Monopropellant system for regenerative fuel cell and method for mono-propulsion using same

Abstract

The present invention relates to a monopropellant system for a regenerative fuel cell (RFC) and a method for mono-propulsion using same and, more specifically, to a monopropellant system for an RFC which can, when operating an electrically propelled airplane adopting an RFC system, secure more energy via a monopropellant than conventional methods and use same as a propulsion source for airplane takeoff and so on, and to a method for mono-propulsion using the monopropellant system for an RFC.

Claims

1. A monopropellant flying system comprising: (1) a power supply configured to supply electricity: (2) a fuel cell configured to use hydrogen and oxygen to generate electricity and water as byproduct; (3) a propeller configured to use electricity from the power supply and/or the fuel cell; (4) a storage configured to store a monopropellant and further configured to receive the water from the fuel cell such that, upon receiving water from the fuel cell, the monopropellant is mixed with the water in the storage; and (5) a propulsion device configured to use the monopropellant or a mixture of the monopropellant and water from the storage to generate propulsion force at the time of take-off.

2. The system of claim 1, wherein the propulsion device further comprises a catalyst configured to enable catalytic reaction of the monopropellant or the mixture from the storage.

3. The system of claim 1, further comprising a monopropellant tank configured to contain the monopropellant and connected to the storage for supplying monopropellant to the storage, wherein the monopropellant comprises a hydrogen peroxide.

4. The system of claim 2, further comprising a controller configured to control to electrolysis of the water from the storage using electricity from the power supply to generate hydrogen and oxygen, wherein the system further comprises a hydrogen tank for storing the hydrogen from the electrolysis and a oxygen tank for storing the oxygen from the electrosis.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a diagram of a configuration of a monopropellant system for a regenerative fuel cell according to an exemplary embodiment of the present invention.

(2) FIG. 2 is a diagram of a configuration of a monopropellant system for a regenerative fuel cell according to another exemplary embodiment of the present invention.

(3) FIG. 3 is a flowchart of a mono-propulsion method for a regenerative fuel cell according to the present invention.

(4) TABLE-US-00001 -Explanation of Reference Numerals- 100: power supply portion 200: fuel cell portion 201: fuel supply portion 210: hydrogen tank 220: oxygen tank 300: controller 400: driver 500: fuel storage portion 510: hydrogen peroxide tank 600: propulsion portion 700: catalyst portion S100: propelling S200: driving S210: fuel cell driving S211: reactant storing S220: solar cell driving S221: electrolyzing

BEST MODE

(5) The present invention will now be described more fully with reference to the accompanying drawings, in which exemplary embodiments of the invention are shown.

(6) The accompanying drawings are merely an example illustrated for explanation of the features of the present invention in detail and, thus, the features of the present invention are not limited to the embodiments illustrated in the accompanying drawings.

(7) FIG. 1 is a diagram of a configuration of a monopropellant system for a regenerative fuel cell according to an exemplary embodiment of the present invention and FIG. 2 is a diagram of a configuration of a monopropellant system for a regenerative fuel cell according to another exemplary embodiment of the present invention.

(8) As shown in FIGS. 1 and 2, a monopropellant system for a regenerative fuel cell according to the present invention may include a power supply portion 100, a fuel cell portion 200, a controller 300, a driver 400, a fuel storage portion 500, and a propulsion portion 600.

(9) The power supply portion 100 may generate electricity or store electricity. For example, the power supply portion 100 may be a renewable energy source for generating electricity using solar energy, such as a solar cell, or a general energy storage device for storing electricity, such as a battery.

(10) The fuel cell portion 200 may be a fuel cell for generating electricity and water using hydrogen and oxygen. In more detail, the fuel cell portion 200 may be connected to a fuel supply portion 201 for supplying hydrogen and oxygen. The fuel supply portion 201 may include, for example, a hydrogen tank 210 and an oxygen tank 220 and the fuel cell portion 200 may be connected to each of the hydrogen tank 210 and the oxygen tank 220. The hydrogen tank 210 may fully accommodate hydrogen and the oxygen tank 220 may fully accommodate oxygen. That is, hydrogen and oxygen accommodated in the hydrogen tank 210 and the oxygen tank 220 react with each other in the fuel cell portion 200 to generate electricity and a reactant. The generated electricity may be used to drive the driver 400 and the reactant may be moved and stored in the fuel storage portion 500. In this case, the reactant may be water or hydrogen peroxide. The reactant may be a hydrogen peroxide aqueous solution obtained by mixing water and hydrogen peroxide.

(11) The controller 300 may control the power supply portion 100 or the fuel cell portion 200 to generate electricity depending on the cases.

(12) For example, when the power supply portion 100 is a solar cell, the controller 300 may control the solar cell to generate electricity during the daytime when sunlight is present and, in this case, the generated electricity may drive the driver 400 or control the driver 400 to enable electrolysis of a reactant accommodated in the fuel storage portion 500. The controller 300 may perform control to store hydrogen and oxygen that are generated via electrolysis of the reactant in the hydrogen tank 210 and the oxygen tank 220, respectively.

(13) The controller 300 may perform control to generate electricity using a fuel cell at nighttime. In more detail, the fuel cell portion 200 may allow hydrogen and oxygen accommodated in the hydrogen tank 210 and the oxygen tank 220 to react with each other to generate electricity and the electricity may drive the driver 400. In this case, water may be generated via reaction between hydrogen and oxygen and stored in the fuel storage portion 500.

(14) When the power supply portion 100 is a battery, the controller 300 may perform control to enable electrolysis of the reactant accommodated in the fuel storage portion 500 using electricity stored in the battery. When propulsion force is required, the controller 300 may control the propulsion portion 600 to generate propulsion force using the fuel or reactant accommodated in the fuel storage portion 500.

(15) The driver 400 may be driven using electricity that is generated or stored in the power supply portion 100 or the fuel cell portion 200. For example, the driver 400 may be driven using electricity generated from a solar cell during the daytime and may be driven using electricity generated from the fuel cell portion 200 at nighttime. In this case, in an aircraft employing a regenerative fuel cell (RFC) system, the driver 400 may be, for example, a propeller.

(16) The fuel storage portion 500 may accommodate fuel or store a reactant generated from the fuel cell portion 200.

(17) Referring to FIG. 1 according to an exemplary embodiment of the present invention, the fuel storage portion 500 may accommodate fuel therein. The fuel may be accommodated with mixture of water and hydrogen peroxide. In the case of an aircraft employing an RFC system, the fuel may be used when the largest amount of energy is required during take-off. That is, an aircraft employing an RFC system using a monopropellant system for a regenerative fuel cell according to the present invention may enable catalytic reaction of fuel accommodated in the fuel storage portion 500 to generate propulsion force from the propulsion portion 600 during take-off. The reactant may include any one selected from the group consisting of a hydrogen peroxide aqueous solution obtained by mixing water and hydrogen peroxide, water, or hydrogen peroxide.

(18) Referring to FIG. 2 according to another exemplary embodiment of the present invention, the fuel storage portion 500 may be connected to a hydrogen peroxide tank 510 that accommodates hydrogen peroxide. In this case, the fuel storage portion 500 may accommodate only water and hydrogen peroxide may be introduced to the fuel storage portion 500 from the hydrogen peroxide tank 510 and may be mixed with water. The mixed water and hydrogen peroxide may generate propulsion force via catalytic reaction in a catalyst portion 700.

(19) The propulsion portion 600 may generate propulsion force using fuel obtained via catalytic reaction in the catalyst portion 700. That is, in an aircraft employing an RFC system, the propulsion portion 600 may be a propellant such as a rocket engine.

(20) The propulsion portion 600 may generate the largest amount of propulsion force during take-off of an aircraft employing an RFC system. Then, much propulsion force is not required during the flight and, thus, electricity may be generated by a solar cell or a fuel cell to drive the driver 400 (propeller) to enable flight.

(21) The catalyst portion 700 may enable catalytic reaction of fuel of the fuel storage portion 500. That is, propulsion force may be generated from the propulsion portion 600 via catalytic reaction of fuel of the fuel storage portion 500.

(22) Hereinafter, a mono-propulsion method using the aforementioned monopropellant system for a regenerative fuel cell is described.

(23) FIG. 3 is a flowchart of a mono-propulsion method using a monopropellant system for a regenerative fuel cell.

(24) With reference to FIG. 3, a mono-propulsion method using a monopropellant system for a regenerative fuel cell according to the present invention is described below with regard to, for example, an aircraft employing an RFC system driven using a solar cell and a fuel cell.

(25) As described above, the aircraft employing the RFC system flies using a solar cell and a fuel cell.

(26) However, the aircraft employing the RFC system requires a large amount of propulsion force during take-off. To overcome this, according to the present invention, a monopropellant is used during take-off and a large amount of propulsion force is not required during the flight and, thus, the air craft may fly using electricity generated from the solar cell and the fuel cell.

(27) The mono-propulsion method using the monopropellant system for the regenerative fuel cell according to the present invention may include propelling S100 and driving S200.

(28) In the propelling S100, propulsion force may be generated using fuel accommodated in the fuel storage portion 500. That is, when an aircraft employing an RFC system takes off, the aircraft may generate a large amount of propulsion force using the fuel accommodated in the fuel storage portion 500 to take off.

(29) In this case, the fuel may be used in a state in which water and hydrogen peroxide are mixed.

(30) The fuel storage portion 500 may accommodate water therein and may be connected to the hydrogen peroxide tank 510. That is, hydrogen peroxide accommodated in the hydrogen peroxide tank 510 may be introduced to the fuel storage portion 500 and may be mixed with water.

(31) The propelling S100 may enable catalytic reaction of the fuel accommodated in the fuel storage portion 500 to generate propulsion force.

(32) Accordingly, the propelling S100 may generate propulsion force using the fuel accommodated in the fuel storage portion 500 to enable take-off the aircraft. In this case, the fuel accommodated in the fuel storage portion 500 may be entirely consumed. Then, during the flight, water generated from the fuel cell may be stored in the empty fuel storage portion 500.

(33) In the driving S200, when the aircraft employing an RFC system, which has taken off through the propelling S100, flies using constant propulsion force, much propulsion force is not required and, thus, the aircraft may fly using the solar cell or the fuel cell.

(34) For example, the aircraft employing an RFC system may fly using a fuel cell through the driving S200 at nighttime when sunlight is not present. In this case, the driving S200 may include fuel cell driving S210 and reactant storing S211.

(35) In the fuel cell driving S210, when electricity is generated from the fuel cell, hydrogen and oxygen accommodated in the hydrogen tank 210 and the oxygen tank 220 may be combined to generate electricity. Then, the generated electricity may be used in the driver 400 (propeller).

(36) In the reactant storing S211, water generated via combination between hydrogen and oxygen in the fuel cell driving S210 may be stored in the fuel storage portion 500. In this case, the water stored in the fuel storage portion 500 may be electrolyzed to be dissolved to hydrogen and oxygen when the solar cell is driven to generate electricity.

(37) On the other hand, an aircraft employing an RFC system may fly using a solar cell through the driving S200 during the daytime when sunlight is present. In this case, the driving S200 may include solar cell driving S220 and electrolyzing S221.

(38) In the solar cell driving S220, when electricity is generated from the solar cell, electricity may be generated by the solar cell and may be used in the driver 400 (propeller).

(39) In the electrolyzing S221, the water generated by the fuel cell may be electrolyzed to be dissolved to hydrogen and oxygen using a portion of the electricity generated by the solar cell. In this case, the dissolved hydrogen and oxygen may be stored in the hydrogen tank 210 and the oxygen tank 220, respectively and, when a fuel cell is used, hydrogen and oxygen may be used.

(40) A monopropellant system for a regenerative fuel cell according to the present invention may be applied to vehicles, vessels, other mobile devices, power supplies, and so on as well as an aircraft employing an RFC system.

(41) The present invention is not limited to the abovementioned exemplary embodiments, and may be variously applied, and may be variously modified without departing from the gist of the present invention claimed in the claims.