CN201364129Y - Bracket for installing dial gauge for turbine rotor fixed core - Google Patents
Bracket for installing dial gauge for turbine rotor fixed core Download PDFInfo
- Publication number
- CN201364129Y CN201364129Y CNU2008201582565U CN200820158256U CN201364129Y CN 201364129 Y CN201364129 Y CN 201364129Y CN U2008201582565 U CNU2008201582565 U CN U2008201582565U CN 200820158256 U CN200820158256 U CN 200820158256U CN 201364129 Y CN201364129 Y CN 201364129Y
- Authority
- CN
- China
- Prior art keywords
- rotor
- dial gauge
- turbine rotor
- fixed core
- bracket
- 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 - Fee Related
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Abstract
The utility model relates to turbine installation tools, in particular to a tool for installing a turbine rotor fixed core. A bracket for installing a dial gauge for a turbine rotor fixed core is connected to a rotor, and comprises a connecting bottom plate, a panel and a vertical rib plate, wherein the connecting bottom plate is fixed on the end face of the rotor through a bolt; the panel is horizontally arranged, and one end is fixedly connected with the connecting bottom plate; and the vertical rib plate is vertically welded with the panel, and one end thereof is fixedly connected with the connecting bottom plate. The utility model can make the installation of the measuring instrument for fixing the core on the bracket convenient and firm, thereby improving the precision of the fixed core arranged between the rotor and the motor.
Description
Technical field
The utility model turbine erecting tools relates in particular to the instrument that the turbine rotor static core rack is established.
Background technology
Behind turbine rotor and the motor installation in position, shaft coupling between the two must carry out centering and decide core, rotor is accurate, visual plant, rotor to decide core work extremely important, because the spacing between rotor-end shaft coupling and the motor-end shaft coupling is bigger, and is very big to the core work difficulty, if inaccurate to core, to influence the normal operation of equipment, cause industrial accident.
Summary of the invention
The utility model is intended to solve the defective of existing pipeline counterpart welding manner, provides a kind of turbine rotor static core rack to establish the support of dial gauge.The utility model makes that the measuring appliance be used for deciding core sets up on support not only convenient but also firm, thereby improve the degree of accuracy of deciding core between rotor and the motor.
The utility model is achieved in that
A kind of turbine rotor static core rack is established the support of dial gauge, and it is connected on the rotor, and it comprises:
One connects base plate, and it is to be bolted on the rotor end-face;
One panel, it is horizontally disposed with, and an end is fixedly connected on and connects on the base plate;
One vertical rib plate, it vertically is welded to connect panel, and an end is fixedly connected on and connects on the base plate.
Described turbine rotor static core rack is established the support of dial gauge, and described vertical rib plate is provided with some through holes.
Described turbine rotor static core rack is established the support of dial gauge, and described through hole has 3-5.
The utility model special stand fixed base plate connects and can directly be fixed on the rotor by bolt, itself and rotor is become one and as the extension of rotor; Support is connected base plate and adopts the t=20mm steel plate with rotor, support adopts T type structure, panel adopts the t=14mm steel plate, vertical rib plate adopts the steel plate of t=10mm to be made, and respectively in hole that 4 diameters of stud twist drill are Φ 120mm, guaranteeing to alleviate the weight of support under the prerequisite of rigidity, be convenient to move and install; Carry out finishing in the bracket head end parts, guarantee its flatness, make that the plane magnetic force interlock of the magnetic chassis of survey instrument dial gauge and support is more firm; Thereby not only improve dial gauge set up and use in stability and also improved the degree of accuracy of deciding core between rotor and the motor greatly.
Description of drawings
Below, further specify the utility model in conjunction with the accompanying drawings:
Fig. 1 is the utility model front view;
Fig. 2 is the utility model left view;
Fig. 3 is the utility model vertical view.
Embodiment
As Fig. 1, Fig. 2 and shown in Figure 3: a kind of turbine rotor static core rack is established the support of dial gauge, and it is connected on the rotor, and it comprises:
One connects base plate 1, and it (fails among the figure to express) to be bolted on the rotor end-face, as the extension of rotor;
One panel 2, it is horizontally disposed with, and an end is fixedly connected on and connects on the base plate 1;
One vertical rib plate 3, it vertically is welded to connect panel 2, one ends and is fixedly connected on the connection base plate 1;
Described vertical rib plate 3 is provided with 3-5 hole, and present embodiment has 4;
More firm for the plane magnetic force interlock of the magnetic chassis that makes the survey instrument dial gauge and support, the head end of described support needs finishing.
Claims (3)
1. a turbine rotor static core rack is established the support of dial gauge, and it is connected on the rotor, it is characterized in that, it comprises:
One connects base plate, and it is to be bolted on the rotor end-face;
One panel, it is horizontally disposed with, and an end is fixedly connected on and connects on the base plate;
One vertical rib plate, it vertically is welded to connect panel, and an end is fixedly connected on and connects on the base plate.
2. turbine rotor static core rack according to claim 1 is established the support of dial gauge, it is characterized in that, described vertical rib plate is provided with some through holes.
3. turbine rotor static core rack according to claim 2 is established the support of dial gauge, it is characterized in that, described through hole has 3-5.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201582565U CN201364129Y (en) | 2008-12-30 | 2008-12-30 | Bracket for installing dial gauge for turbine rotor fixed core |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201582565U CN201364129Y (en) | 2008-12-30 | 2008-12-30 | Bracket for installing dial gauge for turbine rotor fixed core |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201364129Y true CN201364129Y (en) | 2009-12-16 |
Family
ID=41474797
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201582565U Expired - Fee Related CN201364129Y (en) | 2008-12-30 | 2008-12-30 | Bracket for installing dial gauge for turbine rotor fixed core |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201364129Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104111022A (en) * | 2014-07-24 | 2014-10-22 | 苏州南新电机有限公司 | Stator perpendicularity pressurizing testing method |
| CN106091894A (en) * | 2016-06-30 | 2016-11-09 | 洛阳双瑞精铸钛业有限公司 | A kind of detection method of turbine rotor blade |
-
2008
- 2008-12-30 CN CNU2008201582565U patent/CN201364129Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104111022A (en) * | 2014-07-24 | 2014-10-22 | 苏州南新电机有限公司 | Stator perpendicularity pressurizing testing method |
| CN104111022B (en) * | 2014-07-24 | 2017-03-22 | 苏州南新电机有限公司 | Stator perpendicularity pressurizing testing method |
| CN106091894A (en) * | 2016-06-30 | 2016-11-09 | 洛阳双瑞精铸钛业有限公司 | A kind of detection method of turbine rotor blade |
| CN106091894B (en) * | 2016-06-30 | 2018-11-16 | 洛阳双瑞精铸钛业有限公司 | A kind of detection method of turbine rotor blade |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091216 Termination date: 20101230 |