CN207673404U - A kind of enging cabin exhaust apparatus - Google Patents

A kind of enging cabin exhaust apparatus Download PDF

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Publication number
CN207673404U
CN207673404U CN201721324153.7U CN201721324153U CN207673404U CN 207673404 U CN207673404 U CN 207673404U CN 201721324153 U CN201721324153 U CN 201721324153U CN 207673404 U CN207673404 U CN 207673404U
Authority
CN
China
Prior art keywords
fuselage
enging cabin
exhaust apparatus
box body
cabin exhaust
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.)
Expired - Fee Related
Application number
CN201721324153.7U
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Chinese (zh)
Inventor
董金燕
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chongqing Jialing-Jiapeng Industrial Co., Ltd.
Original Assignee
Xinchang Chengtan Town Xicchuang Machinery And Accessories Factory
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 Xinchang Chengtan Town Xicchuang Machinery And Accessories Factory filed Critical Xinchang Chengtan Town Xicchuang Machinery And Accessories Factory
Priority to CN201721324153.7U priority Critical patent/CN207673404U/en
Application granted granted Critical
Publication of CN207673404U publication Critical patent/CN207673404U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of enging cabin exhaust apparatus, its structure includes motor, fuselage, radiator-grid, gas outlet, clarifier, exhaust pipe, nut, disk, regulating valve, connector, the fuselage is V-configuration, it is divided into part and lower part, motor is equipped in the fuselage, the back divides the radiator-grid of left side welded mesh trellis, the exhaust pipe set altogether there are three and it is equilateral in the same size, extend through and be connected in back.A kind of enging cabin exhaust apparatus of the utility model, equipped with clarifier, start filter by the switch knob in clarifier, the pernicious gas of enging cabin exhaust apparatus discharge is accurately filtered, pernicious gas is set to be filtered into clean oxygen, it avoids the pernicious gas that enging cabin exhaust apparatus is discharged that from seriously polluteing the air of ambient enviroment, causes the plant of ambient enviroment to be easy death, ensure that the survival rate of ambient enviroment plant.

Description

A kind of enging cabin exhaust apparatus
Technical field
The utility model is a kind of enging cabin exhaust apparatus, belongs to exhaust equipment field.
Background technology
Exhaust apparatus refers to loaded on after turbine exhaust cylinder, exhaust gas to be discharged to and be had the effects that the device of cooling, noise reduction.
Prior art discloses application No. is:A kind of enging cabin exhaust apparatus of CN201220655647.4, including hair Motivation, enging cabin, exhaust pipe;Engine is installed in enging cabin, and engine includes exhaust emission suction system, and feature exists In the import of exhaust pipe is connected to enging cabin, and the outlet of exhaust pipe is communicated with the external world, the outlet and exhaust of exhaust emission suction system The import of pipe is aligned, and the hot-air in the exhaust gas and enging cabin of engine is extraneous by exhaust pipe flow direction.But its deficiency The air of ambient enviroment can seriously be polluteed by being in the pernicious gas being discharged in enging cabin exhaust apparatus, lead to ambient enviroment Plant is easy death.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of enging cabin exhaust apparatus, with solution The pernicious gas of certainly existing enging cabin exhaust apparatus discharge can seriously pollute the air of ambient enviroment, lead to ambient enviroment Plant be easy dead problem.
To achieve the goals above, the utility model is to realize by the following technical solutions:A kind of enging cabin row Device of air, structure include motor, fuselage, radiator-grid, gas outlet, clarifier, exhaust pipe, nut, disk, regulating valve, connection Part, the fuselage are V-configuration, are divided into part and lower part, and motor, a back point left side are equipped in the fuselage The radiator-grid of side welded mesh trellis, the exhaust pipe set altogether there are three and it is equilateral in the same size, extend through and be connected to fuselage In top, the gas outlet of the exhaust pipe front end welding hollow circular, the exhaust inner tube layer lower middle portion welds clarifier, institute It states underbelly point to be integrated with connector, disk front surface is welded in the connector bottom, and the nut passes through spiral shell Line, which forward rotates, is embedded into disk internal layer, and totally two, nut, and the connector middle-end is coordinated with rotating regulation valve using transition; The clarifier is by box body, motor, filter, air inlet and outlet, switch knob, operation panel, indicator lamp groups at the box The body internal layer lower right corner is equipped with motor, and the both ends of the latticed filter in the internal layer center are separately connected the internal layer of box body, described Box body left side is through connection hollow air inlet, the air outlet of the box body front surface epimere welded mesh trellis, the box body top Operation panel bottom is welded in portion, and a half part of three indicator lights is respectively embedded in the inside of operation panel, the behaviour Make panel surface and be equipped with switch knob, switch knob is circle, radius 1cm.
Further, the exhaust pipe integral cylinder structure, section are rectangle.
Further, the upper part of the fuselage and lower part are in 75 ° of angles.
Further, the back divides bottom end welded connections 10.
Further, the nut is circle, and radius 0.5cm is equipped with two altogether.
Further, gas outlet there are three being set on the back point top.
Further, there are four the indicator light is set altogether, be set to low pollution indicator light, intermediate pollution indicator light, Highly polluted indicator light, superelevation pollute indicator light.
Advantageous effect
A kind of enging cabin exhaust apparatus of the utility model is equipped with clarifier, was started by the switch knob in clarifier Filter accurately filters the pernicious gas of enging cabin exhaust apparatus discharge, pernicious gas is made to be filtered into clean oxygen, It avoids the pernicious gas that enging cabin exhaust apparatus is discharged that from seriously polluteing the air of ambient enviroment, leads to the plant of ambient enviroment Object is easy death, ensures that the survival rate of ambient enviroment plant.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of enging cabin exhaust apparatus of the utility model;
Fig. 2 is the clarifier schematic diagram of the utility model;
Fig. 3 is a kind of connector schematic diagram of enging cabin exhaust apparatus of the utility model.
In figure:Motor -1, fuselage -2, radiator-grid -3, gas outlet -4, clarifier -5, box body -501, motor -502, filtering Device -503, air inlet -504, air outlet -505, switch knob -506, operation panel -507, indicator light -508, exhaust pipe -6, spiral shell Mother -7, disk -8, regulating valve -9, connector -10.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below In conjunction with specific implementation mode, the utility model is expanded on further.
- Fig. 3 is please referred to Fig.1, the utility model provides a kind of technical solution:A kind of enging cabin exhaust apparatus, structure Including motor 1, fuselage 2, radiator-grid 3, gas outlet 4, clarifier 5, exhaust pipe 6, nut 7, disk 8, regulating valve 9, connector 10, The fuselage 2 is V-configuration, is divided into part and lower part, is equipped with motor 1 in the fuselage 2, part on the fuselage 2 The radiator-grid 3 of left side welded mesh trellis, the exhaust pipe 6 set altogether there are three and it is equilateral in the same size, extend through and be connected to In 2 top of fuselage, the gas outlet 4 of hollow circular, the welding of 6 internal layer lower middle portion of the exhaust pipe are welded in 6 front end of the exhaust pipe Clarifier 5,2 lower part of the fuselage are integrated with connector 10, and table before disk 8 is welded in 10 bottom of the connector Face, the nut 7 is forward rotated by screw thread is embedded into 8 internal layer of disk, and totally two, nut 7,10 middle-end of the connector with Rotating regulation valve 9 is coordinated using transition;The clarifier 5 is by box body 501, motor 502, filter 503, air inlet 504, outlet air Mouth 505, switch knob 506, operation panel 507, indicator light 508 form, and the 501 internal layer lower right corner of the box body is equipped with motor 502, The both ends of the latticed filter 503 in the internal layer center are separately connected the internal layer of box body 501, and 501 left side of the box body is passed through Connection hollow air inlet 504 is worn, the air outlet 505 of 501 front surface epimere welded mesh trellis of the box body, the box body 501 is pushed up 507 bottom of operation panel is welded in portion, and a half part of three indicator lights 508 is respectively embedded in the inside of operation panel 507 In, 507 surface of the operation panel is equipped with switch knob 506, and switch knob 506 is circle, radius 1cm.
There is filter 503 described in this patent filtering function, the indicator light 508 can show the pollution of pernicious gas Degree.
It is carrying out in use, exhaust pipe 6 is used to connect clarifier 5 first, filter 503 has filtering function, the finger Show that lamp 508 can show the dustiness of pernicious gas, filter 503 is started by the switch knob 506 in clarifier 5, to starting The pernicious gas of cabin exhaust apparatus discharge is accurately filtered, and so that pernicious gas is filtered into clean oxygen, is avoided engine The pernicious gas of cabin exhaust apparatus discharge can seriously pollute the air of ambient enviroment, cause the plant of ambient enviroment to be easy dead It dies, ensures that the survival rate of ambient enviroment plant.
It is the pernicious gas that enging cabin exhaust apparatus is discharged that the utility model, which solves the problems, such as, can seriously pollute surrounding The air of environment causes the plant of ambient enviroment to be easy death, and the utility model is combined with each other by above-mentioned component, by net The switch knob changed in device starts filter, is accurately filtered to the pernicious gas of enging cabin exhaust apparatus discharge, makes to be harmful to Gas filtration avoids the pernicious gas that enging cabin exhaust apparatus is discharged that from seriously polluteing ambient enviroment at clean oxygen Air causes the plant of ambient enviroment to be easy death, ensures that the survival rate of ambient enviroment plant.It is described in detail below:
The clarifier 5 by box body 501, motor 502, filter 503, air inlet 504, air outlet 505, switch knob 506, Operation panel 507, indicator light 508 form, and the 501 internal layer lower right corner of the box body is equipped with motor 502, the grid in the internal layer center The both ends of shape filter 503 are separately connected the internal layer of box body 501, and 501 left side of the box body is through connection hollow air inlet 504, operation panel 507 is welded at the air outlet 505 of 501 front surface epimere welded mesh trellis of the box body, 501 top of the box body One half part of bottom, three indicator lights 508 is respectively embedded in the inside of operation panel 507, the operation panel 507 Surface is equipped with switch knob 506, and switch knob 506 is circle, radius 1cm.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiment being appreciated that.

Claims (6)

1. a kind of enging cabin exhaust apparatus, structure includes motor (1), fuselage (2), radiator-grid (3), gas outlet (4), purification Device (5), exhaust pipe (6), nut (7), disk (8), regulating valve (9), connector (10), the fuselage (2) are V-configuration, altogether It is divided into part and lower part, is equipped with motor (1) in the fuselage (2), part left side welded mesh trellis on the fuselage (2) Radiator-grid (3), the exhaust pipe (6) set altogether there are three and it is equilateral in the same size, extend through and be connected to fuselage (2) top It is interior, it is characterised in that:
The gas outlet (4) of exhaust pipe (6) the front end welding hollow circular, exhaust pipe (6) the internal layer lower middle portion welding are net Change device (5), fuselage (2) lower part is integrated with connector (10), and disk is welded in connector (10) bottom (8) front surface, the nut (7) is forward rotated by screw thread is embedded into disk (8) internal layer, and totally two, nut (7), the company Fitting (10) middle-end is coordinated with rotating regulation valve (9) using transition;
The clarifier (5) by box body (501), motor (502), filter (503), air inlet (504), air outlet (505), open Button (506), operation panel (507), indicator light (508) composition are closed, box body (501) the internal layer lower right corner is equipped with motor (502), The both ends of the latticed filter (503) in the internal layer center are separately connected the internal layer of box body (501), and the box body (501) is left Side is through connection hollow air inlet (504), the air outlet (505) of box body (501) the front surface epimere welded mesh trellis, institute It states and welds operation panel (507) bottom at the top of box body (501), a half part of three indicator lights (508) is respectively embedded in In the inside of operation panel (507), operation panel (507) surface is equipped with switch knob (506), and switch knob (506) is circle Shape, radius 1cm.
2. a kind of enging cabin exhaust apparatus according to claim 1, it is characterised in that:The exhaust pipe (6) is integrally round Column structure, section are rectangle.
3. a kind of enging cabin exhaust apparatus according to claim 1, it is characterised in that:The upper part of the fuselage (2) It is in 75 ° of angles with lower part.
4. a kind of enging cabin exhaust apparatus according to claim 1, it is characterised in that:Part bottom on the fuselage (2) Hold welded connections (10).
5. a kind of enging cabin exhaust apparatus according to claim 1, it is characterised in that:The nut (7) is circle, partly Diameter is 0.5cm, is equipped with two altogether.
6. a kind of enging cabin exhaust apparatus according to claim 1, it is characterised in that:It is partly pushed up on the fuselage (2) Gas outlet (4) there are three being set on end.
CN201721324153.7U 2017-10-16 2017-10-16 A kind of enging cabin exhaust apparatus Expired - Fee Related CN207673404U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721324153.7U CN207673404U (en) 2017-10-16 2017-10-16 A kind of enging cabin exhaust apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721324153.7U CN207673404U (en) 2017-10-16 2017-10-16 A kind of enging cabin exhaust apparatus

Publications (1)

Publication Number Publication Date
CN207673404U true CN207673404U (en) 2018-07-31

Family

ID=62953337

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721324153.7U Expired - Fee Related CN207673404U (en) 2017-10-16 2017-10-16 A kind of enging cabin exhaust apparatus

Country Status (1)

Country Link
CN (1) CN207673404U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20190411

Address after: 400033 Shapingba District Jingkou Industrial Park, Chongqing

Patentee after: Chongqing Jialing-Jiapeng Industrial Co., Ltd.

Address before: 312500 4, 32 (1) Jiao Cheng Road, Chengtan Town, Xinchang, Shaoxing, Zhejiang.

Patentee before: Xinchang Chengtan Town, xicchuang machinery and accessories factory

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180731

Termination date: 20191016