KR20220038026A - 4 connected fans on an axle turbine : 1. The inner fans on the axle in inner cylinder, 2. The outer fans on the axle in outer cylinder &3. The duct fans on the outer fans inside in 2 outer cylinders and 2 inner cylinders, 4. The blades on the duct fans ring in the duct with an inlet and an oulet with another Cylinder - Google Patents
4 connected fans on an axle turbine : 1. The inner fans on the axle in inner cylinder, 2. The outer fans on the axle in outer cylinder &3. The duct fans on the outer fans inside in 2 outer cylinders and 2 inner cylinders, 4. The blades on the duct fans ring in the duct with an inlet and an oulet with another Cylinder Download PDFInfo
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- 230000000704 physical effect Effects 0.000 claims abstract description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 26
- 238000003466 welding Methods 0.000 claims description 4
- 230000002093 peripheral effect Effects 0.000 claims 1
- 230000002457 bidirectional effect Effects 0.000 description 11
- 239000007789 gas Substances 0.000 description 5
- XLYOFNOQVPJJNP-ZSJDYOACSA-N Heavy water Chemical compound [2H]O[2H] XLYOFNOQVPJJNP-ZSJDYOACSA-N 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000010248 power generation Methods 0.000 description 4
- 230000001681 protective effect Effects 0.000 description 4
- 238000005086 pumping Methods 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 239000000428 dust Substances 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000005485 electric heating Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000003517 fume Substances 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000009527 percussion Methods 0.000 description 2
- 239000000779 smoke Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 230000002572 peristaltic effect Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/02—Wind motors with rotation axis substantially parallel to the air flow entering the rotor having a plurality of rotors
- F03D1/025—Wind motors with rotation axis substantially parallel to the air flow entering the rotor having a plurality of rotors coaxially arranged
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/04—Wind motors with rotation axis substantially parallel to the air flow entering the rotor having stationary wind-guiding means, e.g. with shrouds or channels
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/10—Stators
- F05B2240/12—Fluid guiding means, e.g. vanes
- F05B2240/123—Nozzles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/37—Multiple rotors
- F05B2240/372—Multiple rotors coaxially arranged
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Abstract
Description
1. 인너 팬들의 인너 실린더와1. Inner cylinder of inner fans and
2. 아웃터 팬들의 아웃터 실린더와2. With the outer cylinder of outer fans
3. 양쪽 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 인너 팬들을 이은 아웃터 팬들링에 덕트팬들과 덕트3. Both 1. Inner cylinders and 2. Duct fans and ducts in the outer fan ring that connects the inner fans between the outer cylinders
4 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 아웃터 팬들의 아웃터 팬링과 3. 덕트팬들과 덕트팬링에 블레이드와 블레이드 외부 덕트형틀4 1. Inner cylinders and 2. Outer fan ring of outer fan between outer cylinders, and 3. Blade and blade outer duct frame in duct fan and duct fan ring
중세의 풍차와 수차에서 발안하고Inspired by medieval windmills and waterwheels
산업혁명시대 초기 터빈들에서 단순한 공기터빈들을 2합 공기터빈인 공기터빈과 덕트터빈을 합한 것과 인너터빈과 아웃터터빈을 합한 것과In the early turbines of the industrial revolution era, simple air turbines were combined with an air turbine and a duct turbine, which are two air turbines, and an inner turbine and an outer turbine.
3합 공기터빈인 인너터빈과 아웃터터빈을 합한 것에 덕트터빈을 합한 것과A combination of an inner turbine and an outer turbine, which are three-air turbines, and a duct turbine
상기의 터빈들의 물성이 공기, 가스, 스팀 물이라는 같은 터빈에서The properties of the above turbines are air, gas, steam and water in the same turbine.
4합은 상기의 터빈들의 물성이 공기, 가스, 스팀 물 터빈에 더하여 같거나 다른 상기의 터빈들의 물성이 공기, 가스, 스팀 물을 보내어 고압에서 다른 구동형태에 고압을 더하여 이용하는 것으로In addition to the air, gas, steam and water turbine, the physical properties of the above turbines are the same or different from that of the air, gas, and steam water turbines.
본 발명인이 이전에 출원한 특허문헌을 인용한 내용 :
일(1)터빈에 3합한 터빈에서 타 물성으로 3합한 터빈의 일축을 구동해야 하는 과제(1) The task of driving a single shaft of a turbine with three combinations of turbines with other properties
일(1)터빈에 3합한 터빈에서 타 물성으로 3합한 터빈의 일축을 구동할 때 타 물성을 가변시켜야 하는 과제(1) A task to change other properties when driving one shaft of a turbine with three combinations of turbines with other properties
본 발명에서in the present invention
일(1)터빈에 3합한 터빈에서 타물성으로 3합한 터빈의 일축을 구동해야 하는과제 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 양쪽 실린더들을 연결하며 인너 팬들을 이은 아웃터 팬들링에 덕트팬들과 덕트과 타 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 양쪽 실린더들을 연결하며 인너 팬들을 이은 아웃터 팬들링에 덕트팬들과 덕트(타물성을 아웃터 팬들링 외부로 순환시키는 수단과The task of driving the single shaft of the turbine that is combined with the one (1) turbine by the other physical properties Fans and ducts and other 1. Inner cylinders and 2. Both cylinders are connected between the outer cylinders, and duct fans and ducts (meaning and
4 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 아웃터 팬들의 아웃터 팬링과 3. 덕트팬들과 덕트팬링에 블레이드와 블레이드 외부 덕트형틀 내의 타 물성으로 블레이드를 구동시키는 수단4 1. Inner cylinders and 2. Outer fan ring of outer fans between outer cylinders, 3. In duct fans and duct fan ring, means to drive the blade with other properties in the blade and the blade outer duct frame
본 발명이 성공적으로 이행하게 되면When the present invention is successfully implemented
본 발명은 흡입구가 인너 실린더들은 전방이라면 2. 아웃터 실린더들의 흡입구는 후방이 되고 측면은 덕트터빈에서 이루어지지만 4합은 동일 물성이나 타물성으로 흡입구와 배출구를 다르게 동력전달수단으로 하는 것과In the present invention, if the intake port is the front of the inner cylinders 2. The intake port of the outer cylinders is the rear, and the side is made in a duct turbine, but the 4 is the same or different properties, so that the inlet and outlet are differently used as power transmission means
공기터빈에 스팀으로 다른 흡입구에서 흡입하고 다른 배출구로 배출하여 공기와 스팀을 같이 구동수단으로 하든지 수터빈에 스팀을 가하여 동력전달수단으로 하는 것과Steam is sucked into an air turbine from another inlet and discharged through another outlet to use air and steam as a driving means or to apply steam to a water turbine as a power transmission means;
물속 프로펠러를 이용한 추진기에 배의 물탱크 내 스팀탱크의 스팀관으로 추진기 실린더에 외주시켜 스팀관으로 구동하는 전혀 다른 곳에서 구동수단으로 타물성을 이용하는 일 물성 이상의 구동수단으로 터빈을 이용할 수있는 효과가 있다.The effect of using a turbine as a driving means with more than one physical property that uses other properties as a driving means in a completely different place where the propulsion using a propeller in the water is driven by a steam pipe by outer circumference of the propeller cylinder with the steam pipe of the steam tank in the water tank of the ship there is
도면1은 4합 터빈에 대한X150, Y330, Z180의 입체도면이다.
도면2(a),(b),(c)는 인너 실린더 내의 인너 팬들과 서포터(909)들에 대한 설명도이다.
도면3(a),(b),(c)는 인너 실린더 내의 인너 팬들과 서포터(909)들과 아웃터 실린더와 아웃터 팬들과 서포터들에 대한 설명도이다.
도면4는 도면3(a),(b),(c)에 덕트터빈을 합한 설명도이다.
도면5는 도면1은 4합 터빈을 인너 실린더 내의 인너 팬들과 서포터(909)들과 아웃터 실린더와 아웃터 팬들과 서포터들에 대해 줄인 대한X150, Y330, Z180의 입체도면이다.
부호설명
inner Cylinder (ic), outer Cylinder (oc), 거치대(Supoters)(s), Axle (a), (hub)(h), inner fans(if), outer fans(of), 공기회유원판(U), 연결살(k), 원통형 fans(f) ring (fr), blades(b), (duct)통관(db)의 인렛(ib), 원통형 blades)(b) ring(br), 덕트(duct)통관(db), 인렛(Inlet)(ib), 아웃렛(Outlet)(ob), 4번째 터빈(4t), turbine(t)
공기, 물 등의 3합 터빈(공기터빈 축에 1. 인너 팬들의 인너 실린더와 2. 아웃터 팬들의 아웃터 실린더와 3. 양쪽 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 아웃터 팬들에 덕트팬들과 덕트터빈에 물성이 다른 외장덕트를 더한 터빈
(특허문헌 14) (압력공기)터보엔진 10-2005-0131732
(특허문헌 15) 자가연속공기펌핑분출장치(I), 태엽(V), 회전연속격발공기발사기 (II), 에어 콘푸레서(III), 에어콘푸레서(IV), 자석엔진(VI)과 더불어 배터리(VII), 조절판(VIII)과 열선(IX)을 가지는 시스템 10-2005-0131733
(특허문헌 16) (압력공기) 터빈 10-2005-0133691
(특허문헌 21) 압력공기 터빈엔진 10-2007-0037258
(특허문헌 22) (압력공기) 터보엔진 10-2007-0037259
(특허문헌 29) 공기터빈엔진, 자석엔진(베어링)과 압축공기발사기를 이용한 발전기 10-2013-0049703
(특허문헌 30) 압축공기터빈 10-2013-0073137
(특허문헌 37) 기계 회전축에 설치되어 회전축이 회전할 때 상기 기계회전축에 설치되는 Air Pumper와 Air Tank로 하는 Compressor로 압축 공기발사기 Cylinder들 내부에 Spring 을 압축하는 것과 같은 극의 전자자석과 영구자석으로 하는 압축공기생성장치가 내장된 압축공기발사기 10-2015-0021433
(특허문헌 38) 선박의 조향기구, 'Air, Steam Turbine Engine'과 'Water Tank & Boiler System', 'Air, Water, Steam Propulsor'를 가지는 System 10-2015-0031408
(특허문헌 39) 연과 낙하산, 날개들을 가지는 배낭 10-2016-0071178
(특허문헌 40) 공기터빈과 덕트 터빈을 합한 터빈 10-2016-0071179
(특허문헌 41) 여러 종류의 공기터빈들의 조합으로 형성하는 공기추진기들로 비행하게 하는 여러 장치와 조정 장치를 가진 비행기구 10-2016-0090125
(특허문헌 42) A prefabricated furnace에 설치한 a scaffolding과 an air furnace combined with 3 different air turbines들을 조합 이용하여 산사태 지역, 축대, 지진피해 저감과 중수 재활용과 눈, 빙판을 해결한 길 (도로)
(특허문헌 52) 신체프레임과 날개를 단 배낭과 변형하는 외부 Body(문, 지붕, 바닥) 프레임과 날개를 더 단 비행기구들의 장비를 이용하는 장치들 10-2017-0137338
(특허문헌 59) 수상 재난 대응 구조선과 장비들 {The secure ships & equipments of the Aqua accident} 10-2018-0034283
(특허문헌 60) 미세먼지를 줄이기 위해 필요한 장비들 {Equipments needed to reduce of (ultra)fine dust} 10-2018-0039921
(특허문헌 61) 화재진압에 필요한 장비들{The secure equipments needed to fire combat} 10-2018-0107032
(특허문헌 62) 퀵보드 등 승용기구바퀴(회전자)와 바퀴덮개(고정자)에 설치하는 발전기 {The Generator of wheel(s) with Kickboard(etc)} 10-2020-0052213
(특허문헌 63)자전거바퀴(회전자)와 바퀴덮개(고정자)에 설치하는 발전기 {The Generator of wheel(s) with Bicycle} 10-2020-0052638
(특허문헌 64) 발판보드에 설치하는 발전기 {The Generator of wheel(s) with Footboard} 10-2020-0053218
(특허문헌 65) 자전거와 리어캐리어에 설치하는 발전기 {The Generator of wheel(s) with Bicycle and Rear Carrie} 10-2020-0053666
(특허문헌 66) 수상보드에 설치하는 발전기 {The Generator with Aqua board} 10-2020-0054507
(특허문헌 67) 헬스차량에 설치하는 발전기 {The Generator with Health Vehicle} 10-2020-0055267
(특허문헌 0068) 보트에 설치하는 발전기 {The Generator with Boat} 10-2020-0055932
(특허문헌 0069) 수차와 공기 컴프레서를 이용한 공기 터빈구조 발전기와 바퀴구조 발전기를 합한 발전기 {Air Turbine type Generator connected Wheels type Generator used by Falling water & Air Compressor } 10-2020-0056031
(특허문헌 0070) 펠티어소자를 이용한 공기, 물 컨디션너 조절장치 내에 설치한 발전기 {The Generator installed in air and water conditioner control device using Peltier modules } 10-2020-0062927
(특허문헌 0071) "공기 터빈구조 발전기"와 "바퀴구조를 합한 발전기"를 "발열소자를 이용한 발전기"와 적용 양방향 모터(양방향 프로펠러)를 양방향공기추진기(Propulsor)와 결합 장착한 드론 {Drone with generators that change the rotation direction of the propeller motor using the Peltier element as a power generation element} 10-2020-0073012
(특허문헌 0072) 역방향 모터(양방향 프로펠러)의 추진에 맞는 관성을 이기는 팬이 없는 양방향 공기 추진기(Propullor)를 장착한 드론{The Drone equipped with the Fanless bidirectional the Jet engine(other than the Propullor) that overcome the inertia suitable for the propulsion of a bidirectional Motor (bidirectional propeller) - similar to a slow Scram jet 2type & with a directional Motor similar to a slow Scram jet 1 type } 10-2020-0080402
(특허문헌 0073) 전동 오토바이 모터의 정격에 맞는 오토바이바퀴에 회전자와 물받이 고정자 발전기를 설치한 오토바이에 모터가 장착된 항공기 공기추진기와 장착한 드론의 프로펠러(Propullor)를 장착하는 제조기술) {A power generation motorcycle in which a rotor and a stator generator in a drip tray are installed on a motorcycle wheel that meets the rating of the electric(Generator) motorcycle motor. Aircraft propullor and drone propulsor are installed as options} 10-2020-0110057
(특허문헌 0074) 전동 오토바이에 설치한 모터가 장착된 항공기 공기추진기와 장착한 프로퓰러(Propullor)로 구성한 오토에어크라프트(Autoaircraft) {The auto aircraft propullor and drone propulsor are installed as options electric(Generator) motorcycle motor} 10-2021-0011018
(특허문헌 0075) 산사태에 대비, 대응하는 에어 레이어들 블록들이 형성된 거대장비들(에어 레이어들 블록들){Large equipment made of air layers blocks to prepare for and respond to landslides(earth slide, mudslide)} 10-2021-0023260
(특허문헌 0076) 전동에어버스 {The airbus electric(Generator)} 10-2021-0037914
(특허문헌 0077) 전동에어버스에 설치하는 연기(분연), 재 포집장치 {A device that collects fire smoke, volcanic fumes and ash installed in airbus electric(Generator) } 10-2021-0039765
(특허문헌 0078) 전기에어카 {The aircar electric(Generator) } 10-2021-0042049
(특허문헌 0079) 전기에어버스를 강풍, 태풍에 구조하는 보조날개와 보조출입문 장치 {Auxiliary wings and auxiliary door devices to rescue airbus electric(Generator) from strong winds and typhoons } 10-2021-0048062
(특허문헌 0080) 모터가 장착된 회전축에 다량의 회전자바퀴와 다량의 고정자바퀴발전기를 설치한 전동보드 {An electric board with a large number of rotor wheels and a large number of stator wheel generators on a motorized shaft} 10-2021-0054360
(특허문헌 0081) 의료용 전동보드 {The medical electric board} 10-2021-0068477에 적용한 구동수단과 샤프트와 터빈과 관련된 문헌을 인용한 것으로
본 발명에서는
일(1)터빈에 3합한 터빈에서 타물성으로 3합한 터빈의 일축을 구동해야 하는과제 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 양쪽 실린더들을 연결하며 인너 팬들을 이은 아웃터 팬들 링에 덕트 팬들과 덕트과 타 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 양쪽 실린더들을 연결하며 인너 팬들을 이은 아웃터 팬들 링에 덕트 팬들과 덕트(타물성을 아웃터 팬들 링 외부로 순환시키는 수단과
4 1. 인너 실린더들과 2. 아웃터 실린더들의 사이에 아웃터 팬들의 아웃터 팬링과 3. 덕트 팬들과 덕트 팬링에 블레이드와 블레이드 외부 덕트 형틀 내의 타 물성으로 블레이드를 구동시키는 수단을 찾고자 하며
도면을 통하여 상세 설명하고자 한다.
도면1은 4합 터빈에 대한X150, Y330, Z180의 입체도면이다.
실린더(Cylinder)(c)를 인너(inner)와 아웃터(outer)로 이중으로 설치하고 상기 인너(inner)(Cylinder)(ic)와 아웃터(outer)실린더(Cylinder)(oc)들을 뛰우고 상기 (Cylinder)(c)들 사이에 터빈(turbine) 축(axle)(a)에 인너(inner)팬(fans)(if)들과 아웃터(outer)팬(fans)(if)들을 설치한 상기 아웃터(outer)팬(fans)(if)에 덕트 팬(duct fans)(df)들을 설치하고 상기 덕트 팬(duct fans)(df)들을 덮는 덕트를 쒸우며 상기 덕트 팬(duct fans)(df)들링을 형성하고 상기 덕트 팬(duct fans)(df)들링에 블레이드(blades)(b)들을 설치하고 상기 블레이드(blades)(b)들을 덮는 다른 실린더(Cylinder) (c3)를 형성하며 상기 실린더(Cylinder)(c3)에 흡입구(Inlet)(i)와 배출구(Outlet)(o)를 형성한 터빈(turbine) (t)에 대한 것이다.
도면2(a),(b),(c)는 인너 실린더 내의 인너 팬들과 서포터(909)들에 대한 설명도이다.
상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)를 거치대(Supoters)(s)로 연결하되
상기 거치대(Supoters)(s)들을 정형되게 나누어 설치된 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)의 축(Axle)(a)의 앞과 뒤에는 축(Axle)(a)허브(hub)(h)를 형성하고 앞, 뒤 상기 허브(hub)(h)에는 축(Axle)(a)허브(hub)(h)에서 앞, 뒤 상기 아웃터(outer)실린더(Cylinder)(oc)까지 상기 거치대(Supoters)(s)들을 정형되게 나누어 설치하여 축(Axle)(a)허브(hub)(h)에 연결되어 축(Axle)(a)이 구동하게 되는 것이다.
도면3(a),(b),(c)는 인너 실린더 내의 인너 팬들과 서포터(909)들과 아웃터 실린더와 아웃터 팬들과 서포터들에 대한 설명도이다.
상기 아웃터(outer)실린더(Cylinder)(oc) 내에 상기 아웃터(outer)실린더(Cylinder)(oc)의 길이 보다 짧은 상기 인너(inner)실린더(Cylinder)(ic)들을 여러개 설치하고 상기 거치대(Supoters)(s)들로 연결하되 상기 축(Axle)(a)에는 팬스(fans)(f)들을 설치하며 상기 아웃터(outer)실린더(Cylinder)(oc) 내에 상기 인너(inner)실린더(Cylinder)(ic)들 내에 상기 축(Axle)(a)에는 인너(inner)팬스fans(if)들을 설치하고 상기 인너(inner)실린더(Cylinder)(ic)들과 상기 인너(inner)실린더(Cylinder)(ic)들 사이에는 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들 끝들에 반대방향의 공기흐름이 발생되는 아웃터(outer)팬스fans(of)들과 연결되게 형성하여
상기 아웃터(outer)실린더(Cylinder)(oc) 내에 상기 인너(inner)실린더(Cylinder)(ic)들 내에 상기 축(Axle)(a)에는 인너(inner)팬스fans(if)들과 상기 인너(inner)실린더(Cylinder)(ic)들과 상기 인너(inner)실린더(Cylinder)(ic)들 사이에는 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들과 아웃터(outer)팬스fans(of)들을 구동되며
상기 아웃터(outer)실린더(Cylinder)(oc)외주면에서 상기 인너(inner)실린더(Cylinder)(ic) 내주까지 공기회유원판(U) 형성하고 상기 공기회유원판(U)에서 상기 축(Axle)(a)의 허브(hub)(h)까지 연결살()을 설치하여 상기 아웃터(outer)실린더(Cylinder)(oc)에서 인너(inner)팬스fans(if) 앞 인렛(Inlet) 까지공기회유원판(U)을 형성하여 상기 아웃터(outer)실린더(Cylinder)(oc)에서 상기 인너(inner)실린더(Cylinder)(ic)으로 바람을 되돌려 인너(inner)실린더(Cylinder)(ic)와 아웃터(outer)실린더(Cylinder)(oc) 터빈(turbine)(t)에 대한 것이다.
도면4는 도면3(a),(b),(c)에 덕트터빈을 합한 설명도이다.
상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이에 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들과 아웃터(outer)팬스fans(of)들을 연결되게 형성하며 인너(inner)팬스fans(if)들과 아웃터(outer)팬스fans(of)들은 바람흐름 방향이 반대로 팬스fans(f)들의 각이 반대로 형성하며, 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들을 아웃터(outer)팬스 fans(of)들과 연결된 팬스fans(f)들의 끝에는 원통형 팬스fans(f)링(ring)(fr)을 형성하고 일정한 간격의 블레이드blades(b)들을 설치하여 상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이는 상기 블레이드blades(b)들을 외주하는 덕트(duct)통관(d)에 용접하여 형성하는 것 내지 접면에 고정체로 고정하고 인렛을 형성하며, 상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이에 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들을 아웃터(outer)팬스fans(of)들과 연결된 팬스fans(f)들의 끝에는 원통형 팬스fans(f)링(ring)(r)을 형성하고 일정한 간격의 블레이드blades(b)들을 설치하여 상기 덕트(duct)통관(db)의 블레이드blades(b)들의 공기인렛(Inlet)(i)에서 흡입된 후 상기 아웃터(outer)팬스fans(of)들과 연결된 상기 축(Axle)(a)을 구동하며 바람흐름방향에 더하여 지는 것이다.
도면5는 도면1은 4합 터빈을 인너 실린더 내의 인너 팬들과 서포터(909)들과 아웃터 실린더와 아웃터 팬들과 서포터들에 대해 줄인 대한X150, Y330, Z180의 입체도면이다.
상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이는 상기 블레이드blades(b)들을 외주하는 덕트(duct)통관(d)에 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들을 상기 아웃터(outer)팬스fans(of)들과 연결된 팬스fans(f)들의 끝의 원통형 팬스fans(f)링(ring)(fr)에 형성된 일정한 간격의 블레이드blades(b)들을 연결하는 원통형 블레이드blades(b)링(ring)(br)을 형성하고 외주하는 덕트(duct)통관(db)을 상기 아웃터(outer)실린더(Cylinder)(oc1)와 상기 아웃터(outer)실린더(Cylinder)(oc2)들의 연결면과 용접하여 형성하는 것 내지 접면에 고정체로 고정하고 인렛(Inlet)(ib)과 아웃렛(Outlet)(ob)을 형성하여 상기 덕트(duct)통관(db)의 인렛(Inlet)(ib)에서 상기 아웃터(outer)실린더(Cylinder)(oc)로 들어가지 않고 상기 아웃렛(Outlet)(ob)으로 출력되면서도 상기 축(Axle)(a)을 구동하는 것으로
상기 아웃터(outer)실린더(Cylinder)(oc) 뒤에서 흡입되고 상기 인너(inner)실린더(Cylinder)(ic)들 앞에서 흡입되어 상기 축(Axle)(a)에는 인너(inner)팬스(fans)(if)들과 상기 인너(inner)실린더(Cylinder)(ic)들과 상기 인너(inner)실린더(Cylinder)(ic)들 사이에는 상기 축(Axle)(a)의 인너(inner)팬스(fans)(if)들과 아웃터(outer)팬스(fans)(of)들을 구동되며 상기 아웃터(outer)실린더(Cylinder)(oc)에서 상기 인너(inner)실린더(Cylinder)(ic)로 상기 공기회유원판(U)공기를 되돌려 주입하여 상기 축(Axle)(a)의 상기 인너(inner)실린더(Cylinder)(ic)의 상기 인너(inner)팬스(fans)(if)들을 구동하며 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc) 터빈(turbine)(t)을 형성하는 것과;
상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이에 상기 축(Axle)(a)의 인너(inner)팬스(fans)(if)들을 아웃터(outer)팬스(fans)(of)들과 연결된 팬스(fans)(f)들의 끝에는 원통형 팬스(fans)(f)링(ring)(fr)을 형성하고 일정한 간격의 블레이드(blades)(b)들을 설치하여 상기 덕트(duct)통관(db)의 블레이드(blades)(b)들의 공기인렛(Inlet)(i)에서 흡입된 후 상기 아웃터(outer)팬스(fans)(of)들과 연결된 상기 축(Axle)(a)을 구동하며 상기 인너(inner)실린더Cylinder(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)의 외부로부터 흡입된 공기는 상기 블레이드blades(b)들이 있는 상기 덕트(duct)통관(db)의 공기인렛(Inlet)(i)에서 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)로 들어가는 터빈turbine(t)을 형성하는 것과;
상기 아웃터(outer)팬스(fans)(of)들과 연결된 상기 아웃터(outer)팬스(fans)(of)들의 끝의 원통형 팬스(fans)(f)링(ring)(fr)에 형성된 일정한 간격의 블레이드(blades)(b)들을 연결하는 원통형 블레이드(blades)(b)링(ring)(br)을 형성하고 외주하는 상기 덕트(duct)통관(db)의 상기 인렛(Inlet)(ib)에는 증기, 물, 공기 등을 주입시키고 상기 아웃렛(Outlet)(ob)으로 배출하여 상기 덕트(duct)통관(d)의 공기인렛(Inlet)에서 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)로 들어가는 터빈(turbine)(t)과 다른 물성으로도 상기 축(Axle)(a)을 구동하게 형성하는 것을 특징으로 하는 상기 덕트(duct)통관(d)의 공기인렛(Inlet)에서 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)에 외주하는 블레이드(blades)(b)링(ring)(br)이 형성된 상기 덕트(duct)통관(db)이 있는 터빈(turbine)(t)에 대한 것이며 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc) 터빈(turbine)(t)을 줄여 4합 터빈을 나타냈다.Figure 1 is a three-dimensional view of X150, Y330, Z180 for the quadruple turbine.
2(a), (b), and (c) are explanatory views of the inner fans and supporters 909 in the inner cylinder.
3(a), (b), and (c) are explanatory views of the inner fans and supporters 909 and the outer cylinder and the outer fans and supporters in the inner cylinder.
Fig. 4 is an explanatory view in which the duct turbine is combined with Figs. 3 (a), (b) and (c).
FIG. 5 is a three-dimensional view of X150, Y330, and Z180 of FIG. 1 in which the quadruple turbine is reduced with respect to the inner fans and supporters 909 in the inner cylinder, and the outer cylinder and outer fans and supporters.
Code Explanation
inner Cylinder (ic), outer Cylinder (oc), Supporters(s), Axle (a), (hub)(h), inner fans(if), outer fans(of), Air circulation disk(U) , connecting spokes (k), cylindrical fans (f) ring (fr), blades (b), (duct) inlet (ib) of clearance (db), cylindrical blades) (b) ring (br), duct (duct) Clearance(db), Inlet(ib), Outlet(ob), 4th turbine(4t), turbine(t)
A triple turbine of air, water, etc. (on the air turbine shaft, 1. Inner cylinder of inner fans, 2. Outer cylinder of outer fans, 3. Both 1. Inner cylinders and 2. Between outer cylinders, duct fan to outer fans Turbine with external ducts with different properties added to field and duct turbines
(Patent Document 14) (Pressure Air) Turbo Engine 10-2005-0131732
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(Patent Document 16) (Pressure Air) Turbine 10-2005-0133691
(Patent Document 21) Pressure Air Turbine Engine 10-2007-0037258
(Patent Document 22) (Pressure Air) Turbo engine 10-2007-0037259
(Patent Document 29) Generator using air turbine engine, magnet engine (bearing) and compressed air launcher 10-2013-0049703
(Patent Document 30) Compressed Air Turbine 10-2013-0073137
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(Patent Document 38) System 10-2015-0031408 with a ship's steering mechanism, 'Air, Steam Turbine Engine', 'Water Tank & Boiler System', and 'Air, Water, Steam Propulsor'
(Patent Document 39) Backpack with kite, parachute and wings 10-2016-0071178
(Patent Document 40) Turbine combining an air turbine and a duct turbine 10-2016-0071179
(Patent Document 41) Aircraft with various devices and control devices for flying with air thrusters formed by a combination of various types of air turbines 10-2016-0090125
(Patent Document 42) A road that uses a combination of a scaffolding and an air furnace combined with 3 different air turbines installed in A prefabricated furnace to reduce damage to landslide areas, shafts and earthquakes, recycle heavy water, and solve snow and ice (road)
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(Patent Document 60) Equipment needed to reduce fine dust {Equipments needed to reduce of (ultra)fine dust} 10-2018-0039921
(Patent Document 61) Equipment required for fire suppression {The secure equipments needed to fire combat} 10-2018-0107032
(Patent Document 62) Generator installed on the wheel (rotor) and wheel cover (stator) of riding equipment such as quick board {The Generator of wheel(s) with Kickboard(etc)} 10-2020-0052213
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(Patent Document 66) Generator installed on a water board {The Generator with Aqua board} 10-2020-0054507
(Patent Document 67) Generator installed in health vehicle {The Generator with Health Vehicle} 10-2020-0055267
(Patent Document 0068) Generator installed on a boat {The Generator with Boat} 10-2020-0055932
(Patent Document 0069) Generator combining an air turbine structure generator and a wheel structure generator using a water wheel and an air compressor {Air Turbine type Generator connected Wheels type Generator used by Falling water & Air Compressor } 10-2020-0056031
(Patent Document 0070) Generator installed in air and water conditioner control device using Peltier element {The Generator installed in air and water conditioner control device using Peltier modules } 10-2020-0062927
(Patent Document 0071) "Air turbine structure generator" and "generator combining wheel structure" are applied to "generator using a heating element" A drone equipped with a bidirectional motor (bidirectional propeller) combined with a bidirectional air propulsor {Drone with generators that change the rotation direction of the propeller motor using the Peltier element as a power generation element} 10-2020-0073012
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(Patent Document 0073) Manufacturing technology of installing a motor-equipped aircraft air thruster and a drone equipped with a propeller on a motorcycle in which a rotor and a drip tray stator generator are installed on a motorcycle wheel that meets the rating of an electric motorcycle motor) {A power generation motorcycle in which a rotor and a stator generator in a drip tray are installed on a motorcycle wheel that meets the rating of the electric(Generator) motorcycle motor. Aircraft propulsor and drone propulsor are installed as options} 10-2020-0110057
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(Patent Document 0077) A device that collects fire smoke, volcanic fumes and ash installed in airbus electric (Generator) } 10-2021-0039765
(Patent Document 0078) Electric air car {The aircar electric (Generator) } 10-2021-0042049
(Patent Document 0079) Auxiliary wings and auxiliary door devices to rescue airbus electric (Generator) from strong winds and typhoons } 10-2021-0048062
(Patent Document 0080) An electric board with a large number of rotor wheels and a large number of stator wheel generators on a motorized shaft } 10-2021-0054360
(Patent Document 0081) The medical electric board {The medical electric board} 10-2021-0068477 as a reference to the literature related to the drive means, shaft and turbine
In the present invention
The task to drive the uniaxial turbine of the three-unit turbine due to other physical properties in the one-turbine three-turbine turbine: 1. Inner cylinders and 2. The outer cylinders are connected between both cylinders and the duct to the outer fan ring that connects the inner fans Fans and ducts and other 1. Inner cylinders and 2. Both cylinders are connected between the outer cylinders, and the duct fans and ducts (meaning and
4 1. Inner cylinders and 2. Outer fan ring of outer fan between outer cylinders, 3. In duct fan and duct fan ring, we want to find a means to drive the blade with other properties in the blade and the outer duct frame of the blade.
It will be described in detail with reference to the drawings.
Figure 1 is a three-dimensional view of X150, Y330, Z180 for the quadruple turbine.
A cylinder (c) is installed double as an inner and an outer, and the inner (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) are run and the (Cylinder) ) (c) the outer (fans) (if) and outer fans (fans) (if) installed on the turbine shaft (axle) (a) between the (if) ) Install duct fans (df) in the fan (fans) (if), cover the duct covering the duct fans (df), and form the duct fans (df) ring and installing blades (b) on the duct fans (df) ring and forming another cylinder (c3) covering the blades (b), the cylinder (Cylinder) ( It relates to a turbine (t) having an inlet (i) and an outlet (o) in c3).
2(a), (b), and (c) are explanatory views of the inner fans and supporters 909 in the inner cylinder.
The inner cylinder (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) are connected to the supporters (Supoters) (s), but
In front and behind the axis (Axle) (a) of the inner cylinder (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) installed by dividing the supporters (s) in a regular fashion Axle (a) forms a hub (h), and front and rear the hub (h) has an axle (Axle) (a) hub (h) front and rear the outer ( Outer) The Supporters(s) are divided and installed up to the Cylinder(oc) to be connected to the Axle(a)Hub and the Axle(a) is driven will be done
3(a), (b), and (c) are explanatory views of the inner fans and supporters 909 and the outer cylinder and the outer fans and supporters in the inner cylinder.
A plurality of inner cylinders (Cylinders) (ic) shorter than the length of the outer cylinder (Cylinder) (oc) are installed in the outer cylinder (Cylinder) (oc), and the supporters (Supoters) (s), but installing fans (f) on the axle (Axle) (a), and the inner cylinder (Cylinder) (ic) in the outer cylinder (Cylinder) (oc) ) in the shaft (Axle) (a), install inner fan fans (if), and the inner cylinder (Cylinder) (ic) and the inner cylinder (Cylinder) (ic) Between the shafts (Axle) (a) formed to be connected to the ends of the inner fan fans (if) the air flow in the opposite direction to the outer (outer) fan fans (of)
In the outer cylinder (Cylinder) (oc), in the inner cylinder (Cylinder) (ic), in the shaft (Axle) (a), the inner fan (if) and the inner ( Inner (Cylinder) (ic) and the inner (Cylinder) (ic) between the inner (Axle) (a) between the inner fan (if) and the outer (outer) Fans(of) are driven
An air circulating disk U is formed from the outer circumferential surface of the outer cylinder (oc) to the inner periphery of the inner cylinder (Cylinder), and the shaft (Axle) ( Install the connecting rib ( ) to the hub (h) of a), and from the outer cylinder (oc) to the inner fan fan (if) the air circulating disc ( U) is formed to return the wind from the outer cylinder (Cylinder) (oc) to the inner cylinder (Cylinder) (ic), and the inner cylinder (Cylinder) (ic) and the outer (outer) Cylinder (oc) is for turbine (turbine) (t).
Fig. 4 is an explanatory view in which the duct turbine is combined with Figs. 3 (a), (b) and (c).
Inner fans (if) and outer (if) of the shaft (Axle) (a) between the outer (Cylinder) (oc) and the outer (Cylinder) (oc) ) form the fans (of) to be connected, and the inner fan fans (if) and the outer fan fans (of) have the opposite wind direction and form the opposite angle of the fan fans (f), The inner fan fans (if) of the axle (a) are connected to the outer fan fans (of) and at the end of the fan fans (f) are cylindrical fans (f) ring (fr) Forming and installing blade blades (b) at regular intervals between the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc) to the outer circumference of the blade blades (b) Formed by welding to the duct pipe (d) or fixed to the contact surface with a fixture to form an inlet, the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc) ) between the inner fan fans (if) of the axis (Axle) (a) and the outer fan fans (of) and the ends of the fan fans (f) connected to the cylindrical fan fan (f) ring (ring) ) (r) is formed and the blade blades (b) are installed at regular intervals to be sucked in from the air inlet (i) of the blade blades (b) of the duct passage (db) and then the outer (outer) ) It drives the axis (Axle) (a) connected to the fans (of) and is added to the wind flow direction.
FIG. 5 is a three-dimensional view of X150, Y330, and Z180 of FIG. 1 in which the quadruple turbine is reduced with respect to the inner fans and supporters 909 in the inner cylinder, and the outer cylinder and outer fans and supporters.
Between the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc), the shaft (Axle) in a duct passing (d) around the blade blades (b) The inner fan fans (if) of (a) are formed in a cylindrical fan fan (f) ring (fr) at the end of the fan fans (f) connected to the outer fan fans (of) The outer cylinder (Cylinder) (oc1) forms a cylindrical blade blade (b) that connects the blade blades (b) at regular intervals and forms a ring (br) and a duct passage (db) on the outer periphery and the outer cylinder (Cylinder) (oc2) formed by welding with the connecting surface or fixed to the contact surface with a fixed body and forming an inlet (ib) and an outlet (ob) to form the duct ( duct) The shaft (Axle) (a) while outputting to the Outlet (ob) without entering the outer cylinder (oc) from the inlet (ib) of the clearance (db) by driving
Suctioned from behind the outer cylinder (Cylinder) (oc) and sucked in front of the inner cylinder (Cylinder) (ic) to the shaft (Axle) (a) an inner fan (fans) (if ) and the inner cylinder (Cylinder) (ic) and the inner cylinder (Cylinder) (ic) between the inner (fans) of the shaft (Axle) (a) ( if) and outer fans (of) are driven and the air circulating disk U from the outer cylinder (Cylinder) (oc) to the inner cylinder (Cylinder) (ic) ) by injecting back air to drive the inner fan (fans) (if) of the inner cylinder (Cylinder) (ic) of the shaft (Axle) (a) and the inner cylinder ( Cylinder (ic) and the outer cylinder (Cylinder) (oc) forming a turbine (turbine) (t);
Between the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc) the inner fan (fans) (if) of the shaft (Axle) (a) to the outer ( A cylindrical fan (f) is formed at the end of the fan (f) connected to the outer fan (fans) (of), and blades (b) at regular intervals are formed. The shaft ( Axle) (a) is driven and the air sucked from the outside of the inner cylinder (ic) and the outer cylinder (Cylinder) (oc) is the duct with the blades (b). ) to form a turbine (t) entering the inner cylinder (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) from the air inlet (i) of the clearance (db) with;
At regular intervals formed in the cylindrical fan (f) (f) ring (fr) of the ends of the outer (fans) (of) connected to the outer (fans) (f) (f) A cylindrical blade (b) connecting the blades (b) forms a ring (br) and the inlet (ib) of the duct passage (db) on the outer periphery has steam , water, air, etc. are injected and discharged to the outlet ob, and the inner cylinder (Cylinder) (ic) and the outer at the air inlet of the duct passage (d) The duct passage (d) characterized in that it is formed to drive the shaft (Axle) (a) even with a physical property different from the turbine (t) entering the (outer) cylinder (oc) The inner cylinder (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) in the air inlet of For a turbine (t) with the duct clearance (db) formed, the inner cylinder (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) turbine (turbine) )(t) was reduced to indicate a quadruple turbine.
..
Claims (1)
실린더(Cylinder)(c)를 인너(inner)와 아웃터(outer)로 이중으로 설치하고 상기 인너(inner)(Cylinder)(ic)와 아웃터(outer)실린더(Cylinder)(oc)들을 뛰우고 상기 (Cylinder)(c)들 사이에 터빈(turbine) 축(axle)(a)에 인너(inner)팬(fans)(if)들과 아웃터(outer)팬(fans)(if)들을 설치한 상기 아웃터(outer)팬(fans)(if)에 덕트 팬(duct fans)(df)들을 설치하고 상기 덕트 팬(duct fans)(df)들을 덮는 덕트를 쒸우며 상기 덕트 팬(duct fans)(df)들링을 형성하고 상기 덕트 팬(duct fans)(df)들링에 블레이드(blades)(b)들을 설치하고 상기 블레이드(blades)(b)들을 덮는 다른 실린더(Cylinder) (c3)를 형성하며 상기 실린더(Cylinder)(c3)에 흡입구(Inlet)(i)와 배출구(Outlet)(o)를 형성한 터빈(turbine) (t)에 대한 것으로
구성은
상기 인너(inner)실린더(Cylinder)(c)와 상기 아웃터(outer)실린더(Cylinder)(c)를 거치대(Supoters)(s)로 연결하되
상기 거치대(Supoters)(s)들을 정형되게 나누어 설치된 상기 인너(inner)실린더(Cylinder)(c)와 상기 아웃터(outer)실린더(Cylinder)(c)의 축(Axle)(a)의 앞과 뒤에는 축(Axle)(a)허브(hub)(h)를 형성하고 앞, 뒤 상기 허브(hub)(h)에는 축(Axle)(a)허브(hub)(h)에서 앞, 뒤 상기 아웃터(outer)실린더(Cylinder)(c)까지 상기 거치대(Supoters)(s)들을 정형되게 나누어 설치하여 축(Axle)(a)허브(hub)(h)에 연결되어 축(Axle)(a)이 구동하게 되는 것과;
2. 상기 아웃터(outer)실린더(Cylinder)(oc) 내에 상기 아웃터(outer)실린더(Cylinder)(oc)의 길이 보다 짧은 상기 인너(inner)실린더(Cylinder)(ic)들을 여러개 설치하고 상기 거치대(Supoters)(s)들로 연결하되 상기 축(Axle)(a)에는 팬스(fans)(f)들을 설치하며 상기 아웃터(outer)실린더(Cylinder)(oc) 내에 상기 인너(inner)실린더(Cylinder)(ic)들 내에 상기 축(Axle)(a)에는 인너(inner)팬스fans(if)들을 설치하고 상기 인너(inner)실린더(Cylinder)(ic)들과 상기 인너(inner)실린더(Cylinder)(ic)들 사이에는 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들 끝들에 반대방향의 공기흐름이 발생되는 아웃터(outer)팬스fans(of)들과 연결되게 형성하여
상기 아웃터(outer)실린더(Cylinder)(oc) 내에 상기 인너(inner)실린더(Cylinder)(ic)들 내에 상기 축(Axle)(a)에는 인너(inner)팬스fans(if)들과 상기 인너(inner)실린더(Cylinder)(ic)들과 상기 인너(inner)실린더(Cylinder)(ic)들 사이에는 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들과 아웃터(outer)팬스fans(of)들을 구동되며 상기 아웃터(outer)실린더(Cylinder)(oc)외주면에서 상기 인너(inner)실린더(Cylinder)(ic) 내주까지 공기회유원판(U) 형성하고 상기 공기회유원판(U)에서 상기 축(Axle)(a)의 허브(hub)(h)까지 연결살()을 설치하여 상기 아웃터(outer)실린더(Cylinder)(oc)에서 인너(inner)팬스fans(if) 앞 인렛(Inlet) 까지공기회유원판(U)을 형성하여 상기 아웃터(outer)실린더(Cylinder)(oc)에서 상기 인너(inner)실린더(Cylinder)(ic)으로 바람을 되돌려 인너(inner)실린더Cylinder(c)와 아웃터(outer)실린더Cylinder(oc) 터빈turbine(t)을 형성하는 것과;
3. 상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이에 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들과 아웃터(outer)팬스fans(of)들을 연결되게 형성하며 인너(inner)팬스fans(if)들과 아웃터(outer)팬스fans(of)들은 바람흐름 방향이 반대로 팬스fans(f)들의 각이 반대로 형성하며, 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들을 아웃터(outer)팬스fans(of)들과 연결된 팬스fans(f)들의 끝에는 원통형 팬스fans(f)링(ring)(r)을 형성하고 일정한 간격의 블레이드blades(b)들을 설치하여 상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이는 상기 블레이드blades(b)들을 외주하는 덕트(duct)통관(d)에 용접하여 형성하는 것 내지 접면에 고정체로 고정하고 인렛을 형성하며, 상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이에 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들을 아웃터(outer)팬스fans(of)들과 연결된 팬스fans(f)들의 끝에는 원통형 팬스fans(f)링(ring)(fr)을 형성하고 일정한 간격의 블레이드blades(b)들을 설치하여 상기 덕트(duct)통관(d)의 블레이드blades(b)들의 공기인렛(Inlet)(i)에서 흡입된 후 상기 아웃터(outer)팬스fans(of)들과 연결된 상기 축(Axle)(a)을 구동하며 바람흐름방향에 더하여 지는 것과;
4. 상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이는 상기 블레이드blades(b)들을 외주하는 덕트(duct)통관(d)에 상기 축(Axle)(a)의 인너(inner)팬스fans(if)들을 상기 아웃터(outer)팬스fans(of)들과 연결된 팬스fans(f)들의 끝의 원통형 팬스fans(f)링(ring)(fr)에 형성된 일정한 간격의 블레이드blades(b)들을 연결하는 원통형 블레이드blades(b)링(ring)(br)을 형성하고 외주하는 덕트(duct)통관(db)을 상기 아웃터(outer)실린더(Cylinder)(oc1)와 상기 아웃터(outer)실린더(Cylinder)(oc2)들의 연결면과 용접하여 형성하는 것 내지 접면에 고정체로 고정하고 인렛(Inlet)(ib)과 아웃렛(Outlet)(ob)을 형성하여 상기 덕트(duct)통관(db)의 인렛(Inlet)(ib)에서 상기 아웃터(outer)실린더(Cylinder)(oc)로 들어가지 않고 상기 아웃렛(Outlet)(ob)으로 출력되면서도 상기 축(Axle)(a)을 구동하는 것으로
상기 아웃터(outer)실린더(Cylinder)(oc) 뒤에서 흡입되고 상기 인너(inner)실린더(Cylinder)(ic)들 앞에서 흡입되어 상기 축(Axle)(a)에는 인너(inner)팬스(fans)(if)들과 상기 인너(inner)실린더(Cylinder)(ic)들과 상기 인너(inner)실린더(Cylinder)(ic)들 사이에는 상기 축(Axle)(a)의 인너(inner)팬스(fans)(if)들과 아웃터(outer)팬스(fans)(of)들을 구동되며 상기 아웃터(outer)실린더(Cylinder)(oc)에서 상기 인너(inner)실린더(Cylinder)(ic)로 상기 공기회유원판(U)공기를 되돌려 주입하여 상기 축(Axle)(a)의 상기 인너(inner)실린더(Cylinder)(ic)의 상기 인너(inner)팬스(fans)(if)들을 구동하며 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc) 터빈(turbine)(t)을 형성하는 것과;
상기 아웃터(outer)실린더(Cylinder)(oc)와 상기 아웃터(outer)실린더(Cylinder)(oc) 사이에 상기 축(Axle)(a)의 인너(inner)팬스(fans)(if)들을 아웃터(outer)팬스(fans)(of)들과 연결된 팬스(fans)(f)들의 끝에는 원통형 팬스(fans)(f)링(ring)(r)을 형성하고 일정한 간격의 블레이드(blades)(b)들을 설치하여 상기 덕트(duct)통관(d)의 블레이드(blades)(b)들의 공기인렛(Inlet)(i)에서 흡입된 후 상기 아웃터(outer)팬스(fans)(of)들과 연결된 상기 축(Axle)(a)을 구동하며 상기 인너(inner)실린더Cylinder(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)의 외부로부터 흡입된 공기는 상기 블레이드blades(b)들이 있는 상기 덕트(duct)통관(d)의 공기인렛(Inlet)에서 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)로 들어가는 터빈turbine(t)을 형성하는 것과;
상기 아웃터(outer)팬스(fans)(of)들과 연결된 상기 아웃터(outer)팬스(fans)(f)들의 끝의 원통형 팬스(fans)(f)링(ring)(fr)에 형성된 일정한 간격의 블레이드(blades)(b)들을 연결하는 원통형 블레이드(blades)(b)링(ring)(br)을 형성하고 외주하는 상기 덕트(duct)통관(db)의 상기 인렛(Inlet)(i)에는 증기, 물, 공기 등을 주입시키고 상기 아웃렛(Outlet)(o)으로 배출하여 상기 덕트(duct)통관(db)의 공기인렛(Inlet)에서 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)로 들어가는 터빈(turbine)(t)과 다른 물성으로도 상기 축(Axle)(a)을 구동하게 형성하는 것을 특징으로 하는 상기 덕트(duct)통관(db)의 공기인렛(Inlet)(i)에서 상기 인너(inner)실린더(Cylinder)(ic)와 상기 아웃터(outer)실린더(Cylinder)(oc)에 외주하는 블레이드(blades)(b)링(ring)(br)이 형성된 상기 덕트(duct)통관(db)이 있는 터빈(turbine)(t)을 특징으로 하는 대한 것이다.the present invention
A cylinder (c) is installed double as an inner and an outer, and the inner (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) are run and the (Cylinder) ) (c) the outer (fans) (if) and outer fans (fans) (if) installed on the turbine shaft (axle) (a) between the (if) ) Install duct fans (df) in the fan (fans) (if), cover the duct covering the duct fans (df), and form the duct fans (df) ring and installing blades (b) on the duct fans (df) ring and forming another cylinder (c3) covering the blades (b), the cylinder (Cylinder) ( It is for a turbine (t) having an inlet (i) and an outlet (o) in c3).
configuration is
Connect the inner cylinder (Cylinder) (c) and the outer cylinder (Cylinder) (c) with the supporters (s), but
In front and behind the axle (Axle) (a) of the inner cylinder (C) and the outer cylinder (Cylinder) (c) installed by dividing the supporters (s) in a regular fashion Axle (a) forms a hub (h), and front and rear the hub (h) has an axle (Axle) (a) hub (h) front and rear the outer ( Outer) The Supporters(s) are divided and installed up to the Cylinder(c) to be connected to the Axle(a)Hub and the Axle(a) is driven to be done;
2. A plurality of inner cylinders (Cylinder) (ic) shorter than the length of the outer cylinder (Cylinder) (oc) are installed in the outer cylinder (Cylinder) (oc), and the holder ( Supoters) (s), but installing fans (f) on the axle (Axle) (a), the inner cylinder (Cylinder) in the outer cylinder (Cylinder) (oc) In the (ic), the shaft (Axle) (a) is installed with inner fan fans (if), and the inner cylinder (Cylinder) (ic) and the inner cylinder (Cylinder) ( ic) between the axes (Axle) (a) to be connected to the ends of the inner fan fans (if) to be connected to the outer fan fans (of) in which the air flow in the opposite direction is generated.
In the outer cylinder (Cylinder) (oc), in the inner cylinder (Cylinder) (ic), in the shaft (Axle) (a), the inner fan (if) and the inner ( Inner (Cylinder) (ic) and the inner (Cylinder) (ic) between the inner (Axle) (a) between the inner fan (if) and the outer (outer) Fans (of) are driven, and an air circulating disk (U) is formed from the outer peripheral surface of the outer cylinder (Cylinder) (oc) to the inner periphery of the inner cylinder (Cylinder) (ic), and the air circulating disk (U) is formed. ) from the outer cylinder (oc) to the hub (h) of the axle (a) to the inlet in front of the inner fan fan (if) Form an air circulating disk (U) up to (Inlet) and return the wind from the outer cylinder (Cylinder) (oc) to the inner cylinder (Cylinder) (ic) to return the inner cylinder (c) ) and an outer cylinder (oc) to form a turbine (t);
3. Between the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc) the inner fan (if) of the shaft (Axle) (a) and the outer The (outer) fans (of) are formed to be connected, and the inner (inner) fans (if) and the outer (outer) fans (of) have the opposite wind direction and the opposite angle of the fan fans (f) are formed. , At the end of the inner fan fans (if) of the axis (Axle) (a) and the outer fan fans (of) and the fan fans (f) connected to the cylindrical fan fan (f) ring (ring) ( r) and installing the blade blades (b) at regular intervals between the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc) the blade blades (b) Formed by welding to the circumferential duct passage (d) or fixed to the contact surface with a fixed body to form an inlet, the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc) between the inner fan fans (if) of the shaft (Axle) (a) and the outer fan fans (of) and the ends of the fan fans (f) connected to the cylindrical fan fan (f) ring (ring) (fr) is formed and blade blades (b) are installed at regular intervals to be sucked in from the air inlet (i) of the blade blades (b) of the duct passage (d), and then the outer (outer) driving the axis (Axle) (a) connected to the fans (of) and adding to the wind flow direction;
4. Between the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc), the shaft ( Axle) (a) of the inner fan fans (if) connected to the outer fan fans (of) and the cylindrical fan fan (f) of the end of the fan fan (f) ring (fr) A cylindrical blade blade (b) connecting the blade blades (b) at regular intervals formed in the outer cylinder (Cylinder) ( oc1) and the outer cylinder (Cylinder) (oc2) formed by welding with the connecting surface or fixed to the contact surface with a fixed body and forming an Inlet (ib) and an Outlet (ob) to form the In the inlet (ib) of the duct clearance (db), the shaft (Axle) ( by driving a)
Suctioned from behind the outer cylinder (Cylinder) (oc) and sucked in front of the inner cylinder (Cylinder) (ic) to the shaft (Axle) (a) an inner fan (fans) (if ) and the inner cylinder (Cylinder) (ic) and the inner cylinder (Cylinder) (ic) between the inner (fans) of the shaft (Axle) (a) ( if) and outer fans (of) are driven and the air circulating disk U from the outer cylinder (Cylinder) (oc) to the inner cylinder (Cylinder) (ic) ) by injecting back air to drive the inner fan (fans) (if) of the inner cylinder (Cylinder) (ic) of the shaft (Axle) (a) and the inner cylinder ( Cylinder (ic) and the outer cylinder (Cylinder) (oc) forming a turbine (turbine) (t);
Between the outer cylinder (Cylinder) (oc) and the outer cylinder (Cylinder) (oc) the inner fan (fans) (if) of the shaft (Axle) (a) to the outer ( A cylindrical fan (f) is formed at the end of the fan (f) connected to the outer fan (fans) (of), and blades (b) at regular intervals are formed. After being installed and sucked from the air inlet (i) of the blades (b) of the duct passage (d), the shaft ( Axle) (a) is driven and the air sucked from the outside of the inner cylinder (ic) and the outer cylinder (Cylinder) (oc) is the duct with the blades (b). ) forming a turbine (t) entering the inner cylinder (Cylinder) (ic) and the outer cylinder (Cylinder) (oc) at the air inlet (Inlet) of the clearance (d);
At regular intervals formed in the cylindrical fan (f) ring (fr) of the ends of the outer (fans) (f) connected to the outer (fans) (fans) (of) A cylindrical blade (b) connecting the blades (b) forms a ring (br), and the inlet (i) of the duct passage (db) on the outer periphery has steam , water, air, etc. are injected and discharged to the outlet (o), and the inner cylinder (Cylinder) (ic) and the outer at the air inlet of the duct passage (db) The duct passage (db) characterized in that it is formed to drive the shaft (Axle) (a) even with a physical property different from the turbine (t) entering the (outer) cylinder (oc) In the air inlet (i) of the blade (blades) (b) ring (ring) ( br) is for characterized in that the turbine (turbine) (t) with the duct (duct) passage (db) is formed.
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| KR1020220024604A KR20220038026A (en) | 2022-02-24 | 2022-02-24 | 4 connected fans on an axle turbine : 1. The inner fans on the axle in inner cylinder, 2. The outer fans on the axle in outer cylinder &3. The duct fans on the outer fans inside in 2 outer cylinders and 2 inner cylinders, 4. The blades on the duct fans ring in the duct with an inlet and an oulet with another Cylinder |
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| KR1020220024604A KR20220038026A (en) | 2022-02-24 | 2022-02-24 | 4 connected fans on an axle turbine : 1. The inner fans on the axle in inner cylinder, 2. The outer fans on the axle in outer cylinder &3. The duct fans on the outer fans inside in 2 outer cylinders and 2 inner cylinders, 4. The blades on the duct fans ring in the duct with an inlet and an oulet with another Cylinder |
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2022
- 2022-02-24 KR KR1020220024604A patent/KR20220038026A/en not_active Application Discontinuation
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| "공기 터빈구조 발전기"와 "바퀴구조를 합한 발전기"를 "발열소자를 이용한 발전기"와 적용 양방향 모터(양방향 프로펠러)를 양방향공기추진기(Propulsor)와 결합 장착한 드론 {Drone with generators that change the rotation direction of the propeller motor using the Peltier element as a power generation element} 10-2020-0073012 |
| "압축공기 pumping장치" 들과 "압축 Air발사기" 들과 "같은 극면의 반발력을 이용한 자석엔진", 전기열선을 내장한 "압축공기터빈" 을 이용한 "발전기"와 "태엽 spring case" 들을 Starter로 이용하며, "전기 열선을 내장한 Steam 탱크와 Steam 터빈" 을 응용한 water condition과 air condition과 Steam 기관의 복합장치 10-2015-0002033 |
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| 기계 회전축에 설치되어 회전축이 회전할 때 상기 기계회전축에 설치되는 Air Pumper와 Air Tank로 하는 Compressor로 압축 공기발사기 Cylinder들 내부에 Spring 을 압축하는 것과 같은 극의 전자자석과 영구자석으로 하는 압축공기생성장치가 내장된 압축공기발사기 10-2015-0021433 |
| 기계 회전축에 설치하여 공기 Tank들에 내장된 Floor Board들을 연동 반복운동을 시키는 Air Pumper와 공기 Ring Tube와 압축공기가 필요한 곳에 연결하는 Pipe의 복합장치 10-2014-0113976 |
| 날개를 단 배낭과 변형하는 외부 Body(문, 지붕)프레임과 Body(문, 지붕)와 날개를 더 단 비행기구 10-2017-0133894 |
| 모터가 장착된 회전축에 다량의 회전자바퀴와 다량의 고정자바퀴 발전기를 설치한 전동보드 {An electric board with a large number of rotor wheels and a large number of stator wheel generators on a motorized shaft} 10-2021-0054360 |
| 미세먼지를 줄이기 위해 필요한 장비들 {Equipments needed to reduce of (ultra)fine dust} 10-2018-0039921 |
| 발판보드에 설치하는 발전기 {The Generator of wheel(s) with Footboard} 10-2020-0053218 |
| 보트에 설치하는 발전기 {The Generator with Boat} 10-2020-0055932 |
| 산사태에 대비, 대응하는 에어 레이어들 블록들이 형성된 거대장비들(에어 레이어들 블록들){Large equipment made of air layers blocks to prepare for and respond to landslides(earth slide, mudslide)} 10-2021-0023260 |
| 선박의 조향기구, 'Air, Steam Turbine Engine'과 'Water Tank & Boiler System', 'Air, Water, Steam Propulsor'를 가지는 System 10-2015-0031408 |
| 수상 재난 대응 구조선과 장비들 {The secure ships & equipments of the Aqua accident} 10-2018-0034283 |
| 수상보드에 설치하는 발전기 {The Generator with Aqua board} 10-2020-0054507 |
| 수차와 공기 컴프레서를 이용한 공기 터빈구조 발전기와 바퀴구조 발전기를 합한 발전기 {Air Turbine type Generator connected Wheels type Generator used by Falling water & Air Compressor } 10-2020-0056031 |
| 역방향 모터(양방향 프로펠러)의 추진에 맞는 관성을 이기는 팬이 없는 양방향 공기 추진기(Propullor)를 장착한 드론{The Drone equipped with the Fanless bidirectional the Jet engine(other than the Propullor) that overcome the inertia suitable for the propulsion of a bidirectional Motor (bidirectional propeller) - similar to a slow Scram jet 2type & with a directional Motor similar to a slow Scram jet 1 type } 10-2020-0080402 |
| 의료용 전동보드 {The medical electric board}10-2021-0068477에 적용한 구동수단과 샤프트와 터빈과 관련된 문헌을 인용한 것으로 |
| 자가연속공기펌핑분출장치(I), 태엽(V), 회전연속격발공기발사기 (II), 에어 콘푸레서(III), 에어콘푸레서(IV), 자석엔진(VI)과 더불어 배터리(VII), 조절판(VIII)과 열선(IX)을 가지는 시스템 10-2005-0131733 |
| 자전거바퀴(회전자)와 바퀴덮개(고정자)에 설치하는 발전기 {The Generator of wheel(s) with Bicycle} 10-2020-0052638 |
| 자전거와 리어캐리어에 설치하는 발전기 {The Generator of wheel(s) with Bicycle and Rear Carrie} 10-2020-0053666 |
| 전기에어버스를 강풍, 태풍에 구조하는 보조날개와 보조출입문 장치 {Auxiliary wings and auxiliary door devices to rescue airbus electric(Generator) from strong winds and typhoons } 10-2021-0048062 |
| 전기에어카 {The aircar electric(Generator) } 10-2021-0042049 |
| 전동 오토바이 모터의 정격에 맞는 오토바이바퀴에 회전자와 물받이 고정자 발전기를 설치한 오토바이에 모터가 장착된 항공기 공기추진기와 장착한 드론의 프로펠러(Propullor)를 장착하는 제조기술) {A power generation motorcycle in which a rotor and a stator generator in a drip tray are installed on a motorcycle wheel that meets the rating of the electric(Generator) motorcycle motor. Aircraft propullor and drone propulsor are installed as options} 10-2020-0110057 |
| 전동 오토바이에 설치한 모터가 장착된 항공기 공기추진기와 장착한 프로퓰러(Propullor)로 구성한 오토에어크라프트(Autoaircraft) {The auto aircraft propullor and drone propulsor are installed as options electric(Generator) motorcycle motor} 10-2021-0011018 |
| 전동에어버스 {The airbus electric(Generator)} 10-2021-0037914 |
| 전동에어버스에 설치하는 연기(분연), 재 포집장치 {A device that collects fire smoke, volcanic fumes and ash installed in airbus electric(Generator) } 10-2021-0039765 |
| 퀵보드 등 승용기구바퀴(회전자)와 바퀴덮개(고정자)에 설치하는 발전기 {The Generator of wheel(s) with Kickboard(etc)} 10-2020-0052213 |
| 탄성을 가진 공기주머니들을 연동상반운동으로 회전수단과 자가 공기펌핑 분출(에어 Compressure)수단으로 전환하는 장치 10-2005-0117342 |
| 펠티어소자를 이용한 공기, 물 컨디션너 조절장치 내에 설치한 발전기 {The Generator installed in air and water conditioner control device using Peltier modules } 10-2020-0062927 |
| 헬스보트 {The health boat} 10-2018-0031520 |
| 헬스차량에 설치하는 발전기 {The Generator with Health Vehicle} 10-2020-0055267 |
| 화재진압에 필요한 장비들{The secure equipments needed to fire combat} 10-2018-0107032 |
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