KR950033007A - Turbocomb Pound Cylindrical Cylinder Engine - Google Patents

Turbocomb Pound Cylindrical Cylinder Engine Download PDF

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Publication number
KR950033007A
KR950033007A KR1019940010213A KR19940010213A KR950033007A KR 950033007 A KR950033007 A KR 950033007A KR 1019940010213 A KR1019940010213 A KR 1019940010213A KR 19940010213 A KR19940010213 A KR 19940010213A KR 950033007 A KR950033007 A KR 950033007A
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KR
South Korea
Prior art keywords
gas turbine
annular cylinder
cylinder
shaft
fixed
Prior art date
Application number
KR1019940010213A
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Korean (ko)
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KR100305426B1 (en
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변상복
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변상복
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Priority to KR1019940010213A priority Critical patent/KR100305426B1/en
Publication of KR950033007A publication Critical patent/KR950033007A/en
Application granted granted Critical
Publication of KR100305426B1 publication Critical patent/KR100305426B1/en

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02—Engines with prolonged expansion
    • F02B41/10—Engines with prolonged expansion in exhaust turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/04—Charge admission or combustion-gas discharge
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/12—Ignition

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

본 발명은 환상의 실린더(ANNULAR CYLINDER)(또는 RING CYLINDER)내에 수용한 호형피스톤(ARCPISTON)을 써서 압축한 공기내에 경유 등 비교적 저질유를 분사하여 연소팽창케 하는 2사이클 “디이젤 엔진”의 체적형 “압력에너지 사이클”과 환상실린더 중심의 큰 중공부에 “콤팩트”하게 수장한 통상의 “래디얼가스터어빈”의 “속도에너지 사이클”을 합성한 것으로 전체열효율 및 출력에 대폭 향상되어서 연료비를 크게 낮추고, 배기가스도 깨끗하게 한 경량의 호형피스톤 엔진과 가스터어빈의 “하이브리도(HYBRED) 시스템(SYSTEM)”이다.The present invention is a volumetric type of a two-cycle “diesel engine” that uses a arc piston housed in an annular cylinder (or ring cylinder) to inject and expand a relatively low quality oil such as light oil in the compressed air. Combining the “pressure energy cycle” and the “speed energy cycle” of the conventional “radial gas turbine”, which is compactly packed in a large hollow in the center of the annular cylinder, greatly improving the overall thermal efficiency and output and significantly reducing fuel costs. It is a lightweight arc piston engine that also cleans the exhaust gas and the gas turbine "HYBRED" system (SYSTEM).

종래의 “피스톤엔진”(PISTON ENGINE)은 부피, 무게가 큰데다 고속성이 결여되고 종래의 “가스터어빈”(GAS TURBINE)은 열효율이 낮고 부피, 무게의 대형화가 불가피하여 발전기 또는 대형선박등에 흔히 쓰이고 있을 뿐 자동차, 오토바이, 소선박, 농기구 등 비교적 소마력용은 실용화되지 못하고 있는 현실이다.Conventional "piston engine" (PISTON ENGINE) is large in volume and weight and lacks high speed, and conventional "GAS TURBINE" is low in thermal efficiency and inevitably increases in volume and weight. It is being used but relatively small horsepower such as automobiles, motorcycles, small ships, farm equipment, etc. is not practical.

본 발명은 소경체(小輕체)로서 전체열효율을 70%정도로 높이고, CO,HC등 유해물질 및 소음도, 대폭감고케한 것으로서 특히 “연소가스”의 기밀, 윤활, 냉각성을 확보하였기 때문에 내구성, 안전성이 높고, 정미마력당 중량 및 구조가 간단하여 연료 및 “엔진”원가가 크게 절감되는 잇점이 있다.The present invention is a small-sized body to increase the overall thermal efficiency to about 70%, and significantly reduced the harmful substances and noise, such as CO, HC, and especially, because it ensures the airtightness, lubrication, and cooling of the "combustion gas" durability, The high safety, simple weight and structure per net horsepower have the potential to significantly reduce fuel and “engine” costs.

Description

터어보컴 파운드 환상 실린더 엔진Turbocomb Pound Cylindrical Cylinder Engine

본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음Since this is an open matter, no full text was included.

제1도는 본 발명의 평면도, 제2도는 제1도의 A-A선 단면도.1 is a plan view of the present invention, Figure 2 is a cross-sectional view taken along the line A-A of FIG.

Claims (1)

분할형으로 조합케 된 환상 실린더(ANNULAR CYLINDER)(또는 RING CYLTNDER)(1) 내 상방에 소기공(掃氣孔)(2)의 “밸브”(2′)가 장착된 격벽(3)을 고정하고, 이 격벽(3)의 좌우측에 가스연소실(4)과 공기압축실(5)이 구분형성토록 긴 윤활유통로(6)와 윤활유 회수공(6′)가 친설된 호형피스톤(ARC PISTON)(7)을 수용하고 호형피스톤(7)의 중간 측방에 고식되어 환상실린더(1)측벽의 긴 안내공(8)외로 돌출케 한 “핀”(9)은 환상실린더(1) 우측의 부랙키트(BRACKET)를 관통한 축(10) 일단에 고정된 “플라이휘일(11)주변의 “핀”(12)에는 커넥팅로드(13) 양단을 연결하고 축(10)의 타단에는 주동(主動) “휠”(14)을 고정한다. 그리고 환상실린더(1) 중심의 큰 중공부에는 통상의 “래디얼가스터어빈”(15)을 수용하여 실린더(1)의 플랜지(1′)볼트에 고정하고 환상실린더(1)내 호형피스톤(7)의 하사점에는 “가스터어빈”(15)에 연통토록 배기관(16)을 연결하고 “가스터어빈”(15)축(17)말단에 고정된 출력치차(18)의 “클러치”(19)에는 스프링(20)의 탄력을 받으면서 공전하는 종동(從動) 휠(21)의 통상적인 오우버러닝 클러치(22)가 착탈토록 물리고 가스연소실(4)에는 연료분사펌프(23)와 점화프러그(24)을 장착하고 공기 압축실(5) 내벽에는 공기 흡입밸브(25)를 장착함을 특징으로 하는 열효율 높은 하이브리드 가스터어빈 엔진.Fix the bulkhead (3) equipped with the "valve" (2 ') of the micropore (2) above the divided cylinder (ANNULAR CYLINDER) (or RING CYLTNDER) (1) The arc piston (ARC PISTON) having a long lubrication oil passage 6 and a lubricating oil return hole 6 'so as to form a gas combustion chamber 4 and an air compression chamber 5 on the left and right sides of the partition 3 is formed. ) And the pin (9) protruded out of the long guide hole (8) on the side wall of the annular cylinder (1) and is fixed on the middle side of the arc piston (7) is a rack kit on the right side of the annular cylinder (1). Connect the both ends of the connecting rod 13 to the “pin” (12) around the “fly wheel” (11) fixed at one end of the shaft (10) that has passed through the shaft (10) and the main wheel (wheel) at the other end of the shaft (10). Secure (14). In the large hollow portion in the center of the annular cylinder (1), a conventional "radial gas turbine" (15) is accommodated and fixed to the flange (1 ') bolt of the cylinder (1) and the arc shaped piston (7) in the annular cylinder (1). Connect the exhaust pipe 16 to the “gas turbine” (15) at the bottom dead center of the spring and the “clutch” (19) of the output gear 18 fixed to the end of the “gas turbine” (15) shaft (17). The conventional overrunning clutch 22 of the driven wheel 21 revolving while receiving the elasticity of 20 is detached and the fuel injection pump 23 and the ignition plug 24 are inserted into the gas combustion chamber 4. And a heat-efficient hybrid gas turbine engine, characterized in that the air inlet chamber (5) mounted on the inner wall of the air intake valve (25). ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
KR1019940010213A 1994-05-10 1994-05-10 Engine with turbo-compound annular cylinder KR100305426B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1019940010213A KR100305426B1 (en) 1994-05-10 1994-05-10 Engine with turbo-compound annular cylinder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019940010213A KR100305426B1 (en) 1994-05-10 1994-05-10 Engine with turbo-compound annular cylinder

Publications (2)

Publication Number Publication Date
KR950033007A true KR950033007A (en) 1995-12-22
KR100305426B1 KR100305426B1 (en) 2001-11-30

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Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019940010213A KR100305426B1 (en) 1994-05-10 1994-05-10 Engine with turbo-compound annular cylinder

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20010074188A (en) * 2001-04-06 2001-08-04 김동현 Turbine Engine generating power by gas explosion

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101155434B1 (en) 2009-10-05 2012-06-18 변상복 super power piston engine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3938480A (en) * 1974-02-04 1976-02-17 Yanda Leon M Internal combustion engine
JPS5460605A (en) * 1977-10-24 1979-05-16 Tadashi Iwata Twoocycle engine
JPS56138401A (en) * 1980-03-28 1981-10-29 Masanosuke Nakahira Reciprocating half rotation compact engine
JPS57101128A (en) * 1980-12-16 1982-06-23 Caterpillar Mitsubishi Ltd Sliding joint
KR910008909B1 (en) * 1984-07-18 1991-10-24 변상복 Rotary engine
KR890002703B1 (en) * 1986-05-15 1989-07-24 박영근 Internal combustion engine
US5555730A (en) * 1994-10-24 1996-09-17 Haeco Partners, Ltd. Cooling for gas turbine-two stroke piston compound engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20010074188A (en) * 2001-04-06 2001-08-04 김동현 Turbine Engine generating power by gas explosion

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