KR950000601B1 - Rotary engine - Google Patents

Rotary engine Download PDF

Info

Publication number
KR950000601B1
KR950000601B1 KR1019920016055A KR920016055A KR950000601B1 KR 950000601 B1 KR950000601 B1 KR 950000601B1 KR 1019920016055 A KR1019920016055 A KR 1019920016055A KR 920016055 A KR920016055 A KR 920016055A KR 950000601 B1 KR950000601 B1 KR 950000601B1
Authority
KR
South Korea
Prior art keywords
rotor
shaft
rotary engine
compression
block
Prior art date
Application number
KR1019920016055A
Other languages
Korean (ko)
Other versions
KR940007346A (en
Inventor
전병수
Original Assignee
전병수
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 전병수 filed Critical 전병수
Priority to KR1019920016055A priority Critical patent/KR950000601B1/en
Publication of KR940007346A publication Critical patent/KR940007346A/en
Application granted granted Critical
Publication of KR950000601B1 publication Critical patent/KR950000601B1/en

Links

Classifications

    • 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
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Abstract

The rotor of a rotary engine transfers the power to the shaft through the powerful torque because the angle between the direction of exposure and the shaft is 90≰. And the rotary engine has a simple structure to make the manufacture of the rotary engine easy. This engine comprises a suction, exhaust valve block (17) in a casting block (15); a compression cap (5) having a compression room (19); a rotational body (20) with a rotor (14); a bellside block (9) to engage with gears (4,3,2,1).

Description

로터리 엔진(Rotary engine)Rotary engine

제 1 도는 본 발명의 주요구성부분중 일부를 분해한 분해사시도.1 is an exploded perspective view in which some of the major components of the present invention are disassembled.

제 2 도는 본 발명의 요부 압축캠 사시도.2 is a perspective view of the main compression cam of the present invention.

제 3 도는 원동축의 로터를 형성하기 위한 압축캡사이의 각 속도 기어의 동작도.3 shows the operation of each speed gear between compression caps to form a rotor of a coaxial shaft.

제 4 도는 제 1, 2, 3, 4 도는 압축캡과 로터의 동작을 4행정으로 표현한 행정도.4 is a first, second, third, and fourth degree strokes representing the operation of the compression cap and the rotor in four strokes.

* 도면의 주요부분에 대한 부호의 설명* Explanation of symbols for main parts of the drawings

1 : 피동축 기어(사이클로이드 차측기어)1: driven shaft gear (cycloidal side gear)

2, 3 : 원동축과 사이클로이드 차측기어의 유동기어2, 3: Flow gears of the primary shaft and cycloidal side gear

4 : 원동축기어 5 : 압축캡4: Original shaft gear 5: Compression cap

6 : 원동축 7 : 흡기밸브6: driven shaft 7: intake valve

8 : 배기밸브 9 : 벨사이드 블록(block)8: exhaust valve 9: bellside block

10 : 원동축공 11 : 압축캡축공10: circular shaft hole 11: compression cap shaft hole

12 : 배기밸브축공 13 : 흡기밸브축공12: exhaust valve shaft hole 13: intake valve shaft hole

14 : 로터(roter) 15 : 케이싱 블록14: rotor 15: casing block

16 : 실린더 내경 17 : 흡, 배기밸브 블록16: cylinder bore 17: intake and exhaust valve block

본 발명은 로터의 회전운동이 직접 원동축으로 동력 전달되어지는 로터리 엔진(Rotary engine)에 관한 것이다. 로터리 엔진에 대하여서는 이미 세계적으로 널리 알려져 있으며, 기관의 종류도 다양하며 또한 기관에 관한 새로운 분야로 관심의 대상이 되어지고 있다.The present invention relates to a rotary engine in which the rotational motion of the rotor is directly transmitted to the driving shaft. Rotary engines are already well known around the world, and there are many different types of engines and are attracting attention as a new field of engines.

본 발명 또한 상기한 로터리 엔진의 한 기관에 관한 것으로서 지금까지 로터리 엔진에서의 흡배기상의 구조적 방법을 탈피하고, 로터가 원동축에 간접적 연결없이 원동축에 동력을 전달하며, 로터가 폭발시킨 내압의 각이 연동축과 90도가 되어 큰 토오크로서 로터에서 축으로 동력이 전달되어져 큰 힘을 얻을 수 있게 함과, 또한 구조가 간단하도록 함으로 그로인한 제작과 압축이 용이하게 하기 위하여 보다 진보발전된 발명인 것이다.The present invention also relates to an engine of the rotary engine as described above, and thus far from the structural method on the intake and exhaust of the rotary engine, the rotor transmits power to the prime shaft without indirect connection to the prime shaft, and the angle of internal pressure of the rotor exploded. It is a more advanced invention in order to be able to obtain a large force by transferring power from the rotor to the shaft as a large torque at 90 degrees with the interlocking shaft, and also to simplify the structure and thereby make the compression easier.

본 발명의 구조적 특징은 본 발명인의 선출원 발명에서의 실린더내에 두 개의 로터가 있어 릴레이식(바톤식)기관운동을 하게 되어 있으며, 두 로터의 유도장치로 별도의 크랭크로 유지되어져 원동축에 동력 전달이 되어지지만 본 발명은 실린더내에는 하나로 회전체와 일체로 구성된 로터가 존재하며, 동심형의 진원을 실린더로 로터가 원운동하게 된다.The structural feature of the present invention is that the two rotors in the cylinder in the present invention of the inventors of the present invention is to perform a relay (baton type) engine movement, is maintained in a separate crank by the induction device of the two rotors to transmit power to the drive shaft In the present invention, but the rotor is formed in one cylinder and integrally with the rotating body, the rotor is circular motion to the concentric circles of the cylinder.

이때 제 1 도에서의 각속도 유동장치의 기어가 압축캡(5)을 로터(14)의 표면을 감싸면서 로터가 압축캡(5)내를 압축함으로써 압축캡은 제 3 도에서와 같이 압축캡(5)의 "C"형 압축공간으로 로터(14)가 슬라이드되면서 가스를 압축 폭발시키게 되는 것이다.In this case, the gear of the angular velocity flow apparatus in FIG. 1 surrounds the surface of the rotor 14 and the rotor compresses the inside of the compression cap 5 so that the compression cap is compressed as shown in FIG. Compressing and exploding gas while the rotor 14 slides into the “C” type compression space of 5).

이하, 이를 첨부도면에 의해 보다 상세히 설명한다.Hereinafter, this will be described in more detail with reference to the accompanying drawings.

제 1 도는 본 발명의 분해사시도로서 케이싱블록(15)에 흡기 및 배기 밸브블록(17)이 형성되고, 이에 각 밸브(7)(8)가 유착되며, 실린더 내경(16)에는 원동축(6)을 가진 회전체(20)을 축설치하되 회전체(20)에는 돌출된 로터(14)가 구비되고, 상기 흡기 및 배기블록(17)사이의 실린더 내경(16)에 형성된 압축캡(5) 수장부(18)에 압축실(19)을 가지는 압축캡(5)이 축설치되어 벨사이드블록(9)이 케이싱블록(15)에 밀폐되도록 체결되는 것으로서 제 4 도에서와 같이 압축캡(5)은 원동축(6)에 의해 피동축기어(3)(1)을 연동시키면서 제 3 도에서와 같이 작동이 이루어지고 이때 피동축기어에 축연결된 압축캡(5)이 회전되면서 로터(14)가 상기 압축캡(5)의 압축실(19)로 이동되어 압축실(19)내의 가스를 압축시키면 공지와 같이 점화플러그에 의해 점화 폭발하게 된다.1 is an exploded perspective view of the present invention, the intake and exhaust valve block 17 is formed in the casing block 15, each valve (7) (8) is bonded to the cylinder inner diameter (16) of the driving shaft (6) Compressing cap 5 formed in the cylinder inner diameter 16 between the intake and exhaust block 17 is provided with a rotor 14 protruding from the rotor 20, the shaft 20 is installed Compression cap (5) having a compression chamber (19) is axially installed in the storage unit 18 is fastened so that the bellside block (9) is sealed to the casing block (15), as shown in FIG. ) Is operated as shown in FIG. 3 while interlocking the driven shaft gears (3) and (1) by the primary shaft (6), and the rotor (14) while the compression cap (5) axially connected to the driven shaft gear is rotated. When the gas is moved to the compression chamber 19 of the compression cap 5 to compress the gas in the compression chamber 19, the ignition explosion is caused by the ignition plug as known.

이때 제 4 도의 (2)에서와 같이 압축실(19)이 형성되어지며, 하나의 로터에 두 개의 실린더를 가지게 되므로 내강이 커지게 된다.At this time, as shown in (4) of FIG. 4, the compression chamber 19 is formed, and the lumen is increased because the rotor has two cylinders.

이에 따라 로터가 압축한 압축공기의 팽창을 직접받아 축으로부터 90도의 큰 토오크로서 동력을 전달하게 되어 기존 엔진보다 보다큰 토오크(T)가 형성하게되는 것이다. 이로 인한 연료절감 효과를 가져오며, 뿐만 아니라 원리는 복잡하나 구조가 간단하고 제작이 쉬우며, 전체 엔진무게와 부피가 적으며, 진동조절이 쉽게 순간 고속회전에 매우 용이한 특징을 가진다.Accordingly, the rotor receives the expansion of the compressed air compressed directly, and transmits power as a large torque of 90 degrees from the shaft, thereby forming a larger torque (T) than the existing engine. This results in a fuel saving effect, as well as the principle is complicated, but the structure is simple, easy to manufacture, the overall engine weight and volume is small, and the vibration control is easy, it is very easy to instantaneous high speed rotation.

제 3 도의 유동장치외에 제나바기어나 간헐기어 또는 너클기어 등으로도 압축캡을 유도할 수 있다.In addition to the flow apparatus of FIG. 3, the compression cap may also be guided by a Zenaba gear, an intermittent gear, a knuckle gear, or the like.

Claims (1)

원호상의 실린더내경(16)을 구성하는 케이싱블록(15)에 흡, 배기 밸브블록(17)을 구성하여 흡기, 배기밸브(7)(8)을 형성하되, 실린더 내경(16)의 흡기, 배기밸브(7)(8)사이에 수장요부(18)을 형성압축실(19)을 가지는 압축캡(5)을 구비하고 실린더 내경(16)에 로터(14)를 돌출형성한 회전체(20)를 축설시켜 원동축(6)과 압축캡(5)축을 원동축기어(4), 유동기어(3)(2) 및 피동축기어(1)를 구성한 유동장치로서 압축캡(5)을 연동 구성하여 벨사이드블록(9)으로 체결함을 특징으로 하는 구조의 로터리 엔진(Rotary engine).Intake and exhaust valve blocks 17 are formed in the casing block 15 constituting the circular cylinder inner diameter 16 to form the intake and exhaust valves 7 and 8, but the intake and exhaust of the cylinder inner diameter 16 are formed. Rotor 20 having a compression cap 5 having a compression chamber 19 between the valves 7 and 8 and having a compression chamber 19 formed therein and protruding the rotor 14 to the cylinder inner diameter 16. Compression cap (5) is interlocked as a flow device consisting of the primary shaft (6) and the compression cap (5) shaft consisting of the primary shaft gear (4), the flow gear (3) (2) and the driven shaft gear (1) Rotary engine (Rotary engine) of the structure characterized in that the fastening to the bell side block (9).
KR1019920016055A 1992-09-03 1992-09-03 Rotary engine KR950000601B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1019920016055A KR950000601B1 (en) 1992-09-03 1992-09-03 Rotary engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019920016055A KR950000601B1 (en) 1992-09-03 1992-09-03 Rotary engine

Publications (2)

Publication Number Publication Date
KR940007346A KR940007346A (en) 1994-04-27
KR950000601B1 true KR950000601B1 (en) 1995-01-26

Family

ID=19339033

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019920016055A KR950000601B1 (en) 1992-09-03 1992-09-03 Rotary engine

Country Status (1)

Country Link
KR (1) KR950000601B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012115379A2 (en) * 2011-02-21 2012-08-30 Heon-Kyu Kim Gear type connection device for transmitting rotating power of rotors of rotary engine to output gear shaft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012115379A2 (en) * 2011-02-21 2012-08-30 Heon-Kyu Kim Gear type connection device for transmitting rotating power of rotors of rotary engine to output gear shaft
WO2012115379A3 (en) * 2011-02-21 2012-12-20 Heon-Kyu Kim Gear type connection device for transmitting rotating power of rotors of rotary engine to output gear shaft
CN103502688A (en) * 2011-02-21 2014-01-08 金宪奎 Gear type connection device for transmitting rotating power of rotors of rotary engine to output gear shaft

Also Published As

Publication number Publication date
KR940007346A (en) 1994-04-27

Similar Documents

Publication Publication Date Title
US4071000A (en) Double crankshaft valved two cycle engine
US4257752A (en) Rotary alternating piston machine with coupling lever rotating around offset crankpin
JP2000104556A (en) Rotary internal combustion engine
US3895610A (en) Rotary Nutating engine
KR950000601B1 (en) Rotary engine
US1237696A (en) Explosion-engine.
CN110500177A (en) A kind of birotor is the same as journey internal combustion engine
CN2269469Y (en) Double head piston rotary engine
CN109611195B (en) Flow guiding type rotor internal combustion engine between rotor and stator
JPH1162605A (en) Rotary type internal combustion engine
KR960038073A (en) Non-Valve Rotary Combustion Chambers
US3750630A (en) Rotary combustion engine
JPH03151523A (en) Rotary machine
KR920002243B1 (en) Rotary engine
WO1986004637A1 (en) Axial shaft piston engine
JPH03229923A (en) Rotary piston type internal combustion engine
KR960011722B1 (en) Rotary engine
KR940003525B1 (en) Rotary engine
JPH03182631A (en) Four-cycle rotary piston engine
JPH06323103A (en) Rotary transmission mechanism
KR970001461B1 (en) Internal combustion engine of oscillating piston engines
KR20010053816A (en) Rotary engine
JPS58183823A (en) Engine providing complete circular motion
JPH11210484A (en) Swing type rotary engine
KR920000990B1 (en) Rotary engine

Legal Events

Date Code Title Description
A201 Request for examination
G160 Decision to publish patent application
E701 Decision to grant or registration of patent right
NORF Unpaid initial registration fee