CN209510491U - Turbocharger tube - Google Patents

Turbocharger tube Download PDF

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Publication number
CN209510491U
CN209510491U CN201920052709.4U CN201920052709U CN209510491U CN 209510491 U CN209510491 U CN 209510491U CN 201920052709 U CN201920052709 U CN 201920052709U CN 209510491 U CN209510491 U CN 209510491U
Authority
CN
China
Prior art keywords
surrounding edge
wall
big
small
interface position
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
CN201920052709.4U
Other languages
Chinese (zh)
Inventor
林磊
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.)
Ruian Tongda Electrical Accessories Factory
Original Assignee
Ruian Tongda Electrical 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 Ruian Tongda Electrical Accessories Factory filed Critical Ruian Tongda Electrical Accessories Factory
Priority to CN201920052709.4U priority Critical patent/CN209510491U/en
Application granted granted Critical
Publication of CN209510491U publication Critical patent/CN209510491U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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

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  • Supercharger (AREA)

Abstract

The utility model discloses a kind of turbocharger tubes, including tube body, one end of tube body is equipped with interface position, interface position includes the big surrounding edge and small surrounding edge of arc, the side mouth of small surrounding edge and the side mouth of big surrounding edge are intersected, connected between big surrounding edge and the side mouth of small surrounding edge by connection strap, the convex wall of arc is convexly equipped on the inner wall of big surrounding edge, the inner wall of the side wall of the convex wall and small surrounding edge forms circular running-on, the both ends of convex wall pass through telescopic strap respectively and are connected with the side opening end of small surrounding edge, are also arranged with clip on interface position.The telescopic technical effect of nozzle bore is just reached in this way, so that applicability is wider, has been connected to improve from different engines.

Description

Turbocharger tube
Technical field
The utility model relates to the accessories in a kind of automobile engine, and in particular to a kind of turbocharger tube.
Background technique
Engine turbine pressurization principle be in the identical unit time, can be the mixing of more air and fuel oil Gas pressure, which squeezes into cylinder and carries out compression, fires movement, and bigger compared with natural intake engine move just can be generated under identical revolving speed Power output.In general, engine can promote 30%-40%'s after the movement for cooperating such a " forcing air inlet " at least Extra power.Obtain perfect efficiency of combustion and power allowed to significantly improve, be exactly turbo charge system can be provided to Where the maximum value of vehicle.Turbocharger tube is the air scoop section for being connected to engine, and whirlpool during being linked and packed Wheel pressure inlet will be connected in the air inlet pipe road junction of engine, since turbocharger tube can generate error sometimes mouth in production Diameter can cannot be matched with engine, be easy to cause the turbocharger tube of production to generate and scrapped, moreover the end mouthful of turbocharger tube Diameter is that fixation can only be connect with the engine to match, and applicability is lower.
Summary of the invention
To solve the above problems, the purpose of this utility model is to provide a kind of telescopic turbochargings of nozzle bore Pipe connects to improve from different engines so that applicability is wider.
To achieve the above object, the utility model provides following technical solution: a kind of turbocharger tube, including tube body, One end of the tube body is equipped with interface position, and the interface position includes the big surrounding edge and small surrounding edge of arc, the small surrounding edge Side mouth and the big surrounding edge side mouth intersect, pass through between the big surrounding edge and the side mouth of the small surrounding edge One connection strap connects, and the convex wall of arc, the side wall of the convex wall and the small surrounding edge are convexly equipped on the inner wall of the big surrounding edge Inner wall forms circular running-on, and the both ends of the convex wall pass through a telescopic strap respectively and are connected with the side opening end of the small surrounding edge It connects, is also arranged with clip on the interface position.
The two sides side wall of the telescopic strap is respectively equipped with the flexible groove of dentation.
The defining flange of annular is additionally provided between the tube body and the interface position.
This structure of the utility model, big surrounding edge and small surrounding edge are formed by running-on and are realized by connection strap and telescopic strap The flexible adjustment of the size of bore, the spy for having telescopicing performance bigger compared to the elastic telescopic of conventional turbine pressure inlet rubber material Point is able to satisfy the biggish connectivity port of size range, is suitable for more engine model, improves being applicable in for turbocharger tube Property, just reach the telescopic technical effect of nozzle bore in this way, so that applicability is wider, has connected to improve from different engines It connects.
The utility model is further described with reference to the accompanying drawings and detailed description.
Detailed description of the invention
Fig. 1 is the perspective view of specific embodiment of the present invention.
Specific embodiment
The utility model is specifically described below by embodiment, is served only for carrying out the utility model further Illustrate, should not be understood as the restriction to scope of protection of the utility model.
As shown in Figure 1, present embodiment discloses a kind of turbocharger tube, including tube body 1, one end of tube body 1 are equipped with interface Position 2, is additionally provided with the defining flange 3 of annular between tube body 1 and interface position 2, and interface position 2 includes the big surrounding edge 21 of arc With small surrounding edge 22, the side mouth of small surrounding edge 22 and the side mouth of big surrounding edge 21 are intersected, the side of big surrounding edge 21 and small surrounding edge 22 Connected between portion's opening by connection strap 23, the convex wall 211 of arc is convexly equipped on the inner wall of big surrounding edge 21, the convex wall 211 The inner wall of side wall and small surrounding edge 22 forms circular running-on 4, and the both ends of convex wall 211 pass through a telescopic strap 24 and small surrounding edge 22 respectively Side opening end be connected, the two sides side wall of the telescopic strap 24 is respectively equipped with the flexible groove of dentation, telescopic strap 24 is turned up Telescopicing performance, while clip 5 is also arranged on interface position 2.
Through the above technical solutions, big surrounding edge 21 and small surrounding edge 22, which are formed by running-on 4, passes through connection strap 23 and telescopic strap 24 realize the flexible adjustment of the size of bore, have telescopicing performance bigger compared to the elastic telescopic of conventional turbine pressure inlet rubber material The characteristics of, it is able to satisfy the biggish connectivity port of size range, is suitable for more engine model, improves the suitable of turbocharger tube With property, the telescopic technical effect of nozzle bore is just reached in this way, so that applicability is wider, to improve and different engines Connection.

Claims (3)

1. one end of a kind of turbocharger tube, including tube body, the tube body is equipped with interface position, it is characterised in that: described connects Oral area position includes the big surrounding edge and small surrounding edge of arc, the side mouth friendship of the side mouth of the small surrounding edge and the big surrounding edge Fork, is connected between the big surrounding edge and the side mouth of the small surrounding edge by a connection strap, on the inner wall of the big surrounding edge It is convexly equipped with the convex wall of arc, the side wall of the convex wall and the inner wall of the small surrounding edge form circular running-on, the both ends of the convex wall It is connected respectively by a telescopic strap with the side opening end of the small surrounding edge, is also arranged with clip on the interface position.
2. turbocharger tube according to claim 1, it is characterised in that: the two sides side wall of the telescopic strap is respectively equipped with tooth The flexible groove of shape.
3. turbocharger tube according to claim 2, it is characterised in that: between the tube body and the interface position It is additionally provided with the defining flange of annular.
CN201920052709.4U 2019-01-14 2019-01-14 Turbocharger tube Expired - Fee Related CN209510491U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920052709.4U CN209510491U (en) 2019-01-14 2019-01-14 Turbocharger tube

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920052709.4U CN209510491U (en) 2019-01-14 2019-01-14 Turbocharger tube

Publications (1)

Publication Number Publication Date
CN209510491U true CN209510491U (en) 2019-10-18

Family

ID=68200569

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920052709.4U Expired - Fee Related CN209510491U (en) 2019-01-14 2019-01-14 Turbocharger tube

Country Status (1)

Country Link
CN (1) CN209510491U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
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: 20191018

Termination date: 20210114