CN203257976U - Rotor system automatic balancing device with thermal radiation control - Google Patents
Rotor system automatic balancing device with thermal radiation control Download PDFInfo
- Publication number
- CN203257976U CN203257976U CN 201320221771 CN201320221771U CN203257976U CN 203257976 U CN203257976 U CN 203257976U CN 201320221771 CN201320221771 CN 201320221771 CN 201320221771 U CN201320221771 U CN 201320221771U CN 203257976 U CN203257976 U CN 203257976U
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- rotor
- thermal radiation
- automatic balancing
- system automatic
- rotor system
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Abstract
The utility model relates to a rotor system automatic balancing device with thermal radiation control. The rotor system automatic balancing device with the thermal radiation control is widely applied to rotary mechanical rotor unbalanced systems. The rotor system automatic balancing device with the thermal radiation control is characterized in that the device is arranged at the position of a shaft shoulder of an unbalanced rotor, hollow shaft sections and bearing end covers arranged at two ends of the hollow shaft sections are sealed to form cavites on the middle portion, and pneumatic pistons are arranged on the hollow shaft sections and are communicated with the cavities; sleeve barrels are arranged on the bearing end covers and are used for being connected with the unbalanced rotor; end cover windows are further arranged on the bearing end covers, and the end cover windows are coated with thermal energy absorption materials; thermal radiation sources are arranged at the positions opposite to the end cover windows, and stepping motors are connected with the thermal radiation sources. The rotor system automatic balancing device with the thermal radiation control aims to be capable of eliminating the imbalance of a rotary mechanical rotor system, and due to controllable thermal radiation, the device is made to be high in adjusting precision and convenient to adjust, and the balance of a rotor system is made to achieve the best state.
Description
Technical field
The utility model relates to a kind of rotor-support-foundation system automatic balancing arrangement that adopts thermal radiation to control, and is widely used in the rotary machine rotor unbalanced system.
Background technique
The rotor of rotating machinery is because being subject to the impacts such as quality of materials and processing technique, and epitrochanterian quality is axisymmetric and have bias utterly, forms during rotor periodically that centrifugal force disturbs, and makes machine produce vibration, i.e. rotor unbalance.Even each rotor part is done strict dynamic balancing, and it is good that centering is installed, but still stronger vibration may occur during the system that forms operation.The solution that adopts both at home and abroad at present is the imbalance that the complete machine full speed dynamic balance is eliminated this rotor axial system, but the method needs the repeatedly starting and stopping unit, not only incurs loss through delay the duration, also causes huge economic loss.
Summary of the invention
Uneven in order to overcome the rotary machine rotor system, and the deficiency that makes up present balancing technique, the utility model provides a kind of automatic balancing arrangement, this device can be eliminated the imbalance of rotary machine rotor system, and due to controlled thermal radiation, make this device adjust precision higher and easy to adjust, make balancing rotor system reach the optimum state.
The utility model is achieved through the following technical solutions:
A kind of rotor-support-foundation system automatic balancing arrangement that adopts thermal radiation to control, it is characterized in that: this device is arranged on unbalanced rotor shaft shoulder position, the bearing (ball) cover sealing that hollow shaft part and two ends arrange forms the cavity at middle part, hollow shaft part is provided with pneumatic piston and air valve, and pneumatic piston and air valve communicate with cavity; Bearing (ball) cover is provided with sleeve, is used for being connected with unbalanced rotor; Also be provided with the end cap window on bearing (ball) cover, scribble absorption heat energy material on end cap window local location; The position relative with the end cap window is provided with infrared source, and the device that is connected with infrared source is a stepper motor.
It is a plurality of being arranged on and scribbling the local location that absorbs the heat energy material on the end cap window, respectively with the different heights setting.
The cavity that hollow shaft part and bearing (ball) cover sealing form is four groups, and the pneumatic piston that communicates with cavity is also four groups, the Axis Cross setting.
Advantage and effect: the beneficial effects of the utility model are that this Equilibrator has automaticity, controllability, precision high, eliminates uneven effect remarkable, and apparatus structure is simple, cost is low, greatly reduces the cost of balancing technique before this.
Description of drawings:
Fig. 1 is unitary construction figure of the present utility model (partial cutaway);
Fig. 2 is the side view of Fig. 1;
Fig. 3 is the utility model motion principle schematic diagram;
Fig. 4 is the utility model external heat source of radiation work schematic diagram;
Fig. 5 is the A-A sectional view of Fig. 1.
Mark in figure: 1, hollow shaft part, 2, pneumatic piston, 3, seal ring Isosorbide-5-Nitrae, air valve, 5, bearing (ball) cover, 6, seal ring 2,7, end cap window, 8 stepper motors, 9 infrared sources, 10 absorb heat energy material, I piston movement (fine setting), II gas (coarse adjustment), III heat.
Mode of execution:
Main design of the present utility model is: this device is arranged on unbalanced rotor shaft shoulder position.This device scribbles the end cap window 7 that absorbs the heat energy material, seal ring 3 and 6, sleeve, pneumatic piston 2, air valve 4, infrared source 9 etc. by hollow shaft part 1, bearing (ball) cover 5, surface and partly forms, pneumatic piston 2 and air valve 4 are arranged on respectively in the cavity of the four hollow shaft parts 1 in chamber, end cap window 7 is arranged on bearing (ball) cover 5, bearing (ball) cover 5 is arranged on respectively hollow shaft part 1 two ends, shaft part is fastened on unbalanced rotor by sleeve, above-mentioned good air-proof condition is installed.When a certain side of determining rotor is uneven, detect the amount of unbalance information such as uneven direction, quality and phase place by sensor, determine the load balance condition, automatic control air-valve 4 increases the pressure of reverse cavity, and when the rotor time control heats source of radiation 9 these end cap windows of heating, heat is imported in this cavity, the internal gas expanded by heating, the pneumatic piston rod that promotes this cavity moves laterally a section and moves, movement due to the piston rod center of gravity, make the amount of unbalance of this side increase, reach with this and eliminate the unbalanced purpose of rotor-support-foundation system; Can also be by opening simultaneously a plurality of air valves 4 and infrared source 9, the pneumatic piston rod of a plurality of cavitys of promotion (or interior survey) laterally is mobile, adjusts amount of unbalance, reaches accurate adjustment and eliminates unbalanced purpose; In addition, a plurality of these automatic balancing arrangements can be arranged on unbalanced rotor in the time of necessary, reach the effect of better elimination rotor unbalance, make system balancing reach the optimum state.
Hollow shaft part 1 can be 1 with the cavity that bearing (ball) cover 5 forms, also can be for a plurality of, the rotor-support-foundation system automatic balancing arrangement that the utility model provides a kind of thermal radiation of four cavity configurations to control, that is: hollow shaft part 1 is four groups with the cavity that bearing (ball) cover 5 sealings form, the pneumatic piston 2 that communicates with cavity is also four groups, Axis Cross arranges, and this spline structure is the simplest, compact, is convenient to be fixed on unbalanced rotor.
Below in conjunction with Figure of description, by embodiment, the utility model is described further:
Motion principle schematic diagram 3 has illustrated the motion principle of this device, analyze unitary construction Fig. 1 and side view 2, in Fig. 1 and Fig. 2, unbalanced rotor is placed in hollow shaft part 1, when detecting in the rotor motion process, sensor occurs when uneven, because the end of automatic control air-valve 4 is communicated with cavity, air valve 4 can oppositely increase the pressure of corresponding cavitys; Meanwhile, by controlling infrared source 9 emission heat energy, the surface scribbles the end cap window 7 that absorbs heat energy material 10 and absorbs heat energy, and heat energy is imported in cavity, acting that in cavity, when gases are heated, they expand, promote pneumatic piston 2 and move laterally, and then make the amount of unbalance of this side increase, reach with this and eliminate the unbalanced purpose of rotor-support-foundation system.Leakage Gas occurs when using small-sized sealing circle 3 to prevent the interior gas push piston movement of cavity.
In Fig. 4, scribble 4 local locations that absorb heat energy material 10 on the end cap window 7 of the utility model device, difference called after a, b, c, d represents different height on this cavity footpath, infrared source 9 is regulated its position that moves up and down automatically by the control of stepper motor 8, so radiant light can shine on end cap window 7 by highly corresponding hole accordingly.Because rotor is to rotate continuously in the course of the work, therefore just can realize the needs cavity is added heat control by the height of controlling infrared source 9.
Shown in Figure 5 is the rotation A-A cut-away view of whole device, carries out the tightness protection by another seal ring 6 between shaft part end cap 5 and cavity, with the airtight precision that guarantees that having of this device is very high.
Due to uniform four pistons of this device, therefore can also open simultaneously a plurality of air valves 4 and infrared source 9, the pneumatic piston rod that promotes a plurality of cavitys (or interior survey) laterally is mobile, adjusts amount of unbalance, reaches accurate adjustment and eliminates unbalanced purpose.
In addition, a plurality of these automatic balancing arrangements can be arranged on unbalanced rotor in the time of necessary, reach the effect of better elimination rotor unbalance, make system balancing reach the optimum state.
Claims (3)
1. rotor-support-foundation system automatic balancing arrangement that adopts thermal radiation to control, it is characterized in that: this device is arranged on unbalanced rotor shaft shoulder position, hollow shaft part (1) seals with the bearing (ball) cover (5) that two ends arrange the cavity that forms the middle part, hollow shaft part (1) is provided with pneumatic piston (2) and air valve (4), and pneumatic piston (2) and air valve (4) communicate with cavity; Bearing (ball) cover (5) is provided with sleeve, is used for being connected with unbalanced rotor; Also be provided with end cap window (7) on bearing (ball) cover (5), scribble absorption heat energy material (10) on end cap window (7) local location; The position relative with end cap window (7) is provided with infrared source (9), and the device that is connected with infrared source (9) is a stepper motor (8).
2. the rotor-support-foundation system automatic balancing arrangement controlled of employing thermal radiation according to claim 1, it is characterized in that: it is a plurality of being arranged on and scribbling the local location that absorbs heat energy material (10) on end cap window (7), respectively with the different heights setting.
3. the rotor-support-foundation system automatic balancing arrangement controlled of employing thermal radiation according to claim 1, it is characterized in that: hollow shaft part (1) is four groups with the cavity that bearing (ball) cover (5) sealing forms, the pneumatic piston that communicates with cavity (2) is also four groups, the Axis Cross setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320221771 CN203257976U (en) | 2013-04-27 | 2013-04-27 | Rotor system automatic balancing device with thermal radiation control |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320221771 CN203257976U (en) | 2013-04-27 | 2013-04-27 | Rotor system automatic balancing device with thermal radiation control |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203257976U true CN203257976U (en) | 2013-10-30 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320221771 Expired - Lifetime CN203257976U (en) | 2013-04-27 | 2013-04-27 | Rotor system automatic balancing device with thermal radiation control |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203257976U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103234003A (en) * | 2013-04-27 | 2013-08-07 | 东北大学 | Rotor system automatic balancing device controlled by thermal radiation |
-
2013
- 2013-04-27 CN CN 201320221771 patent/CN203257976U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103234003A (en) * | 2013-04-27 | 2013-08-07 | 东北大学 | Rotor system automatic balancing device controlled by thermal radiation |
| CN103234003B (en) * | 2013-04-27 | 2015-02-04 | 东北大学 | Rotor system automatic balancing device controlled by thermal radiation |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20131030 Effective date of abandoning: 20150204 |
|
| RGAV | Abandon patent right to avoid regrant |