY RECORDED AT REEL: 68238 FRAME: 929. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Apr 3, 2025
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 070721/0187 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 9, 2024
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 068238/0928 →
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 →
CHANGE OF NAME Recorded Aug 22, 2014
From: INTERTECHNIQUE
To: ZODIAC AEROTECHNICS
Reel/Frame 033593/0266 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 23, 2013
From: RITTNER, WOLFGANG; MECKES, RUDIGER; BOOMGAARDEN, GUNTER; HOLLM, MARCO
To: INTERTECHNIQUE
Reel/Frame 031255/0548 →
Continuity (2)
Provisional Application 61665486 · Jun 28, 2012
Related Publication 20140000592A1 · Jan 2, 2014