KR200368688Y1 - Control valve of starting air valve for marine engine - Google Patents

Control valve of starting air valve for marine engine Download PDF

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Publication number
KR200368688Y1
KR200368688Y1 KR20-2004-0023373U KR20040023373U KR200368688Y1 KR 200368688 Y1 KR200368688 Y1 KR 200368688Y1 KR 20040023373 U KR20040023373 U KR 20040023373U KR 200368688 Y1 KR200368688 Y1 KR 200368688Y1
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South Korea
Prior art keywords
air
valve
air chamber
control valve
starting air
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KR20-2004-0023373U
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Korean (ko)
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김상훈
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김상훈
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Priority to KR20-2004-0023373U priority Critical patent/KR200368688Y1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N9/00Starting of engines by supplying auxiliary pressure fluid to their working chambers
    • F02N9/04Starting of engines by supplying auxiliary pressure fluid to their working chambers the pressure fluid being generated otherwise, e.g. by compressing air
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H21/00Use of propulsion power plant or units on vessels
    • B63H21/12Use of propulsion power plant or units on vessels the vessels being motor-driven
    • B63H21/14Use of propulsion power plant or units on vessels the vessels being motor-driven relating to internal-combustion engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/04Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for starting by means of fluid pressure

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Ocean & Marine Engineering (AREA)
  • Fluid-Driven Valves (AREA)

Abstract

본 고안은 선박엔진용 스타팅 에어밸브에 제어밸브에 관한 것으로 보다 상세하게는 최초 선박엔진이 구동 될 때, 선박엔진의 실린더 블럭 상측에 장치된 스타팅 에어밸브에서 고압의 스타팅 에어를 실린더로 주입하면, 상기 실린더가 압축되면서 연료가 분사되어 폭발하게 되므로서 최초 엔진이 구동되는 것으로, 종래의 스타팅 에어밸브는 스타팅 에어를 개폐하기 위하여 다수의 흡기 또는 배기밸브가 장착되므로서 각 포트를 개폐하는 밸브의 수가 많아 복잡하고 작동하기 어려운 문제점이 있었으나 본 고안은 스타팅 에어밸브의 각 포트를 한번에 제어 할 수 있게 하기 위하여, 다수의 통기 유로를 가진 에어 제어밸브를 제공하는 것이다The present invention relates to a control valve to a starting air valve for a ship engine. More specifically, when a high speed starting air is injected into a cylinder from a starting air valve installed above a cylinder block of a ship engine when the first ship engine is driven, As the cylinder is compressed and fuel is injected and exploded, the first engine is driven. The conventional starting air valve is equipped with a plurality of intake or exhaust valves for opening and closing the starting air, so that the number of valves for opening and closing each port There are many problems that are complicated and difficult to operate, but the present invention provides an air control valve having a plurality of ventilation flow paths so that each port of the starting air valve can be controlled at one time.

Description

선박엔진용 스타팅 에어밸브의 제어밸브{CONTROL VALVE OF STARTING AIR VALVE FOR MARINE ENGINE}CONTROL VALVE OF STARTING AIR VALVE FOR MARINE ENGINE

본 고안은 선박엔진용 스타팅 에어밸브의 제어밸브에 관한 것으로 보다 상세하게는 최초 선박엔진이 구동 될 때, 선박엔진의 실린더 블럭 상측에 장치된 스타팅 에어밸브에서 고압의 스타팅 에어를 실린더로 주입하면, 상기 실린더가 압축되면서 연료가 분사되어 폭발하게 되므로서 최초 엔진이 구동되는 것으로, 상기 스타팅 에어밸브를 작동하는 제어밸브를 제공하는 것이다The present invention relates to a control valve of a starting air valve for a ship engine. More specifically, when a high speed starting air is injected into a cylinder from a starting air valve installed above a cylinder block of a ship engine when the first ship engine is driven, As the cylinder is compressed and fuel is injected and exploded, the first engine is driven to provide a control valve for operating the starting air valve.

종래의 선박엔진용 스타팅 에어밸브는 선박엔진의 실린더로 주입되는 스타팅 에어를 개폐하기 위하여 각 포트마다 흡기 또는 배기 에어밸브를 장치하므로서 다수의 에어밸브가 장치되어야 하기 때문에 그 구조가 복잡하고 또한 각 포트를 개폐하는 작동이 어려운 문제점이 있었다The conventional air engine starting air valve is complicated in structure because each air port must be equipped with an intake or exhaust air valve for each port to open and close the starting air injected into the cylinder of the ship engine. There was a problem that the operation to open and close the

이에 본 고안은 상기와 같은 종래의 문제점을 해소하고자 안출된 것으로서 스타팅 에어밸브의 각 포트를 한번에 제어 할 수 있게 하기 위하여, 다수의 통기 유로를 가진 에어 제어밸브를 구성한 것인데, 이를 첨부된 도면에 의거 보다 상세하게 설명하면 다음과 같다The present invention has been made to solve the conventional problems as described above in order to be able to control each port of the starting air valve at a time, to configure an air control valve having a plurality of air flow passages, based on the accompanying drawings In more detail,

도 1은 본 고안의 제어밸브 사시도1 is a perspective view of a control valve of the present invention

도 2는 본 고안의 제어밸브 단면도2 is a cross-sectional view of the control valve of the present invention

도 3은 본 고안의 제어밸브 블럭을 절단한 분해 사시도Figure 3 is an exploded perspective view cut the control valve block of the present invention

도 4는 본 고안의 제어밸브 내부부품을 분해한 분해 사시도4 is an exploded perspective view illustrating the internal parts of the control valve of the present invention.

도 5는 본 고안을 선박엔진용 스타팅 에어밸브에 장착된 사용 상태도Figure 5 is a state of use mounted on the starting air valve for the ship engine of the present invention

도 6은 도 5의 다른 방향에서 도시한 단면 예시도6 is an exemplary cross-sectional view shown in another direction of FIG.

* 도면의 주요부품에 대한 부호설명 ** Explanation of code for main parts of drawing *

1, 1a, 2, 2a, 3, 3a, 4, 4a, 5, 5a, 6: 에어 연통 유로1, 1a, 2, 2a, 3, 3a, 4, 4a, 5, 5a, 6: air communication flow path

A1, A2, A3, A4: 공기실A1, A2, A3, A4: Air chamber

가: 제어밸브 A: 제어압A: Control valve A: Control pressure

나: 스타팅 에어밸브 B: 대기압B: Starting air valve B: Atmospheric pressure

다: 선박엔진 C: 스타팅 에어C: Marine Engine C: Starting Air

Ho: 하우징 Co: 커버Ho: Housing Co: Cover

Ri: 링 Pi1, Pi2, Pi3: 피스톤Ri: ring Pi1, Pi2, Pi3: piston

Sd: 스핀들 C1: 통공Sd: Spindle C1: Through Hole

C2: 연통로 Cu: 컵C2: communication path Cu: cup

Di: 디스크 Sh: 축Di: Disc Sh: Axis

Sp: 스프링 St: 마개Sp: Spring St: Spigot

Sn: 스냅링 Nu: 너트Sn: Snap ring Nu: Nut

Bo: 볼트Bo: Bolt

선박엔진(다)의 실린더 블록 상측에 외부에서 유입되는 스타팅 에어(C)를 개폐하는 공지된 선박 엔진용 스타팅 에어밸브에 있어서,In the known air engine starting air valve for opening and closing the starting air (C) flowing from the outside to the cylinder block of the ship engine (C),

상기 스타팅 에어밸브(나)에 대기압(B)이 투입되는 1번유로(1a)와, 에어밸브를 개방하는 2번유로(2a)와, 에어밸브를 패쇄하는 3번유로(3a)와, 잔여에어를 외부로 배출되는 4번유로(4a) 및 5번유로(5a)를 각각 구성하여 상측의 제어밸브(가)와 서로 연통되게 장치하고,The first flow passage 1a into which the atmospheric pressure B is introduced into the starting air valve b, the second flow passage 2a to open the air valve, the third flow passage 3a to close the air valve, and the remaining Fourth passage (4a) and the fifth passage (5a) for discharging the air to the outside are respectively configured to be in communication with the upper control valve (a),

상기 제어밸브(가)는 본체 내에 양측으로 상하 공기실(A1)(A2)(B1)(B2)을 각각 구비하여 우측의 하측공기실(A2)과 좌측의 상측공기실(B1)에 연통된 1번유로(1)와, 우측의 상측공기실(A1)과 하측공기실(A2)에 연통된 2번유로(2)와, 좌측의 상측공기실(B1)과 하측공기실(B2)에 연통된 3번유로(3)와, 우측의 상측공기실(A1)에 연통된 4번유로(4)와, 좌측의 하측공기실(B2)에 연통된 5번유로(5)를 각각 구성하며,The control valve (A) has upper and lower air chambers (A1), (A2), (B1) and (B2), respectively, on both sides of the main body to communicate with the lower air chamber (A2) on the right side and the upper air chamber (B1) on the left side. To the first flow passage 1, the second flow passage 2 connected to the upper air chamber A1 and the lower air chamber A2 on the right side, and the upper air chamber B1 and the lower air chamber B2 on the left side. The channel 3 connected to the third channel 3, the channel 4 connected to the upper air chamber A1 on the right side, and the channel 5 5 connected to the lower air chamber B2 on the left side, respectively. ,

상기 양측의 상하 공기실(A1)(A2)(B1)(B2) 내에 상측은 피시톤(Pi1)Pi2)을구비하고, 하측은 컵(Cu)을 배치하여 축(Sh)간 결합하며, 하측의 컵(Cu)은 스프링(Sp)을 탄설하여 피스톤(Pi1)(Pi2)이 항상 위로 승강되게 장치하고, 상기 우측의 상측공기실(A1)과 좌측의 상측공기실(B1)은 피스톤(Pi1)(Pi2) 상측으로 연통되는 연통유로(6)를 구성하여, 우측의 상측공기실(A1)에 제어압(A)을 투입하는 투입구로 이루어진 선반엔진용 스타팅 밸브의 제어밸브를 제공하는 것이다In the upper and lower air chambers A1, A2, B1, and B2 of the two sides, the upper side is equipped with the Piton Pi1, the lower side is arranged between the shafts Sh by arranging the cup Cu, and the lower side. The cup Cu is installed with a piston Sp so that the piston Pi1 and Pi2 are always elevated upward, and the upper air chamber A1 on the right side and the upper air chamber B1 on the left side are piston Pi1. (Pi2) to provide a control valve of the starting valve for the lathe engine comprising an inlet for injecting the control pressure (A) into the upper air chamber (A1) on the right side of the communication passage (6).

즉, 상기 스타팅 에어밸브(나)의 구조는 커버(Co)와 링(Ri)이 결합된 하우징(Ho) 상측의 내통에 피스톤(Pi3)을 배치하여, 스핀들(Sd)과 축(Sh)간 결합하고, 상기 피스톤(Pi3)은 저면에 스프링(Sp)을 탄설하여 항상 피스톤(Pi3)이 위로 승강되게 구성되며, 상기 하우징(Ho) 하측은 다수의 통공(C1)이 선박엔진(다)의 외부에서 투입되는 스타팅에어(C)의 투입구와 연통되어, 스핀들이 하강하면 엔진으로 스타팅 에어(C)가 투입되고, 스핀들이 승강하면 중단되게 한 공지된 것에서,That is, the structure of the starting air valve (B) is arranged between the spindle (Sd) and the shaft (Sh) by arranging the piston (Pi3) in the inner cylinder of the upper side of the housing (Ho) coupled with the cover (Co) and the ring (Ri) Coupling, the piston (Pi3) is constructed so that the piston (Pp) in the bottom surface is always raised to the piston (Pi3), and the lower portion of the housing (Ho) is a plurality of through holes (C1) of the ship engine (C) In the known communication with the inlet of the starting air (C) which is supplied from the outside, the starting air (C) is introduced into the engine when the spindle is lowered, and stopped when the spindle is raised,

상기 스타팅 에어밸브(나)의 각 에어 연통 유로를 설명 하면, 먼저 1번유로(1a)는 외부의 대기압(B)이 투입되는 투입로를 구성하여 제어밸브(가)의 1번유로(1)로 연통되게 한 것이고, 2번유로(2a)는 피스톤(Pi3)의 상측에 구성하여 제어밸브(가)의 2번유로(2)에서 배출된 에어압이 피스톤(Pi3)을 하강시켜 스핀들(Sd)을 개방되게 하므로서 최초 선박엔진(다)의 스타팅 에어(C)를 투입되게 하는 것이며, 3번유로(3a)는 피스톤(Pi3)의 하측에 연통되어 제어밸브(가)의 3번유로(3)에서 배출된 에어압이 피스톤(Pi3)을 승강시켜 개방된 스핀들(Sd)을 다시 폐쇄되게 하는 것이고, 4번유로(4a)와 5번유로(5a)는 그냥 외부로 노출되어 제어밸브(가)에서 사용되고 남은 잔여 에어를 외부로 토출되게 한 것이다Referring to each air communication flow path of the starting air valve (b), first flow path (1a) constitutes an input path through which the external atmospheric pressure (B) is introduced, the first flow path (1) of the control valve (A) The second flow path 2a is formed on the upper side of the piston Pi3, and the air pressure discharged from the second flow path 2 of the control valve A lowers the piston Pi3 so that the spindle Sd ) To open the starting air (C) of the first ship engine (C), the third flow path (3a) is communicated to the lower side of the piston (Pi3), the third flow path of the control valve (A) (3) ), The air pressure discharged from the pump raises the piston Pi3 to close the opened spindle Sd again, and the 4th flow path 4a and the 5th flow path 5a are just exposed to the outside and the control valve ) Is used to discharge the remaining air to the outside

또한 상기 제어밸브(가)의 구조는 하우징(Ho)의 상부 커버(Co)를 볼트(Bo)로 결합시키고, 하부는 마개(St)를 스냅링(Sn)으로 고정하여 좌,우측과 상,하에 각각의 공기실(A1)(A2)(B1)(B2)을 구비한 것이며, 상기 상측공기실(A1)(B1)에는 두개의 피스톤(Pi1)(Pi2)을 각각 배치하고, 하측공기실(A2)(B2)에는 상기 피스톤과 같은 역활을 하는 컵(Cu)을 구비하여 각 연통로를 막는 디스크(Di)를 장착하여 너트(Nu)로 축(Sh)간 결합하되, 하측의 컵(Cu)은 저면에 스프링(Sp)을 탄설하여 항상 피스톤(Pi1)(Pi2)이 승강되도록 이루어진 것으로,In addition, the structure of the control valve (A) is coupled to the upper cover (Co) of the housing (Ho) with a bolt (Bo), the lower part is fixed to the stopper (St) by the snap ring (Sn) left, right, up and down Each air chamber A1 (A2) (B1) (B2) is provided, and two pistons Pi1 (Pi2) are disposed in the upper air chambers A1 and B1, respectively, and the lower air chambers ( A2) (B2) is provided with a cup (Cu), which serves as the piston, and is equipped with a disk (Di) that blocks each communication path, and is coupled between the shaft (Sh) with a nut (Nu), but the lower cup (Cu) ) Is constructed so that the piston Pi1 (Pi2) is always raised and lowered by sprinkling the spring Sp on the bottom,

평상 시(에어밸브를 작동하지 않을 때) 항상 1번유로(1)를 통해 에어압이 충만된 상태이며, 이 에어압은 좌측의 피스톤(Pi2) 승강시킨 상태로 3번유로(3)로 배출되며, 작동 시(에어밸브를 작동코져 할 때)에는 우측의 투입구에 충만된 에어압 보다 높은 제어압(A)을 투입하면 우측의 피스톤(Pi1)이 하강되는 동시에 연통유로(6)를 통해 좌측 피스톤(Pi2)도 같이 하강되며, 이때 1번유로(1)를 통해 3번유로(3)로 빠져나가는 에어가 막히게 되어 2번유로(2)로 빠지게 작동되는 것이다Normally (when the air valve is not operated), the air pressure is always filled through the 1st flow path (1), and this air pressure is discharged to the 3rd flow path (3) while raising the piston (Pi2) on the left side. During operation (when operating the air valve), if the control pressure (A) higher than the air pressure filled in the inlet on the right side is input, the piston (1) on the right is lowered and the left side through the communication passage (6). Piston (Pi2) is also lowered at this time, the air going through the first flow path (1) to the third flow path (3) is blocked and is operated to fall into the second flow path (2).

따라서 이를 선박엔진(다)에 장착된 스타팅 에어밸브(나)와 제어밸브(나)를 상호 연계시켜 설명하면, 평상 시 에는 에어밸브(나)의 투입구로 공급된 대기압(B)이 1번유로(1a)를 통해 제어밸브(가)의 1번유로(1)로 연통되어 3번유로(3)로 배출되고, 다시 에어밸브(나)의 3번유로(3a)로 공급된 에어압은 피스톤(Pi3)을 승강시켜 스핀들(Sd)을 항상 폐쇄시키고 있는 상태이고, 또한 선박엔진(다)의 스타팅 에어(C)도 에어밸브(나)의 하우징(Ho) 통공(D1)를 통해 상부의 연통공(D2)으로 투입되어 스프링(Sp)과 더불어 피스톤(Pi3)을 항상 승강시키고 있는 상태이다Therefore, if this is explained in connection with the starting air valve (B) and the control valve (B) installed in the ship engine (C), the atmospheric pressure (B) supplied to the inlet of the air valve (B) is 1 euro. The air pressure supplied to channel 3 (3) of the control valve (A) and discharged to channel 3 (3) through the (1a), and then supplied to the channel 3 (3a) of the air valve (B) is a piston The spindle Sd is always closed by raising (Pi3), and the starting air (C) of the ship engine (C) also communicates with the upper part through the through hole (D1) of the housing (H) of the air valve (B). It is put into the ball D2, and the piston Pi3 is always raised and lowered together with the spring Sp.

한편, 작동 시 에는 제어밸브(가)의 제어압(A) 투입구에서 대기압(B)보다 높은 에어의 제어압(A)을 공급하면 우측 피스톤(Pi1)과 좌측 피스톤(Pi2)이 모두 하강하게 되어 1번유로(1)(1a)에서 3번유로(3)(3a)의 통로가 막히고, 1번유로(1)(1a)에서 2번유로(2)(2a)의 통로가 개방됨에 따라, 스타팅 에어밸브(나)의 2번유로(2a)로 대기압(B)이 공급되어 에어밸브(나)의 피스톤(Pi3)이 하강하게 되면 스핀들(Sd)이 개방되면서 스타팅 에어(C)가 선반엔진(다)의 실린더로 공급되기 때문에 최초엔진이 구동되게 하며, 이때 제어밸브(가)의 양측 피스톤(Pi1)(Pi2)이 하강하면서 좌측 하부의 공기실(B2)에 있던 에어압은 4번유로(4)(4a)를 통해 외부로 토출되고, 작동이 끝났을 땐 다시 평상 시 상태로 원위치되면서 우측 상부의 공기실(A1)에 있던 에어압 또한 5번유로(5)(5a)를 통해 외부로 토출되게 작동하는 것이다On the other hand, in operation, when the control pressure (A) inlet of the control valve (A) is supplied with a control pressure (A) of air higher than atmospheric pressure (B), both the right piston Pi1 and the left piston Pi2 are lowered. As passages of passage 1 (1) (1a) to passage 3 (3) (3a) are blocked, and passages of passage 1 (1) (1a) to passage 2 (2) (2a) open, When atmospheric pressure (B) is supplied to the second flow path (2a) of the starting air valve (B) and the piston (Pi3) of the air valve (B) is lowered, the spindle (Sd) is opened and the starting air (C) is turned into the lathe engine. As it is supplied to the cylinder of (C), the initial engine is driven. At this time, the air pressure in the air chamber B2 at the lower left is 4, while both pistons Pi1 and Pi2 of the control valve are lowered. (4) (4a) is discharged to the outside, the air pressure in the air chamber (A1) of the upper right also returned to the normal state when the operation is finished, also through the flow path (5) (5a) Discharge To work

이와 같이 구성된 본 고안은 종래와 같이 스타팅 에어밸브에 일일이 포트를 개폐하는 다수의 밸브를 별도를 장치하여 각 밸브를 별도로 작동할 필요없이 본 고안의 제어장치 하나로 모두 제어 할 수 있어, 그 구조를 단순화 하고 사용상 편의성을 높힐 수 있는 이점이 있는 것이다The present invention configured as described above is equipped with a plurality of valves that open and close ports individually in the starting air valve as in the prior art, so that the control device of the present invention can be controlled all without the need to operate each valve separately, thereby simplifying the structure. There is an advantage that can increase the ease of use.

Claims (1)

선박엔진(다)의 실린더 블록 상측에 외부에서 유입되는 스타팅 에어(C)를 개폐하는 공지된 선박 엔진용 스타팅 에어밸브에 있어서,In the known air engine starting air valve for opening and closing the starting air (C) flowing from the outside to the cylinder block of the ship engine (C), 상기 스타팅 에어밸브(나)에 대기압(B)이 투입되는 1번유로(1a)와, 에어밸브를 개방하는 2번유로(2a)와, 에어밸브를 패쇄하는 3번유로(3a)와, 잔여에어를 외부로 배출되는 4번유로(4a) 및 5번유로(5a)를 각각 구성하여 상측의 제어밸브(가)와 서로 연통되게 장치하고,The first flow passage 1a into which the atmospheric pressure B is introduced into the starting air valve b, the second flow passage 2a to open the air valve, the third flow passage 3a to close the air valve, and the remaining Fourth passage (4a) and the fifth passage (5a) for discharging the air to the outside are respectively configured to be in communication with the upper control valve (a), 상기 제어밸브(가)는 본체 내에 양측으로 상하 공기실(A1)(A2)(B1)(B2)을 각각 구비하여 우측의 하측공기실(A2)과 좌측의 상측공기실(B1)에 연통된 1번유로(1)와, 우측의 상측공기실(A1)과 하측공기실(A2)에 연통된 2번유로(2)와, 좌측의 상측공기실(B1)과 하측공기실(B2)에 연통된 3번유로(3)와, 우측의 상측공기실(A1)에 연통된 4번유로(4)와, 좌측의 하측공기실(B2)에 연통된 5번유로(5)를 각각 구성하며,The control valve (A) has upper and lower air chambers (A1), (A2), (B1) and (B2), respectively, on both sides of the main body to communicate with the lower air chamber (A2) on the right side and the upper air chamber (B1) on the left side. To the first flow passage 1, the second flow passage 2 connected to the upper air chamber A1 and the lower air chamber A2 on the right side, and the upper air chamber B1 and the lower air chamber B2 on the left side. The channel 3 connected to the third channel 3, the channel 4 connected to the upper air chamber A1 on the right side, and the channel 5 5 connected to the lower air chamber B2 on the left side, respectively. , 상기 양측의 상하 공기실(A1)(A2)(B1)(B2) 내에 상측은 피시톤(Pi1)Pi2)을 구비하고, 하측은 컵(Cu)을 배치하여 축(Sh)간 결합하며, 하측의 컵(Cu)은 스프링(Sp)을 탄설하여 피스톤(Pi1)(Pi2)이 항상 위로 승강되게 장치하고,In the upper and lower air chambers A1, A2, B1, and B2 of the two sides, the upper side is provided with the Piston Pi1, and the lower side is coupled between the shafts Sh by arranging the cup Cu. The cup Cu is installed with a spring Sp, so that the piston Pi1 and Pi2 are always elevated upwards, 상기 우측의 상측공기실(A1)과 좌측의 상측공기실(B1)은 피스톤(Pi1)(Pi2) 상측으로 연통되는 연통유로(6)를 구성하여, 우측의 상측공기실(A1)에 제어압(A)을 투입하는 투입구로 이루어진 선반엔진용 스타팅 밸브의 제어밸브The upper air chamber A1 on the right side and the upper air chamber B1 on the left side constitute a communication passage 6 communicating with the piston Pi1 and Pi2, and control pressure is applied to the upper air chamber A1 on the right side. Control valve of the starting valve for a lathe engine consisting of an inlet for injecting (A)
KR20-2004-0023373U 2004-08-16 2004-08-16 Control valve of starting air valve for marine engine KR200368688Y1 (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101625596B1 (en) 2016-04-27 2016-05-30 (주)성산하이텍 Solenoide Valve Integral Type Starting Valve for Ship Engine
KR101968495B1 (en) * 2017-11-15 2019-04-12 박상일 Main starting valve
KR20240053825A (en) 2022-10-18 2024-04-25 주식회사 코밸 integrated air starting valve module

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101625596B1 (en) 2016-04-27 2016-05-30 (주)성산하이텍 Solenoide Valve Integral Type Starting Valve for Ship Engine
KR101968495B1 (en) * 2017-11-15 2019-04-12 박상일 Main starting valve
KR20240053825A (en) 2022-10-18 2024-04-25 주식회사 코밸 integrated air starting valve module

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