CN203365064U - Leakproof detection gas tightness device for turbine compressor casing - Google Patents
Leakproof detection gas tightness device for turbine compressor casing Download PDFInfo
- Publication number
- CN203365064U CN203365064U CN 201320354283 CN201320354283U CN203365064U CN 203365064 U CN203365064 U CN 203365064U CN 201320354283 CN201320354283 CN 201320354283 CN 201320354283 U CN201320354283 U CN 201320354283U CN 203365064 U CN203365064 U CN 203365064U
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- CN
- China
- Prior art keywords
- turbocompressor
- shell
- undetected
- impermeability
- sealing
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- 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 - Lifetime
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Abstract
The utility model discloses a leakproof detection gas tightness device for a turbine compressor casing. A positioning device is fixed on a rack. A turbine compressor casing to be detected is positioned in a locking manner on the positioning device. An air inlet passage is also disposed on the positioning device. An air inlet of the turbine compressor casing communicates with an air source in a sealed manner through the air inlet passage. A seal pressing plate is positioned on the rack. The seal pressing plate can seal an air outlet of the turbine compressor casing on the positioning device. A leakproof detection dot drill is positioned on the rack. The leakproof detection dot drill can mark the surface of the turbine compressor casing on the position device. A gas tightness detector is capable of conducting gas tightness detection on the sealed ventilative turbine compressor casing and signaling a controller. The controller is capable of controlling first and second drive devices to respectively drive the seal pressing plate and the leakproof detection dot drill to move. According to the utility model, the production yield and the safety of use of a turbine compressor are improved, fewer materials are wasted and the production efficiency is improved.
Description
Technical field
The utility model relates to a kind of turbocompressor shell checkout equipment, and especially a kind of turbocompressor shell is prevented undetected impermeability equipment.
Background technology
The turbocompressor shell all needs to carry out the impermeability detection in becoming the product process, detecting qualified turbocompressor shell through impermeability enters into subsequent processing and further processes, detect underproof turbocompressor shell and just need to scrap processing, turbocompressor shell impermeability does not have mark after having detected at present, be easy to occur to detect underproof product and not product after testing be fed directly to subsequent processing, to turbocompressor, production brings hidden danger, find again in subsequent detection that impermeability is defective and cause again waste, make production cost high, yields is low.
The utility model content
In order to overcome above-mentioned defect, the utility model provides a kind of turbocompressor shell to prevent undetected impermeability equipment, and the anti-undetected impermeability equipment of this turbocompressor shell is detecting on qualified product and forming the marking clearly through impermeability, is convenient to certified products identification.
The technical scheme that the utility model adopts in order to solve its technical matters: a kind of turbocompressor shell is prevented undetected impermeability equipment, comprise frame, the anti-undetected drill bit of getting ready, sealing clamp, locating device, source of the gas, air-leakage detector, controller and first, two drive units, described locating device is fixed on frame, turbocompressor shell to be detected can be positioned on locating device in stop, also be provided with inlet channel on locating device, this inlet channel is communicated with turbocompressor shell air intake opening with the source of the gas sealing, sealing clamp is positioned on frame, described sealing clamp can be by turbocompressor shell gas outlet sealing on locating device, the anti-undetected drill bit of getting ready is positioned on frame, the described anti-undetected drill bit of getting ready can be stamped the marking in the turbocompressor shell surface on locating device, air-leakage detector can carry out the impermeability detection and be messaging in controller to the turbocompressor shell of sealing ventilation, controller can control first, two drive units drive respectively sealing clamp and the anti-undetected drill bit movement of getting ready.
As further improvement of the utility model, described locating device comprises locating piece, sealing compression leg and the 3rd drive unit, described locating piece is fixed in the frame below, and the sealing compression leg vertically can slide and be positioned directly over locating piece, and the 3rd drive unit drives the motion of sealing compression leg.
As further improvement of the utility model, be formed with the groove with turbocompressor shell profile coupling on described locating piece.
As further improvement of the utility model, described sealing clamp vertically can slide and be positioned on the frame directly over turbocompressor shell gas outlet, and first drives and can drive the sealing clamp longitudinal sliding motion.
As further improvement of the utility model get ready drill bit can be on locating device the turbocompressor shell slide and be positioned on frame, get the drill bit end ready and be provided with and get mould ready, the second drive unit can drive gets the drill bit rectilinear motion ready.
Also be provided with alarm as further improvement of the utility model, described controller is controlled alarm and is given the alarm.
Be cylinder as described first and second drive unit of further improvement of the utility model.
The beneficial effects of the utility model are: the utility model forms the marking clearly by the anti-undetected drill bit of getting ready through impermeability, detecting qualified turbocompressor shell surface, whether qualifiedly through the impermeability detection be convenient to identify this turbocompressor shell, the turbocompressor shell of avoiding unacceptable product and detecting without impermeability flows into subsequent processing, yields and safety in utilization that turbocompressor is produced have been improved, reduce waste of material, improved production efficiency.
The accompanying drawing explanation
Fig. 1 is structural principle front view of the present utility model;
Fig. 2 is structural principle left view of the present utility model.
Embodiment
Embodiment: a kind of turbocompressor shell is prevented undetected impermeability equipment, comprise frame 2, the anti-undetected drill bit 4 of getting ready, sealing clamp 7, locating device, source of the gas, air-leakage detector, controller and first, two drive units 1, 6, described locating device is fixed on frame 2, turbocompressor shell to be detected can be positioned on locating device in stop, also be provided with inlet channel on locating device, this inlet channel is communicated with turbocompressor shell air intake opening with the source of the gas sealing, sealing clamp 7 is positioned on frame 2, described sealing clamp 7 can be by turbocompressor shell gas outlet sealing on locating device, the anti-undetected drill bit 4 of getting ready is positioned on frame 2, the described anti-undetected drill bit 4 of getting ready can be stamped the marking in the turbocompressor shell surface on locating device, air-leakage detector can carry out the impermeability detection and be messaging in controller to the turbocompressor shell of sealing ventilation, controller can control first, two drive units 1, 6 drive respectively sealing clamp 7 and the anti-undetected drill bit 4 of getting ready to move, turbocompressor shell 10 is placed on to stationary positioned on locating device, the product gas outlet is pushed down in sealing clamp 7 sealings simultaneously, guarantee that product cavity is seal cavity, then gas by the inlet channel in locating device under inflation in the product cavity seal cavity, impermeability detects and starts, after impermeability has detected, if gas product pressing lattice, the anti-undetected drill bit 4 of getting ready starts, get the marking clearly on goods, direct visual finding, if air pressure is defective, the anti-undetected drill bit 4 of getting ready will not be got ready, complete with this shell impermeability fixture leakproof operation of calming the anger, on turbocompressor shell after testing, the obvious marking is arranged, be convenient to naked eyes identification, to prevent that the turbocompressor shell from not carrying out airtight test and just flowing into next process.
Described locating device comprises locating piece 9, sealing compression leg 5 and the 3rd drive unit 3, described locating piece 9 is fixed in frame 2 belows, sealing compression leg 5 vertically can slide and be positioned directly over locating piece 9, the 3rd drive unit 3 drives 5 motions of sealing compression leg, the 3rd rotating band motive seal compression leg 5 vertically compresses the turbocompressor shell and realizes turbocompressor shell stop location, the 3rd to drive can be cylinder, can be also the crank block structure etc. of motor powered.
Be formed with the groove with turbocompressor shell profile coupling on described locating piece 9.
Described sealing clamp 7 vertically can slide and be positioned on the frame 2 directly over turbocompressor shell gas outlet, the first driving can drive sealing clamp 7 longitudinal sliding motions, certainly sealing clamp 7 can be also that horizontal slip or rotation mode block the sealing of turbocompressor shell gas outlet, this replacing structure that is equal to that is this patent.
Getting drill bit ready can be positioned on frame 2 on locating device in the slip of turbocompressor shell, getting the drill bit end ready is provided with and gets mould ready, the second drive unit 6 can drive gets the drill bit rectilinear motion ready, compress turbocompressor shell surface by the feeding of getting drill bit ready, get mould ready and just on turbocompressor shell surface, extrude mark clearly, be convenient to the workman and whether identify it through impermeability detection specification product.
Also be provided with alarm, described controller is controlled alarm and is given the alarm, and when air-leakage detector, the turbocompressor shell to be detected defective, just is messaging in controller, controller is controlled warning horn and is sent defective alert notification workman, and warning horn can be that hummer can be also display.
Described first and second drive unit 1,6 is cylinder.
Claims (7)
1. a turbocompressor shell is prevented undetected impermeability equipment, it is characterized in that: comprise frame (2), the anti-undetected drill bit (4) of getting ready, sealing clamp (7), locating device, source of the gas, air-leakage detector, controller and first, two drive units (1, 6), described locating device is fixed on frame (2), turbocompressor shell to be detected can be positioned on locating device in stop, also be provided with inlet channel on locating device, this inlet channel is communicated with turbocompressor shell air intake opening with the source of the gas sealing, sealing clamp (7) is positioned on frame (2), described sealing clamp (7) can be by turbocompressor shell gas outlet sealing on locating device, the anti-undetected drill bit (4) of getting ready is positioned on frame (2), the described anti-undetected drill bit (4) of getting ready can be stamped the marking in the turbocompressor shell surface on locating device, air-leakage detector can carry out the impermeability detection and be messaging in controller to the turbocompressor shell of sealing ventilation, controller can control first, two drive units (1, 6) drive respectively sealing clamp (7) and the anti-undetected drill bit (4) of getting ready to move.
2. turbocompressor shell according to claim 1 is prevented undetected impermeability equipment, it is characterized in that: described locating device comprises locating piece (9), sealing compression leg (5) and the 3rd drive unit (3), described locating piece (9) is fixed in frame (2) below, sealing compression leg (5) vertically can slide and be positioned directly over locating piece (9), and the 3rd drive unit (3) drives sealing compression leg (5) motion.
3. the anti-undetected impermeability equipment of turbocompressor shell according to claim 2, is characterized in that: be formed with the groove with turbocompressor shell profile coupling on described locating piece (9).
4. turbocompressor shell according to claim 1 is prevented undetected impermeability equipment, it is characterized in that: described sealing clamp (7) frame (2) be positioned directly over turbocompressor shell gas outlet of vertically can sliding is upper, and first drives and can drive sealing clamp (7) longitudinal sliding motion.
5. turbocompressor shell according to claim 1 is prevented undetected impermeability equipment, it is characterized in that: getting drill bit ready can be positioned on frame (2) on locating device in the slip of turbocompressor shell, get the drill bit end ready and be provided with and get mould ready, the second drive unit (6) can drive gets the drill bit rectilinear motion ready.
6. turbocompressor shell according to claim 1 is prevented undetected impermeability equipment, it is characterized in that: also be provided with alarm, described controller is controlled alarm and is given the alarm.
7. turbocompressor shell according to claim 1 is prevented undetected impermeability equipment, and it is characterized in that: described first and second drive unit (1,6) is cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320354283 CN203365064U (en) | 2013-06-19 | 2013-06-19 | Leakproof detection gas tightness device for turbine compressor casing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320354283 CN203365064U (en) | 2013-06-19 | 2013-06-19 | Leakproof detection gas tightness device for turbine compressor casing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203365064U true CN203365064U (en) | 2013-12-25 |
Family
ID=49812810
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320354283 Expired - Lifetime CN203365064U (en) | 2013-06-19 | 2013-06-19 | Leakproof detection gas tightness device for turbine compressor casing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203365064U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104236801A (en) * | 2013-06-19 | 2014-12-24 | 远轻铝业（中国）有限公司 | Detection-omission-preventing air tightness device for turbine compressor casing |
| CN113008478A (en) * | 2020-07-29 | 2021-06-22 | 广州阿普顿自动化系统有限公司 | Simple axial inflation sealing performance testing device and method and processing method |
-
2013
- 2013-06-19 CN CN 201320354283 patent/CN203365064U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104236801A (en) * | 2013-06-19 | 2014-12-24 | 远轻铝业（中国）有限公司 | Detection-omission-preventing air tightness device for turbine compressor casing |
| CN113008478A (en) * | 2020-07-29 | 2021-06-22 | 广州阿普顿自动化系统有限公司 | Simple axial inflation sealing performance testing device and method and processing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20131225 |