CN106091886A - A kind of turbine blade Bearing testing equipment - Google Patents
A kind of turbine blade Bearing testing equipment Download PDFInfo
- Publication number
- CN106091886A CN106091886A CN201610628077.2A CN201610628077A CN106091886A CN 106091886 A CN106091886 A CN 106091886A CN 201610628077 A CN201610628077 A CN 201610628077A CN 106091886 A CN106091886 A CN 106091886A
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- CN
- China
- Prior art keywords
- support bar
- plate
- turbine blade
- testing equipment
- side plate
- 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.)
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Classifications
-
- 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
- G01B5/061—Measuring arrangements characterised by the use of mechanical techniques for measuring length, width or thickness for measuring thickness height gauges
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
A kind of turbine blade Bearing testing equipment that the present invention provides, described bearing block is in rectangular-shaped thin-slab structure, two short brinks at cuboid are vertically connected with side plate, baffle plate it is provided with between biside plate, described three cylindrical rod its upper and lower two can be guide rod, a middle cylindrical rod is leading screw, one end of described leading screw is connected with motor, the inner side of described side plate is provided with a limiting plate, described limiting plate is connected on side plate by two guide pillars, and the guide pillar between described limiting plate and side plate is socketed with spring.Beneficial effects of the present invention: simple in construction, easily operates, and improves detection efficiency, it is ensured that accuracy of detection, and reduces the labor intensity of operator, and beneficially batch machining produces.
Description
Technical field
The present invention relates to hydro-electric power generating equipment detection technique field, particularly relate to a kind of turbine blade Bearing testing equipment.
Background technology
In hydro-electric power generating equipment, in the hydraulic turbine, there is multiple parts of bearings, before assembling wheel mechanism, need composition water
The all parts of turbine detects, and it is qualified to detect whether, and for bearing parts, it needs to be arranged in equipment in use
Mate with dead eye size and length, often occur that in Production of bearing technique the height dimension of bearing is overproof, directly affects axle
The assembly performance held.
Traditional bearing height measuring method uses manual mode to carry out mostly, carries out elevation carrection, detection efficiency one by one
Low, accuracy of detection is poor, and fatigue resistance is big, it is impossible to meet batch production.
Summary of the invention
In view of this, it is desirable to provide a kind of turbine blade Bearing testing equipment, simple in construction, easily operate, improve
Detection efficiency, reduces labor intensity.
For reaching above-mentioned purpose, the technical scheme is that and be achieved in that:
A kind of turbine blade Bearing testing equipment, including bin body, for the bearing block of holding multiple pieces bearing and amesdial,
Described bearing block is positioned on bin body, is positioned on the bin body of described bearing block side vertical along the length direction of bearing block
Two supports are set, on vertical plane, are arranged with three cylindrical rod between two described supports in parallel, on three cylindrical rod
Slip is provided with sliding seat；The inner side of described sliding seat has the slotted hole of two parallel settings, between two described slotted holes
It is bolted the first support bar, described first support bar has been vertically connected with the second support bar, described second support bar
End away from the first support bar is arranged at above bearing block, and described amesdial is vertically installed on the second support bar.
Further, described bearing block is in rectangular-shaped thin-slab structure, the most affixed at two short brinks of cuboid
There is side plate, between biside plate, be provided with baffle plate.
Further, described three cylindrical rod its upper and lower two can be guide rod, and a middle cylindrical rod is silk
Thick stick, one end of described leading screw is connected with motor.
Further, the inner side of described side plate is provided with a limiting plate, and described limiting plate is connected to side plate by two guide pillars
On, the guide pillar between described limiting plate and side plate is socketed with spring.
Further, described second support bar has multiple round tube hole for arranging amesdial.
Relative to prior art, a kind of turbine blade Bearing testing equipment of the present invention has the advantage that structure
Simply, easily operate, improve detection efficiency, it is ensured that accuracy of detection, and reduce the labor intensity of operator, be conducive to criticizing
Amount processing.
Accompanying drawing explanation
The accompanying drawing of the part constituting the present invention is used for providing a further understanding of the present invention, and the present invention's is schematic real
Execute example and illustrate for explaining the present invention, being not intended that inappropriate limitation of the present invention.In the accompanying drawings:
Fig. 1 is the structural representation of a kind of turbine blade Bearing testing equipment described in the embodiment of the present invention；
Fig. 2 is the partial enlargement structural representation shown in Fig. 1 at A；
Fig. 3 is the structural representation removing bin body in Fig. 1.
Description of reference numerals:
1-bin body；2-bearing block；3-support；4-sliding seat；5-amesdial；6-leading screw；7-motor；8-guide rod；21-side
Plate；22-baffle plate；23-limiting plate；24-guide pillar；41-body；42-the first support bar；43-the second support bar；411-slotted hole.
Detailed description of the invention
It should be noted that in the case of not conflicting, the embodiment in the present invention and the feature in embodiment can phases
Combination mutually.
In describing the invention, it is to be understood that term " " center ", " longitudinally ", " laterally ", " on ", D score,
Orientation or the position relationship of the instruction such as "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ", " interior ", " outward " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of the description present invention and simplifies description rather than instruction or dark
The device or the element that show indication must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that right
The restriction of the present invention.Additionally, term " first ", " second " etc. are only used for describing purpose, and it is not intended that indicate or hint phase
To importance or the implicit quantity indicating indicated technical characteristic.Thus, the feature defining " first ", " second " etc. can
To express or to implicitly include one or more this feature.In describing the invention, except as otherwise noted, " multiple "
It is meant that two or more.
In describing the invention, it should be noted that unless otherwise clearly defined and limited, term " is installed ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be fixing connection, it is also possible to be to removably connect, or be integrally connected；Can
To be mechanical connection, it is also possible to be electrical connection；Can be to be joined directly together, it is also possible to be indirectly connected to by intermediary, Ke Yishi
The connection of two element internals.For the ordinary skill in the art, above-mentioned term can be understood by concrete condition
Concrete meaning in the present invention.
Describe the present invention below with reference to the accompanying drawings and in conjunction with the embodiments in detail.
A kind of turbine blade Bearing testing equipment, referring to the drawings shown in 1, including bin body 1, for holding multiple pieces bearing
Bearing block 2 and amesdial 5, bearing block 2 is positioned on bin body 1, is positioned on the bin body 1 of bearing block 2 side along bearing block 2
Length direction be vertically arranged two supports 3, on vertical plane, be arranged with three cylindrical rod between two supports 3 in parallel, three
Slide on root cylindrical rod and be provided with sliding seat 4, be manually displaced sliding seat 4 to desired location.
It is also possible that three cylindrical rod its upper and lower two can be guide rod 8, a middle cylindrical rod is leading screw 6,
One end of leading screw 6 is connected with motor 7, drives sliding seat 4 to move to desired location by motor 7.
Especially, referring to the drawings shown in 2, the inner side of sliding seat 4 has a slotted hole 411 of two parallel settings, two
It is bolted the first support bar 41 between slotted hole 411, the first support bar 41 has been vertically connected with the second support bar 42,
Second support bar 42 is placed in above bearing block 2 away from the end of the first support bar 41, and amesdial 5 is vertically installed in the second support bar
On 42；By regulating first support bar 41 position on sliding seat 4, to meet the needs of multiple bearing size.
Preferably, the second support bar 42 has multiple round tube hole for arranging amesdial 5, can realize bearing to be measured
Multiple spot detection.
Referring to the drawings shown in 3, wherein, bearing block 2 is in rectangular-shaped thin-slab structure, and two short brinks at cuboid hang down
Directly it is connected with side plate 21, between biside plate 21, is provided with baffle plate 22, it is ensured that when polylith bearing to be measured is placed, it is possible to concordant placement.
Preferably, the inner side of side plate 21 is provided with a limiting plate 23, and limiting plate 23 is connected to side plate 21 by two guide pillars 24
On, the guide pillar 24 between limiting plate 23 and side plate 21 is socketed with spring；The side of polylith bearing is carried out by this design
Fixing.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention
Within god and principle, any modification, equivalent substitution and improvement etc. made, should be included within the scope of the present invention.
Claims (5)
1. a turbine blade Bearing testing equipment, it is characterised in that: include bin body (1), axle for holding multiple pieces bearing
Bearing (2) and amesdial (5), described bearing block (2) is positioned on bin body (1), is positioned at the bin of described bearing block (2) side
On body (1), the length direction along bearing block (2) is vertically arranged two supports (3), at vertical plane between two described supports (3)
On be arranged with three cylindrical rod in parallel, on three cylindrical rod slide be provided with sliding seat (4)；
The inner side of described sliding seat (4) has a slotted hole (411) of two parallel settings, two described slotted holes (411) it
Between be bolted the first support bar (41), described first support bar (41) is vertically connected with the second support bar (42),
Described second support bar (42) is arranged at bearing block (2) top away from the end of the first support bar (41), and described amesdial (5) hangs down
Directly it is arranged on the second support bar (42).
A kind of turbine blade Bearing testing equipment the most according to claim 1, it is characterised in that: described bearing block (2) is
In rectangular-shaped thin-slab structure, two short brinks at cuboid are vertically connected with side plate (21), and biside plate is provided with between (21)
Baffle plate (22).
A kind of turbine blade Bearing testing equipment the most according to claim 1, it is characterised in that: described three cylindrical rod
Its upper and lower two can be guide rod (8), and a middle cylindrical rod is leading screw (6), one end of described leading screw (6) and motor (7)
It is connected.
A kind of turbine blade Bearing testing equipment the most according to claim 2, it is characterised in that: described side plate (21) interior
Side is provided with a limiting plate (23), and described limiting plate (23) is connected on side plate (21) by two guide pillars (24), is positioned at described limit
It is socketed with spring on guide pillar (24) between position plate (23) and side plate (21).
A kind of turbine blade Bearing testing equipment the most according to claim 1, it is characterised in that: described second support bar
(42) multiple round tube hole for arranging amesdial (5) is had on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610628077.2A CN106091886A (en) | 2016-07-29 | 2016-07-29 | A kind of turbine blade Bearing testing equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610628077.2A CN106091886A (en) | 2016-07-29 | 2016-07-29 | A kind of turbine blade Bearing testing equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106091886A true CN106091886A (en) | 2016-11-09 |
Family
ID=57453653
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610628077.2A Pending CN106091886A (en) | 2016-07-29 | 2016-07-29 | A kind of turbine blade Bearing testing equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106091886A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107192719A (en) * | 2017-06-20 | 2017-09-22 | 江苏三杰新能源有限公司 | A kind of lithium battery pole slice cuts burr detection device |
| CN107289890A (en) * | 2017-08-24 | 2017-10-24 | 苏州光照精密仪器有限公司 | Detector and detecting system |
| CN108731581A (en) * | 2018-06-05 | 2018-11-02 | 芜湖优能自动化设备有限公司 | A kind of pump core detection impeller clearance detection device |
| CN112611294A (en) * | 2020-12-28 | 2021-04-06 | 天津仲宇博金属制品有限公司 | Lead screw position precision gauge |
| CN112611294B (en) * | 2020-12-28 | 2024-05-31 | 天津仲宇博金属制品有限公司 | Screw rod position accuracy gauge |
-
2016
- 2016-07-29 CN CN201610628077.2A patent/CN106091886A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107192719A (en) * | 2017-06-20 | 2017-09-22 | 江苏三杰新能源有限公司 | A kind of lithium battery pole slice cuts burr detection device |
| CN107289890A (en) * | 2017-08-24 | 2017-10-24 | 苏州光照精密仪器有限公司 | Detector and detecting system |
| CN108731581A (en) * | 2018-06-05 | 2018-11-02 | 芜湖优能自动化设备有限公司 | A kind of pump core detection impeller clearance detection device |
| CN112611294A (en) * | 2020-12-28 | 2021-04-06 | 天津仲宇博金属制品有限公司 | Lead screw position precision gauge |
| CN112611294B (en) * | 2020-12-28 | 2024-05-31 | 天津仲宇博金属制品有限公司 | Screw rod position accuracy gauge |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161109 |
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| WD01 | Invention patent application deemed withdrawn after publication |