KR20080100938A - Rotary engine - Google Patents

Rotary engine Download PDF

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Publication number
KR20080100938A
KR20080100938A KR1020070047003A KR20070047003A KR20080100938A KR 20080100938 A KR20080100938 A KR 20080100938A KR 1020070047003 A KR1020070047003 A KR 1020070047003A KR 20070047003 A KR20070047003 A KR 20070047003A KR 20080100938 A KR20080100938 A KR 20080100938A
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South Korea
Prior art keywords
housing
rotor
roll
compressed air
center
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KR1020070047003A
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Korean (ko)
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변상복
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변상복
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Priority to KR1020070047003A priority Critical patent/KR20080100938A/en
Publication of KR20080100938A publication Critical patent/KR20080100938A/en

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/04Charge admission or combustion-gas discharge
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B55/00Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
    • F02B55/02Pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2730/00Internal combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/01Internal combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
    • 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

Abstract

Provided is a rotary engine with less mechanical loss caused by noise, vibration and friction and improved thermal efficiency due to the airtightness. A rotor(4) with a vane(3) is fixed to a center output axis(2) of a housing(1). On the circumferential surface of the rotor, a roll(7) with a compressed air room(6) and a recess(5) are press-welded and rotate oppositely. Short shafts integrally protruded on a side housing are inserted in the compressed air room formed in the center of the roll and support the roll to rotate. A fuel nozzle and an ignition plug(9) are set up on the short shafts. A partition(12) in which a spring is intervened in an axis is set up on a concave inner wall(10) of the housing bottom. An air intake(13) and an exhaust hole(14) are punched on the right and left of the partition. A U-shaped elastic seal(16) is inserted in the vane close to the housing and side housing. A seal ring(16') of spring washer type is inserted in a circular groove formed on the periphery of the rotor.

Description

로우터리엔진{rotary engine}Rotary engine

도 1은 본 발명의 종단면도1 is a longitudinal cross-sectional view of the present invention;

도 2는 도1의 작동상태를 표시한 종단면도Figure 2 is a longitudinal cross-sectional view showing the operating state of Figure 1

도 3은 도 1의 A-A선 종단면도3 is a cross-sectional view taken along the line A-A of FIG.

* 도면의 주요부분에 대한 부호 설명 *Explanation of symbols on the main parts of the drawings

1 : 하우징(Housing) 2 : 중심출력축 3 : 날개(Vane)1: Housing 2: Center Output Shaft 3: Vane

4 : 로오터(rotor) 5 : 요부(凹部) 6 : 압축공기실4: rotor 5: main part 6: compressed air chamber

7 : 롤(Roll) 8 : 연료분사변 9 : 점화플러그7 roll 8 fuel injection side 9 spark plug

10 : 요면(凹面) 11 : 스프링 11' : 축10: concave surface 11: spring 11 ': shaft

12 : 간막이(Partition) 13 : 흡기공 14 : 배기공12: Partition 13: Intake hole 14: Exhaust hole

15,15' : 사이드하우징 16 : U자형 시일(seal)15,15 ': Side housing 16: U-shaped seal

16' : 시일링(seal ring) 17,17' : 단축(短軸)16 ': seal ring 17,17': short axis

18 : 냉각수실 19 : 동력휠(Wheel)18: cooling water chamber 19: power wheel (Wheel)

20 : 시일링(Seal ring)20: Seal ring

종래의 왕복동 내연기관은 토오크(torque)변동이 커서 충격,신호,소음이 클뿐만 아니라 크랭크 피스톤의 왕복동에 따른 관성저항이 커서 기계적 효율이 크게 떨어지고 또 로우터리 기관(rotary engine)인 반켈엔진(Wankel engine)은 그 회전 로오터가 삼각형으로 되어 있기 때문에 그 에이펙스시일(Apex Seal)과 하우징간의 기밀 및 윤활 냉각이 곤란하고 하우징 각부의 온도차에 의한 열팽창의 차, 열변형의 처리가 곤란하여 열효율이 낮고, 하우징, 로오터등 제작성의 어려움으로 생산원가가 상승하는 결점이 있었다.Conventional reciprocating internal combustion engines have a large torque change and thus have a high impact, signal, and noise, as well as large inertia resistance due to reciprocation of the crank piston, resulting in a significant drop in mechanical efficiency and a rotary engine, a Wankel engine. Since the rotary rotor is triangular, the airtight and lubrication cooling between the apex seal and the housing is difficult, and the difference in thermal expansion and thermal deformation due to the temperature difference between the housing parts is difficult. Due to the difficulty in manufacturing, housing, rotor, etc., there was a defect that the production cost increased.

이러한 결점은 삼각형 로우터의 본질적인 결함에서 오는 결점이기 때문에 앞으로도 개량될 여지가 거의 없다.Since these drawbacks come from the inherent drawbacks of triangular rotors, there is little room for improvement.

본 발명은 이상과 같은 종래 엔진의 결점을 해결하여 작동실내의 기밀확보, 윤활,냉각,소음,진동,제작의 난이성,열효율등 내연기관으로서의 필수요건을 모두 충족하여 마력당 중량 및 부피를 작게하고 저렴한 고연비의 간헐 연소 사이클 엔진을 목적으로 안출한 것이다.The present invention solves the deficiencies of the conventional engine as described above to meet the essential requirements as an internal combustion engine, such as airtightness, lubrication, cooling, noise, vibration, manufacturing difficulty, thermal efficiency in the operating room to reduce the weight and volume per horsepower and It is designed for the purpose of inexpensive, high fuel consumption, intermittent combustion cycle engine.

상술한 목적을 달성하기 위하여 왕복동 내연기관의 결점인 관성저항을 제거하고 토오크(torque)변화없이 원활한 회전운동으로 소음,진동,마찰력으로 인한 기계적 손실 등을 개선하고 간단한 구조로서 마력당 중량 및 부피를 줄이고 기밀성, 내구성 및 생산원가를 절감한 고연비의 로우터리 엔진을 개발한다.In order to achieve the above object, it eliminates inertia resistance which is a defect of reciprocating internal combustion engine, improves mechanical loss due to noise, vibration and friction by smooth rotational movement without changing torque, and improves weight and volume per horsepower as a simple structure. The company develops a fuel-efficient rotary engine with reduced airtightness, durability and cost of production.

하우징(1)의 중심출력축(2)에 날개(Vane)(3)가 돌설(突設)된 로오터(4)를 고 정하고 이 로오터(4)의 원주면에는 요부(凹部)(5)와 중심의 압축공기실(6)이 형성된 롤(Roll)(7)을 압점(

Figure 112007504526890-PAT00002
接)케 하여 반대로 회전케 하고 그 롤(7)중심에 형성된 압축공기실(6)에는 사이드하우징(15)(15')에서 동일체로 돌성(突成)된 단축(短軸)(17)(17')이 유삽(遊揷)되어서 롤(7)을 회전케 하고 그 양쪽단축(17)(17')에는 통상의 연료분사변(8)및 점화플러그(9)를 설치하고 하단의 하우징(1)내벽요면(凹面)(10)에는 축(11')에 스프링(11)이 개입(介入)된 간막이(Partition)(12)을 설치하고 그 좌우 양측에는 흡기공(13)과 배기공(14)을 천설(穿設)하고 날개(Yane)(3)에는 하우징(1)및 사이드하우징(15)(15')에 밀접토록 탄성의 U자형 시일(Seal)(16)을 감설(嵌設)하고 로오터(4)주연에 삭설(削設)한 원형의 홈에는 스프링와셔(spring washer)형의 시일링(Seal ring)(16')을 끼워서 된 것이다.A rotor (4) with vanes (3) protruding from the center output shaft (2) of the housing (1) is fixed, and a recess (5) on the circumferential surface of the rotor (4). And the roll 7 formed with the compressed air chamber 6 at the center thereof.
Figure 112007504526890-PAT00002
In the compressed air chamber 6 formed at the center of the roll 7 so as to be rotated in the opposite direction and formed in the same direction in the side housings 15 and 15 '. 17 ') is rotated to rotate the rolls 7, and both fuel shafts 8 and ignition plugs 9 are installed on both short shafts 17 and 17' and the lower housing ( 1) An inner wall recessed surface 10 is provided with a partition 12 having a spring 11 interposed on a shaft 11 ', and an intake hole 13 and an exhaust hole on both left and right sides thereof. 14, and the wings 3 are housed with elastic U-shaped seals 16 close to the housing 1 and the side housings 15 and 15 '. And a spring washer-type seal ring (16 ') is inserted into a circular groove cut around the rotor (4).

도면중 미설명부호 17,17'는 단축(短軸), 18은 냉각수실, 19는 동력휠(Wheel)(20)은 시일링(Seal ring)을 표시한 것임.In the drawings, reference numerals 17 and 17 'are short axis, 18 is a coolant chamber, 19 is a wheel 20, and a seal ring is indicated.

이상과 같이 구성된 본 발명의 작용을 표시하면 다음과 같다.The operation of the present invention configured as described above is as follows.

로오터(4)가 화살표 방향으로 회전하면 동일체로 돌출된 날개(Vane)(3)의 한쪽면이 흡기공(13)으로부터 새로운 공기를 흡입하고 반대쪽면은 먼저 흡입되었던 공기를 압축하고, 로오터(4)상면에 밀접되어서 반대로 회동하는 롤(Roll)(7)의 요부(5)에 날개(3)가 맞물리게 될 무렵에는 크게 압축된 공기가 롤(7)중심에 형성된 작은 압축공기실(6)로 밀려들어 가고 날개(3)가 도2에 표시한 바와 같이 우측으로 이동하여 회전하는 롤(7)의 요부(5)에서 벗어날 무렵에 압축공기실(6)내에 연료분사변(8)에서 연료가 분사됨과 동시에 점화플러그(9)에 의하여 착화하여 폭발케 한 다.When the rotor 4 rotates in the direction of the arrow, one side of the vane 3 protruding into the same sucks fresh air from the intake hole 13, and the other side compresses the previously sucked air. (4) A small compressed air chamber in which a large compressed air is formed at the center of the roll 7 by the time the blade 3 is engaged with the recess 5 of the roll 7 which is close to the upper surface and rotates in the opposite direction. In the compressed air chamber (6) in the compressed air chamber (6) when the blade (3) is pushed out and the wing (3) moves to the right and moves away from the recess (5) of the roll (7) as shown in FIG. At the same time fuel is injected, it is ignited by the spark plug (9) to explode.

이와 같이 로오터(4) 1 회전에 한번 폭발된 연소가스는 급속히 팽창하여 날개(3)에 고압력을 가하여 중심출력축(2)을 원활히 회전케 하고 그 팽창되는 배기는 하방의 하우징(1)에 천설한 배기공(14)으로 급속히 배출된다.In this manner, the combustion gas exploded once per revolution of the rotor 4 rapidly expands and exerts high pressure on the blade 3 to smoothly rotate the center output shaft 2, and the expanded exhaust gas is applied to the lower housing 1. It is rapidly discharged to the snow exhaust hole 14.

상술과 같이 로오터(4)의 날개(3)가 하우징(1)내벽에 밀접하여 회전하다가 하방의 간막이(Partition)(12)를 밀면서 지나갈때는 축(11')에 개입된 스프링(11)의 탄력에 항(抗)하여 잠시 하우징(1)하단 내벽에 형성된 요면(10)에 포개져 누어 있다가 날개(3)가 지나간 순간에 또 다시 원상으로 복귀하여 로오터(4)에 밀접되므로 배기의 일부가 흡기공(13)쪽으로 이동하는 것을 차단하고 계속 배기공(14)으로 유도하여 배출한다.As described above, when the wing 3 of the rotor 4 rotates close to the inner wall of the housing 1 and passes while pushing the lower partition 12, the spring 11 intervening in the shaft 11 'is moved. Due to its elasticity, it rests on the concave surface 10 formed on the inner wall of the lower part of the housing 1 for a while, and then returns to its original shape again at the moment when the wing 3 passes, and closes to the rotor 4 so that A part is blocked from moving toward the intake hole 13 and continues to guide the exhaust hole 14 to be discharged.

그리고 로오터(4)주연에 삭설(削設)한 원형의 홈에 끼운 스프링와셔(spring washer)형의 실링(seal ring)(16')과 로오터 날개(3)에 감입(嵌入)된 U 자형 시일(seal)(16)은 하우징(1)내벽과 사이드하우징(15)(15')내벽에 긴밀히 탄압하기 때문에 연소가스누설(leakage)이 억제되므로 열효율이 향상된다.And a U was inserted into the rotor blade 3 and a spring washer-shaped seal ring 16 'fitted in a circular groove cut around the rotor 4; Since the seal 16 is tightly pressed against the inner wall of the housing 1 and the inner wall of the side housings 15 and 15 ′, leakage of the combustion gas is suppressed, thereby improving thermal efficiency.

본 발명을 실시함에 있어서, 롤(7)의 직경이 로오터(4)의 1/2인 경우 날개(3)를 2개로 증설하면 로오터(4) 1회전에 2번 폭발하므로 이론상 출력이 2배로 향상된다.In the practice of the present invention, in the case where the diameter of the roll 7 is 1/2 of the rotor 4, when the blades 3 are expanded to two, the output of the rotor 7 explodes twice in one revolution of the rotor 4. Improved by 2x

본 발명은 하우징(1)내에서의 로오터(rotor)및 롤(Roll)이 모두 회전운동이므로 기계손실이 적고, 소음,진동이 거의 없고 로오터(4)의 날개(Vane)(3)에 감입( 嵌入)된 U자형 시일(Seal)(16)과 시일링(seal ring)(16')은 하우징(1)및 사이드하우징(15)의 내벽에 밀접되어서 기밀(氣

Figure 112007504526890-PAT00003
)이 확보되므로 열효율 향상으로 연비가 높아진다.In the present invention, since both the rotor and the roll in the housing 1 are rotational movements, the machine loss is small, there is little noise and vibration, and the vanes 3 of the rotor 4 are provided. The enclosed U-shaped seal 16 and seal ring 16 ′ are in close contact with the inner walls of the housing 1 and the side housing 15 to be hermetically sealed.
Figure 112007504526890-PAT00003
), The fuel efficiency is increased by improving the thermal efficiency.

그리고 엔진의 중량, 부피가 작아서 마력당의 중량이 적고 제작성이 용이하므로 생산원가가 절감되는 잇점이 있다.In addition, since the weight and volume of the engine are small, the weight per horsepower is small and the manufacturing is easy, thus reducing the production cost.

Claims (1)

하우징(1)의 중심출력축(2)에 날개(3)가 돌설(突設)된 로오터(Rotor)(4)를 고정하고 이 로오터(4)의 원주면에는 요부(凹部)(5)와 중심의 압축공기실(6)이 형성된 롤(Roll)(7)을 압접(
Figure 112007504526890-PAT00004
接)케 하여 반대로 회전케 하고 그 롤(7)중심에 형성된 원형의 압축공기실(6)에는 사이드하우징(15)(15')에서 동일체로 돌성(突成)된 단축(短軸)(17)(17')이 유삽(遊揷)되어서 롤(7)을 회전케 하고 그 양쪽단축(17)(17')에는 통상의 연료분사변(8)및 점화플러그(9)를 설치하고 하단의 하우징(1)내벽요면(凹面)(10)에는 축(11')에 스프링(11)이 개입(介入)된 간막이(Partition)(12)을 설치하고 그 좌,우 양측에는 흡기공(13)과 배기공(14)을 천설(穿設)하고 날개(vane)(3)에는 하우징(1)및 사이드 하우징(15)(15')에 밀접토록 탄성의 U자형 시일(seal)(16)을 감설(嵌設)하고 로오터(4)주연에 삭설(削設)한 원형의 "홈"에는 스프링와셔(spring washer)형의 시일링(seal ring)(16')을 끼워서 된 것을 특징으로 하는 로우터리 엔진.
The rotor 4 in which the blade 3 protrudes is fixed to the center output shaft 2 of the housing 1, and the recessed part 5 is provided in the circumferential surface of this rotor 4; And press the roll 7 in which the compressed air chamber 6 in the center is formed (
Figure 112007504526890-PAT00004
In the circular compressed air chamber 6 formed at the center of the roll 7, and is formed in the same direction in the side housings 15 and 15 '. (17 ') is rotated to rotate the roll (7), and both fuel shafts (8) and spark plugs (9) are installed at both ends (17) and (17'). The inner wall concave surface 10 of the housing 1 is provided with a partition 12 having a spring 11 interposed on the shaft 11 'and an intake hole 13 on both left and right sides thereof. And exhaust holes 14 are laid, and vanes 3 are provided with a U-shaped seal 16 elastically close to the housing 1 and the side housings 15 and 15 '. A circular "groove" cut in the periphery of the rotor 4 is fitted with a spring washer-type seal ring 16 '. Rotary engine.
KR1020070047003A 2007-05-15 2007-05-15 Rotary engine KR20080100938A (en)

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