CN104847703A - Flow regulation mechanism surge proof and blocking proof for gas compressor - Google Patents

Flow regulation mechanism surge proof and blocking proof for gas compressor Download PDF

Info

Publication number
CN104847703A
CN104847703A CN201510285830.8A CN201510285830A CN104847703A CN 104847703 A CN104847703 A CN 104847703A CN 201510285830 A CN201510285830 A CN 201510285830A CN 104847703 A CN104847703 A CN 104847703A
Authority
CN
China
Prior art keywords
gas
proof
flow
regulation mechanism
gas compressor
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.)
Pending
Application number
CN201510285830.8A
Other languages
Chinese (zh)
Inventor
沈艳
叶震杰
袁玺
刘贵升
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.)
WUXI KEBO SUPERCHARGER CO Ltd
Original Assignee
WUXI KEBO SUPERCHARGER 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 WUXI KEBO SUPERCHARGER CO Ltd filed Critical WUXI KEBO SUPERCHARGER CO Ltd
Priority to CN201510285830.8A priority Critical patent/CN104847703A/en
Publication of CN104847703A publication Critical patent/CN104847703A/en
Pending legal-status Critical Current

Links

Abstract

The invention discloses a flow regulation mechanism surge proof and blocking proof for a gas compressor. The flow regulation mechanism comprises a compression shell; an impeller is disposed within the compression shell; the compression shell is provided with an air inlet; a center line of the air inlet and an axial center line of the impeller overlap; an air passage is arranged around the edge of the compression shell and is communicated with the air inlet. The flow regulation mechanism is characterized in that the compression shell is provided with a circular groove around the air inlet, the bottom of the circular groove is provided with gas regulating holes, the gas regulation holes are communicated with a passage between the air inlet and the air passage and correspond to the middle of the impeller of a turbine. The flow regulation mechanism has the advantages that surging or blocking of the gas compressor can be avoided, the running and service life of a supercharger can be prolonged and surging of the gas compressor of the supercharger during low flow and blocking thereof during high flow can be eliminated.

Description

Gas compressor anti-surge anti-plugging flow control device
Technical field
The present invention relates to a kind of compressor casing.Specifically, the flow control device of blocking phenomenon when being used to surge when eliminating the gas compressor small flow of automobile booster and large discharge.
Background technique
All know at pressurized machine production industry, when vehicle traveling process slows down, due to the unexpected minimizing of the gas flow of impeller inlet, pressurized machine there will be violent surge.And when the gas flow of impeller inlet is larger, there will be again flow blocking phenomenon.No matter be that surging phenomenon occurs, or blocking phenomenon, all can bring adverse effect to the operation of pressurized machine and working life.
Summary of the invention
The problem to be solved in the present invention is to provide a kind of gas compressor anti-surge anti-plugging flow control device.Adopt this mechanism, the generation of compressor surge and blocking phenomenon can be avoided, be conducive to the operation of pressurized machine and the prolongation in working life.
The problems referred to above that the present invention will solve are realized by following technological scheme:
Gas compressor anti-surge anti-plugging flow control device of the present invention comprises pressure shell, and have impeller in pressure shell, pressure shell has intake grill, the center line of described intake grill overlaps with the longitudinal center line of impeller.Pressure shell edge surrounding has air channel, and described air channel is communicated with intake grill.The pressure shell being characterized in intake grill surrounding has circular groove, the bottom land of circular groove has gas regulation hole, this gas regulation hole be connected with the passage between intake grill with air channel and with the blade of turbine in the middle of corresponding.
Take such scheme, have the following advantages:
As can be seen from the above scheme, the pressure shell due to intake grill surrounding has circular groove, the bottom land of circular groove has gas regulation hole, this gas regulation hole be connected with the passage between intake grill with air channel and with the blade of turbine in the middle of corresponding.When intake grill gas flow reduces suddenly, by the gas regulation hole on circular groove bottom land, can supplement gas flow, avoid the generation of surge condition.When there is gas flow increase, flow blocking phenomenon, by the gas regulation hole on circular groove bottom land, can drain gas flow in runner, the flow in runner is regulated.Generally speaking, by the gas regulation hole on circular groove bottom land, can regulate gas flow, thus avoid the generation of surge and blocking phenomenon, not only ensure the normal operation of pressurized machine, also can extend the working life of pressurized machine.
Accompanying drawing explanation
Fig. 1 is gas compressor anti-surge anti-plugging flow control device schematic diagram of the present invention, and this figure is that the gas of gas flow when reducing suddenly moves towards schematic diagram;
When Fig. 2 is gas flow increase, flow blocking phenomenon, the gas of gas compressor anti-surge anti-plugging flow control device moves towards schematic diagram.
Embodiment
As depicted in figs. 1 and 2, gas compressor anti-surge anti-plugging flow control device of the present invention comprises pressure shell 3, and be provided with impeller 5 in pressure shell 3, pressure shell 3 be processed with intake grill 1, the center line of described intake grill 1 overlaps with the longitudinal center line of impeller 5.Pressure shell 3 edge surrounding is processed with air channel 4, and described air channel 4 is communicated with intake grill 1.The pressure shell 3 of intake grill 1 surrounding is processed with circular groove 2, the bottom land of circular groove 2 is processed with gas regulation hole 6, this gas regulation hole be connected with the passage between intake grill 1 with air channel 4 and with the blade of turbine 5 in the middle of corresponding.
See figure, 1, when the gas flow of intake grill 1 reduces suddenly, by the gas regulation hole 6 on circular groove 2 bottom land, can supplement gas flow, avoid the generation of surge condition.See Fig. 2, when there is gas flow increase, flow blocking phenomenon, by the gas regulation hole 6 on circular groove 2 bottom land, can drain gas flow in runner, the flow in runner is regulated.Generally speaking, by the gas regulation hole 6 on circular groove 2 bottom land, can regulate gas flow, thus avoid the generation of surge and blocking phenomenon.

Claims (1)

1. gas compressor anti-surge anti-plugging flow control device, comprises pressure shell (3), has impeller (5) in pressure shell (3), pressure shell (3) has intake grill (1), and the center line of described intake grill (1) overlaps with the longitudinal center line of impeller (5); Pressure shell (3) edge surrounding has air channel (4), and described air channel (4) are communicated with intake grill (1); The pressure shell that it is characterized in that intake grill (4) surrounding has circular groove, the bottom land of circular groove has gas regulation hole, this gas regulation hole be connected with the passage between intake grill with air channel and with the blade of turbine in the middle of corresponding.
CN201510285830.8A 2015-05-29 2015-05-29 Flow regulation mechanism surge proof and blocking proof for gas compressor Pending CN104847703A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510285830.8A CN104847703A (en) 2015-05-29 2015-05-29 Flow regulation mechanism surge proof and blocking proof for gas compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510285830.8A CN104847703A (en) 2015-05-29 2015-05-29 Flow regulation mechanism surge proof and blocking proof for gas compressor

Publications (1)

Publication Number Publication Date
CN104847703A true CN104847703A (en) 2015-08-19

Family

ID=53847594

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510285830.8A Pending CN104847703A (en) 2015-05-29 2015-05-29 Flow regulation mechanism surge proof and blocking proof for gas compressor

Country Status (1)

Country Link
CN (1) CN104847703A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107338340A (en) * 2017-03-01 2017-11-10 北京福生智源科技有限公司 A kind of device and method for being used to prevent RECOVERY OF CONVERTER GAS blower fan surge
CN110332043A (en) * 2019-08-14 2019-10-15 凤城市东宁动力有限公司 A kind of turbocharger air inlet buffer structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3038398B2 (en) * 1991-09-02 2000-05-08 石川島播磨重工業株式会社 Centrifugal compressor
CN1542290A (en) * 2003-04-30 2004-11-03 奥尔塞特工程有限公司 Compressor
JP5630488B2 (en) * 2012-09-17 2014-11-26 株式会社豊田自動織機 Centrifugal compressor
CN104564831A (en) * 2014-12-26 2015-04-29 珠海格力电器股份有限公司 Diffuser structure applied to compressor
CN204663989U (en) * 2015-05-29 2015-09-23 无锡科博增压器有限公司 Gas compressor anti-surge anti-plugging flow control device

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3038398B2 (en) * 1991-09-02 2000-05-08 石川島播磨重工業株式会社 Centrifugal compressor
CN1542290A (en) * 2003-04-30 2004-11-03 奥尔塞特工程有限公司 Compressor
JP5630488B2 (en) * 2012-09-17 2014-11-26 株式会社豊田自動織機 Centrifugal compressor
CN104564831A (en) * 2014-12-26 2015-04-29 珠海格力电器股份有限公司 Diffuser structure applied to compressor
CN204663989U (en) * 2015-05-29 2015-09-23 无锡科博增压器有限公司 Gas compressor anti-surge anti-plugging flow control device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107338340A (en) * 2017-03-01 2017-11-10 北京福生智源科技有限公司 A kind of device and method for being used to prevent RECOVERY OF CONVERTER GAS blower fan surge
CN110332043A (en) * 2019-08-14 2019-10-15 凤城市东宁动力有限公司 A kind of turbocharger air inlet buffer structure

Similar Documents

Publication Publication Date Title
US10066638B2 (en) Centrifugal compressor and turbocharger
CN104405685A (en) Self-circulation and circumferential groove hybrid treater box for improving performance of air compressor
CN110762051A (en) Surging prevention structure of magnetic suspension air compressor
CN104879320A (en) Surging-prevent compressor volute structure for turbocharger
CN104847703A (en) Flow regulation mechanism surge proof and blocking proof for gas compressor
CN204663989U (en) Gas compressor anti-surge anti-plugging flow control device
CN201858159U (en) Air inlet valve of screw air compressor
CN201582215U (en) Width adjusting mechanism of vaneless diffuser of turbocharger
CN201991572U (en) Labyrinth gland with combined main teeth, side teeth and honeycomb belt
CN102996507A (en) Internally circulating device of centrifugal air compressor
CN203051237U (en) Surge-preventing structure for aero-engine compressor
CN103032579B (en) Pressure air intake and exhaust volume amplifying device of exhaust valve
CN217271008U (en) Compressor casing and turbo charger with low noise flow expands wide groove
CN105298921A (en) Inter-stage U-shaped mixing diffuser for two-stage centrifugal gas compressor
CN206309640U (en) A kind of cavitation-preventive noise reduction sound oil piping system for tooth type centrifugal compressor
CN214424587U (en) Bearing cavity sealing system and turbine engine
CN104712588A (en) Novel mine axial flow ventilation diffuser
CN212454562U (en) Coal fired power plant feed pump steam turbine steam supply pipeline system with stable steam source switching
CN202811143U (en) Electric fuel pump of integrated pressure regulating valve
CN104747440A (en) Roots blower
CN216841836U (en) Turbine structure capable of reducing axial thrust through bidirectional balance
CN102022572B (en) Pressure limiting valve of vehicle or engineering machine air pressure regulating system
CN202007804U (en) Throttle valve with pressure protection function
CN201090514Y (en) Anti-surging impeller cover
CN206111645U (en) Assembled centrifugal compressor adjusting shim

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20150819