Method for operating an air fractionization installation for obtaining oxygen on board an aircraft
View Patent ↗The method serves for operating an air fractionization installation for obtaining oxygen on board an aircraft, with at least two molecular sieve chambers. A part mass flow of the oxygen obtained in the respective adsorbing molecular sieve chamber is supplied for flushing a desorbing molecular sieve chamber. The quantity of the flushing oxygen led to the desorbing molecular sieve chamber is controlled by way of this.
1. A method for operating an air fractionization installation for obtaining oxygen on board an aircraft, with at least two molecular sieve chambers, the method comprising:
providing a throttle valve located in a feed conduit;
feeding a part mass flow of oxygen obtained in a respective adsorbing molecular sieve chamber for flushing a desorbing molecular sieve chamber, said adsorbing molecular sieve chamber being connected to said desorbing molecular sieve chamber via said feed conduit; and
controlling a feed cross section of said throttle valve located in said feed conduit such that a quantity of the flushing oxygen fed to the desorbing molecular sieve chamber is based on an oxygen concentration and on the mass flow of product gas delivered from said adsorbing molecular sieve chamber.
2. A method for operating an air fractionization installation according to claim 1 , wherein the quantity control of the flushing oxygen fed to the desorbing molecular sieve chamber is additionally controlled by changing a plurality of feed times.
3. A method for operating an air fractionization installation according to claim 2 , wherein said control means determines an opening time of said throttle valve such that said throttle valve is closed upon reaching a flushing oxygen gas quantity desorption threshold.
4. A method for operating an air fractionization installation according to claim 1 , wherein said product gas is delivered to an oxygen supply of an aircraft.
5. A method for operating an air fractionization installation according to claim 1 , wherein said feed cross section is reduced to a minimum feed cross section throughput when said oxygen concentration is a maximum oxygen concentration value, said feed cross section being varied such that a maximum feed cross section throughput is associated with a minimum oxygen concentration value.
6. An aircraft air fractionization installation for obtaining oxygen on board an aircraft, the air fractionization installation comprising:
a first molecular sieve chamber;
a second molecular sieve chamber, said first molecular sieve chamber and said second molecular sieve chamber defining an air fractionization structure;
a conduit supplying gas to said air fractionization structure and receiving product gas exiting from said air fractionization structure;
a feed conduit connecting said first molecular sieve chamber to said second molecular sieve chamber such that one of said chambers, as a desorbing molecular sieve chamber, is flushed with oxygen of product gas of another of said chambers, as an absorbing molecular sieve chamber;
a sensing means located downstream of said air fractionization structure for sensing oxygen concentration and mass flow of said product gas exiting from said air fractionization structure;
a throttle valve located in said feed conduit and having a throughput cross section that may be varied from a minimum to a maximum throughput;
a control means for controlling said throughput cross section to continuously vary said throughput cross section corresponding to variations in oxygen concentration and in mass flow of the product gas sensed by said sensing means, said control means controlling an amount of said product gas supplied to said desorbing molecular sieve chamber from said adsorbing molecular sieve chamber.
7. An air fractionization installation according to claim 6 , wherein said control means comprises a time control by way of which the opening time of the feed valve is controlled.
8. An air fractionization installation according to claim 7 , wherein said control means determines an opening time of said throttle valve such that said throttle valve is closed upon reaching a flushing oxygen gas quantity desorption threshold.
9. An air fractionization installation according to claim 6 , wherein said product gas is delivered to an oxygen supply of an aircraft.
10. An air fractionization installation according to claim 6 , wherein said minimum throughput is associated with a maximum oxygen concentration value, said maximum throughput being associated with a minimum oxygen concentration value.
11. A method for obtaining oxygen on board an aircraft, the method comprising:
providing a bypass conduit;
providing a throttle valve located in said bypass conduit having a variable feed cross section;
providing an air fractionization installation with a first molecular sieve chamber and a second molecular sieve chamber, said first molecular sieve chamber being in communication with said second molecular sieve chamber via said bypass conduit;
delivering gas to said air fractionization installation and providing product gas exiting from said air fractionization installation;
sensing oxygen concentration and mass flow of said product gas exiting said air fractionization installation with a sensor located downstream of said air fractionization installation;
continuously varying said feed cross section of said throttle valve based on a variation of said oxygen concentration and a variation of mass flow detected via said sensor such that one of said molecular sieve chambers as a desorbing molecular sieve chamber is flushed with oxygen of product gas of another of said chambers as an adsorbing molecular sieve chamber, whereby said feed cross section of said throttle valve controls an amount of said product gas supplied to one of said molecular sieve chambers functioning as a desorbing molecular sieve chamber from another of said chambers functioning as an adsorbing molecular sieve chamber.
12. A method for operating an air fractionization installation according to claim 11 , wherein the quantity control of the flushing oxygen fed to the desorbing molecular sieve chamber is controlled by changing a plurality of feed times.
13. A method for operating an air fractionization installation according to claim 11 , wherein said control means comprises at least one throttle valve with a controlled throughput cross section.
14. A method for operating an air fractionization installation according to claim 12 , wherein said control means comprises a time control by way of which the opening time of the feed valve is controlled.
15. A method for operation an air fractionization installation according to claim 13 , wherein said control means determines an opening time of said throttle valve such that said throttle valve is closed upon reaching a flushing oxygen gas quantity desorption threshold.
16. A method for operating an air fractionization installation according to claim 11 , wherein said product gas is delivered to an oxygen supply of an aircraft.
17. A method for operating an air fractionization installation according to claim 11 , wherein said throughput cross section is varied from a minimum to a maximum throughput, said minimum throughput being associated with a maximum oxygen concentration value, said maximum throughput being associated with a minimum oxygen concentration value.