CN201497481U - Multipurpose turbine device axiality checking device - Google Patents

Multipurpose turbine device axiality checking device Download PDF

Info

Publication number
CN201497481U
CN201497481U CN2009203111335U CN200920311133U CN201497481U CN 201497481 U CN201497481 U CN 201497481U CN 2009203111335 U CN2009203111335 U CN 2009203111335U CN 200920311133 U CN200920311133 U CN 200920311133U CN 201497481 U CN201497481 U CN 201497481U
Authority
CN
China
Prior art keywords
connecting link
circle
measuring bar
rod
checking
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 - Lifetime
Application number
CN2009203111335U
Other languages
Chinese (zh)
Inventor
张世清
郭俊
王铁钢
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.)
Wuhan iron and Steel Group Gas Co Ltd
Original Assignee
Wuhan Iron and Steel Group Corp
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 Wuhan Iron and Steel Group Corp filed Critical Wuhan Iron and Steel Group Corp
Priority to CN2009203111335U priority Critical patent/CN201497481U/en
Application granted granted Critical
Publication of CN201497481U publication Critical patent/CN201497481U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • A Measuring Device Byusing Mechanical Method (AREA)

Abstract

The utility model relates to the alignment technique of mechanical equipment couplings, which is particularly applicable to checking turbine type compressor checking axiality, and discloses a multipurpose turbine device axiality checking device, which comprises a measuring bar, wherein a dial indicator is installed on the measuring bar, the measuring bar is connected with an end surface of a compressor coupling, the multipurpose turbine device axiality checking device is characterized by further comprising a connecting rod and a measuring bar frame, wherein the connecting rod is connected with the measuring bar frame, the length of the connecting rod and the measuring bar can be adjusted, one end of the connecting rod is connected on the central position of a speed increaser coupling, and the other end is movably connected with the measuring bar through the measuring bar frame. The device can rapidly and accurately locate, executes axiality finding, has accurate measurement, high working efficiency, simple structure, low cost, small volume, light weight, convenient operation and low labor intensity, and is a necessary attaching device for checking turbine equipment in the industries such as oil chemical industry, steel metallurgy, gas separation and the like, and has wide market prospect.

Description

A kind of multi-usage turbine equipment axiality detection device
Technical field
The utility model relates to the centering technology of plant equipment shaft coupling, is particularly useful for the detection of turbo-compressor maintenance right alignment.
Background technology
Turbo-compressor is one of important production equipment of deep cooling industry, is widely used in industries such as petrochemical complex, Ferrous Metallurgy and gas separation.Need dismantle the shaft coupling between motor and booster engine, booster engine and the compressor during turbo-compressor maintenance, check, adjust its right alignment.Searching of turbo-compressor transmission shaft right alignment is a rather important link in the maintenance operation, and its measurement data is one of important comparable data of Plant maintenance quality, is that assurance equipment is steady, the precondition of safe operation.
With right alignment centering between booster engine and the compressor is example, and the unsteady coupling shaft of booster engine, compressor chamber is removed in maintenance before this earlier, is that benchmark is installed special-purpose centering connecting pipe with the booster engine; Lean on compressor one side by radially reaching three dial gauges of axial installation at the centering connecting pipe; Hanging belt one end is fixed on the connecting screw and around booster engine takes over three circles, the other end is connected to the bottle gouard moved by hands that hangs on the overhead traveling crane suspension hook; The pulling cucurbit makes hanging belt drive the rotation of speedup arbor, and each half-twist is carried out the record of centering value, by calculating the right alignment value of booster engine and compressor.
There is following defective in existing special-purpose centering connecting pipe in upkeep operation:
1. because of each coupling shaft shaft coupling size of compressor, spacing difference, the diameter of special-purpose connecting pipe, length are also different, do not have a versatility, and spare part is deposited inconvenience at storehouse.
2. the centering connecting pipe quality of available technology adopting, volume big (long 1.5M, diameter 0.5M, wall thickness 10mm, heavy 150Kg) are installed, dismounting labour intensity height, need each 1 of craneman, frame worker, 3 use overhead traveling cranes of pincers worker cooperate install, measurement.
The utility model content
Technical problem to be solved in the utility model provides a kind of multi-usage turbine equipment axiality detection device, it has the building block that comprises connecting link, sounding rod and measurement bridge, and connecting link and sounding rod adjustable length make this device can be applied to the characteristics that all kinds of turbocompressor maintenance right alignmenies are searched.
For solving the problems of the technologies described above, a kind of multi-usage turbine equipment axiality detection device that the utility model provides comprises sounding rod, dial gauge is installed on the sounding rod, and sounding rod is connected with the compressor coupling end-face, it is characterized in that, also comprise connecting link and measure bridge
Described connecting link is connected with the measurement bridge, connecting link and sounding rod adjustable length, and an end of connecting link is connected booster engine shaft coupling center position, and the other end flexibly connects by measuring bridge and described sounding rod.
To being improved to of above-mentioned foundation structure, described connecting link comprises the head rod and second connecting link, one end of head rod is connected booster engine shaft coupling center position, the other end is connected by removable mode with the end of second connecting link, the other end of second connecting link flexibly connects by measuring bridge and sounding rod, realizes the connecting link adjustable length by increase and decrease connecting link quantity.
The another of above-mentioned foundation structure is improved to, also comprise movable shoulder circle, described movable shoulder snare is contained on the connecting link, the circle heart of movable shoulder circle is positioned on the connecting link axis, have the hole on around the movable shoulder circle, hole on the wire rope one end connection activity shoulder circle, other end connecting screw rod, screw rod is connected with screw on the booster engine shaft coupling.
To the structure after the above-mentioned improvement be further improved into, also comprise movable shoulder circle, described movable shoulder snare is contained on second connecting link, the circle heart of movable shoulder circle is positioned on the connecting link axis, have the hole on around the movable shoulder circle, hole on the wire rope one end connection activity shoulder circle, other end connecting screw rod, screw rod is connected with screw on the booster engine shaft coupling.
Said structure further is improved to the scalable adjusting of described measurement bridge.
Advantage of the present utility model is:
1. a kind of multi-usage turbine equipment axiality detection device is provided, and the adjustable length of its connecting link and sounding rod can satisfy the actual demand that all kinds of turbocompressor maintenance of industries such as petrochemical complex, Ferrous Metallurgy and gas separation right alignment is searched and measured.Solved prior art because of each shaft coupling diameter of compressor, spacing difference, the diameter of special-purpose connecting pipe, length are also different, do not have a problem of versatility, and have also solved the problem that special-purpose spare part is not easy to deposit in the prior art.
2. easy and simple to handle, efficient is high: the operator only needs on request that order connect each parts, and the level of adjusting can begin to search right alignment, measures accurately, reliable rapidly.
3. the more piece connecting link interconnects the utility model by adopting, the mode that flexibly connects between connecting link and measurement bridge, the sounding rod, utilize that each volume is light, the less accessory of weight need carry out flexible assembly to the scene, centering connecting pipe than available technology adopting, can reduce to install, dismantle labour intensity, only need each 1 of craneman, frame worker and pincers worker, can use overhead traveling crane to cooperate and install, measure.
This device can quick and precisely be located, the enforcement right alignment is searched, it is measured accurately, high efficiency, simple in structure, cost is low, volume is little, in light weight, control conveniently, labour intensity is low, be the requisite auxiliary devices of industry turbine overhaul of the equipments such as petrochemical complex, Ferrous Metallurgy and gas separation, market outlook are good.
Description of drawings
Below in conjunction with the drawings and specific embodiments the technical solution of the utility model is further described in detail.
Fig. 1 is the utility model work synoptic diagram.
Fig. 2 is special-purpose centering connecting pipe work synoptic diagram.
Wherein, the 1-head rod, 2-second connecting link, 3-measures bridge, the 4-sounding rod, the movable shoulder circle of 5-, 6-wire rope, 7-nut, the 8-screw rod, 9-dial gauge support, 10-dial gauge, 11-booster engine shaft coupling, 12-compressor shaft coupling, 13-speedup arbor, 14-are connected to the wire rope of bottle gouard moved by hands on the little hook of overhead traveling crane, 15-compressor shaft, the 16-connecting pipe of feeling relieved, the 17-compressor, the 18-booster engine, 19-jackscrew, 20-chain block.
Embodiment
The utility model work synoptic diagram that reference is shown in Figure 1: at first, process the head rod 1 and second connecting link 2, utilize the threaded hole of booster engine shaft coupling center, head rod 1 one ends are processed matching thread and are connected the shaft coupling center, be connected by removable mode between head rod 1 and second connecting link 2, the preferred employing is threaded.Measure the top that bridge 3 is inserted into second connecting link 2, and circumferentially fixing with four jackscrews.
For measuring bridge 3, preferred design proposal is, measures bridge 3 and can freely adjust the length of stretching out within the specific limits, can adjust the spacing with connecting link in right amount, and the scope of this spacing is 0 ~ 20mm preferably.
Then, process a sounding rod 4, sounding rod 4 interts in the measurement bridge 3, and is circumferentially fixing with two jackscrews 19, and three dial gauges 10 are fixed on the sounding rod 4.Search and measure in order to make the utility model can be applied to all kinds of turbocompressor maintenance right alignmenies, the length of sounding rod 4 is wanted can be adjustable, can process the sounding rod 4 of different length according to the diameter of distinct device shaft coupling, also sounding rod 4 can be designed to be matched with sleeve by screw mandrel, regulate the structure of length by being threaded.
For the levelness between the interconnective head rod 1 of more accurate adjusting and second connecting link 2, prevent to occur because of its following of generation of conducting oneself with dignity around phenomenon because of connecting link is long, set up the end that movable shoulder circle 5 is sleeved on connecting link 2, offer four fabrication holes on the movable shoulder circle 5, put on wire rope 6 respectively, wire rope 6 other ends are installed with screw rod 8.
Sketch principle of work of the present utility model below in conjunction with accompanying drawing.After according to above-mentioned connected mode the utility model being assembled, the utility model is installed on the turbo-compressor: utilize the thread end that matches with booster engine shaft coupling 11 center threaded holes on the connecting link that the utility model is connected with booster engine 18; Fix three dial gauges 10 on sounding rod 4, it is vertical and keep certain pressure to guarantee that dial gauge bar and compressor are taken over 12 end faces, in the measurement range obstacle must not be arranged; Wire rope 6 is installed in the screw of booster engine shaft coupling 11 by screw rod 8 and nut 7, by adjusting the screwing length of four nuts 7 and screw rod 8, tense wire rope 6 cooperates winding degree (rigidity) and the levelness of adjusting between the interconnective head rods 1 and second connecting link 2; For ease of operating and making the utility model can be applicable to large-scale or large equipment, with wire rope 14 on speedup arbor 13, during use, cooperate pulling to lead the manual jiggering of chain with overhead traveling crane, each half-twist, carry out survey record,, require to adjust its right alignment according to correlation technique then by calculating the right alignment value of booster engine and compressor.
Connected mode between the connecting link is not limited to above-mentioned, can also optionally take other type of attachment, reach requirement and can realize purpose described in the utility model as long as reach the right alignment that makes between the connecting link and winding degree (rigidity), those skilled in the art can understand fully, so do not enumerate one by one.
It should be noted last that, above embodiment is only unrestricted in order to the explanation the technical solution of the utility model, although the utility model is had been described in detail with reference to preferred embodiment, those of ordinary skill in the art is to be understood that, can make amendment or be equal to replacement the technical solution of the utility model, and not breaking away from the spirit and scope of technical solutions of the utility model, it all should be encompassed in the middle of the claim scope of the present utility model.

Claims (5)

1. a multi-usage turbine equipment axiality detection device comprises sounding rod, and dial gauge is installed on the sounding rod, and sounding rod is connected with the compressor coupling end-face, it is characterized in that, also comprise connecting link and measure bridge,
Described connecting link is connected with the measurement bridge, connecting link and sounding rod adjustable length, and an end of connecting link is connected booster engine shaft coupling center position, and the other end flexibly connects by measuring bridge and described sounding rod.
2. a kind of multi-usage turbine equipment axiality detection device as claimed in claim 1, it is characterized in that, described connecting link comprises the head rod and second connecting link, one end of head rod is connected booster engine shaft coupling center position, the other end is connected by removable mode with the end of second connecting link, the other end of second connecting link flexibly connects by measuring bridge and sounding rod, realizes the connecting link adjustable length by increase and decrease connecting link quantity.
3. a kind of multi-usage turbine equipment axiality detection device as claimed in claim 1, it is characterized in that, also comprise movable shoulder circle, described movable shoulder snare is contained on the connecting link, the movable circle heart of takeing on circle is positioned on the connecting link axis, and movable shoulder circle has the hole all around, the hole on the wire rope one end connection activity shoulder circle, other end connecting screw rod, screw rod is connected with screw on the booster engine shaft coupling.
4. a kind of multi-usage turbine equipment axiality detection device as claimed in claim 2, it is characterized in that, also comprise movable shoulder circle, described movable shoulder snare is contained on second connecting link, the movable circle heart of takeing on circle is positioned on the connecting link axis, and movable shoulder circle has the hole all around, the hole on the wire rope one end connection activity shoulder circle, other end connecting screw rod, screw rod is connected with screw on the booster engine shaft coupling.
5. as any described a kind of multi-usage turbine equipment axiality detection device in the claim 1 to 4, it is characterized in that the scalable adjusting of described measurement bridge.
CN2009203111335U 2009-09-23 2009-09-23 Multipurpose turbine device axiality checking device Expired - Lifetime CN201497481U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009203111335U CN201497481U (en) 2009-09-23 2009-09-23 Multipurpose turbine device axiality checking device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009203111335U CN201497481U (en) 2009-09-23 2009-09-23 Multipurpose turbine device axiality checking device

Publications (1)

Publication Number Publication Date
CN201497481U true CN201497481U (en) 2010-06-02

Family

ID=42440685

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009203111335U Expired - Lifetime CN201497481U (en) 2009-09-23 2009-09-23 Multipurpose turbine device axiality checking device

Country Status (1)

Country Link
CN (1) CN201497481U (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102288096A (en) * 2011-05-18 2011-12-21 中国航空动力机械研究所 Shaft declination angle measurement device
CN102506668A (en) * 2011-10-28 2012-06-20 中国核工业二三建设有限公司 No-deflection centering device
CN102829705A (en) * 2012-08-09 2012-12-19 江苏兴达钢帘线股份有限公司 Concentricity detection device
CN104034531A (en) * 2014-05-26 2014-09-10 芜湖水泵制造有限公司 Four-claw clamping type centering device for engine simulation experiment
CN104061247A (en) * 2014-06-23 2014-09-24 山东电力建设第一工程公司 Center aligning disk driving device for rotor coupling of steam turbine generator unit
CN104062052A (en) * 2014-05-26 2014-09-24 芜湖水泵制造有限公司 Central calibration device between progressive engine and dynamometer
CN104090582A (en) * 2014-08-06 2014-10-08 芜湖水泵制造有限公司 Center calibration device for engine vibration experiment
CN104089779A (en) * 2014-08-06 2014-10-08 芜湖水泵制造有限公司 Spiral push type centering device for engine simulation experiment
WO2015066950A1 (en) * 2013-11-08 2015-05-14 李君� Coaxiality detection apparatus
CN105066919A (en) * 2015-07-15 2015-11-18 南车株洲电机有限公司 Testing system and synchronous testing device thereof
CN105170702A (en) * 2015-09-25 2015-12-23 宝钢特钢有限公司 Center measurement and adjustment method for steel pipe heat extruder
CN105841972A (en) * 2016-04-26 2016-08-10 中科合肥微小型燃气轮机研究院有限责任公司 Alignment device for gas turbine testing stand
CN114459307A (en) * 2022-02-23 2022-05-10 桂林广陆数字测控有限公司 Digital display dial gauge

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102288096A (en) * 2011-05-18 2011-12-21 中国航空动力机械研究所 Shaft declination angle measurement device
CN102506668A (en) * 2011-10-28 2012-06-20 中国核工业二三建设有限公司 No-deflection centering device
CN102506668B (en) * 2011-10-28 2015-07-29 中国核工业二三建设有限公司 Without deflection centering device
CN102829705A (en) * 2012-08-09 2012-12-19 江苏兴达钢帘线股份有限公司 Concentricity detection device
WO2015066950A1 (en) * 2013-11-08 2015-05-14 李君� Coaxiality detection apparatus
CN104034531A (en) * 2014-05-26 2014-09-10 芜湖水泵制造有限公司 Four-claw clamping type centering device for engine simulation experiment
CN104062052A (en) * 2014-05-26 2014-09-24 芜湖水泵制造有限公司 Central calibration device between progressive engine and dynamometer
CN104061247A (en) * 2014-06-23 2014-09-24 山东电力建设第一工程公司 Center aligning disk driving device for rotor coupling of steam turbine generator unit
CN104061247B (en) * 2014-06-23 2016-03-02 山东电力建设第一工程公司 Rotor of turbogenerator set coupling center centering shaft turning gear
CN104089779A (en) * 2014-08-06 2014-10-08 芜湖水泵制造有限公司 Spiral push type centering device for engine simulation experiment
CN104090582A (en) * 2014-08-06 2014-10-08 芜湖水泵制造有限公司 Center calibration device for engine vibration experiment
CN104090582B (en) * 2014-08-06 2017-02-15 芜湖水泵制造有限公司 Center calibration device for engine vibration experiment
CN105066919A (en) * 2015-07-15 2015-11-18 南车株洲电机有限公司 Testing system and synchronous testing device thereof
CN105170702A (en) * 2015-09-25 2015-12-23 宝钢特钢有限公司 Center measurement and adjustment method for steel pipe heat extruder
CN105170702B (en) * 2015-09-25 2018-06-01 宝钢特钢有限公司 A kind of steel pipe heat extruder center measurement, method of adjustment
CN105841972A (en) * 2016-04-26 2016-08-10 中科合肥微小型燃气轮机研究院有限责任公司 Alignment device for gas turbine testing stand
CN105841972B (en) * 2016-04-26 2019-04-30 中科合肥微小型燃气轮机研究院有限责任公司 Aligning device for test bench for gas turbine
CN114459307A (en) * 2022-02-23 2022-05-10 桂林广陆数字测控有限公司 Digital display dial gauge

Similar Documents

Publication Publication Date Title
CN201497481U (en) Multipurpose turbine device axiality checking device
CN206132036U (en) Hole awl measuring device
CN102284925B (en) Tool and method for replacing shaft bushing at big end of connecting rod of diesel engine of million-kilowatt-class nuclear power plant
CN204228409U (en) RV speed reduction unit drive characteristic test macro
CN207557140U (en) Piston face defect detecting device
CN202188833U (en) Roundness measurement instrument of steel pipe
CN209877824U (en) Measuring device for vertical displacement of beam bridge superstructure
CN101126635A (en) Method for measuring large-scale workpiece taper using ring-plane method
CN203672292U (en) Shaft neck roundness detector
CN201876250U (en) Tool for measuring diameter of inner hole of cylinder sleeve
CN107036800B (en) Radial characteristic detecting system of mine head sheave rope groove
CN206321193U (en) A kind of special gauge for IC engine airframe cylinder holes coaxality measurement
CN106768746B (en) Torsion degree measuring method and device for large gear box base
CN202281582U (en) Positioning device for standard inner ring of locomotive bearing radial play measuring instrument
CN205449380U (en) Pulling force pressure test machine
CN202836423U (en) Form and location tolerance detection tool for motor base spigot of motor
CN114486514A (en) Strain strengthening detection device for low-temperature liquid tank container barrel
CN210322337U (en) Auxiliary measuring device for load correction of support hanger
CN208818131U (en) Tooling is examined in the installation of large-sized low-speed exhaust valve of marine diesel engine conical ring
CN205117241U (en) Special bearing fixed chuck of marine well head production tree
CN211783258U (en) Hole site concentricity detection tool for water lubrication oil-free air compressor flange
CN214446003U (en) Cylinder piston rod screwing-out tool
CN204525246U (en) Anchor winch spindle mounted V-type bracket
CN213301501U (en) High-precision thermocouple temperature measuring device
CN210154487U (en) Nuclear power plant pump impeller size measuring tool

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20170721

Address after: 430080, Baiyu mountain, Wuhan City, Hubei province (Gate No. 20, Wuhan)

Patentee after: Wuhan iron and Steel Group Gas Co Ltd

Address before: 430083 Qingshan District, Hubei, Wuhan factory before the door No. 2

Patentee before: Wuhan Iron & Steel (Group) Corp.

TR01 Transfer of patent right
CX01 Expiry of patent term

Granted publication date: 20100602

CX01 Expiry of patent term