CN205981068U - Axiality debugging and verifying attachment - Google Patents
Axiality debugging and verifying attachment Download PDFInfo
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- CN205981068U CN205981068U CN201620439294.2U CN201620439294U CN205981068U CN 205981068 U CN205981068 U CN 205981068U CN 201620439294 U CN201620439294 U CN 201620439294U CN 205981068 U CN205981068 U CN 205981068U
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- equipment
- axiality
- positioning disk
- gyroaxis
- debugging
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Abstract
The utility model discloses an axiality debugging and verifying attachment for the axiality of the revolving axle between debugging and inspection machine, include: a pedestal, the base is used for the activity to set up first equipment and second equipment, makes the one end of the revolving axle of first equipment with the one end of the revolving axle of second equipment is relative, still includes: first positioning disk, second positioning disk and duo gen feeler gauge, the centre bore of first positioning disk can be used to wear the cover and is in the one end of the revolving axle of first equipment, the centre bore of second positioning disk can be used to wear the cover and is in the one end of the revolving axle of second equipment, be provided with a plurality of positioning channel section on the edge of first positioning disk, be provided with a plurality of the 2nd positioning channel section on the edge of second positioning disk, one a positioning channel section and one the 2nd positioning channel section corresponds, each root the feeler gauge can be used to to imbed corresponding each a positioning channel section and each among the 2nd positioning channel section. The device accommodation is wider.
Description
Technical field
The utility model is related to axiality debugging and inspection technology field, and more particularly to a kind of axiality is debugged and inspection
Device.
Background technology
" axiality of gyroaxis between equipment " refers in power-transmission system two independences and can mutually transmit power
Misaligned degree between two equipment axiss of rotation.Its actual existence form shows as following several two kinds of forms：(1) two revolution
Axis is mutually inclined；(2) two axiss of rotation offset from each other, and axis of rotation offsets from each other and shows as, two axis be parallel to each other but
Misaligned, offset from each other certain distance.In fact, the not coaxial error of axis of rotation often shows as both the above between equipment
The combination of deviation.It is necessary to the coaxiality error between the revolving body of each component devices is adjusted to allowed band during equipment assembling
Interior, guarantee dynamical system is reliably run.If not being adjusted to, in the range of permission, be likely to occur in the equipment course of work
Stronger vibration and noise, it is also possible to leading to equipment fault, shortening the life-span, possibly even cause security incident when serious.
At present, the debugging of axis of rotation axiality and the method for inspection are generally：First the power-equipment needing docking is placed
The axiality of gyroaxis on reference platform so as to after axis of rotation is substantially aligned, is measured using dial gauge or amesdial；If
There is not coaxial error, realize little position in the form of copper rod taps power-equipment and move, gradually returning two power-equipments
Within the scope of shaft axis are adjusted to the axiality allowing.But, existing axiality debugging is had the following disadvantages with the method for inspection：First
First, some occasions are less due to the spacing between two power-equipments, and the dial gauge of measurement axiality or amesdial are subject to space
Restriction cannot be installed；Also the shaft diameter of appearance revolution sometimes is too little, and the magnetic support absorption of installation dial gauge is unreliable to also often result in survey
Amount is inaccurate；Secondly, check the axiality of two power-equipment axiss of rotation according to the method described above, need to fix an one rotating shaft,
Rotate another one rotating shaft, that is, two axles need relative motion simultaneously.For already installed dynamical system, because shaft coupling
The presence of device, two one rotating shafts can only synchronous rotary it is impossible to realize relative motion.So, power system operational for a period of time after,
The axiality of equipment room gyroaxis cannot be checked under the conditions of not dismounting couplers.That is, according to the existing method of inspection,
The axiality of gyroaxis between two power-equipments of dynamical system, is not verifiable under its working condition.Therefore, it is badly in need of out
The axiality debugging sending out equipment room gyroaxis a kind of and verifying attachment.
Utility model content
The purpose of this utility model is to provide a kind of axiality debugging and verifying attachment, is not limited by bulk,
Accommodation is wider, can achieve that not tearing shaft coupling open just can check axiality, can recheck between the equipment of dynamical system online
Axiality.
The technical solution of the utility model is as follows：
A kind of debugging of axiality and verifying attachment, for debug and check equipment room gyroaxis axiality, including：Bottom
Seat, described base is used for activity setting the first equipment and the second equipment, makes one end of gyroaxis of described first equipment and described
One end of the gyroaxis of the second equipment relatively, also includes：First positioning disk, the second positioning disk and Duo Gen feeler gauge, described first is fixed
The centre bore of position disk can be used for being set on one end of the gyroaxis of described first equipment, and the centre bore of described second positioning disk can use
Multiple first locator cards are provided with the one end of the gyroaxis being set on described second equipment, the edge of described first positioning disk
Groove, the edge of described second positioning disk is provided with multiple second locating grooves, described first locating groove and an institute
State the second locating groove to correspond to, each described feeler gauge can be used for embedding corresponding each described first locating groove and each
In described second locating groove.
Further：Multiple described first locating grooves are uniformly distributed on the edge of described first positioning disk, multiple described
Second locating groove is uniformly distributed on the edge of described second positioning disk.
Further：The quantity of described first locating groove is four, and the quantity of described second locating groove is four, described
The quantity of feeler gauge is four.
Further：When each described feeler gauge all can be respectively embedded into corresponding each described first locating groove and every simultaneously
When in the second locating groove described in, the gyroaxis of the gyroaxis of described first equipment and described second equipment is in coaxial shape
State.
Further：Described first positioning disk and described second positioning disk are circle.
Further：Described first positioning disk and the area equation of described second positioning disk.
Compared with prior art, the utility model has advantages below：
1st, axiality debugging of the present utility model and verifying attachment, without using dial gauge or amesdial, are not subject to space chi
Very little restriction, accommodation is wider.
2nd, axiality debugging of the present utility model and verifying attachment, without using dial gauge or amesdial, therefore, measured
Cheng Buyong reading, record, easy to operate.
3rd, axiality debugging of the present utility model and verifying attachment, need not carry out relative motion between equipment axis of rotation,
In the case of may be implemented in the shaft coupling between not detaching equipment, recheck the axiality of axis, reduce answering of axiality inspection
Miscellaneous degree, improves simple operation degree and quality inspection.
4th, axiality of the present utility model debugging and verifying attachment can be applicable to Aeronautics and Astronautics, weapons, ship, robot,
Between the power-equipment in the fields such as automobile, wind-power electricity generation, the energy, the debugging of the axiality of gyroaxis is rechecked with online.
Brief description
Fig. 1 is the use state explosive view of axiality debugging of the present utility model and verifying attachment.
Specific embodiment
Understandable for enabling above-mentioned purpose of the present utility model, feature and advantage to become apparent from, below in conjunction with the accompanying drawings and real
Apply example to be described in further detail.
The utility model discloses a kind of axiality debugging and verifying attachment.The debugging of this axiality is used for adjusting with verifying attachment
The axiality of the gyroaxis of examination and inspection equipment room, particularly, axiality debugging is used for debugging with verifying attachment and upchecks
The axiality of the gyroaxis of equipment room that shaft coupling connects.
As shown in figure 1, the use state explosive view for axiality debugging of the present utility model and verifying attachment.This axiality
Debugging is included with verifying attachment：Base 4, the first positioning disk 1, the second positioning disk 2 and Duo Gen feeler gauge 3.Base 4 is used for activity setting
First equipment 5 and the second equipment 6, make one end of gyroaxis 51 of the first equipment 5 and one end phase of the gyroaxis 61 of the second equipment 6
Right.Preferably, the chute that this base 4 can be cooperated by setting and slideway, the first equipment 5 and the second equipment 6 are arranged
Slideway make the first equipment 5 slide to adjust the relative position of the first equipment 5 and the second equipment 6 on chute with the second equipment 6
Put, make the gyroaxis 51 of the first equipment 5 and the axis almost coaxial of the gyroaxis 61 of the second equipment 6.
The centre bore of the first positioning disk 1 can be used for being set on one end of the gyroaxis 51 of the first equipment 5.Second positioning disk 2
Centre bore can be used for being set on one end of the gyroaxis 61 of the second equipment 6.It is provided with multiple on the edge of the first positioning disk 1
One locating groove 11.Multiple second locating grooves 21 are provided with the edge of the second positioning disk 2.One the first locating groove 11 He
One the second locating groove 21 is corresponding.Each feeler gauge 3 can be used for embedding corresponding every one first locating groove 11 and each
In second locating groove 21.
Preferably, multiple first locating grooves 11 are uniformly distributed on the edge of the first positioning disk 1.Multiple second locator cards
Groove 21 is uniformly distributed on the edge of the second positioning disk 2.
Preferably, the quantity of the first locating groove 11 is four.The quantity of the second locating groove 21 is four.Feeler gauge 3
Quantity is four.
Preferably, when each feeler gauge 3 all can be respectively embedded into corresponding every one first locating groove 11 and every 1 simultaneously
When in two locating grooves 21, the gyroaxis 61 of the gyroaxis 51 of the first equipment 5 and the second equipment 6 is in coaxial state.
Preferably, the first positioning disk 1 and the second positioning disk 2 is circle so that the inspection to axiality is more accurate.Excellent
Choosing, the area equation of the first positioning disk 1 and the second positioning disk 2 is so that the inspection to axiality is more accurate.
Preferably, this axiality debugging is also included with verifying attachment：Trip bolt 8.Gyroaxis 51 when first equipment 5
One end of the gyroaxis 61 of one end and the second equipment 6 pass through shaft coupling 7 connect when, trip bolt 8 be used for by the first positioning disk 1,
Second positioning disk 2 is connected with shaft coupling 7 respectively, thus the first positioning disk 1, the second positioning disk 2 are fixed on one with shaft coupling 7
Rise.
Axiality debugging of the present utility model is following with the occupation mode of verifying attachment (to be lifted with the quantity of feeler gauge 3 for four
Example explanation)：First the first equipment 5 and the second equipment 6 are movably disposed on base 4.First positioning disk 1 is arranged on
One end of the gyroaxis 51 of one equipment 5, the second positioning disk 2 is arranged on one end of the gyroaxis 61 of the second equipment 6.Then unclamp
Locking nut on shaft coupling 7, one end of one end of the gyroaxis 51 of the first equipment 5 and the gyroaxis 61 of the second equipment 6 is divided
Do not penetrate in shaft coupling 7 from the two ends of shaft coupling 7.Move repeatedly the first equipment 5 and the second equipment 6, make returning of the first equipment 5
The axis almost coaxial of the gyroaxis 61 of rotating shaft 51 and the second equipment 6.In this process, four feeler gauges 3 are respectively embedded into simultaneously
First locating groove 11 of the first positioning disk 1 neutralizes in the second locating groove 21 of the second positioning disk 2, until four feeler gauges 3 are complete
Portion can be embedded in the first locating groove 11 and the second locating groove 21, shows that the gyroaxis 51 of the first equipment 5 and second sets
The axiality of standby 6 gyroaxis 61 has adjusted and has put in place, and now the nut on locking shaft coupling 7, completes to assemble and debug.Debugging
After finishing, the trip bolt 8 at the first positioning disk 1 and the second positioning disk 2 two ends and shaft coupling 7 are fixed together, prevent at a high speed
During rotation, between the first positioning disk 1, the second positioning disk 2 and shaft coupling 7, there is relative slip.
After equipment runs a period of time, the first locating groove 11 that feeler gauge 3 can be placed on the first positioning disk 1 neutralizes second
In second locating groove 21 of positioning disk 2.If four feeler gauges 3 can be simultaneously placed to corresponding four group first locating groove
It was demonstrated that coaxial between the gyroaxis 61 of the gyroaxis 51 of the first equipment 5 and the second equipment 6 in 11 neutralization the second locating grooves 21
Degree keeps good, and equipment can work on；Otherwise, illustrate the gyroaxis 51 of the first equipment 5 and the second equipment 6 gyroaxis 61 it
Between axiality occurred in that deviation, need to re-start regulation.
In sum, axiality debugging of the present utility model and verifying attachment, without using dial gauge or amesdial, are not subject to
The restriction of bulk, accommodation is wider, and measurement process is without reading, record, easy to operate, between equipment axis of rotation no
Relative motion need to be carried out, in the case of may be implemented in the shaft coupling between not detaching equipment, recheck the axiality of axis, reduce
The complexity of axiality inspection, improves simple operation degree and quality inspection.
Based on above-mentioned beneficial effect, axiality debugging of the present utility model and verifying attachment can be applicable to Aeronautics and Astronautics,
Between the power-equipment in the fields such as weapons, ship, robot, automobile, wind-power electricity generation, the energy debugging of the axiality of gyroaxis with
Online reinspection.
Above to the technical solution of the utility model, it is described in detail, specific case used herein is to this reality
It is set forth with new principle and embodiment, the explanation of above example is only intended to help understanding of the present utility model
Core concept；Simultaneously for one of ordinary skill in the art, according to the thought of the utility model embodiment, it is being embodied as
All will change in mode and range of application, in sum, this specification content should not be construed as real to the utility model
Apply the restriction of example.
Claims (6)
1. a kind of debugging of axiality and verifying attachment, for debug and check equipment room gyroaxis axiality, including：Bottom
Seat, described base is used for activity setting the first equipment and the second equipment, makes one end of gyroaxis of described first equipment and described
One end of the gyroaxis of the second equipment is relatively it is characterised in that also include：First positioning disk, the second positioning disk and Duo Gen feeler gauge,
The centre bore of described first positioning disk can be used for being set on one end of the gyroaxis of described first equipment, described second positioning
The centre bore of disk can be used for being set on one end of the gyroaxis of described second equipment, and the edge of described first positioning disk is provided with
Multiple first locating grooves, the edge of described second positioning disk is provided with multiple second locating grooves, and one described first fixed
Position draw-in groove and described second locating groove correspond to, and each described feeler gauge can be used for embedding corresponding each described first
In locating groove and each described second locating groove.
2. axiality as claimed in claim 1 debugging with verifying attachment it is characterised in that：Multiple described first locating grooves exist
It is uniformly distributed on the edge of described first positioning disk, multiple described second locating grooves are equal on the edge of described second positioning disk
Even distribution.
3. axiality as claimed in claim 2 debugging with verifying attachment it is characterised in that：The quantity of described first locating groove
For four, the quantity of described second locating groove is four, and the quantity of described feeler gauge is four.
4. as described in any one of claims 1 to 3 axiality debugging with verifying attachment it is characterised in that：When each described plug
When rule all can be respectively embedded in corresponding each described first locating groove and each described second locating groove simultaneously, described
The gyroaxis of the gyroaxis of the first equipment and described second equipment is in coaxial state.
5. axiality as claimed in claim 1 debugging with verifying attachment it is characterised in that：Described first positioning disk and described
Two positioning disks are circle.
6. axiality as claimed in claim 1 debugging with verifying attachment it is characterised in that：Described first positioning disk and described
The area equation of two positioning disks.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620439294.2U CN205981068U (en) | 2016-05-16 | 2016-05-16 | Axiality debugging and verifying attachment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620439294.2U CN205981068U (en) | 2016-05-16 | 2016-05-16 | Axiality debugging and verifying attachment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205981068U true CN205981068U (en) | 2017-02-22 |
Family
ID=58019443
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620439294.2U Expired - Fee Related CN205981068U (en) | 2016-05-16 | 2016-05-16 | Axiality debugging and verifying attachment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205981068U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107687822A (en) * | 2017-09-22 | 2018-02-13 | 中核（天津）机械有限公司 | A kind of axiality detects method of adjustment |
-
2016
- 2016-05-16 CN CN201620439294.2U patent/CN205981068U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107687822A (en) * | 2017-09-22 | 2018-02-13 | 中核（天津）机械有限公司 | A kind of axiality detects method of adjustment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170222 Termination date: 20190516 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |