IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0360672
(2003-02-07)
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발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
9 인용 특허 :
2 |
초록
▼
The present invention includes a method for a dual-mode propulsion system. During the first mode of operation, intake air is liquefied through a cooling heat exchanger and condenser using a combination of stored liquid hydrogen (LH 2 ) and stored liquid nitrogen (LN 2 ) as coolants. The liquefied
The present invention includes a method for a dual-mode propulsion system. During the first mode of operation, intake air is liquefied through a cooling heat exchanger and condenser using a combination of stored liquid hydrogen (LH 2 ) and stored liquid nitrogen (LN 2 ) as coolants. The liquefied air is then separated into separated liquid oxygen ( S LO 2 ) and separated liquid nitrogen ( S LN 2 ), which may contain molecules of each other or other elements commonly found in air. The stored liquid nitrogen is replaced with S LO 2 , while the S LN 2 is pumped back through the system with the stored nitrogen in a regeneration process. The S LN 2 , LN 2 , and LH 2 become gaseous as they pass through the condenser and heat exchanger and are burned in the dual mode rocket thrust chamber to produce thrust. In the second mode, the same thrust chamber is operated as a liquid hydrogen-oxygen rocket, where the liquid oxygen is the S LO 2 collected during the first mode.
대표청구항
▼
1. A method for a dual-mode aerospace vehicle propulsion system comprising:separately storing liquid hydrogen and liquid nitrogen;during a first mode:intaking air from atmosphere;liquefying said air;separating said liquefied air into separated liquid oxygen and separated liquid nitrogen;storing a po
1. A method for a dual-mode aerospace vehicle propulsion system comprising:separately storing liquid hydrogen and liquid nitrogen;during a first mode:intaking air from atmosphere;liquefying said air;separating said liquefied air into separated liquid oxygen and separated liquid nitrogen;storing a portion of said separated liquid oxygen and pumping a remaining portion of said separated liquid oxygen into a combustion chamber;pumping liquid hydrogen, liquid nitrogen, and separated liquid nitrogen, and heating said liquid hydrogen, liquid nitrogen, and separated liquid nitrogen to their gaseous states; andburning said gaseous hydrogen, nitrogen, separated nitrogen and said remaining portion of said separated liquid oxygen in said combustion chamber to produce thrust; andduring a second mode:pumping hydrogen and stored separated oxygen into said chamber; andburning said pumped hydrogen and stored separated oxygen in said combustion chamber to produce thrust. 2. The method of claim 1, wherein the liquid hydrogen, liquid nitrogen, and separated liquid nitrogen are pumped through a heat exchange cooler and condenser to liquefy the air and the air is used to heat the hydrogen, liquid nitrogen and separated liquid nitrogen to their gaseous states. 3. The method of claim 2, wherein the step of storing the separated liquid oxygen includes storing the separated liquid oxygen in a tank initially storing liquid nitrogen. 4. A system for providing a dual-mode propulsion system comprising:at least one tank of liquid hydrogen;a plurality of second tanks of liquid nitrogen;a combustion chamber and nozzle assembly;a plurality of pumps;a first mode of operation including:a collector inlet to intake air from atmosphere;a cooler heat exchanger and a condenser to liquefy the air;a separator to separate liquid oxygen and liquid nitrogen from the air to define separated liquid oxygen and separated liquid nitrogen, a portion of the separated liquid oxygen is stored and a remaining portion of the separated liquid oxygen is allowed to flow into said combustion chamber; andthe plurality of pumps to pressurize and pump the liquid hydrogen, the liquid nitrogen, and the regenerative coolant separated liquid nitrogen, collectively fluids, through the condenser and the heat exchanger, such that the fluids aid in liquefying the air and air aids in heating the fluids to their gaseous states, and the gaseous fluids are further allowed to flow into said combustion chamber and nozzle assembly where the fluids and said remaining portion of separated liquid oxygen are burned to create thrust; anda second mode of operating including:the plurality of pumps to pressurize and pump the liquid hydrogen and the stored separated liquid oxygen into said combustion chamber and nozzle assembly where the liquid hydrogen and the stored separated liquid oxygen are burned to create thrust. 5. In a method of performing a first and second mode of propulsion, utilizing a single combustion chamber nozzle assembly, the method comprises:burning at least gaseous hydrogen, gaseous nitrogen and liquid oxygen in the combustion chamber to produce thrust, defining a first mode of propulsion; andburning at least liquid hydrogen and liquid oxygen in the combustion chamber to produce thrust, defining a second mode of propulsion. 6. The method of claim 5 further comprising:collecting air in the first mode of propulsion and separating liquid oxygen therefrom for which a portion of the separated liquid oxygen is burned in said first mode and the remaining portion of the separated liquid oxygen is burned in said second mode of propulsion. 7. The method of claim 6 further comprising storing liquid hydrogen for use in the first and second mode of propulsion. 8. The method of claim 7 further comprising storing liquid nitrogen for use in the first mode of propulsion. 9. The method of claim 8 further comprising pumping the stored liquid hydrogen and the stored liquid nitrogen through a condenser and heat exchanger to liquefy the collected air prior to separating liquid oxygen therefrom, and wherein the stored liquid hydrogen and stored liquid nitrogen becomes gaseous as a result of passing through the condenser and heat exchanger, and the gaseous hydrogen and gaseous nitrogen is used in the first mode of propulsion. 10. The method of claim 9 further comprising separating nitrogen from the liquefied air and mixing the separated liquid nitrogen with the stored liquid nitrogen prior to the step of pumping through a condenser and heat exchanger, thereby using the separated liquid nitrogen in regenerative fashion. 11. The method of claim 10 further comprising storing a portion of said separated liquid oxygen in tanks initially used to store the liquid nitrogen. 12. In a method of performing a first and second mode of propulsion, the method comprises:collecting air during the first mode of propulsion and separating liquid oxygen from said air;burning at least gaseous hydrogen, gaseous nitrogen and a portion of said separated liquid oxygen in a combustion chamber to produce thrust, defining the first mode of propulsion; andburning at least liquid hydrogen and a portion of said separated liquid oxygen in the combustion chamber to produce thrust, defining the second mode of propulsion. 13. The method of claim 12 further comprising storing liquid hydrogen for use in the first and second mode of propulsion. 14. The method of claim 13 further comprising storing liquid nitrogen for use in the first mode of propulsion. 15. The method of claim 14 further comprising pumping the stored liquid hydrogen and the stored liquid nitrogen through a condenser and heat exchanger to liquefy the collected air prior to separating liquid oxygen therefrom, and wherein the stored liquid hydrogen and stored liquid nitrogen becomes gaseous as a result of passing through the condenser and heat exchanger, and the gaseous hydrogen and gaseous nitrogen is used in the first mode of propulsion. 16. The method of claim 15 further comprising separating nitrogen from the liquefied air and mixing the separated liquid nitrogen with the stored liquid nitrogen prior to the step of pumping through a condenser and heat exchanger, thereby using the separated liquid nitrogen in regenerative fashion. 17. The method of claim 16 further comprising storing the separated liquid oxygen in tanks initially used to store the liquid nitrogen.
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