CN113532269A - Sample plate for measuring movable blade shroud of steam turbine - Google Patents
Sample plate for measuring movable blade shroud of steam turbine Download PDFInfo
- Publication number
- CN113532269A CN113532269A CN202011061211.8A CN202011061211A CN113532269A CN 113532269 A CN113532269 A CN 113532269A CN 202011061211 A CN202011061211 A CN 202011061211A CN 113532269 A CN113532269 A CN 113532269A
- Authority
- CN
- China
- Prior art keywords
- measuring
- blade
- shroud
- arc measuring
- blade shroud
- 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.)
- Pending
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B11/00—Measuring arrangements characterised by the use of optical techniques
- G01B11/14—Measuring arrangements characterised by the use of optical techniques for measuring distance or clearance between spaced objects or spaced apertures
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
- G01B5/02—Measuring arrangements characterised by the use of mechanical techniques for measuring length, width or thickness
- G01B5/06—Measuring arrangements characterised by the use of mechanical techniques for measuring length, width or thickness for measuring thickness
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The invention provides a sample plate for measuring a turbine moving blade shroud, which can be used for measuring the pitch of the shroud and the position of the shroud, and meanwhile, the measurement result is more accurate. The blade crown inner arc measuring device comprises a blade crown inner arc measuring bottom plate and a blade crown back arc measuring bottom plate, wherein a blade crown inner arc measuring block is connected onto the blade crown inner arc measuring bottom plate, a blade crown back arc measuring block is connected onto the blade crown back arc measuring bottom plate, a blade crown inner arc measuring surface is arranged on the blade crown inner arc measuring block, a blade crown back arc measuring surface is arranged on the blade crown back arc measuring block, the shape of the blade crown inner arc measuring surface corresponds to the shape of the inner radial surface of a blade crown standard component, and the shape of the blade crown back arc measuring surface corresponds to the shape of the back radial surface of the blade crown standard component.
Description
Technical Field
The invention relates to the technical field of blade measurement, in particular to a sample plate for measuring a movable blade shroud of a steam turbine.
Background
The turbine moving blade needs to detect the blade shroud in the machining process so as to be repaired and adjusted in time, the stability of the finished product blade shroud during assembly is guaranteed, and the pitch of the blade shroud is one of the contents needing to be detected. The traditional sample plate for detecting the pitch of the blade shroud can be seen in a measuring tool for the pitch of the blade shroud and a boss with the publication number of CN102519333A, wherein the traditional measuring tool comprises an inner arc pitch sample plate and a back arc pitch sample plate which are respectively connected with guide blocks at two sides of a measuring frame, and whether the pitch size of the blade shroud is qualified or not is judged by measuring gaps among an inner working surface and a back working surface of the blade shroud, the inner arc pitch sample plate and a back arc pitch sample plate detection surface; however, the thickness of the detection surface of the conventional measuring tool is often very thin, the pitch measurement is carried out through line contact with the tip shroud, and the conventional measuring tool is not generally used for measuring the position of the tip shroud because the contact surface is too small and the measurement is inaccurate.
Disclosure of Invention
The invention provides a sample plate for measuring a movable blade shroud of a steam turbine, aiming at the problem that a traditional measuring tool for measuring the pitch of the blade shroud is inaccurate when used for measuring the position of the blade shroud, and the sample plate can be used for measuring the pitch of the blade shroud and the position of the blade shroud, and meanwhile, the measuring result is more accurate.
The technical scheme is as follows: a model for measuring steam turbine movable blade shroud, it includes that the shroud inner arc measures bottom plate, shroud back arc and measures the bottom plate, its characterized in that: the blade crown inner arc measuring device is characterized in that a blade crown inner arc measuring block is connected to the blade crown inner arc measuring bottom plate, a blade crown back arc measuring block is connected to the blade crown back arc measuring bottom plate, a blade crown inner arc measuring surface is arranged on the blade crown inner arc measuring block, a blade crown back arc measuring surface is arranged on the blade crown back arc measuring block, the shape of the blade crown inner arc measuring surface corresponds to the shape of the inner radial surface of a blade crown standard component, and the shape of the blade crown back arc measuring surface corresponds to the shape of the back radial surface of the blade crown standard component.
It is further characterized in that:
the thickness of the inner arc measuring surface of the blade shroud is larger than that of the inner arc measuring bottom plate of the blade shroud; the thickness of the blade shroud back arc measuring surface is larger than that of the blade shroud back arc measuring bottom plate;
the blade shroud inner arc measuring block comprises a first connecting part and a first measuring part, the first connecting part is used for being connected with the blade shroud inner arc measuring bottom plate, and one end part of the measuring part is provided with the blade shroud inner arc measuring surface;
the blade shroud back arc measuring block comprises a second connecting part and a second measuring part, the second connecting part is used for being connected with the blade shroud back arc measuring bottom plate, and two end parts of the measuring part are provided with the blade shroud back arc measuring surface.
The invention has the beneficial effects that: the measuring tool can be used for measuring the pitch of the blade shroud like the traditional pitch measuring tool, and can also be used for measuring the position of the blade shroud by using the sample plate, and the measuring surface is the shape of the whole surface of the corresponding surface of the blade shroud standard component, so that the measuring result of the position of the blade shroud is more accurate; the whole template can be used for measuring the pitch and the position of the blade shroud, so that the manufacturing cost is reduced, the production preparation period is shortened, and the production field management is easy.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a view from the A direction of FIG. 1;
FIG. 3 is a view from the direction B of FIG. 1;
FIG. 4 is a schematic view of the structure of the inner arc measuring block of the tip shroud;
FIG. 5 is a schematic view of a blade shroud back arc measurement block.
Detailed Description
The sample plate for measuring the blade shroud of the turbine moving blade shown in fig. 1 to fig. 3 includes a blade shroud inner arc measuring bottom plate 1 and a blade shroud back arc measuring bottom plate 2, the blade shroud inner arc measuring bottom plate 1 is connected with a blade shroud inner arc measuring block 11, the blade shroud back arc measuring bottom plate 2 is connected with a blade shroud back arc measuring block 21, the blade shroud inner arc measuring block 11 is provided with a blade shroud inner arc measuring surface 111, the blade shroud back arc measuring block 21 is provided with a blade shroud back arc measuring surface 211, the shape of the blade shroud inner arc measuring surface 111 corresponds to the shape of the inner radial surface of the blade shroud standard component, and the shape of the blade shroud back arc measuring surface 211 corresponds to the shape of the back radial surface of the blade shroud standard component. Specifically, referring to fig. 4, the tip shroud inner arc measuring block 11 includes a first connecting portion 12 and a first measuring portion 13, the first connecting portion 12 is used for being connected with the tip shroud inner arc measuring bottom plate 1 in a positioning manner through a screw, a positioning pin and other components, and the tip of the first measuring portion 13 is provided with a tip shroud inner arc measuring surface 111; the blade shroud back arc measuring block 21 comprises a second connecting part 22 and a second measuring part 23, the second connecting part 21 is used for being connected with the blade shroud back arc measuring bottom plate 2 in a positioning mode through parts such as screws and positioning pins, and the end part of the second measuring part 23 is provided with a blade shroud back arc measuring surface 211.
When the measuring device is used, the sample plate is arranged on the measuring frame like a traditional measuring tool and is positioned through the clamping foot 3, when the position of the blade shroud is measured, the inner radial surface of the blade shroud is attached to the inner arc measuring surface 111 of the blade shroud of the inner arc measuring block 11 of the blade shroud by using a standard sample plate method, and the light leakage value is measured; the radial surface of the blade shroud back is attached to the blade shroud back arc measuring surface 211 of the blade shroud back arc measuring block 21, the position of the blade shroud can be measured by measuring the light leakage value, whether the blade shroud is qualified or not is judged, the measuring result is accurate, and the use is convenient and efficient; when the blade shroud pitch measurement needs to be carried out, the inner radial surface of the blade shroud can be attached to the inner arc measuring surface 111 of the blade shroud of the inner arc measuring block 11 in a traditional mode, the gap value between the back arc measuring block 21 of the blade shroud and the pitch surface of the blade shroud is measured through a feeler gauge, and then the gap value is converted into the pitch size of the blade.
In addition, the thickness of the blade shroud inner arc measuring surface 111 can be larger than that of the blade shroud inner arc measuring bottom plate 1 by adopting an assembly type design, namely a design that the measuring block is connected to the bottom plate; the thickness of face 211 is measured to leaf shroud back of the body arc can be greater than the thickness that bottom plate 2 is measured to leaf shroud back of the body arc, compares in the design of traditional integral type for the thickness of measuring the face is not influenced by bottom plate thickness, has saved manufacturing cost, and the while can also directly change the measuring block and be used for the leaf shroud of different models to measure convenient to use.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present invention are included in the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (4)
1. A model for measuring steam turbine movable blade shroud, it includes that the shroud inner arc measures bottom plate, shroud back arc and measures the bottom plate, its characterized in that: the blade crown inner arc measuring device is characterized in that a blade crown inner arc measuring block is connected to the blade crown inner arc measuring bottom plate, a blade crown back arc measuring block is connected to the blade crown back arc measuring bottom plate, a blade crown inner arc measuring surface is arranged on the blade crown inner arc measuring block, a blade crown back arc measuring surface is arranged on the blade crown back arc measuring block, the shape of the blade crown inner arc measuring surface corresponds to the shape of the inner radial surface of a blade crown standard component, and the shape of the blade crown back arc measuring surface corresponds to the shape of the back radial surface of the blade crown standard component.
2. The template for measuring turbine bucket shrouds according to claim 1, wherein: the thickness of the inner arc measuring surface of the blade shroud is larger than that of the inner arc measuring bottom plate of the blade shroud; the thickness of the blade shroud back arc measuring surface is larger than that of the blade shroud back arc measuring bottom plate.
3. The template for measuring turbine bucket tip shrouds according to claim 1 or 2, wherein: the blade shroud inner arc measuring block comprises a first connecting part and a first measuring part, the first connecting part is used for being connected with the blade shroud inner arc measuring bottom plate, and one end part of the measuring part is provided with the blade shroud inner arc measuring surface.
4. The template for measuring turbine bucket tip shrouds according to claim 1 or 2, wherein: the blade shroud back arc measuring block comprises a second connecting part and a second measuring part, the second connecting part is used for being connected with the blade shroud back arc measuring bottom plate, and two end parts of the measuring part are provided with the blade shroud back arc measuring surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011061211.8A CN113532269A (en) | 2020-09-30 | 2020-09-30 | Sample plate for measuring movable blade shroud of steam turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011061211.8A CN113532269A (en) | 2020-09-30 | 2020-09-30 | Sample plate for measuring movable blade shroud of steam turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113532269A true CN113532269A (en) | 2021-10-22 |
Family
ID=78094286
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011061211.8A Pending CN113532269A (en) | 2020-09-30 | 2020-09-30 | Sample plate for measuring movable blade shroud of steam turbine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113532269A (en) |
-
2020
- 2020-09-30 CN CN202011061211.8A patent/CN113532269A/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN2847213Y (en) | Internal and external structure relative position size measuring device for rack piston | |
| CN203443507U (en) | Combined detection measuring tool of steam turbine blade with dovetail-shaped blade root | |
| CN105066848B (en) | Dove-tail form blade tenon pressure face angle measurement unit and method | |
| CN105133152A (en) | Device for calibrating special fixed ruler for air-jet loom auxiliary nozzles | |
| CN201852553U (en) | Point-contact type check fixture for fast measuring flatness | |
| CN102353314B (en) | Detection method for outline of main blade of helicopter | |
| CN105444647B (en) | The device measured for turbine blade shroud and boss pitch | |
| CN102564260A (en) | Detection apparatus of arc tenon-tooth blade-root molded line and intermediate molded line | |
| CN213842035U (en) | Sample plate for measuring movable blade shroud of steam turbine | |
| CN113532269A (en) | Sample plate for measuring movable blade shroud of steam turbine | |
| CN201397109Y (en) | Cylinder body bearing seat lateral face position inspection device | |
| CN204286267U (en) | A kind of device detecting the aperture oral area chamfering of the product of numerically-controlled machine processing | |
| CN213179810U (en) | Measuring device for accurately measuring depth of deep inner hole groove and width of notch | |
| CN212806952U (en) | Device for detecting position degree of scratch board scribed line of aircraft assembly tool | |
| CN204874999U (en) | Air jet loom assists special set pattern calibration equipment of nozzle | |
| CN211346649U (en) | Tool for detecting span length of inner gear ring of slewing bearing | |
| CN204085363U (en) | A kind of toe shape rocking arm hole and centre distance comprehensive test measurer | |
| CN109724497B (en) | Method for online detecting radius value of inner sphere | |
| CN208155199U (en) | A kind of axial dimension measuring device | |
| CN219714253U (en) | Comb gap measuring ruler | |
| CN205981066U (en) | Reverse gear shaft blank terminal surface straightness detection device that hangs down | |
| CN218994221U (en) | Measuring tool | |
| CN212645608U (en) | Forward-pushing type digital display measuring tool | |
| CN219064393U (en) | Non-whole circular surface contour measuring gauge | |
| CN218994237U (en) | Measuring tool that suitability is strong |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |