CN201138272Y - Integral dynamic balancing machine for turbo-charger - Google Patents

Integral dynamic balancing machine for turbo-charger Download PDF

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Publication number
CN201138272Y
CN201138272Y CNU2007200164204U CN200720016420U CN201138272Y CN 201138272 Y CN201138272 Y CN 201138272Y CN U2007200164204 U CNU2007200164204 U CN U2007200164204U CN 200720016420 U CN200720016420 U CN 200720016420U CN 201138272 Y CN201138272 Y CN 201138272Y
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pipe
air inlet
balancing machine
dynamic balancing
mouth
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Expired - Fee Related
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CNU2007200164204U
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Chinese (zh)
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刘长祥
胡鼎生
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Abstract

The utility model relates to a global dynamic balancing machine of a turbocharger used for detecting and repairing the global dynamic unbalance of the turbocharger, which is suitable for an explosive motor turbocharger manufacture to measure and repair the dynamic unbalance and research the characteristics of a gas compressor. The design proposal of the global dynamic balancing machine is as follows: mechanical and hydraulic structures are used to simulate loading conditions that the compressor casing end of the turbocharger presses fresh air into the combustion chamber of the motor at the inlet end of the turbocharger that is to be measured and the suction and extrusion ends of a turbo. Reliable data for the research of the characteristic curve of the gas compressor is provided by obtaining the outlet temperature Tk2, the inlet temperature tK1, the outlet pressure PK2 and the inlet pressure PK1 of a tested object in operating conditions. The outlet temperature Tk2, the inlet temperature tK1, the outlet pressure PK2 and the inlet pressure PK1 of the measured object are obtained by an inlet temperature sensor and a pressure transmitter arranged on the tube of an air-intake double-button flow meter as well as an outlet temperature sensor and a pressure transducer installed on an equalizing pipe. A manual control valve controls the outlet pressure of the compressor casing of the measure object and the flow rate of the tube of the air-intake double-button flow meter. So the parameter of the surge point of the characteristic curve of the gas compressor can be obtained for calculation in different operating conditions.

Description

The whole dynamic balancing machine of turbosupercharger
Technical field
The utility model relates to the whole dynamic balancing machine of a kind of turbosupercharger that detects the also supercharger integrated unbalance dynamic of repairing turbine.The most suitable explosive motor turbosupercharger is manufactured mensuration and the reparation that unbalance dynamic is done by enterprise, to the research of compressor characteristics, and the exploitation of new product.
Background technology
Before the utility model, the structure of similar products at home and abroad is only simulated the part working condition of turbosupercharger on explosive motor, do the mensuration and the reparation of unbalance dynamic, obtain check data parameter deficiency, can not reflect the operating characteristic of turbosupercharger truly.
Summary of the invention
The purpose of this utility model is to overcome the deficiency of prior art on structural design, solve the disadvantage that only can simulate the part working condition of turbosupercharger on explosive motor that prior art exists, to obtain the check data parameter under whole working conditions, make the whole transient equilibrium function of turbosupercharger react the operating characteristic of turbosupercharger truly, all sidedly.Design proposal of the present utility model is at measured workpiece turbosupercharger inlet end, turbine sucks and extrudes end and adopts machinery, hydraulic structure simulation turbocharger air compressor shell end to be pressed into the loading condition of fresh air to engine chamber, thereby make the unbalance dynamic of turbosupercharger when high rotating speed near actual working conditions, to determine the unbalance dynamic quality of product,, enterprise provides more reliable science data for developing new product.Comprised the frame in the prior art in the structure of the whole dynamic balancing machine of this turbosupercharger, the taper support, the Magnetic Induction tachogenerator, digital display screen, the instrument display control program, the volute gas outlet, the compressor casing gas outlet, rubber hose, air intake opening, the technology volute, the compressor casing air intake opening, it also includes the two knob flowmeter assemblies of air inlet on the intermediate support plate that is located at frame, be located at the binary channels pipeline that is connected with the high speed nozzle L type pipe afterbody air inlet mouth of pipe of intermediate support plate below, on the rear frame of frame, be provided with the surge pipe that is connected with compressor casing, reach the manual voltage regulation pipe that is connected with surge pipe with the volute gas outlet.The whole dynamic balancing machine of the utility model turbosupercharger is compared with the prior art more near actual condition, gather the number a tree name accurately, comprehensively, by being installed in inlet temperature sensor, the intake pressure transmitter on the two knob flowmeter trunnions of air inlet and being installed in the outlet temperature t that outlet temperature sensor, outlet pressure sensor on the surge pipe obtains measured piece under the working condition K2, inlet temperature t K1, top hole pressure P K2, intake pressure P K1For compressor performance characteristic curve research provides authentic data; Control measured piece compressor casing top hole pressure by opening and closing manually operated control valve, thereby the charge flow rate of the two knob flowmeter trunnions of control air inlet reaches and obtains the parameter of calculating the compressor performance characteristic curve pumping point under the different working conditions; More than 2 be that prior art institute is out of the question.
Description of drawings
Fig. 1, be the structural representation of the whole dynamic balancing machine of turbosupercharger.Fig. 2, be the left view of Fig. 1.Fig. 3, be the vertical view of Fig. 1.Fig. 4, be the structural representation of surge pipe 9 among Fig. 3.Fig. 5, be the structural representation of the two knob flowmeter assemblies 4 of air inlet among Fig. 1.Fig. 6, be the structural representation of the binary channels pipeline 5 among Fig. 1.Fig. 7, be the structural representation of the high speed nozzle 33 among Fig. 6.Fig. 8, be the structural representation of the manual voltage regulation pipe 10 among Fig. 3.
Embodiment
For structure and principle of work to the whole dynamic balancing machine of the utility model turbosupercharger have further understanding, details are as follows in conjunction with the accompanying drawings:
With reference to accompanying drawing, the structure of the whole dynamic balancing machine of the utility model turbosupercharger (is seen Fig. 1,2,3), among the figure, the back taper support 44 of taper support 2 and high speed nozzle 33 is located at the upper and lower of the intermediate support plate 47 of frame 1 respectively, link together by ring flange and intermediate support plate 47, high speed nozzle 33 (see figure 7)s in taper support 2 are that a top has the isometrical tiny cone opening 43 that is shrunk to, afterbody has the L type pipe of the air inlet mouth of pipe (46), L type pipe and back taper support 44 are welded together, on the circumference in the middle of the L type pipe, be evenly equipped with 4 circular holes 48, above circular hole 48, be provided with the cavity sealed separation that taper support 2 and back taper support 44 are linked to be of taper support 2 welding and become the seal pad 49 of two cavitys up and down, when adopting manual ball valve 35 control pressurized air, pressurized air is along manual draft tube 34, the air inlet mouth of pipe 46 through L type pipe, tiny cone opening 43 forms the turbine rotation that high velocity air promotes the measured piece turbosupercharger; When entering down cavity, the air inlet mouth of pipe 45 that adopts the automatic control of machinery pressurized air along back taper support 44 forms the turbine rotation that high velocity airs promote the measured piece turbosupercharger through 4 apertures 48, tiny cone opening 43.Magnetic induction tachogenerator 3 is connected on the piston rod of its transmission cylinder.Two knob flowmeter assembly 4 (see figure 5)s of air inlet are by 4 T type bolts, stud bolt 23, setting nut 24 is fixed on dovetail groove guide rail 32 on the intermediate support plate 47, flat board 25 bottoms above dovetail groove guide rail 32 have with dovetail groove guide rail 32 and are connected the dovetail groove that matches, on dull and stereotyped 25, fixing the two knob flowmeter trunnions 26 of air inlet with pipe collar, dull and stereotyped 25 pass through bolt contiguous block 31 is connected with cylinder piston rod 30, drive the two knob flowmeter trunnions 26 of air inlet and do tangential movement, on the tube wall of the two knob flowmeter trunnions 26 of air inlet, also be drilled with two apertures 29, an aperture 29 is connected with pressure unit 28 by rubber hose 12, adopt negative pressure numerical value and be used as the calculated flow rate parameter, the inlet temperature sensor 27 of surveying intake air temperature is housed in another aperture 29, the two knob flowmeter assemblies 4 of air inlet can be done the adjusted size of space three-dimensional direction on intermediate support plate 47, to be suitable for the turbosupercharger of different size model.Be located at binary channels pipeline 5 (see figure 6)s that intermediate support plate 47 belows are connected with the air inlet mouth of pipe 46, comprised the manual draft tube 34 that has manual ball valve 35 in its structure, have electric-controlled ball valve 38, tooth bar rotary oil cylinder ball valve 39, the machinery of three-position four-way valve 40 is snorkel 41 automatically, connect manual draft tube 34 and the machinery three-way pipe 36 of snorkel 41 automatically, three-way pipe 36 is also connecting the air inlet mouth of pipe 37 that links to each other with compressor compresses air source of the gas, manually draft tube 34 is connected with the air inlet mouth of pipe 46 of high speed nozzle 33L type pipe, and machinery draft tube 41 automatically is connected with the air inlet mouth of pipe 45 of the back taper support 44 of high speed nozzle 33.Digital display screen 6, instrument display control program 7 are installed in the casing of frame 1.Volute gas outlet 8 is supported on frame 1 rear frame with surge pipe 9 usefulness pipe collars.The structure (see figure 4) of surge pipe 9, be that at one end opening communicates with atmosphere, the other end has in the pipe 21 of end plate 17 and is provided with the hydraulic cylinder 20 that is connected and fixed by bolt and end plate 17, bulb variable valve 16 is connected by the piston rod of connecting link with hydraulic cylinder 20, in pipe 21, be provided with bulb variable valve 16 and pass through bolted grade bar 18, tighten the clock gauge 19 that the set contact contacts with grade bar 18 at pipe 21, the mouth of pipe of end plate 17 left-hand side pipe is an air intake opening 13, upper tube wall is provided with outlet pressure sensor 14, outlet temperature sensor 15, have the mouth of pipe 22 of giving vent to anger that links to each other with the draft tube 51 of manual voltage regulation pipe 10 on the following tube wall, air intake opening 13 links together by rubber hose 12 and measured piece compressor casing gas outlet 11, pressure regulation is the area that changes the mouth of pipe that moves axially that promotes to drive bulb variable valve 16 by hydraulic cylinder piston rod, thereby reach the purpose of pressure regulation, the demonstration of amount of movement is to represent with the perpendicular displacement that clock gauge 19 contacts produce by the grade bar 18 that is fixed on the bulb variable valve 16.It is to be connected to form by draft tube 51 and the manually operated control valve 53 of escape pipe 52 by the centre for manual voltage regulation pipe 10 (see figure 8)s, the mouth of pipe of draft tube 51 is connected with the mouth of pipe 22 of giving vent to anger among Fig. 4, the mouth of pipe of escape pipe 52 is connected with volute gas outlet 8 with movable joint, by opening and closing manually operated control valve 53 control measured piece compressor casing top hole pressures, thereby the charge flow rate of the two knob flowmeter trunnions 26 of control air inlet reaches and obtains the parameter of calculating the compressor performance characteristic curve pumping point under the different working conditions.
The principle of work of this machine is: the measured piece turbosupercharger is installed in the technology volute 42 on the taper support 2,11 insertion rubber hose 12 are connected with the air intake opening 13 of (see figure 4) surge pipe 9 in the compressor casing gas outlet, aim at compressor casing air intake opening 50 then and advance the two knob flowmeter trunnions 26 of air inlet, fall magnetic induction tachogenerator 3 and both opened the valve of compressed air gas source, the pressurized air of simulated engine combustion gas is through binary channels pipeline 5, tiny cone opening 43 (see figure 7)s of high speed nozzle 33 produce the turbine rotation that supersonic airstream makes the measured piece turbosupercharger, and drive the compressor impeller rotation of the other end as power, suck fresh air through the two knob flowmeter trunnions 26 of air inlet, introduce compressor casing and transfer pressurized air to, again the air after the compression is squeezed into the openend that communicates with the atmosphere discharge of the surge pipe 9 of simulation explosive motor combustion chamber of air cylinder.The entire work process type of drive mediates the load form of its rotary body of turbosupercharger and supports the two ends cantilever and bear the state of horizontal radial power effect, the true rotation situation of air stream drives when coming analogue simulation supercharger real work running, flexible deformation that measured piece turbosupercharger axle produces when running up with assurance and vibration situation are the actual values under the actual conditions, carry out reaching the transient equilibrium quality requirements after the unbalance dynamic reparation.By being installed in inlet temperature sensor 27, the intake pressure transmitter 28 on the two knob flowmeter trunnions 26 of air inlet and being installed in the outlet pressure sensor 14 on the surge pipe 9, the outlet temperature t that outlet temperature sensor 15 obtains measured piece under the working condition K2, inlet temperature t K1, top hole pressure P K2, intake pressure P K1Be reacted to digital display screen 6 and instrument display control program 7, for compressor performance characteristic curve research provides authentic data.

Claims (6)

1, the whole dynamic balancing machine of a kind of turbosupercharger, it includes frame (1), taper support (2), Magnetic Induction tachogenerator (3), digital display screen (6), instrument display control program (7), volute gas outlet (8), compressor casing gas outlet (11), rubber hose (12), air intake opening (13), technology volute (42), compressor casing air intake opening (50), it is characterized in that it also includes two knob flowmeter assemblies (4) of air inlet on the intermediate support plate (47) that is located at frame (1), the binary channels pipeline (5) that is being connected with the air inlet mouth of pipe (46) of high speed nozzle (33) L type pipe afterbody in the taper support (2) in intermediate support plate (47) below, the surge pipe that is connected with compressor casing (9) that is provided with on frame (1) rear frame reaches the manual voltage regulation pipe (10) that is connected with surge pipe (9) with volute gas outlet (8).
2, the whole dynamic balancing machine of the described turbosupercharger of root a tree name claim 1, the structure that it is characterized in that the two knob flowmeter assemblies (4) of air inlet has comprised that being located at intermediate support plate (47) goes up by 4 T type bolts, stud bolt (23), the dovetail groove guide rail (32) that setting nut (24) is fixing, the flat board that has dovetail groove (25) that is connected with dovetail groove guide rail (32) in dovetail groove guide rail (32) top, go up with the two knob flowmeter trunnions (26) of the fixing air inlet of pipe collar in dull and stereotyped (25), dull and stereotyped (25) are connecting cylinder piston rod (30) by bolt contiguous block (31), on the tube wall of the two knob flowmeter trunnions (26) of air inlet, be drilled with two apertures (29), be provided with inlet temperature sensor (27) in one of them aperture, another aperture (29) is connecting pressure unit (28) by rubber hose (12), and the two knob flowmeter assemblies (4) of air inlet can be done the adjustment of space three-dimensional direction on intermediate support plate (47).
3, the whole dynamic balancing machine of the described turbosupercharger of root a tree name claim 1, it is characterized in that binary channels pipeline (5) includes the manual draft tube (34) that has manual ball valve (35), the automatic draft tube (41) of machinery that has electric-controlled ball valve (38), tooth bar rotary oil cylinder ball valve (39), three-position four-way valve (40), manually draft tube (34), the automatic draft tube (41) of machinery are connected with three-way pipe (36) respectively with the air inlet mouth of pipe (37) that compressor compresses air source of the gas links to each other.
4, the whole dynamic balancing machine of the described turbosupercharger of root a tree name claim 1, the structure that it is characterized in that surge pipe (9) is, opening at one end, one end has in the pipe (21) of end plate (17) and is provided with by being bolted to the hydraulic cylinder (20) on the end plate (17), bulb variable valve (16) is connected by the piston rod of connecting rod with hydraulic cylinder (20), upward connecting a grade bar (18) that is located in the pipe (21) at bulb variable valve (16) with bolt, the clock gauge (19) that contact contacts with grade bar (18) is fastened on the pipe (21), is provided with outlet pressure sensor (14) on the tube wall of top, end plate (17) left side, outlet temperature sensor (15), the below tube wall is provided with the mouth of pipe of giving vent to anger (22).
5, the whole dynamic balancing machine of the described turbosupercharger of root a tree name claim 1, it is characterized in that manual voltage regulation pipe (10) is to be connected to form by middle manually operated control valve (53) by draft tube (51) and escape pipe (52), the mouth of pipe of its draft tube (51) is connected with the mouth of pipe of giving vent to anger (22) of surge pipe (9), and the mouth of pipe of escape pipe (52) is connected with volute gas outlet (8).
6, the whole dynamic balancing machine of the described turbosupercharger of root a tree name claim 1, it is characterized in that the high speed nozzle (33) that is provided with is an isometrical L type pipe that tiny cone opening (43), afterbody have the air inlet mouth of pipe (46) that is shrunk to suitable for reading in taper support (2), on the circumference in the middle of the L type pipe, be evenly equipped with 4 circular holes (48), be provided with the cavity sealed separation that taper support (2) and back taper support (44) are connected and composed at circular hole (48) upper position and become the seal pad (49) in two chambeies up and down, the lower end of back taper support (44) is air intake opening (45).
CNU2007200164204U 2007-12-01 2007-12-01 Integral dynamic balancing machine for turbo-charger Expired - Fee Related CN201138272Y (en)

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Application Number Priority Date Filing Date Title
CNU2007200164204U CN201138272Y (en) 2007-12-01 2007-12-01 Integral dynamic balancing machine for turbo-charger

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Application Number Priority Date Filing Date Title
CNU2007200164204U CN201138272Y (en) 2007-12-01 2007-12-01 Integral dynamic balancing machine for turbo-charger

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CN201138272Y true CN201138272Y (en) 2008-10-22

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103217255A (en) * 2013-03-12 2013-07-24 中国航空工业集团公司沈阳发动机设计研究所 Field balancing method of aviation product
CN103743521A (en) * 2013-12-30 2014-04-23 常州环能涡轮动力股份有限公司 Integral movable balance clamp of turbocharger
CN104246631A (en) * 2012-03-14 2014-12-24 申克罗泰克有限责任公司 Method and device for pneumatically driving a turbocharger rotor in a balancing machine
CN105458672A (en) * 2016-01-07 2016-04-06 杭州高品自动化设备有限公司 Assembly table for core bodies
CN107939902A (en) * 2017-11-15 2018-04-20 合肥动联自动化科技有限公司 Integrated shock absorption test tool of turbocharger dynamic balance test machine
CN117129143A (en) * 2023-10-26 2023-11-28 国惠智能科技(江苏)有限公司 Turbine dynamic balance testing machine for aero-engine

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104246631A (en) * 2012-03-14 2014-12-24 申克罗泰克有限责任公司 Method and device for pneumatically driving a turbocharger rotor in a balancing machine
CN103217255A (en) * 2013-03-12 2013-07-24 中国航空工业集团公司沈阳发动机设计研究所 Field balancing method of aviation product
CN103217255B (en) * 2013-03-12 2015-08-12 中国航空工业集团公司沈阳发动机设计研究所 A kind of balancing in situ method of aviation series products
CN103743521A (en) * 2013-12-30 2014-04-23 常州环能涡轮动力股份有限公司 Integral movable balance clamp of turbocharger
CN103743521B (en) * 2013-12-30 2016-02-17 常州环能涡轮动力股份有限公司 Integral movable balance clamp of turbocharger
CN105458672A (en) * 2016-01-07 2016-04-06 杭州高品自动化设备有限公司 Assembly table for core bodies
CN105458672B (en) * 2016-01-07 2017-06-27 杭州高品自动化设备有限公司 Core body assembly bench
CN107939902A (en) * 2017-11-15 2018-04-20 合肥动联自动化科技有限公司 Integrated shock absorption test tool of turbocharger dynamic balance test machine
CN107939902B (en) * 2017-11-15 2019-07-02 安徽博联自动化工程技术有限公司 A kind of integrated damping test fixture of turbocharger dynamic balance testing machine
CN117129143A (en) * 2023-10-26 2023-11-28 国惠智能科技(江苏)有限公司 Turbine dynamic balance testing machine for aero-engine
CN117129143B (en) * 2023-10-26 2023-12-22 国惠智能科技(江苏)有限公司 Turbine dynamic balance testing machine for aero-engine

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C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20081022

Termination date: 20101201