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KR20190080675A - A Propellator that Achieves Momentum by Disassembling and Burning Water with Laser Light and Photocatalyst - Google Patents

A Propellator that Achieves Momentum by Disassembling and Burning Water with Laser Light and Photocatalyst Download PDF

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KR20190080675A
KR20190080675A KR1020180000361A KR20180000361A KR20190080675A KR 20190080675 A KR20190080675 A KR 20190080675A KR 1020180000361 A KR1020180000361 A KR 1020180000361A KR 20180000361 A KR20180000361 A KR 20180000361A KR 20190080675 A KR20190080675 A KR 20190080675A
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photocatalyst
laser
water
combustion chamber
pipe
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엄재풍
엄용호
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엄재풍
엄용호
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M25/00Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • F02M25/022Adding fuel and water emulsion, water or steam
    • F02M25/032Producing and adding steam
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M27/00Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like
    • F02M27/02Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like by catalysts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M27/00Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like
    • F02M27/06Apparatus for treating combustion-air, fuel, or fuel-air mixture, by catalysts, electric means, magnetism, rays, sound waves, or the like by rays, e.g. infrared and ultraviolet
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Catalysts (AREA)

Abstract

본 발명은 물을 수증기화 시켜 광촉매를 통과시키는 동시에 레이저광을 조사하여 수증기를 수소와 산소로 분해하며, 분해된 수소와 산소를 연소시켜 그 열과 압력을 분사하여 추진력을 얻는 추진 장치에 관한 것이다.
물을 태양광과 촉매를 이용하여 분해하는 기술은 여러 가지로 시도되고 있으나 그 효율이 약 3~6%로 미미한 실정이다.
따라서 , 물을 수증기로 변환시키고 빛의 밀도가 강한 레이저광을 촉매에 조사하여 그 분해효율을 높이고 연소열에 의해 수증기를 분해하여 다시 연소시켜 추진력을 얻는 추진 장치이다.
하나의 연소챔버 내에서 분해연소과정이 반복되어 발생하여 고온과 고압을 이용하여 분사력을 얻고, 분사된 수증기는 다시 물로 환원되는 방식이다.
따라서 , 기존의 추진 체와는 달리 환경오염물질을 배출하지도 않은 신개념의 추진 체이므로 반드시 필요한 발명이라 할 수 있다.
The present invention relates to a propulsion device for passing water through a photocatalyst, irradiating a laser beam to decompose water vapor into hydrogen and oxygen, and burning the decomposed hydrogen and oxygen to spray the heat and pressure to obtain propulsion.
There have been various attempts to decompose water using sunlight and a catalyst, but the efficiency is only about 3 to 6%.
Therefore, it is a propulsion device that converts water into water vapor and irradiates the laser light having high density of light to the catalyst to increase the decomposition efficiency thereof, decomposes the water vapor by the heat of combustion and re-burn to obtain the propulsion power.
The decomposition combustion process is repeated in one combustion chamber to obtain the spraying power by using the high temperature and the high pressure, and the sprayed steam is reduced to water again.
Therefore, unlike conventional propellants, it is a new concept propellant that does not emit environmental pollutants, so it can be said that it is a necessary invention.

Description

레이저광과 광촉매로 물을 분해 연소시켜 추진력을 얻는 추진 장치{A Propellator that Achieves Momentum by Disassembling and Burning Water with Laser Light and Photocatalyst}[0001] The present invention relates to a propellant that achieves propellant by decomposing and burning water with a laser beam and a photocatalyst, and more particularly, to a Propellator that Achieves Momentum by Disassembling and Burning Water with Laser Light and Photocatalyst,

본 발명은 물을 수증기화 시켜 광촉매를 통과시키는 동시에 레이저광을 조사하여 수증기를 수소와 산소로 분해하며, 분해된 수소와 산소를 연소시켜 그 열과 압력을 분사하여 추진력을 얻는 추진 장치에 관한 것이다.The present invention relates to a propulsion device for passing water through a photocatalyst, irradiating a laser beam to decompose water vapor into hydrogen and oxygen, and burning the decomposed hydrogen and oxygen to spray the heat and pressure to obtain propulsion.

물을 태양광과 촉매를 이용하여 분해하는 기술은 여러 가지로 시도되고 있으나 그 효율이 약 3~6%로 미미한 실정이다.There have been various attempts to decompose water using sunlight and a catalyst, but the efficiency is only about 3 to 6%.

따라서 , 물을 수증기로 변환시키고 빛의 밀도가 강한 레이저광을 촉매에 조사하여 그 분해효율을 높이고 연소열에 의해 수증기를 분해하여 다시 연소시켜 추진력을 얻는 추진 장치이다.Therefore, it is a propulsion device that converts water into water vapor and irradiates the laser light having high density of light to the catalyst to increase the decomposition efficiency thereof, decomposes the water vapor by the heat of combustion and re-burn to obtain the propulsion power.

로켓 엔진은 설계한 추력을 발생시키는 장치로서 추력기를 포함하는 개념이며 로켓 발사체 또는 인공위성 등에 부착되어 설정한 비행 궤도를 따라 비행하도록 해주는 장치이다.A rocket engine is a device that generates a designed thrust. It is a concept that includes a thruster. It is a device that attaches to a rocket launch vehicle or a satellite and makes it fly along a set orbit.

로켓 엔진은 하나의 추진제만으로 구동하는 단일추진제 로켓 엔진과 산화제를 이용하여 연료를 연소시키는 이원추진제 로켓 엔진으로 나누어 질수 있다.The rocket engine can be divided into a single propellant rocket engine driven by one propellant and a binary propellant rocket engine that burns fuel using oxidant.

종래의 이원추진제 로켓 엔진의 경우,In the case of a conventional binary propellant rocket engine,

첫째, 고온의 산화제 유동 흐름에 액상 연료를 분사하여 점화하며 이에 따라 액상의 연료가 기화되는 시간을 포함한 점화 시간을 확보하기 위해 화염 안정기 등을 이용하여 와류를 형성하고 점화하였다. 따라서 별도의 장치 구성으로 인해 고비용 및 고중량의 문제가 있고 점화의 신뢰성이 낮은 단점이 있다.First, the vortex was formed and ignited by using a flame stabilizer or the like in order to secure ignition time including the time of vaporization of the liquid fuel by injecting the liquid fuel into the high temperature oxidant flow stream. Therefore, there is a disadvantage in that there is a problem of high cost and heavy weight due to the separate device configuration, and reliability of ignition is low.

둘째, 액체 상태의 연료를 기화할 때 액적이 남은 경우 연소 지연시간이 길어지고 액적 상태의 연료가 많을수록 불완전 연소율이 높아져 로켓 엔진의 성능이 저하되는 문제점이 있다.Second, when the liquid state fuel is vaporized, the combustion delay time becomes long when the droplet is left, and the incomplete combustion rate becomes higher as the fuel in the droplet state is increased, thereby deteriorating the performance of the rocket engine.

따라서 , 별도의 점화 장치를 구성하지 않고도 액체 상태의 연료를 기체 상태의 활성 연료로 변환하여 점화의 신뢰성을 높이고 연료의 불완전 연소율을 최소화하며 장치 구성의 단순화로 비용 절감 효과가 있는 이원추진제 로켓 엔진의 개발이 요구된다.Therefore, it is possible to reduce the incomplete burning rate of the fuel by converting the liquid fuel into the gaseous active fuel to increase the reliability of the ignition, and to reduce the cost of the apparatus by simplifying the structure of the apparatus. Development is required.

본 발명은 상기와 같은 문제를 해결하기 위해서 안출된 것으로서, 분해 반응열을 이용하여 액체 상태의 연료를 기체 상태의 연료로 변환시켜 공급하는 이원추진제 로켓엔진을 제공하고자 한다.SUMMARY OF THE INVENTION The present invention is conceived to solve the problems as described above, and it is an object of the present invention to provide a dual propellant rocket engine that converts liquid fuel into gaseous fuel using decomposition reaction heat.

본 발명은 별도의 점화 장치가 필요 없어 점화 신뢰성이 높으며 연료의 완전 연소율을 극대화할 수 있는 이원추진제 로켓 엔진을 제공하고자 한다.The present invention is to provide a two-propellant rocket engine in which ignition reliability is high and a complete burning rate of the fuel can be maximized without requiring a separate ignition device.

상기 목적을 달성하기 위하여, 본 발명은 액체인 물을 수증기로 변화시켜 레이저광과 광촉매를 이용하여 물을 수소와 산소로 분리하는 시간을 짧게, 효율을 극대화하였다.In order to achieve the above object, the present invention maximizes efficiency by shortening the time for separating water into hydrogen and oxygen using laser light and a photocatalyst by changing water, which is liquid, into water vapor.

또한, 물이 분해 된 수소와 산소가 촉매부에서 다시 연소를 하는 방지하기 위하여 고압의 압력으로 공급하며, 촉매분해 부를 냉각시키는 장치를 설치하였다.In addition, a device for cooling the catalytic cracking section was provided, supplying hydrogen and oxygen decomposed in water at a high pressure to prevent combustion again in the catalytic section.

또한, 수증기가 수소와 산소로, 수소와 산소가 다시 수증기로 즉, 분해와 연소가 반복하여 나타나면 최대의 압력이 발생됨으로 연소실 개구부를 반 유선형으로 설치하였으므로 외부공기가 가열되어 분사압력을 높일 수가 있다.In addition, when water vapor is hydrogen and oxygen, and hydrogen and oxygen are repeatedly decomposed and burned repeatedly, that is, decomposition and combustion are repeated, maximum pressure is generated, so that the combustion chamber opening is installed in a semi-streamlined manner. .

다른 한편, 연소열에 의한 고압부와 압축기 이송에 의한 저압부의의 공기 흐름을 용이하게 하기위하여 테이퍼형태의 압력집중경사판과 압력유도관을 설치하여 공기가 저압에서 고압으로 흐르는 것을 용이하게 하였다.On the other hand, taper type pressure concentration swash plate and pressure induction pipe are installed to facilitate the flow of air from a low pressure to a high pressure in order to facilitate the air flow of the high pressure part by the combustion heat and the low pressure part by the compressor transfer.

상기에서 기술한 바와 같이 본 발명의 레이저광과 촉매로 물을 분해, 연소시켜 추진력을 얻는 추진 장치는 다음과 같은 효과를 발생시킨다.As described above, the propulsion device for decomposing and burning water by the laser beam and the catalyst of the present invention to obtain propulsion force has the following effects.

첫째, 분해 반응열과 전기 또는 주파수 가열장치를 이용하여 액체 상태의 물을 수증기 상태로 변환한 뒤 촉매분해부에 공급하므로 별도의 점화 장치나 연소 지연시간을 고려한 장치가 불필요하여 단순화, 경량화된 시스템을 구현할 수 있으며 비용 절감의 효과가 있다.First, it converts the liquid water into the water vapor state using the decomposition reaction heat and the electric or frequency heating device, and supplies it to the catalyst decomposition unit. Therefore, there is no need for a separate ignition device or a device considering the combustion delay time, It can be implemented and has a cost saving effect.

둘째, 수증기가 분해된 수소와 산소는 비율이 정확하고 별다른 요소가 없이 연소를 함으로서 불완전 연소율을 최소화하여 엔진 효율을 극대화할 수 있는 장점이 있다.Secondly, the ratio of hydrogen and oxygen, which are decomposed in water vapor, is accurate, and combustion is performed without any other factors, thereby minimizing the incomplete combustion rate, thereby maximizing the engine efficiency.

셋째, 연소된 배기가스가 수증기이므로 환경을 파괴하거나 또는 기타의 문제가 되지 않는다.Third, since the exhausted exhaust gas is water vapor, it does not cause environmental damage or other problems.

넷째, 물은 지구상에 어디에서는 공급받기가 용이하므로 연료걱정을 할 필요가 없다.Fourth, water does not have to worry about fuel because it is easy to get anywhere on earth.

제1도 : 본 발명의 레이저광과 촉매로 물을 분해, 연소시켜 추진력을 얻는 추진 장치의 단면도 및 측면도와 중요부품 조립도.
제2도 : 본 발명의 레이저광과 촉매로 물을 분해, 연소시켜 추진력을 얻는 추진 장치의 작동설명도.
제3도 : 본 발명의 레이저광과 촉매로 물을 분해, 연소시켜 추진력을 얻는 추진 장치의 외관 조감도.
* 도면의 주요한 부호에 대한 설명
01) 레이저발생장치 03) 광촉매 05) 연소챔버
06) 압력유도관 07) 추력장치커버 09) 분사장치
11) 고압발생관 13) 외관커버 15) 수증기발생장치
17) 물탱크 19) 베어링하우징 21) 압축기
23) 공기공급관 25) 고정지지체 27) 발전 모터
28) 클러치 29) 임펠러 31) 실린더
33) 증기공급관 53) 수증기 55) 수소분자
56) 산소분자
* 화살표(

Figure pat00001
)는 바람의 이동방향 및 물체의 이동방향과 회전방향.
표시 없는 사각은 공간과 상용부품임.FIG. 1 is a sectional view and a side view of a propulsion device for obtaining propulsion force by decomposing and burning water with a laser beam and a catalyst according to the present invention, and an assembling view of important parts.
Fig. 2 is an explanatory view of the operation of the propulsion device for obtaining propulsion by decomposing and burning water with the laser beam and the catalyst of the present invention. Fig.
FIG. 3 is a perspective view of the external appearance of a propulsion device for decomposing and burning water with a laser beam and a catalyst according to the present invention to obtain propulsion force.
DESCRIPTION OF REFERENCE NUMERALS
01) Laser generator 03) Photocatalyst 05) Combustion chamber
06) Pressure guide tube 07) Thrust device cover 09) Injection device
11) High Pressure Generating Tube 13) Exterior Cover 15) Steam Generator
17) Water tank 19) Bearing housing 21) Compressor
23) Air supply pipe 25) Fixed support 27) Power generation motor
28) Clutch 29) Impeller 31) Cylinder
33) Steam supply line 53) Water vapor 55) Hydrogen molecule
56) Oxygen molecule
* arrow(
Figure pat00001
) Is the direction of wind movement and the direction and direction of movement of the object.
Square without mark is space and commercial parts.

본 발명의 구성 상태를 제1도에서 제3도까지 제시한 도면에 의거하여 상세하게 설명하면 다음과 같다.The constitutional state of the present invention will be described in detail with reference to the drawings from FIG. 1 to FIG. 3.

물을 수소와 산소로 분해를 함에 있어, 태양광과 광촉매로서 분해하는 것의 효율이 낮은 것은 여러 가지의 저해요소가 있기 때문이며, 몸체부에 다수개의 레이저발생장치(01)의 레이저광을 광촉매(03)로 공급되는 수증기(53)에 집중하여 연속하여 조사하기 위하여, 수증기발생장치(25)와 물탱크(17)를 구비한다.The reason for the low efficiency of decomposition of sunlight and photocatalyst in the decomposition of water into hydrogen and oxygen is that there are various obstacles. The laser light of the plurality of laser generating devices 01 is injected into the body part through the photocatalyst 03 A water vapor generator 25 and a water tank 17 are provided for concentrating and irradiating the water vapor 53 supplied to the water tank 53 continuously.

임펠러(29)가 내장 설치된 실린더(31)의 한쪽에 발전 모터(27)가 설치되고; 상기 실린더(31)의 설치 하부에 내부공간과, 외부를 관통하여 흡입관이 설치되며, 다른 쪽에, 내부공간은 테이퍼 기울기로 점점직경이 작아지고 그 단부에 광촉매(03)[여섯 방향으로 구멍이 관통되어 레이저 빛이 조사됨]가 설치되며, 외부는 테이퍼형태와 원통관이 조합된 형태로 설치된 관의중앙 돌기부에 상기 광촉매(03)가 설치된 증기공급관(33)을 설치한다.A power generation motor 27 is installed on one side of the cylinder 31 in which the impeller 29 is installed; The inner space of the cylinder 31 is provided with an inner space and a suction pipe passing through the outer portion. On the other side, the inner space is gradually reduced in diameter by a taper inclination, and a photocatalyst 03 And a steam supply pipe (33) provided with the photocatalyst (03) is installed at the central protruding part of the pipe provided with a combination of a tapered shape and a circular pipe.

이어서, 상기 증기공급관(33)의 다른 쪽에 연소챔버(05)를 설치하고; 상기 연소챔버(05)는 지름이 작아지고 그 끝단은 점차 넓어지도록 설치한다.Subsequently, a combustion chamber (05) is installed on the other side of the steam supply pipe (33); The combustion chamber (05) is installed to have a smaller diameter and a wider end.

이는 연소된 열에 의하여 외부 공기의 온도를 높이고, 내부에서 연소와 분해 작용이 반복하게 발생하게 하여 연소열과 분사압력을 높일 수 있게 설치한 것이다This is to increase the temperature of the outside air by the burned heat and cause the combustion and decomposition to occur repeatedly in the inside, so that the combustion heat and the injection pressure can be increased

이어서, 상기 수증기발생장치(15)의 출구와 상기 수증기 흡입관을 연결하고, 물탱크(17)와 수증기발생장치(15)를 관이음을 통하여 연결 설치한다.Next, the outlet of the steam generator 15 is connected to the steam suction pipe, and the water tank 17 and the steam generator 15 are connected to each other through pipes.

한편, 상기 고정지지체(25)의 다른 쪽에 압축기(21)의 모터 부를 연결설치하고; 상기 압축기(21)의 임펠러보타 직경이 약간 크게 설치된 공기공급관(23)을 설치하며; 상기공기공급관(23)의 한쪽에 베어링하우징(19)을 설치하고, 다른 쪽에 고압발생관(11) 설치하고; 상기 고압발생관(11) 끝단부에 분사장치(09)를 설치한다.On the other hand, the motor section of the compressor (21) is connected to the other side of the stationary support body (25); An air supply pipe (23) provided with a slightly larger impeller blade diameter of the compressor (21); A bearing housing (19) is provided on one side of the air supply pipe (23) and a high pressure generating pipe (11) is installed on the other side; An injection device (09) is installed at the end of the high pressure generating pipe (11).

이때, 연소챔버(05)와 고압발생관(11)의 사이에 연소챔버(05)쪽은 넓고 고압발생관(11)쪽은 틈새가 좁게 하며, 연소챔버(05)쪽은 밀봉되고 고압발생관(11)쪽은 개방되어 있는 압력조정 판이 설치되며, 이어서 압력 유도관(06)이 연소챔버(05)의 외부에 견고하게 설치되어 내부에 열에 의해 공기의 압력과 온도가 상승하게 되는 압력 발생공간이 설치된다.At this time, between the combustion chamber 05 and the high-pressure generating tube 11, the combustion chamber 05 is wide, the high-pressure generating tube 11 has a narrow gap, the combustion chamber 05 is sealed, The pressure induction pipe 06 is installed firmly on the outside of the combustion chamber 05 so that the pressure and temperature of the air are increased by the heat, Respectively.

또한, 내부에 기 설치된 장치들과 동심을 이루어 설치하여야 하고, 특히, 외부몸체에 설치된 레이저발생장치(01)의 레이저광이 광촉매(03)에 도달할 수 있도록 보호관을 설치하되; 상기 보호관은 렌즈를 포함한 압력이 외부로 유출되지 않도록 하여 설치한다.In addition, it should be installed concentrically with the devices installed in the inside, and in particular, a protective pipe is provided so that the laser light of the laser generator 01 installed in the outer body can reach the photocatalyst 03; The protective tube is installed such that the pressure including the lens is not leaked to the outside.

이어서, 유체의 흐름이 유선형으로 흐르도록 외관커버(13)와 추력장치커버(07)를 설치하면 본 발명의 구성이 완료된다.Subsequently, the outer cover 13 and the thrust device cover 07 are installed so that the flow of the fluid flows in a streamlined manner, thereby completing the construction of the present invention.

이어서, 본 발명의 작용 상태를 제1도에서 제3도까지 제시된 도면에 의거하여 상세히 설명하면 다음과 같다.Next, the operation state of the present invention will be described in detail with reference to the drawings shown from FIG. 1 to FIG. 3.

물을 수소와 산소로 분해를 함에 있어, 태양광과 광촉매로서 분해하는 것의 효율이 낮은 것은 여러 가지의 저해요소가 있기 때문이며, 다수개의 레이저발생장치(01)의 레이저광을 광촉매(03)로 공급되는 수증기(53)에 집중하여 연속하여 조사하면, 레이저광의 빛과 열, 광촉매(03)의 반응에 의하여 수소분자(55)와 산소분자(56)로 분해된다.The reason for the low efficiency of decomposition as sunlight and photocatalyst in the decomposition of water into hydrogen and oxygen is that there are various obstacles. The laser light of the plurality of laser generators 01 is supplied to the photocatalyst 03 The oxygen molecules 56 are decomposed into hydrogen molecules 55 and oxygen molecules 56 by the reaction of the laser light with heat and the photocatalyst 03.

물탱크(17)에서 수증기발생장치(15)로 공급된 물이 수증기(53)로 변하고, 임펠러(29)의 회전에 의하여 수증기(53)가 고압으로 광촉매(03)로 이송되면, 레이저발생장치(01)에서 발생되는 레이저광과 광촉매에 의하여 수증기(53)는 수소(55)와 산소(56)로 분해된다.When the water supplied from the water tank 17 to the steam generator 15 is converted into steam 53 and the steam 53 is transferred to the photocatalyst 03 at a high pressure by the rotation of the impeller 29, The water vapor 53 is decomposed into the hydrogen 55 and the oxygen 56 by the laser light and the photocatalyst generated in the oxygen sensor 01.

이어서, 연소된 열과 부피가 커진 수증기(53)에 의하여 연소챔버(05)내부에 압력이 상승되고, 분해와 연소가 반복하며, 상승된 압력에 의하여 분사장치(09)를 통과하여 외부로 분사된다.Subsequently, the pressure in the combustion chamber 05 is raised by the burned heat and the bulky water vapor 53, decomposition and combustion are repeated, and the gas is injected to the outside through the injector 09 by the elevated pressure .

한편, 압축기(21)로 유입된 공기가 공기공급관(23)을 통하여 이송되는 과정에서 온도와 압력이 상승하게 되고, 압력유도관(06)을 통과하여 고압발생관(11)으로 이송되어, 내부의 연소열에 의하여 고압과 고온으로 변하여 외부로 분사된다.Meanwhile, the temperature and the pressure are increased in the course of the air flowing into the compressor 21 through the air supply pipe 23, and is then transferred to the high pressure generating pipe 11 through the pressure induction pipe 06, The high temperature and the high temperature are changed by the heat of combustion.

이때, 공기공급관(23)과 고압발생관(11)의 사이에는 압력이 낮은 곳에서 높은 곳으로 공기가 이송되어야 하는데, 이는 연소챔버(05)의 외부와 고압발생관(11)사이에 설치된 압력조정판과 압력유도관(06)에 의하여 가능하다.At this time, air must be transferred between the air supply pipe 23 and the high pressure generating pipe 11 from a low pressure to a high pressure. This is because the pressure exerted between the outside of the combustion chamber 05 and the high pressure generating pipe 11 It is possible by adjusting plate and pressure guide pipe (06).

이와 같이 레이저의 광과 광촉매(03)에 의한 수증기(53)를 분해하여 연소시켜 그 압력과 열을 이용하여 물체를 추진할 수 있으며, 이에 따른 레이저 발생장치(01)의 설명은 고체레이저와 기체레이저, 반도체레이저, 화학레이저 등의 장치를 필요에 따라 대체하여 사용할 수 있으며, 이의 설명은 이미 공지기술이므로 설명은 생략한다.As described above, the laser beam and the water vapor 53 generated by the photocatalyst 03 are decomposed and burned, and the object can be propelled by using the pressure and the heat. , A semiconductor laser, a chemical laser, and the like can be used in place of the apparatus according to need, and the description thereof is omitted.

지구상의 70%가 물이며, 이를 연료 화 하여 추진하는 추진체이고, 환경적인 문제도 발생하지 않으므로 이 발명은 반드시 필요하다.This invention is necessary because 70% of the earth is water, it is a propellant that propels it into fuel, and there is no environmental problem.

이상에서 설명한 것은 레이저광과 광촉매로 물을 분해, 연소시켜 추진력을 얻는 추진 장치의 본 발명을 실시하기위한 하나의 실시 예에 불과한 것으로 본 발명은 상기한 실시 예에 한정하지 않고 이하의 특허 청구 범위에서 청구하는 본 발명의 요지를 벗어남이 없이 당해 발명에 속하는 분야에서 통상의 지식을 가진 자라면 누구든지 다양한 변경실시가 가능할 것이다.The present invention is not limited to the above-described embodiment, but may be embodied in the following claims, and may be embodied in the following claims, It will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined in the appended claims.

Claims (4)

임펠러(29)가 내장 설치된 실린더(31)의 한쪽에 발전 모터(27)를 설치하고; 실린더(31)의 다른 쪽에, 내부공간은 테이퍼 기울기로 점점직경이 작아지고 그 단부에 광촉매(03)[여섯 방향으로 구멍이 관통되어 레이저 빛이 조사됨]를 설치하며, 외부는 테이퍼형태와 원통관이 조합된 형태로 설치된 관의중앙 돌기부에 광촉매(03)가 설치된 증기공급관(33)을 설치하고; 증기공급관(33)의 다른 쪽에 연소챔버(05)[연소챔버(05)는 지름이 작아지고 그 끝단은 점차 넓어짐]를 설치하는 레이저발생장치(01)를 포함한 분해와 연소부 설치수단과,
고정지지체(25)의 다른 쪽에 압축기(21)의 모터 부를 연결설치하고; 압축기(21)의 임펠러보타 직경이 크게 설치된 공기공급관(23)을 설치하며; 공기공급관(23)의 한쪽에 베어링하우징(19)을 설치하고, 다른 쪽에 고압발생관(11) 설치하고; 고압발생관(11) 끝단부에 분사장치(09)를 설치하되,
연소챔버(05)와 고압발생관(11)의 사이에 연소챔버(05)쪽은 넓고 고압발생관(11)쪽은 틈새가 좁게 하며, 연소챔버(05)쪽은 밀봉되고 고압발생관(11) 쪽은 개방되어 있는 압력조정 판을 설치하며, 압력 유도관(06)이 연소챔버(05)의 외부에 설치되는 분사부의 설치수단이 특징인 레이저광과 광촉매로 물을 분해 연소시켜 추진력을 얻는 추진 장치.
A power generation motor 27 is installed on one side of the cylinder 31 in which the impeller 29 is installed; On the other side of the cylinder 31, the inner space is gradually reduced in diameter by a tapered inclination, and a photocatalyst 03 (a hole is penetrated in six directions and irradiated with laser light) is provided at the end thereof. A steam supply pipe (33) provided with a photocatalyst (03) is installed at a central protruding portion of a pipe provided with a combination of clearances; A disassembling and burning section installing means including a laser generating apparatus 01 for installing a combustion chamber 05 (the diameter of the combustion chamber 05 is smaller and its end gradually widened) is provided on the other side of the steam supply pipe 33,
Connecting the motor portion of the compressor (21) to the other side of the fixed support (25); Installing an air supply pipe (23) provided with a large impeller blade diameter of the compressor (21); A bearing housing (19) is provided on one side of the air supply pipe (23) and a high pressure generating pipe (11) is provided on the other side; The injection device (09) is installed at the end of the high pressure generating pipe (11)
The gap between the combustion chamber 05 and the high pressure generating tube 11 is wide and the gap between the combustion chamber 05 and the high pressure generating tube 11 is narrow and the combustion chamber 05 is sealed, ) Is provided with an open pressure regulating plate and the pressure induction pipe 06 is provided outside the combustion chamber 05. The means for installing the jetting portion is a laser light and a photocatalyst, Propulsion device.
제1항에 있어서, 레이저발생장치(01)를 고체레이저, 기체레이저, 반도체레이저, 액체화학레이저로 대체하여 설치한 것을 특징으로 하는 레이저광과 광촉매로 물을 분해 연소시켜 추진력을 얻는 추진 장치.The propulsion device according to claim 1, wherein the laser generator (01) is replaced by a solid laser, a gas laser, a semiconductor laser, or a liquid chemical laser. 제1항에 있어서, 수증기발생장치(15)를 히터, 초음파, 고주파에 의한 수증기발생장치로 대체하여 설치한 것을 특징으로 하는 레이저광과 광촉매로 물을 분해 연소시켜 추진력을 얻는 추진 장치.The propulsion device according to claim 1, wherein the water vapor generating device (15) is replaced with a water vapor generating device using a heater, an ultrasonic wave, and a high frequency to provide a propulsion force by decomposing and burning water with a laser beam and a photocatalyst. 제1항에 있어서, 광촉매(03)의 재질을 Sn3O4, TiO2의 재질로 대체하여 설치되는 것이 특징인 레이저광과 광촉매로 물을 분해 연소시켜 추진력을 얻는 추진 장치.The propulsion device according to claim 1, wherein the photocatalyst (03) is replaced by a material selected from the group consisting of Sn3O4 and TiO2, and the propellant is obtained by decomposing and burning the water with laser light and a photocatalyst.
KR1020180000361A 2017-12-28 2017-12-28 A Propellator that Achieves Momentum by Disassembling and Burning Water with Laser Light and Photocatalyst Ceased KR20190080675A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116692036A (en) * 2023-06-20 2023-09-05 上海大学 Ultrasonic water-based propulsion system for adjusting attitude and orbit angle of aircraft and aircraft
CN117533526A (en) * 2023-06-20 2024-02-09 上海大学 An ultrasonic water-based propulsion system and satellite for attitude control of space micro-satellites

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116692036A (en) * 2023-06-20 2023-09-05 上海大学 Ultrasonic water-based propulsion system for adjusting attitude and orbit angle of aircraft and aircraft
CN117533526A (en) * 2023-06-20 2024-02-09 上海大学 An ultrasonic water-based propulsion system and satellite for attitude control of space micro-satellites
CN116692036B (en) * 2023-06-20 2024-09-24 上海大学 Ultrasonic water-based propulsion system and aircraft for aircraft attitude and orbit angle control
CN117533526B (en) * 2023-06-20 2024-11-26 上海大学 An ultrasonic water-based propulsion system for attitude control of space micro-satellite and satellite

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