CN106767239B - A kind of turbine disk assembling assembly blade installation site measuring device - Google Patents
A kind of turbine disk assembling assembly blade installation site measuring device Download PDFInfo
- Publication number
- CN106767239B CN106767239B CN201611068747.6A CN201611068747A CN106767239B CN 106767239 B CN106767239 B CN 106767239B CN 201611068747 A CN201611068747 A CN 201611068747A CN 106767239 B CN106767239 B CN 106767239B
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- Prior art keywords
- telescopic rod
- strut
- main body
- measurement
- bearing
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- 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
- G01B5/003—Measuring of motor parts
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The present invention discloses a kind of turbine disk assembling assembly blade installation site measuring device, including measurement component and positioning component；The positioning component includes main body, the main body has three support arms for being mutually 120 degree of angles, through-hole is set in the support arm, telescopic rod is set in the through-hole, one end of telescopic rod is tapered end, the tapered end is abutted with cone, and external screw thread is arranged in the cone upper end, and the external screw thread and nut cooperate；The bearing of 2 right-angled intersections is arranged with cantilever, the end of the cantilever is fixed in the other end of the telescopic rod；The measurement component includes the strut being fixed in main body, and table folder is also set up on the strut, limited block is arranged in table folder；The end point of strut is arranged in measurement table.The invention has the advantages that this device breaches the influence that turbine disc assemblies are beated between the listrium end face caused by blade difference in assembling process to positioning measurement, fast and stable measurement is realized.
Description
Technical field
The invention belongs to aerial motor spare part detection technique fields, fill more particularly to a kind of turbine disc assemblies blade
With position-measurement device.
Background technique
Turbine disc assemblies largely influence engine performance, need to check leaf position in installation blade process
It is whether qualified.By measurement blade edge template face on a little at radius, can reflect the accuracy of blade installation site.Due to every
There is bounce between listrium end face, bring difficulty to positioning measurement in the difference between a blade；The more, group by installation blade quantity
The factors such as part volume is big influence, more time-consuming using three-dimensional coordinates measurement.
Summary of the invention
In order to solve the above technical problems, purpose of the invention is to provide a kind of simple, accurate measuring device, specific skill
Art scheme is as follows:
A kind of turbine disk assembling assembly blade installation site measuring device, including measurement component and positioning component；It is described fixed
Hyte part includes main body, and the main body has three support arms for being mutually 120 degree of angles, and guide groove is arranged in the support arm, described to lead
Telescopic rod is set into slot, and one end of telescopic rod is tapered end, and the tapered end is abutted with cone, and the cone upper end setting is outer
Screw thread, the external screw thread and nut cooperate；The other end of the telescopic rod is fixed with cantilever, the end setting 2 of the cantilever
The bearing of a right-angled intersection；The measurement component includes the strut being fixed in main body, and table folder is also set up on the strut, described
Limited block is set in table folder, and limited block can slide in table folder, and marking scribing line is distinguished on limited block both sides；Table is measured to be arranged in strut
End point；Rotating nuts realize that cone moves up and down；Telescopic rod is displaced outwardly, and drives cantilever, bearing mobile, until horizontal position
Bearing be bonded with tested part, simultaneously because gravity, vertically disposed bearing is fitted closely with tested part end face, realize dress
The positioning set；Whole process is controlled by nut, and guarantees that the device of the invention can be around the inner circular of tested part by bearing
Zhou Xuanzhuan；
The telescopic rod is two-part, and tension spring is arranged between two sections.
The invention has the advantages that this device breaches turbine disc assemblies listrium end caused by blade difference in assembling process
Influence of the bounce to positioning measurement between face, realizes fast and stable measurement, and can multistage turbine disk component it is general.This structure is new
Grain husk, using reliable, scene feedback application is good, and measurement accuracy meets technique requirement, and substantially increases the measurement effect of part
Rate, measurement result can reflect the actual position of part, facilitate the control to product quality.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the side view of Fig. 1；
Fig. 3 is location structure schematic diagram；
Fig. 4 is in working condition schematic diagram；
Specific embodiment
The present invention is illustrated with reference to the accompanying drawing, and as Figure 1-Figure 4, the present invention includes main body 10, telescopic rod 2, spiral shell
Mother 3, cantilever 4, bearing 5, fulcrum bar component 6, table folder 7, limited block 8, measurement table 9；Main body 10 has three support arms for being mutually 120 °
101, guide groove is set in support arm 101, and three identical telescopic rods 2 are mounted in three guide grooves 101, are fixed, stretched by cover board 11
Tension spring 31 is housed in contracting bar 2, is sprung back after realizing measurement.1 upper end of cone is external screw thread, after the through-hole of 10 center of main body
It is connect with nut 3, rotating nuts 3 realize that cone moves up and down.Cone 1 is fitted closely with three telescopic rods 2 by tension spring, cone
Body 1 moves up, and telescopic rod 2 is displaced outwardly.The bearing of 2 right-angled intersections is installed on the outside of every telescopic rod 2 by two screws
5.Telescopic rod 2 is displaced outwardly, and it is mobile to drive cantilever 4, bearing 5, until the bearing 5 of horizontal position is bonded with tested part, while by
In gravity, vertically disposed bearing 5 is fitted closely with tested part end face, the positioning of realization device.Whole process is controlled by nut 3
System, and guarantee that the device of the invention can be rotated around the internal circumference of tested part by bearing 5.
Fulcrum bar component 6 and the interference fit of main body 10 connect, and are equipped with pin anti-rotation.Fulcrum bar component is by strut, clip, tangential
The components such as clamping composition exports measurement component to position to be measured, and pilot process can carry out multiple degrees of freedom adjustment.It is logical to measure table 9
Cross screw, bushing is connected with table folder 7, table folder 7 is mounted on fulcrum bar component 6.Limited block 8 can slide in table folder 7, both sides difference
Marking scribing line, to the height value for being just afterwards exactly limited block and measurement table.Fulcrum bar component 6 is adjusted, after limited block is adjacent to tested part,
The accurate location for as needing to measure locks strut 6 thereafter through screw.After this process, limited block 8 is moved to and does not interfere position
It sets and locks, rotating body 10 realizes the circumferential measurement under the blade listrium height.
Claims (2)
1. a kind of turbine disk assembling assembly blade installation site measuring device, it is characterised in that: including measurement component and positioning group
Part；The positioning component includes main body, and the main body has three support arms for being mutually 120 degree of angles, setting guiding in the support arm
Slot, the guide groove is interior to be arranged telescopic rod, and one end of telescopic rod is tapered end, and the tapered end is abutted with cone, the cone
External screw thread is arranged in upper end, and the external screw thread and nut cooperate；The other end of the telescopic rod is fixed with cantilever, the cantilever
The bearing of 2 right-angled intersections is arranged in end；The measurement component includes the strut being fixed in main body, is also set up on the strut
Limited block is arranged in the table folder in table folder, and limited block can slide in table folder, and marking scribing line is distinguished on limited block both sides；Measure table
The end point of strut is set；
Rotating nuts realize that cone moves up and down；Telescopic rod is displaced outwardly, and drives cantilever, bearing mobile, until the axis of horizontal position
It holds and is bonded with tested part, simultaneously because gravity, vertically disposed bearing is fitted closely with tested part end face, realization device
Positioning；Whole process is controlled by nut, and guarantees that the device of the invention can socialize around the inner circular of tested part by bearing
Turn.
2. turbine disk assembling assembly blade installation site measuring device according to claim 1, it is characterised in that: described to stretch
Contracting bar is two-part, and tension spring is arranged between two sections.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611068747.6A CN106767239B (en) | 2016-11-29 | 2016-11-29 | A kind of turbine disk assembling assembly blade installation site measuring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611068747.6A CN106767239B (en) | 2016-11-29 | 2016-11-29 | A kind of turbine disk assembling assembly blade installation site measuring device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106767239A CN106767239A (en) | 2017-05-31 |
| CN106767239B true CN106767239B (en) | 2019-09-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611068747.6A Active CN106767239B (en) | 2016-11-29 | 2016-11-29 | A kind of turbine disk assembling assembly blade installation site measuring device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106767239B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108444371B (en) * | 2018-04-02 | 2023-09-26 | 盐城永安科技有限公司 | Gear pitch circle positioning detection device and use method |
| CN110440667B (en) * | 2019-09-06 | 2021-11-26 | 中国航发南方工业有限公司 | Device for measuring mounting edge of guide blade of high-pressure turbine |
| CN114055102B (en) * | 2021-10-20 | 2023-03-07 | 中国航发四川燃气涡轮研究院 | Single turbine blade tip machining method |
Citations (7)
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| CN101216276A (en) * | 2008-01-04 | 2008-07-09 | 洛阳轴研科技股份有限公司 | Method for measuring part inner circle roundness and measuring apparatus |
| CN202066453U (en) * | 2011-05-03 | 2011-12-07 | 天津天海同步科技股份有限公司 | Testing device for planet tooth ring circularity and radial integral deviation |
| CN202119352U (en) * | 2011-05-23 | 2012-01-18 | 北京首钢建设集团有限公司 | Multifunctional adjusting rack |
| CN102425984A (en) * | 2011-09-14 | 2012-04-25 | 瓦房店工业冶金轴承制造有限公司 | Detection apparatus for heavy and large bearings |
| CN203364691U (en) * | 2013-06-13 | 2013-12-25 | 大连冶金轴承股份有限公司 | Portable measuring meter stand |
| CN104677238A (en) * | 2013-11-30 | 2015-06-03 | 王文刚 | Sliding type detection auxiliary tooling |
| CN106091895A (en) * | 2016-08-03 | 2016-11-09 | 中国人民解放军第五七九工厂 | A kind of gas-turbine unit turbine guide vane profile measurement device and measuring method thereof |
-
2016
- 2016-11-29 CN CN201611068747.6A patent/CN106767239B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101216276A (en) * | 2008-01-04 | 2008-07-09 | 洛阳轴研科技股份有限公司 | Method for measuring part inner circle roundness and measuring apparatus |
| CN202066453U (en) * | 2011-05-03 | 2011-12-07 | 天津天海同步科技股份有限公司 | Testing device for planet tooth ring circularity and radial integral deviation |
| CN202119352U (en) * | 2011-05-23 | 2012-01-18 | 北京首钢建设集团有限公司 | Multifunctional adjusting rack |
| CN102425984A (en) * | 2011-09-14 | 2012-04-25 | 瓦房店工业冶金轴承制造有限公司 | Detection apparatus for heavy and large bearings |
| CN203364691U (en) * | 2013-06-13 | 2013-12-25 | 大连冶金轴承股份有限公司 | Portable measuring meter stand |
| CN104677238A (en) * | 2013-11-30 | 2015-06-03 | 王文刚 | Sliding type detection auxiliary tooling |
| CN106091895A (en) * | 2016-08-03 | 2016-11-09 | 中国人民解放军第五七九工厂 | A kind of gas-turbine unit turbine guide vane profile measurement device and measuring method thereof |
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| Publication number | Publication date |
|---|---|
| CN106767239A (en) | 2017-05-31 |
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| CB02 | Change of applicant information |
Address after: 110043 Liaoning Province, Shenyang City District East Street No. 6 Applicant after: Chinese Hangfa Shenyang Liming Aero engine limited liability company Address before: 110043 Liaoning Province, Shenyang City District East Street No. 6 Applicant before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City |
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