CN205477777U - Turbo charger spiral case - Google Patents

Turbo charger spiral case Download PDF

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Publication number
CN205477777U
CN205477777U CN201620231545.8U CN201620231545U CN205477777U CN 205477777 U CN205477777 U CN 205477777U CN 201620231545 U CN201620231545 U CN 201620231545U CN 205477777 U CN205477777 U CN 205477777U
Authority
CN
China
Prior art keywords
intake channel
cavity
cooling cavities
cooling
channel
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
CN201620231545.8U
Other languages
Chinese (zh)
Inventor
汤俊
韩青
曹红艳
胡兵
陆仁杰
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.)
Jiangsu Suotepower Engineering Co Ltd
Original Assignee
Jiangsu Suotepower Engineering 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 Jiangsu Suotepower Engineering Co Ltd filed Critical Jiangsu Suotepower Engineering Co Ltd
Priority to CN201620231545.8U priority Critical patent/CN205477777U/en
Application granted granted Critical
Publication of CN205477777U publication Critical patent/CN205477777U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The utility model relates to a turbo charger spiral case, including casing body, casing body on offered an intake channel, the 2nd intake channel, the 3rd intake channel, the first route of giving vent to anger, second give vent to anger route, cooling cavity, cooling agent route and engine mounting cavity, an intake channel and the 2nd intake channel's one end be linked together, the 2nd intake channel the other end with the cooling cavity be linked together, the cooling cavity be linked together through the 3rd intake channel and engine mounting cavity, the cooling agent route with the cooling cavity be linked together, the second give vent to anger the route and be linked together through first route and the engine mounting cavity of giving vent to anger, casing body on still seted up the branch road that admits air, admit air branch road and an intake channel be linked together, the branch road that admits air in be provided with solenoid valve installation cavity. This design has simple structure, easily makes and practical efficient advantage.

Description

A kind of turbocharger volute
Technical field
This utility model relates to turbo-charger technical field, particularly a kind of turbocharger volute.
Background technology
Turbocharger is used for improving the efficiency of internal combustion engine, obtains waste gas stream by turbine in turbocharger Kinetic energy and the kinetic energy of waste gas stream via the axle of turbine and the common mistake of compressor for air fuel is mixed Compound press-in internal combustion engine.The fixing work of internal combustion engine can be filled by this way with larger amount of mixture Volume, thus can realize bigger lift when burning and therefore realize bigger engine power.
The axle of turbocharger generally by sliding supported condition in turbocharger housing, thus just exist A large amount of frictional energies of hot form at release in the bearing receiving portion of turbocharger housing, existing turbine increases Although the housing of depressor is by pouring the preferable heat conductivity that has that metal constitutes, but costly, improves and produce Cost.
Summary of the invention
This utility model technical issues that need to address are by arranging helical form cooling tube in cooling cavities Extend the gases at high pressure time in cooling cavities, make that coolant contacts with gases at high pressure more fully, from And ensure that temperature when gases at high pressure temperature enters in electromotor meets the requirements;A kind of turbocharger is provided Spiral case.
For solving above-mentioned technical problem, structure of the present utility model includes chassis body, described casing master Offer on body the first intake channel, the second intake channel, the 3rd intake channel, the first air outlet passage, Two air outlet passage, cooling cavities, coolant channel and electromotor install cavity, the first described intake channel Being connected with one end of the second intake channel, the other end of the second described intake channel is connected with cooling cavities Logical, described cooling cavities is installed cavity by the 3rd intake channel with electromotor and is connected, described cooling Agent path is connected with cooling cavities, and the second described air outlet passage is pacified with electromotor by the first air outlet passage Body of behaveing affectedly is connected, and described chassis body is further opened with air inlet branch road, described air inlet branch road and first Intake channel is connected, and is provided with electromagnetic valve and installs cavity in described air inlet branch road.
Further: compressor impeller, the second described air outlet passage are installed in the first described intake channel Turbine wheel, described compressor impeller and turbine wheel coaxial linkage are inside installed.
Further: described cooling cavities is rectangle hollow cavity, the both sides of described cooling cavities are respectively opened Being provided with a through hole, described cooling cavities is connected with coolant channel by the through hole of both sides, described Being provided with helical form cooling tube in cooling cavities, the two ends of described helical form cooling tube are through cooling cavities Sidewall is connected with the second intake channel and the 3rd intake channel respectively.
After using said structure, this utility model extends by arranging helical form cooling tube in cooling cavities The gases at high pressure time in cooling cavities, make that coolant contacts with gases at high pressure is more abundant, thus really Protect temperature when gases at high pressure temperature enters in electromotor to meet the requirements;And the design also has structure letter Single, the easily fabricated and advantage of practicality and high efficiency.
Accompanying drawing explanation
With detailed description of the invention, this utility model is described in further detail below in conjunction with the accompanying drawings.
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the structural representation of cooling cavities.
Detailed description of the invention
A kind of turbocharger volute as shown in Figure 1, including chassis body 1, on described chassis body 1 Offer first intake channel the 2, second intake channel the 3, the 3rd intake channel the 4, first air outlet passage 5, Second air outlet passage 6, cooling cavities 9, coolant channel 7 and electromotor install cavity 10, described first Intake channel 2 is connected with one end of the second intake channel 3, the other end of the second described intake channel 3 Being connected with cooling cavities 9, described cooling cavities 9 is by the 3rd intake channel 4 and electromotor installation cavity Body 10 is connected, and described coolant channel 7 is connected with cooling cavities 9, the second described air outlet passage 6 install cavity 10 by the first air outlet passage 5 with electromotor is connected, and described chassis body 1 is also opened Being provided with air inlet branch road 8, described air inlet branch road 8 is connected with the first intake channel 2, described air inlet branch road It is provided with electromagnetic valve in 8 and cavity 11 is installed, in the first described intake channel 2, compressor impeller 12 is installed, Turbine wheel 13, described compressor impeller 12 and turbine are installed in the second described air outlet passage 6 Impeller 13 coaxial linkage, the design also has simple in construction, the easily fabricated and advantage of practicality and high efficiency.
Cooling cavities 9 as shown in Figure 2 is rectangle hollow cavity, and the both sides of described cooling cavities 9 are respectively opened Being provided with a through hole 16, described cooling cavities 9 is connected with coolant channel 7 by the through hole 16 of both sides, Being provided with helical form cooling tube 15 in described cooling cavities 9, the two ends of described helical form cooling tube 15 are worn The sidewall of supercooling cavity 9 is connected with the second intake channel 3 and the 3rd intake channel 4 respectively.This practicality Novel by arrange in cooling cavities helical form cooling tube extend gases at high pressure in cooling cavities time Between, make that coolant contacts with gases at high pressure is more abundant, ensures that gases at high pressure temperature enters and starts Temperature time in machine meets the requirements.

Claims (3)

1. a turbocharger volute, including chassis body (1), it is characterised in that: described casing master Offer on body (1) the first intake channel (2), the second intake channel (3), the 3rd intake channel (4), First air outlet passage (5), the second air outlet passage (6), cooling cavities (9), coolant channel (7) With electromotor, cavity (10), described the first intake channel (2) and the one of the second intake channel (3) are installed End is connected, and the other end of described the second intake channel (3) is connected with cooling cavities (9), described Cooling cavities (9) is installed cavity (10) by the 3rd intake channel (4) with electromotor and is connected, and described is cold But agent path (7) is connected with cooling cavities (9), and described the second air outlet passage (6) is given vent to anger logical by first Road (5) is installed cavity (10) with electromotor and is connected, and described chassis body (1) is further opened with air inlet and props up Road (8), described air inlet branch road (8) is connected with the first intake channel (2), described air inlet branch road (8) Inside it is provided with electromagnetic valve and cavity (11) is installed.
A kind of turbocharger volute the most according to claim 1, it is characterised in that: described first enters Compressor impeller (12) is installed in gas path (2), in described the second air outlet passage (6), turbine is installed Machine impeller (13), described compressor impeller (12) and turbine wheel (13) coaxial linkage.
A kind of turbocharger volute the most according to claim 1, it is characterised in that: described cooling chamber Body (9) is rectangle hollow cavity, and the both sides of described cooling cavities (9) respectively offer a through hole (16), Described cooling cavities (9) is connected with coolant channel (7) by the through hole (16) of both sides, and described is cold But being provided with helical form cooling tube (15) in cavity (9), the two ends of described helical form cooling tube (15) pass The sidewall of cooling cavities (9) is connected with the second intake channel (3) and the 3rd intake channel (4) respectively.
CN201620231545.8U 2016-03-23 2016-03-23 Turbo charger spiral case Expired - Fee Related CN205477777U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620231545.8U CN205477777U (en) 2016-03-23 2016-03-23 Turbo charger spiral case

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620231545.8U CN205477777U (en) 2016-03-23 2016-03-23 Turbo charger spiral case

Publications (1)

Publication Number Publication Date
CN205477777U true CN205477777U (en) 2016-08-17

Family

ID=56652588

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620231545.8U Expired - Fee Related CN205477777U (en) 2016-03-23 2016-03-23 Turbo charger spiral case

Country Status (1)

Country Link
CN (1) CN205477777U (en)

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
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: 20160817