CN104595536A - One-way check device for marine diesel engine air pipe - Google Patents

One-way check device for marine diesel engine air pipe Download PDF

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Publication number
CN104595536A
CN104595536A CN201510025284.4A CN201510025284A CN104595536A CN 104595536 A CN104595536 A CN 104595536A CN 201510025284 A CN201510025284 A CN 201510025284A CN 104595536 A CN104595536 A CN 104595536A
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CN
China
Prior art keywords
valve
interior cavity
inner cavity
diesel engine
valve body
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
CN201510025284.4A
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Chinese (zh)
Inventor
王学敏
冯君君
屠丹红
程俊华
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Hudong Heavy Machinery Co Ltd
Original Assignee
Hudong Heavy Machinery Co Ltd
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 Hudong Heavy Machinery Co Ltd filed Critical Hudong Heavy Machinery Co Ltd
Priority to CN201510025284.4A priority Critical patent/CN104595536A/en
Publication of CN104595536A publication Critical patent/CN104595536A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K15/00Check valves
    • F16K15/02Check valves with guided rigid valve members
    • F16K15/06Check valves with guided rigid valve members with guided stems
    • 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

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid-Driven Valves (AREA)

Abstract

The invention discloses a one-way check device for a marine diesel engine air pipe, comprising a valve seat, a front valve body and a rear valve body, wherein a front inner cavity and a rear inner cavity are respectively arranged in the front valve body and the rear valve body; the front valve body and the rear valve body are fixedly connected to each other at the positions where the front inner cavity and the rear inner cavity are opposite; the valve seat is embedded in a groove between the front inner cavity and the rear inner cavity and separates the front inner cavity from the rear inner cavity; the valve seat is provided with a vent hole which is communicated with the front inner cavity and the rear inner cavity; a valve block, a compression spring and a spring block orderly penetrate through a bolt located at the center of the valve seat; a lock nut is rotatably arranged on the bolt and jacks the spring block; the valve block is compressed by the compression spring and is laminated on the outer side face of the valve seat and seals the vent hole. The one-way check device for the marine diesel engine air pipe disclosed by the invention can avoid the impact failure of a main starting valve caused by reflux high temperature and high pressure gas from the inside of a cylinder when a cylinder cover starting valve is at failure, and has the advantages of simple structure, low cost, convenient installation and small space occupation, and thus, the effects of small pressure loss and good economy can be achieved.

Description

A kind of marine diesel engine air duct one-way non-return device
Technical field
The present invention relates to the fluid control device that a kind of diesel engine uses, be specifically related to the one-way non-return device in a kind of marine diesel engine air actuation pipe-line system, belong to Diesel Engine Technique Field.
Background technique
The main start mode of marine diesel engine is with pneumatic starting, and thus air actuation pipe-line system is one of requisite component of marine diesel engine.In order to avoid because of cylinder cap starting valve fault, the high temperature and high pressure gas in cylinder is back in air duct main starting valve is damaged, marine diesel engine air actuation pipeline all will be arranged protection mechanism to avoid occurring above-mentioned situation.The effect of the protection mechanism arranged is, when starting valve breaks down, this protection mechanism is opened and in time by emptying for High Temperature High Pressure air, in case there is explosion risk, effectively reduced the percussion to main starting valve.The way that installation protection mechanism is relatively commonly used is that on the air inlet pipeline of each cylinder, install a flame-retardant device, this flame-retardant device can play certain cooling, decompression.But the shortcoming of this way is, the pipeline of each inlet casing needs install flame-retardant device, and be subject to the restriction in marine diesel engine space, installation and the maintenance of numerous flame-retardant device are all not too convenient, and cost is high; In addition, flame-retardant device can play effect of easing stress to the unexpected reflux gas produced, and in normal operation, and time starting air flows through flame-retardant device, crushing is equally also very large, thus causes the waste of energy, reduces the Economy of diesel engine.
Summary of the invention
The object of the invention is to, overcome the deficiency of existing flame-retardant device, a kind of marine diesel engine air duct one-way non-return device is provided, after being arranged on the main starting valve of marine diesel engine air actuation main pipe rail, when cylinder cap starting valve breaks down, reflux gas can be stoped to enter into main starting valve, to avoid reflux gas to the damaging impact of main starting valve.
For achieving the above object, technical solution of the present invention is as follows:
A kind of marine diesel engine air duct one-way non-return device, is installed in marine diesel engine air actuation main pipe rail, it is characterized in that: described one-way non-return device comprises valve seat, front valve shell and rear valve body;
Front interior cavity is provided with in described front valve shell, rear interior cavity is provided with in described rear valve body, this front interior cavity and rear interior cavity are communicated with the starting air pipe of described air actuation main pipe rail respectively, described front valve shell is mutually permanently connected with the position that described front interior cavity is relative with rear interior cavity with rear valve body, and the opposing side of this front interior cavity and rear interior cavity is provided with groove;
Described valve seat is embedded in described groove, described front interior cavity and rear interior cavity is cut off, and this valve seat is provided with the vent being communicated with this front interior cavity and rear interior cavity; The central authorities of described valve seat have placed bolt, this bolt being positioned at described front interior cavity valve block, Compress Spring and spring seat have been placed successively, one locking nut to be spun on described bolt and to hold out against described spring seat, and described valve block is compressed by this Compress Spring and to be fitted on the outer side surface of described valve seat and to be closed by described vent.
As further improvement, between described bolt and described valve block, be provided with lining, this valve block can slide vertically on described lining.
As further improvement, the outer side surface of described valve seat is zigzag fashion sealing surface, which is provided with the sealing sawtooth of Liang Quan six road projection, is provided with six vents between every two circle sawtooth.
As further improvement, described front valve shell and front-end face rear valve body is respectively equipped with in order to be connected with described starting air pipe and ear end face, this front-end face and ear end face are provided with convex surface for sealing and groove, and are respectively equipped with some tapped holes in order to install connecting bolt.
As further improvement, described rear valve body is provided with to discharge the described rear interior cavity of connection of air and outside manual vent hole.
Compared with prior art, the invention has the beneficial effects as follows:
1, structure is simple, low cost of manufacture;
2, the crushing produced when starting air flows through is little;
3, adopt flange method be arranged on starting air manifold road, easy for installation, take up room little.
Accompanying drawing explanation
Fig. 1 is External view of the present invention.
Fig. 2 is structural representation of the present invention.
Embodiment
Below in conjunction with the drawings and specific embodiments, marine diesel engine air duct one-way non-return device of the present invention is described in further detail, but should limit the scope of the invention with this.
Incorporated by reference to consulting Fig. 1 and Fig. 2, diagram marine diesel engine air duct one-way non-return device is installed in marine diesel engine air actuation main pipe rail, described one-way non-return device comprises front valve shell 100 and rear valve body 101, together with this front valve shell 100 and rear valve body 101 to be mutually permanently connected by connecting bolt with flange method; The starting air pipe of air actuation main pipe rail is connected to the front-end face 301 of described front valve shell 100 and the ear end face 302 of rear valve body 101, this front-end face 301 and ear end face 302 are evenly distributed with the tapped hole 402 that eight are installed connecting bolt respectively, the flange of described front-end face 301 and ear end face 302 and connected starting air pipe is provided with convex surface for sealing and groove, and the flange of described starting air pipe is fixedly connected with ear end face 302 with described front-end face 301 respectively by connecting bolt.
Refer to the concrete structure figure of Fig. 2 embodiment of the present invention, front interior cavity 203 is provided with in described front valve shell 100, rear interior cavity 204 is provided with in described rear valve body 101, this front valve shell 100 is interconnected with the position that described front interior cavity 203 is relative with rear interior cavity 204 with rear valve body 101, and the opposing side of this front interior cavity 203 and rear interior cavity 204 is equipped with groove.Described front valve shell 100 is provided with the through hole being communicated with described front interior cavity 203 and starting air pipe, and described rear valve body 101 is provided with the through hole that is communicated with described rear interior cavity 204 and starting air pipe and is communicated with the manual vent hole 202 in order to discharge air of described rear interior cavity 204 and outside.
Set in described front interior cavity 203 and the groove on rear interior cavity 204 opposing side and be fixed with valve seat 102, described front interior cavity 203 cuts off with rear interior cavity 204 by this valve seat 102, and is provided with the vent 201 in order to be communicated with described front interior cavity 203 and rear interior cavity 204 of this valve seat 102 through.Described valve seat 102 is cylindrical body, its central authorities have placed bolt 107, this bolt 107 being positioned at described front interior cavity 203 has placed valve block 103 successively, Compress Spring 104 and spring seat 105, one locking nut 106 to be spun on described bolt 107 and to hold out against described spring seat 105, described valve block 103 to be compressed by this spring seat 105 and Compress Spring 104 and to be fitted on the outer side surface of described valve seat 102 and to be closed by described vent 201 by described locking nut 106, this outer side surface is zigzag fashion sealing surface, plane is provided with the sealing sawtooth of Liang Quan six road projection, six vents are provided with between every two circle sawtooth.
Between the periphery and the center hole of described valve block 103 of described bolt 107, be provided with lining 108, the both ends of the surface of this lining 108 contact with valve seat 102 with described spring seat 105 respectively; Described valve block 103 can slide vertically on described lining 108.
The working principle of marine diesel engine air duct one-way non-return device of the present invention is as follows:
Under normal state, under the spring-force driven dual of Compress Spring 104, the sealing saw face of valve block 103 and valve seat 102 outer side surface, one-way non-return device is in closed condition.Starting air is by after main starting valve, the rear interior cavity 204 of rear valve body 101 is entered by marine diesel engine air actuation main pipe rail, then starting air overcomes the pressure of Compress Spring 104 pairs of valve blocks 103, valve block 103 is promoted along lining 108 forward slip by the vent 201 on valve seat 102, thus back down the front interior cavity 203 that valve block 103 enters front valve shell 100, in the starting air pipe that starting air and then enter is connected with front interior cavity 203, be assigned to each cylinder.Be back in air header when there being pressurized gas in cylinder, and reflux gas pressure is when being greater than starting air pressure, under the acting in conjunction of the gas pressure that valve block 103 is subject to and Compress Spring 104 spring force, the sealing saw face of valve block 103 and valve seat 102, get back to initial closed condition, thus stop the pressurized gas of backflow to flow in main starting valve by rear interior cavity 204, avoid the impact failure of pressurized gas to main starting valve.
Be more than a best embodiment of the present invention, can not limit the scope of the invention with this.What protection scope of the present invention also comprised other is apparent conversion for those skilled in the art and substitutes.

Claims (5)

1. a marine diesel engine air duct one-way non-return device, is installed in marine diesel engine air actuation main pipe rail, it is characterized in that: described one-way non-return device comprises valve seat, front valve shell and rear valve body;
Front interior cavity is provided with in described front valve shell, rear interior cavity is provided with in described rear valve body, this front interior cavity and rear interior cavity are communicated with the starting air pipe of described air actuation main pipe rail respectively, described front valve shell is mutually permanently connected with the position that described front interior cavity is relative with rear interior cavity with rear valve body, and the opposing side of this front interior cavity and rear interior cavity is provided with groove;
Described valve seat is embedded in described groove, described front interior cavity and rear interior cavity is cut off, and this valve seat is provided with the vent being communicated with this front interior cavity and rear interior cavity; The central authorities of described valve seat have placed bolt, this bolt being positioned at described front interior cavity valve block, Compress Spring and spring seat have been placed successively, one locking nut to be spun on described bolt and to hold out against described spring seat, and described valve block is compressed by this Compress Spring and to be fitted on the outer side surface of described valve seat and to be closed by described vent.
2. marine diesel engine air duct one-way non-return device according to claim 1, it is characterized in that: between described bolt and described valve block, be provided with lining, this valve block can slide vertically on described lining.
3. marine diesel engine air duct one-way non-return device according to claim 1 and 2, it is characterized in that: the outer side surface of described valve seat is zigzag fashion sealing surface, which is provided with the sealing sawtooth of Liang Quan six road projection, between every two circle sawtooth, be provided with six vents.
4. marine diesel engine air duct one-way non-return device according to claim 1 and 2, it is characterized in that: described front valve shell and front-end face rear valve body is respectively equipped with in order to be connected with described starting air pipe and ear end face, this front-end face and ear end face are provided with convex surface for sealing and groove, and are respectively equipped with some tapped holes in order to install connecting bolt.
5. marine diesel engine air duct one-way non-return device according to claim 1 and 2, is characterized in that: described rear valve body is provided with to discharge the described rear interior cavity of connection of air and outside manual vent hole.
CN201510025284.4A 2015-01-19 2015-01-19 One-way check device for marine diesel engine air pipe Pending CN104595536A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510025284.4A CN104595536A (en) 2015-01-19 2015-01-19 One-way check device for marine diesel engine air pipe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510025284.4A CN104595536A (en) 2015-01-19 2015-01-19 One-way check device for marine diesel engine air pipe

Publications (1)

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CN104595536A true CN104595536A (en) 2015-05-06

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106090958A (en) * 2016-08-26 2016-11-09 湖北省端胜实业有限公司 Non-return ash valve for acoustic wave ash ejector
CN106246963A (en) * 2016-08-26 2016-12-21 赛洛克流体设备成都有限公司 A kind of check valve being applicable to ultralow temperature medium
CN106246960A (en) * 2016-08-29 2016-12-21 赛洛克流体设备成都有限公司 A kind of check valve being applicable to high-corrosion medium
CN106402435A (en) * 2016-08-29 2017-02-15 赛洛克流体设备成都有限公司 Check valve suitable for ultralow temperature
CN109114266A (en) * 2018-10-15 2019-01-01 盐城项果科技有限公司 Check valve
CN113586305A (en) * 2021-09-16 2021-11-02 中国北方发动机研究所(天津) Air distributor of diesel engine

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3042292A1 (en) * 1979-11-12 1981-05-21 Nova-Werke AG, Effretikon AIR STARTER FOR PISTON ENGINE
CN86107583A (en) * 1985-11-05 1987-11-04 奥格斯堡·纽伦堡机械公司伯迈斯特与韦恩柴油机分公司 The control air distributor of reversible combustion engine
SU1390428A1 (en) * 1986-09-08 1988-04-23 Горьковский Институт Инженеров Водного Транспорта Device for starting and reversing multicylinder internal combustion engine
CN2556447Y (en) * 2002-07-19 2003-06-18 北京嘉润恒水务投资有限公司 Reducing check valve
CN102459851A (en) * 2009-05-07 2012-05-16 Avl里斯脱有限公司 Method for starting an internal combustion engine operating with combustible gas
CN202302129U (en) * 2011-10-18 2012-07-04 江阴市长龄机械制造有限公司 Check valve with flanges
CN204592442U (en) * 2015-01-19 2015-08-26 沪东重机有限公司 A kind of marine diesel engine air duct one-way non-return device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3042292A1 (en) * 1979-11-12 1981-05-21 Nova-Werke AG, Effretikon AIR STARTER FOR PISTON ENGINE
CN86107583A (en) * 1985-11-05 1987-11-04 奥格斯堡·纽伦堡机械公司伯迈斯特与韦恩柴油机分公司 The control air distributor of reversible combustion engine
SU1390428A1 (en) * 1986-09-08 1988-04-23 Горьковский Институт Инженеров Водного Транспорта Device for starting and reversing multicylinder internal combustion engine
CN2556447Y (en) * 2002-07-19 2003-06-18 北京嘉润恒水务投资有限公司 Reducing check valve
CN102459851A (en) * 2009-05-07 2012-05-16 Avl里斯脱有限公司 Method for starting an internal combustion engine operating with combustible gas
CN202302129U (en) * 2011-10-18 2012-07-04 江阴市长龄机械制造有限公司 Check valve with flanges
CN204592442U (en) * 2015-01-19 2015-08-26 沪东重机有限公司 A kind of marine diesel engine air duct one-way non-return device

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106090958A (en) * 2016-08-26 2016-11-09 湖北省端胜实业有限公司 Non-return ash valve for acoustic wave ash ejector
CN106246963A (en) * 2016-08-26 2016-12-21 赛洛克流体设备成都有限公司 A kind of check valve being applicable to ultralow temperature medium
CN106090958B (en) * 2016-08-26 2018-10-12 湖北省端胜实业有限公司 Non-return ash valve for acoustic wave ash ejector
CN106246960A (en) * 2016-08-29 2016-12-21 赛洛克流体设备成都有限公司 A kind of check valve being applicable to high-corrosion medium
CN106402435A (en) * 2016-08-29 2017-02-15 赛洛克流体设备成都有限公司 Check valve suitable for ultralow temperature
CN109114266A (en) * 2018-10-15 2019-01-01 盐城项果科技有限公司 Check valve
CN113586305A (en) * 2021-09-16 2021-11-02 中国北方发动机研究所(天津) Air distributor of diesel engine

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Application publication date: 20150506