CN216742188U - Supercharger with vane diffuser and pneumatic guide vane structure - Google Patents

Supercharger with vane diffuser and pneumatic guide vane structure Download PDF

Info

Publication number
CN216742188U
CN216742188U CN202221183344.7U CN202221183344U CN216742188U CN 216742188 U CN216742188 U CN 216742188U CN 202221183344 U CN202221183344 U CN 202221183344U CN 216742188 U CN216742188 U CN 216742188U
Authority
CN
China
Prior art keywords
diffuser
vane
supercharger
guide
guide sleeve
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.)
Active
Application number
CN202221183344.7U
Other languages
Chinese (zh)
Inventor
刘莹
杨名洋
邓永宏
陈化
朱耀辉
邵同林
朱修鹏
张蕴秋
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.)
Kangyue Technology Shandong Co ltd
Original Assignee
Kangyue Technology Shandong 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 Kangyue Technology Shandong Co ltd filed Critical Kangyue Technology Shandong Co ltd
Priority to CN202221183344.7U priority Critical patent/CN216742188U/en
Application granted granted Critical
Publication of CN216742188U publication Critical patent/CN216742188U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A supercharger with a vane diffuser and a pneumatic guide vane structure relates to the technical field of superchargers and comprises a compressor shell, wherein the compressor shell is provided with the diffuser, a guide sleeve is arranged in the diffuser, and guide vanes are arranged between the inner wall of the diffuser and the outer wall of the guide sleeve. The utility model solves the problems that although the pressure ratio and the efficiency of the supercharger are improved by the diffuser in the traditional technology, the flow range is narrowed, the working requirement of the whole rotating speed range of an engine cannot be met, and low speed and high speed cannot be taken into consideration.

Description

Supercharger with vane diffuser and pneumatic guide vane structure
Technical Field
The utility model relates to the technical field of superchargers, in particular to a supercharger with a vane diffuser and a pneumatic guide vane structure.
Background
In recent years, the supercharging rate of engines, particularly diesel engines, has been greatly improved, but the turbocharger is required to have a more compact structure due to the restrictions on the structure and matching characteristics of the turbocharger. A bearing assembly and a diffuser are installed at one end of a central shaft of the turbocharger, and an impeller cover and a pressure end bearing shell are connected to the diffuser. The performance curve of the compressor can be approximately translated left and right by using the diffuser, so that the working efficiency of the turbocharger is influenced; meanwhile, the diffuser is connected with the impeller cover, and the structure of the diffuser influences the anti-surge vibration effect of the impeller cover.
The prior art discloses a patent of CN206845549U, which includes a compressor casing, a compressor impeller coaxially mounted in an inner hole of the compressor casing and applying work to gas, a diffuser structure provided at an outlet of the compressor impeller, and a vaneless annular diffuser formed at a portion of the diffuser structure corresponding to the compressor casing. The scheme solves the problem of oil leakage at the pressure end of the turbocharger, and improves the utilization rate of lubricating oil.
The prior device gradually exposes the defects of the technology along with the use, and is mainly expressed in the following aspects:
first, although the existing diffuser improves the pressure ratio and efficiency of the supercharger, the flow range is narrowed, the working requirement of the whole rotating speed range of the engine cannot be met, and low speed and high speed cannot be both considered.
Secondly, the existing diffuser is connected with the compressor shell by a connecting piece, the installation procedure is complex, the structure is complex, and the failure rate is high.
In view of the above, the prior art is obviously inconvenient and disadvantageous in practical use, and needs to be improved.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects in the prior art, the utility model solves the problems that although the pressure ratio and the efficiency of the supercharger are improved by the diffuser in the traditional technology, the flow range is narrowed, the working requirement of the whole rotating speed range of the engine cannot be met, and both low speed and high speed cannot be considered; and the existing diffuser is connected with the compressor shell by a connecting piece, so that the installation process is complicated.
In order to solve the above problems, the present invention provides the following technical solutions:
a supercharger with a vane diffuser and a pneumatic guide vane structure comprises a compressor shell, wherein the compressor shell is provided with the diffuser, a guide sleeve is arranged in the diffuser, and guide vanes are arranged between the inner wall of the diffuser and the outer wall of the guide sleeve;
the guide vanes are provided with a plurality of guide vanes and are arranged on the outer wall of the guide sleeve in an enclosing manner;
the guide vanes are arc vanes, and the rotating directions of a plurality of arc vanes are the same;
the outer wall of the flow guide sleeve is positioned in the area between two adjacent arc-shaped blades to form a flow expansion groove.
As an optimized scheme, one end of the diffuser close to the outlet is provided with a flared opening.
As an optimized scheme, the inner cavity of the diffuser is further provided with a limiting bulge part for limiting the flow guide sleeve.
Preferably, the outer wall of the diffuser is in interference fit with the inner wall of the compressor casing.
As an optimized scheme, the guide sleeve is in interference fit with the diffuser.
As an optimized scheme, the length of the guide vane is 24mm, the radian is R80mm, the thickness is 0.8mm, and the height is 2.5 mm.
Compared with the prior art, the utility model has the beneficial effects that:
the guide sleeve and the diffuser are formed in interference fit, a flow expansion groove is formed between the diffuser and the guide sleeve, redundant air entering the compressor shell returns to the inlet of the compressor through the flow expansion groove, and guide blades on the guide sleeve guide the flow direction of the air flow to enable the air flow to rotate; the diffuser and the inner surface of the compressor shell are assembled together in an interference fit manner, so that the structure is simpler, and a connecting piece is omitted;
the air compressor of the supercharger has the advantages of further widening the air inlet flow range, improving the air inlet efficiency, being beneficial to improving the power performance and the economic performance of the engine, simplifying the structure and improving the reliability of the supercharger and the engine.
Drawings
In order to more clearly illustrate the detailed description of the utility model or the technical solutions in the prior art, the drawings that are needed in the detailed description of the utility model or the prior art will be briefly described below. Throughout the drawings, like elements or portions are generally identified by like reference numerals. In the drawings, elements or portions are not necessarily drawn to scale.
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a diffuser according to the present invention;
fig. 3 is a schematic structural view of the flow guide sleeve of the present invention.
In the figure: 1-a compressor casing; 2-a diffuser; 3-a flow guide sleeve; 4-guide vanes; 5-a horn mouth; 6-limiting convex part; 7-rubbing groove.
Detailed Description
Embodiments of the present invention will be described in detail below with reference to the accompanying drawings. The following examples are only for illustrating the technical solutions of the present invention more clearly, and therefore are only examples, and the protection scope of the present invention is not limited thereby.
As shown in fig. 1 to 3, the supercharger with a vane diffuser and pneumatic guide vane structure comprises a compressor casing 1, a diffuser 2 is installed on the compressor casing 1, a guide sleeve 3 is arranged in the diffuser 2, and a guide vane 4 is arranged between the inner wall of the diffuser 2 and the outer wall of the guide sleeve 3;
the guide vanes 4 are provided with a plurality of vanes and are arranged on the outer wall of the guide sleeve 3 in a surrounding manner;
the guide vanes 4 are arc vanes, and the rotating directions of a plurality of arc vanes are the same;
the area of the outer wall of the guide sleeve 3 between two adjacent arc-shaped blades forms an expansion groove 7.
One end of the diffuser 2 close to the outlet is provided with a flared opening 5.
The inner cavity of the diffuser 2 is also provided with a limiting bulge part 6 for limiting the flow guide sleeve 3.
The outer wall of the diffuser 2 is in interference fit with the inner wall of the compressor shell 1.
The guide sleeve 3 is in interference fit with the diffuser 2.
The length of the guide vane 4 is 24mm, the radian is R80mm, the thickness is 0.8mm, and the height is 2.5 mm.
The working principle of the device is as follows:
the guide sleeve 3 and the diffuser 2 are formed by interference fit, a flow expansion groove 7 is formed between the diffuser 2 and the guide sleeve 3, redundant air entering the compressor shell 1 returns to the inlet of the compressor through the flow expansion groove 7, and guide blades 4 on the guide sleeve 3 guide the flow direction of the air flow to enable the air flow to rotate; the diffuser 2 and the inner surface of the compressor shell 1 are assembled together in an interference fit mode.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the utility model has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention, and they should be construed as being included in the following claims and description.

Claims (6)

1. The utility model provides a booster with leaf diffuser and pneumatic guide vane structure which characterized in that: the compressor comprises a compressor shell (1), wherein a diffuser (2) is installed on the compressor shell (1), a guide sleeve (3) is arranged in the diffuser (2), and guide blades (4) are arranged between the inner wall of the diffuser (2) and the outer wall of the guide sleeve (3);
the guide vanes (4) are provided with a plurality of vanes and are arranged on the outer wall of the guide sleeve (3) in an enclosing manner;
the guide vanes (4) are arc-shaped vanes, and the rotating directions of a plurality of arc-shaped vanes are the same;
the outer wall of the flow guide sleeve (3) is positioned in the area between two adjacent arc-shaped blades to form an expansion groove (7).
2. The supercharger of claim 1, wherein the vane diffuser and the air vane structure are configured to: one end of the diffuser (2) close to the outlet is provided with a horn-shaped opening (5).
3. The supercharger of claim 1, wherein the vane diffuser and the air vane structure are configured to: the inner cavity of the diffuser (2) is also provided with a limiting bulge part (6) for limiting the flow guide sleeve (3).
4. The supercharger of claim 1, wherein the vane diffuser and the air vane structure are configured to: the outer wall of the diffuser (2) is in interference fit with the inner wall of the compressor casing (1).
5. The supercharger of claim 1, wherein the vane diffuser and the air vane structure are configured to: the guide sleeve (3) is in interference fit with the diffuser (2).
6. The supercharger of claim 1, wherein the vane diffuser and the air vane structure are configured to: the length of the guide vane (4) is 24mm, the radian is R80mm, the thickness is 0.8mm, and the height is 2.5 mm.
CN202221183344.7U 2022-05-18 2022-05-18 Supercharger with vane diffuser and pneumatic guide vane structure Active CN216742188U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221183344.7U CN216742188U (en) 2022-05-18 2022-05-18 Supercharger with vane diffuser and pneumatic guide vane structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221183344.7U CN216742188U (en) 2022-05-18 2022-05-18 Supercharger with vane diffuser and pneumatic guide vane structure

Publications (1)

Publication Number Publication Date
CN216742188U true CN216742188U (en) 2022-06-14

Family

ID=81921401

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221183344.7U Active CN216742188U (en) 2022-05-18 2022-05-18 Supercharger with vane diffuser and pneumatic guide vane structure

Country Status (1)

Country Link
CN (1) CN216742188U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116557331A (en) * 2023-07-04 2023-08-08 康跃科技(山东)有限公司 Compressor and supercharger

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116557331A (en) * 2023-07-04 2023-08-08 康跃科技(山东)有限公司 Compressor and supercharger
CN116557331B (en) * 2023-07-04 2023-09-22 康跃科技(山东)有限公司 Compressor and supercharger

Similar Documents

Publication Publication Date Title
CN216742188U (en) Supercharger with vane diffuser and pneumatic guide vane structure
KR20140014175A (en) A turbine wheel, a turbine and use thereof
US8480351B2 (en) Compressor unit
CN217814132U (en) Supercharger with vane diffuser and pneumatic flow guide sleeve structure
CN111140341A (en) Segmented adjustable blade vaned diffuser structure
CN217271008U (en) Compressor casing and turbo charger with low noise flow expands wide groove
CN206290437U (en) The fully-closed vortex compressor of Elastic Contact sealing
CN203756315U (en) Small-sized gasoline engine turbine booster
CN108533387A (en) A kind of turbo charging installation of translator/generator
CN111794807B (en) Power turbine inlet guider for fuel-drive compressor unit
CN114151195A (en) Novel exhaust diffuser structure capable of improving pneumatic performance
CN115030784A (en) Bearing cooling device of air bearing turbocharger
CN107023329A (en) A kind of combined flow turbine supercharger heat shield with circular cone inclined-plane
CN108999664B (en) Variable-radial-clearance double-inlet turbine box
CN211082045U (en) Supercharging system and centrifugal compressor thereof
CN220850163U (en) Low-noise compressor shell with replaceable air inlet
CN103953431A (en) Small gasoline engine turbosuperchager
CN217813606U (en) Blast furnace gas excess pressure turbine device
CN206290438U (en) Scroll compressor with elastic cross coupling ring
CN213450595U (en) Turbocharging device
CN219639126U (en) Turbocharger compressor volute with silencing function
CN218177553U (en) Compressor shell assembly of turbocharger
CN220705804U (en) Seal structure for strengthening strength of rotor shaft of turbocharger
CN114738300B (en) Two-stage centrifugal air compressor
CN219733709U (en) Shaft seal structure for turbocharger

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant