CN204283994U - Turbosupercharger - Google Patents

Turbosupercharger Download PDF

Info

Publication number
CN204283994U
CN204283994U CN201420620628.7U CN201420620628U CN204283994U CN 204283994 U CN204283994 U CN 204283994U CN 201420620628 U CN201420620628 U CN 201420620628U CN 204283994 U CN204283994 U CN 204283994U
Authority
CN
China
Prior art keywords
communicating passage
eduction valve
cavity
pressure stabilizing
hyperbaric chamber
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
CN201420620628.7U
Other languages
Chinese (zh)
Inventor
余志文
焦春辉
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.)
Beijing Treasure Car Co Ltd
Original Assignee
Beiqi Foton Motor 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 Beiqi Foton Motor Co Ltd filed Critical Beiqi Foton Motor Co Ltd
Priority to CN201420620628.7U priority Critical patent/CN204283994U/en
Application granted granted Critical
Publication of CN204283994U publication Critical patent/CN204283994U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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

Abstract

The utility model discloses a kind of turbosupercharger, comprise: housing, housing is formed with suction port and air outlet, eduction valve cavity, hyperbaric chamber and the first communicating passage is limited in housing, eduction valve cavity is communicated with suction port, hyperbaric chamber is communicated with air outlet, first communicating passage is connected between eduction valve cavity and hyperbaric chamber, and wherein the cross-section area of the first communicating passage is configured to reduce gradually along from one end be connected with hyperbaric chamber of the first communicating passage towards the direction of one end be connected with eduction valve cavity of the first communicating passage.According to turbosupercharger of the present utility model, gas flows into the process of relief valve cavity from hyperbaric chamber through the first communicating passage, and flowing velocity increases, pressure reduces, and the obstruction that gas is subject to the wall of eduction valve cavity reduces, and vortex phenomenon reduces, flow more smooth and easy, disappointing noise significantly reduces.

Description

Turbosupercharger
Technical field
The utility model relates to technical field of engines, more specifically, relates to a kind of turbosupercharger.
Background technique
Turbosupercharger is the parts of the most NVH risks such as motor high speed, high temperature, multi-part, running speed be changeable.Turbosupercharger when airspeed change with the change of gas temperature, the fluctuation of pressure and the aerodynamic noise that produces thereupon.Wherein, surge noise is one of main noise of turbosupercharger, and the position that noise produces is different with the form of different pressurized machine and the difference of structure.
In order to the property interval making turbocharger operation characteristic conforms desirable, introduce air inlet aerial drainage mechanism.Gas after unnecessary supercharging is mainly back to the inlet end of turbosupercharger by air inlet aerial drainage mechanism by current by pass, in this process, the air-flow of high pressure-temperature often produces the disappointing noise making people unhappy.
In the related, the communicating passage connecting hyperbaric chamber and eduction valve cavity in air inlet aerial drainage mechanism is formed as the constant cylinder type pipeline of sectional area, and in the boundary layer of wall, gas particle is subject to the obstruction of the frictional force that viscosity causes, and gas flow rate reduces.And after entering eduction valve cavity, gas pressure raises, airspeed further reduces, so that in the local of eduction valve cavity, gas particle easily causes the phenomenon that halts, and simultaneously with the phenomenon that gas is separated with wall, and then forms eddy current, produce unnecessary aerodynamic noise, disappointing noise is larger.The structure of turbosupercharger haves much room for improvement.
Model utility content
The utility model is intended to solve one of technical problem in correlation technique at least to a certain extent.For this reason, the utility model proposes a kind of turbosupercharger, the disappointing noise of described turbosupercharger is little.
According to turbosupercharger of the present utility model, comprise: housing, described housing is formed with suction port and air outlet, eduction valve cavity is limited in described housing, hyperbaric chamber and the first communicating passage, described eduction valve cavity is communicated with described suction port, described hyperbaric chamber is communicated with described air outlet, described first communicating passage is connected between described eduction valve cavity and described hyperbaric chamber, the cross-section area of wherein said first communicating passage is configured to reduce gradually along from one end be connected with described hyperbaric chamber of described first communicating passage towards the direction of one end be connected with described eduction valve cavity of described first communicating passage.
According to turbosupercharger of the present utility model, gas flows into the process of relief valve cavity from hyperbaric chamber through the first communicating passage, flowing velocity increases, gas pressure reduces, the obstruction that gas is subject to the wall of eduction valve cavity reduces, the vortex phenomenon produced reduces, and gas flow is more smooth and easy, and the disappointing noise produced due to pressure rapid fluctuation significantly reduces.
In addition, following additional technical characteristics can also be had according to turbosupercharger of the present utility model:
According to an embodiment of the present utility model, the shape of cross section of described first communicating passage is circular, ellipse, long-round-shape or polygonal.
According to an embodiment of the present utility model, described eduction valve cavity comprises the first pressure stabilizing cavity and the second pressure stabilizing cavity that are connected with each other vertically, the free end of described first pressure stabilizing cavity is connected with described first communicating passage, described eduction valve is located at the side away from described first pressure stabilizing cavity of described second pressure stabilizing cavity, and the cross-section area of described first communicating passage is less than the cross-section area of described first pressure stabilizing cavity.
According to an embodiment of the present utility model, the cross-section area of described first pressure stabilizing cavity is greater than the cross-section area of described second pressure stabilizing cavity.
According to an embodiment of the present utility model, described eduction valve cavity also comprises the second communicating passage, and described second communicating passage is connected between described first pressure stabilizing cavity and described suction port.
According to an embodiment of the present utility model, the cross-section area of the entry end of described second communicating passage is greater than the cross-section area of the outlet end of described second communicating passage.
According to an embodiment of the present utility model, described turbosupercharger also comprises eduction valve, and described eduction valve is located at the side away from described first pressure stabilizing cavity of described second pressure stabilizing cavity, and described eduction valve is used for conducting or cuts off described hyperbaric chamber and described suction port.
According to an embodiment of the present utility model, described eduction valve comprises earial drainage portion, and described earial drainage portion to be located in described eduction valve cavity with conducting movably or to cut off described hyperbaric chamber and described suction port.
Additional aspect of the present utility model and advantage will part provide in the following description, and part will become obvious from the following description, or be recognized by practice of the present utility model.
Accompanying drawing explanation
Fig. 1 is the part-structure schematic diagram of the turbosupercharger according to the utility model embodiment.
Reference character:
Turbosupercharger 100;
Housing 1; Hyperbaric chamber 2; First communicating passage 3; Eduction valve cavity 4; First pressure stabilizing cavity 41; Second pressure stabilizing cavity 42; Second communicating passage 5; Suction port 6; Air outlet 7.
Embodiment
Be described below in detail embodiment of the present utility model, the example of described embodiment is shown in the drawings, and wherein same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the utility model, and can not be interpreted as restriction of the present utility model.
In description of the present utility model, it will be appreciated that, term " " center ", " length ", " width ", " thickness ", " on ", D score, " front ", " afterwards ", " left side ", " right side ", " top ", " end " " interior ", " outward ", " axis ", orientation or the position relationship of the instruction such as " radial direction " are based on orientation shown in the drawings or position relationship, only the utility model and simplified characterization for convenience of description, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as restriction of the present utility model.
In addition, term " first ", " second " only for describing object, and can not be interpreted as instruction or hint relative importance or imply the quantity indicating indicated technical characteristics.Thus, be limited with " first ", the feature of " second " can express or impliedly comprise one or more these features.In description of the present utility model, the implication of " multiple " is two or more, unless otherwise expressly limited specifically.
In the utility model, unless otherwise clearly defined and limited, the term such as term " installation ", " being connected ", " connection ", " fixing " should be interpreted broadly, and such as, can be fixedly connected with, also can be removably connect, or integral; Can be mechanical connection, also can be electrical connection; Can be directly be connected, also indirectly can be connected by intermediary, can be the connection of two element internals or the interaction relationship of two elements.For the ordinary skill in the art, the concrete meaning of above-mentioned term in the utility model can be understood as the case may be.
The turbosupercharger 100 according to the utility model embodiment is described in detail below in conjunction with accompanying drawing.
With reference to shown in Fig. 1, the turbosupercharger 100 according to the utility model embodiment comprises housing 1.Housing 1 is formed with suction port 6 and air outlet 7, in housing 1, limits eduction valve cavity 4, hyperbaric chamber 2 and the first communicating passage 3.Eduction valve cavity 4 is communicated with suction port 6, and hyperbaric chamber 2 is communicated with air outlet 7.
First communicating passage 3 is connected between eduction valve cavity 4 and hyperbaric chamber 2, particularly, one end of first communicating passage 3 is connected with eduction valve cavity 4, and the other end of the first communicating passage 3 is connected with hyperbaric chamber 2, and eduction valve cavity 4 is connected by the first communicating passage 3 with hyperbaric chamber 2.Pressurized gas in hyperbaric chamber 2 enter into relief valve cavity 4 by the first communicating passage 3, are then back to suction port 6 place of low voltage terminal further, carry out supercharging in the charging turbine flowing into turbosupercharger 100 further with the gas at suction port 6 place.
The cross-section area of the first communicating passage 3 is configured to reduce gradually along from one end be connected with hyperbaric chamber 2 of the first communicating passage 3 towards the direction of one end be connected with eduction valve cavity 4 of the first communicating passage 3.That is, the first communicating passage 3 is along from hyperbaric chamber 2 on the backflow direction of the direction of eduction valve cavity 4 and gas, and the cross-section area of the first communicating passage 3 reduces gradually.
Thus, on the backflow direction of gas, first communicating passage 3 is formed as the contracted channel of reducing type, and after the gas backstreaming in hyperbaric chamber 2 is by the first communicating passage 3 of this reducing type, the flowing velocity of gas can increase, gas pressure can reduce, when the gas flow that pressure reduces is to eduction valve cavity 4, gas reduces by the obstruction of the wall of eduction valve cavity 4, and the vortex phenomenon of generation reduces, gas flow is more smooth and easy, and the disappointing noise produced due to pressure rapid fluctuation significantly reduces.
In the related, the first communicating passage is formed as cylinder type pipeline, and in the boundary layer of wall, gas particle is subject to the obstruction of the frictional force that viscosity causes, and gas flow rate reduces.And after entering the eduction valve cavity 4 that sectional area becomes large, gas pressure raises, airspeed further reduces, so that in the local of eduction valve cavity 4, gas particle easily causes the phenomenon that halts, and simultaneously with the phenomenon that gas is separated with wall, and then forms eddy current, produce unnecessary aerodynamic noise, disappointing noise is larger.
And according to the worm wheel pressure booster of the utility model embodiment, the first communicating passage 3 being communicated with hyperbaric chamber 2 and eduction valve cavity 4 is formed as the pipeline of reducing type, the pipeline of this reducing type can reduce the pressure and temperature of the air-flow entering eduction valve cavity 4 in advance, avoid gas pressure fluctuation sharply in the process of suction port 6 being directly back to low voltage terminal from turbosupercharger 100 high voltage terminal that cylinder type pipeline Connecting format produces, make gas pressure more steady, disappointing noise significantly reduces.
In brief, optimize the structure of inner current by pass, do not increase extra parts, effectively reduce disappointing noise, reasonable in design according to the turbosupercharger 100 of the utility model embodiment, highly versatile and processing and implementation easily reach.
Be understandable that, the shape of the first communicating passage 3 can be formed as multiple, such as, the shape of cross section of the first communicating passage 3 can be formed as circular, oval, long-round-shape or polygonal etc., and namely the first communicating passage 3 can be formed as the Polygonal column shape pipeline etc. of the cylindrical pipe of reducing type, the elliptical cylinder-shape pipeline of reducing type, the elongated cylindrical pipeline of reducing type or reducing type.
As shown in Figure 1, eduction valve cavity 4 can comprise the first pressure stabilizing cavity 41 and the second pressure stabilizing cavity 42, first pressure stabilizing cavity 41 and the second pressure stabilizing cavity 42 and is connected with each other vertically.The free end of the first pressure stabilizing cavity 41 is connected with the first communicating passage 3.The cross-section area of the first communicating passage 3 is less than the cross-section area of the first pressure stabilizing cavity 41.Thus, gas can flow to the larger eduction valve cavity 4 of cross-section area from the first communicating passage 3 that cross-section area is relatively little, the eduction valve cavity 4 that volume is larger can play the effect of steady air flow pressure.
Further, as shown in Figure 1, the cross-section area of the first pressure stabilizing cavity 41 is greater than the cross-section area of the second pressure stabilizing cavity 42.Compared with the structure equal with the cross-section area of the second pressure stabilizing cavity with the cross-section area of the first pressure stabilizing cavity in correlation technique, when the cross-section area of the second pressure stabilizing cavity 42 is constant, the cross-section area of the first pressure stabilizing cavity 41 is greatly variable, thus make the volume of the first pressure stabilizing cavity 41 significantly become large, gas can flow into the first relatively larger pressure stabilizing cavity 41 of volume from the first communicating passage 3, thus larger voltage stabilizing cavity volume can be reached, play the effect of steady air flow pressure further, disappointing noise is reduced further.
As shown in Figure 1, eduction valve cavity 4 also comprises the second communicating passage 5, second communicating passage 5 and is connected between the first pressure stabilizing cavity 41 and suction port 6.Particularly, one end of the second communicating passage 5 is communicated with the first pressure stabilizing cavity 41, and the other end of the second communicating passage 5 is communicated with suction port 6, and the gas in the first pressure stabilizing cavity 41 is back to suction port 6 place by the second communicating passage 5.
Wherein, one end be communicated with the first pressure stabilizing cavity 41 of the second communicating passage 5 can be formed as entry end, and one end be communicated with suction port 6 of the second communicating passage 5 can be formed as outlet end.In the related, the cross-section area of the entry end of the second communicating passage is close to the cross-section area of outlet end, and the size of entry end is less, causes disappointing noise larger.
Advantageously, in embodiments more of the present utility model, the cross-section area of the entry end of the second communicating passage 5 can be greater than the cross-section area of the outlet end of the second communicating passage 5.Thus, when the cross-section area of the outlet end of the second communicating passage 5 is constant, the cross-section area of the entry end of the second communicating passage 5 can significantly become large, thus make the volume of the outlet cavity volume of the first pressure stabilizing cavity 41 become large, improve pressure stabilization function, make gas pressure more steady, disappointing noise reduces further.
As shown in Figure 1, one end of the second communicating passage 5 can be connected to the side away from the second pressure stabilizing cavity 42 of the first pressure stabilizing cavity 41.That is, the entry end of the second communicating passage 5 can be connected on one end be connected with the first communicating passage 3 of the first pressure stabilizing cavity 41.
According to embodiments more of the present utility model, turbosupercharger 100 also comprises eduction valve (scheming not shown), and eduction valve is located at the side away from the first pressure stabilizing cavity 41 of the second pressure stabilizing cavity 42, and eduction valve can be used for conducting or cuts off hyperbaric chamber 2 and suction port 6.When Decompression valves cuts out, cut off between hyperbaric chamber 2 and suction port 6, gas can not be back to suction port 6 from hyperbaric chamber 2.When Decompression valves is opened, hyperbaric chamber 2 and suction port 6 conducting, the gas in hyperbaric chamber 2 can flow into suction port 6 from the first communicating passage 3, eduction valve cavity 4 successively, and gas is refluxed.Wherein, the backflow direction of gas as shown by the arrows in Figure 1.
Further, eduction valve can comprise earial drainage portion, and earial drainage portion to be located in eduction valve cavity 4 with conducting movably or to cut off hyperbaric chamber 2 and suction port 6.Particularly, earial drainage portion is located in the first pressure stabilizing cavity 41 and the second pressure stabilizing cavity 42 movably.When eduction valve is opened, earial drainage portion can be positioned at the second pressure stabilizing cavity 42, now the first communicating passage 3 can with the first pressure stabilizing cavity 41 conducting, thus make hyperbaric chamber 2 and suction port 6 conducting, the gas in hyperbaric chamber 2 can realize backflow.When eduction valve is closed, earial drainage portion can be positioned at the first pressure stabilizing cavity 41 and earial drainage portion can be connected to the joint of the first pressure stabilizing cavity 41 and the first communicating passage 3, first communicating passage 3 and the first pressure stabilizing cavity 41 are cut off, thus making hyperbaric chamber 2 and suction port 6 realize cutting off, the gas in hyperbaric chamber 2 can not reflux.
Wherein, opening or closing of eduction valve can be arranged according to the situation of the cylinder be connected with turbosupercharger 100.Particularly, cylinder is connected with turbosupercharger 100, and the charging turbine in turbosupercharger 100 carries out supercharging to the gas entering turbosupercharger 100 from suction port 6, and the gas after supercharging can enter in cylinder.When not needing more pressurized gas in cylinder, eduction valve can be closed.Gas now after the superturbo boost of turbosupercharger 100 is back to suction port 6 place of turbosupercharger 100 by the current by pass that hyperbaric chamber 2, first communicating passage 3, eduction valve cavity 4 and the second communicating passage 5 are formed, thus the pressurization gas at air outlet 7 place is reduced, the pressurization gas flowing into cylinder reduces.
According to the utility model implement turbosupercharger 100 other form and operation be known for the person of ordinary skill of the art, be not described in detail at this.
In the description of this specification, specific features, structure, material or feature that the description of reference term " embodiment ", " some embodiments ", " example ", " concrete example " or " some examples " etc. means to describe in conjunction with this embodiment or example are contained at least one embodiment of the present utility model or example.In this manual, to the schematic representation of above-mentioned term not must for be identical embodiment or example.And the specific features of description, structure, material or feature can combine in one or more embodiment in office or example in an appropriate manner.In addition, when not conflicting, the feature of the different embodiment described in this specification or example and different embodiment or example can carry out combining and combining by those skilled in the art.
Although illustrate and described embodiment of the present utility model above, be understandable that, above-described embodiment is exemplary, can not be interpreted as restriction of the present utility model, those of ordinary skill in the art can change above-described embodiment, revises, replace and modification in scope of the present utility model.

Claims (8)

1. a turbosupercharger, is characterized in that, comprising:
Housing, described housing is formed with suction port and air outlet, eduction valve cavity is limited in described housing, hyperbaric chamber and the first communicating passage, described eduction valve cavity is communicated with described suction port, described hyperbaric chamber is communicated with described air outlet, described first communicating passage is connected between described eduction valve cavity and described hyperbaric chamber, the cross-section area of wherein said first communicating passage is configured to reduce gradually along from one end be connected with described hyperbaric chamber of described first communicating passage towards the direction of one end be connected with described eduction valve cavity of described first communicating passage.
2. turbosupercharger according to claim 1, is characterized in that, the shape of cross section of described first communicating passage is circular, ellipse, long-round-shape or polygonal.
3. turbosupercharger according to claim 1, it is characterized in that, described eduction valve cavity comprises the first pressure stabilizing cavity and the second pressure stabilizing cavity that are connected with each other vertically, the free end of described first pressure stabilizing cavity is connected with described first communicating passage, and the cross-section area of described first communicating passage is less than the cross-section area of described first pressure stabilizing cavity.
4. turbosupercharger according to claim 3, is characterized in that, the cross-section area of described first pressure stabilizing cavity is greater than the cross-section area of described second pressure stabilizing cavity.
5. turbosupercharger according to claim 4, is characterized in that, described eduction valve cavity also comprises the second communicating passage, and described second communicating passage is connected between described first pressure stabilizing cavity and described suction port.
6. turbosupercharger according to claim 5, is characterized in that, the cross-section area of the entry end of described second communicating passage is greater than the cross-section area of the outlet end of described second communicating passage.
7. turbosupercharger according to claim 3, it is characterized in that, described turbosupercharger also comprises eduction valve, and described eduction valve is located at the side away from described first pressure stabilizing cavity of described second pressure stabilizing cavity, and described eduction valve is used for conducting or cuts off described hyperbaric chamber and described suction port.
8. turbosupercharger according to claim 7, is characterized in that, described eduction valve comprises earial drainage portion, and described earial drainage portion to be located in described eduction valve cavity with conducting movably or to cut off described hyperbaric chamber and described suction port.
CN201420620628.7U 2014-10-24 2014-10-24 Turbosupercharger Expired - Fee Related CN204283994U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420620628.7U CN204283994U (en) 2014-10-24 2014-10-24 Turbosupercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420620628.7U CN204283994U (en) 2014-10-24 2014-10-24 Turbosupercharger

Publications (1)

Publication Number Publication Date
CN204283994U true CN204283994U (en) 2015-04-22

Family

ID=52867159

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420620628.7U Expired - Fee Related CN204283994U (en) 2014-10-24 2014-10-24 Turbosupercharger

Country Status (1)

Country Link
CN (1) CN204283994U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107489522A (en) * 2016-07-21 2017-12-19 宝沃汽车(中国)有限公司 A kind of booster vacuum tank, gas extraction system and engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107489522A (en) * 2016-07-21 2017-12-19 宝沃汽车(中国)有限公司 A kind of booster vacuum tank, gas extraction system and engine

Similar Documents

Publication Publication Date Title
CN206601239U (en) Aero-engine multistage compressor test structure and its adjustable flow-guiding stator blade
CN103953560B (en) Compressor expands steady system and is applied to compressor mechanism of this system
CN104968944A (en) Centrifugal compressor
CN103277324B (en) There is the centrifugal compressor of asymmetric vaneless diffuser and there is its automobile
CN105570157B (en) A kind of supercharger systems and low noise control method
CN204200674U (en) The centrifugal-flow compressor casing bleed recirculation structure of variable geometry
FI3857070T3 (en) Oil-injected multistage compressor device and method for controlling such a compressor device
CN204283994U (en) Turbosupercharger
CN107109960B (en) The profile portion of the guide vane of guider in turbomachinery, especially in compressor
WO2015077380A1 (en) Two piece compressor housing
CN201582215U (en) Width adjusting mechanism of vaneless diffuser of turbocharger
CN103277344A (en) Inner circulating device of centrifugal gas compressor
CN203374525U (en) Inner circulating device of centrifugal-flow compressor
CN203214108U (en) Turbine blade front edge cooling structure
CN202441654U (en) Elbow-shaped water inlet flow channel
CN202301194U (en) Lemniscate helical air-intake pressurizer
TW200403393A (en) Screw compression flow guide for discharge loss reduction
CN103206273A (en) Diffuser for gas turbine
CN201865751U (en) Air inlet channel of supercharger
CN104500156B (en) Volute outlet structure
CN208749451U (en) A kind of diffuser, compressor and combustion gas turbine
CN203476407U (en) Turbocharger volute assembly
CN109779979B (en) Simple and efficient vaneless diffuser stability expanding system of centrifugal compressor
CN201358951Y (en) Multistage low-speed centrifugal blower
CN105736457B (en) Centrifugal compressor

Legal Events

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

Effective date of registration: 20180413

Address after: No. 188, Miyun District, Miyun District, Beijing, Beijing

Patentee after: Beijing treasure Car Co.,Ltd.

Address before: 102206 Changping District City, Shahe, Sha Yang Road, Beijing

Patentee before: BEIQI FOTON MOTOR Co.,Ltd.

TR01 Transfer of patent right
CP01 Change in the name or title of a patent holder

Address after: No. 188, Miyun District, Miyun District, Beijing, Beijing

Patentee after: Beijing baowo Automobile Co.,Ltd.

Address before: No. 188, Miyun District, Miyun District, Beijing, Beijing

Patentee before: Beijing treasure Car Co.,Ltd.

CP01 Change in the name or title of a patent holder
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150422

Termination date: 20211024

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