CN103831758A - Auxiliary installation structure for locking turbines - Google Patents
Auxiliary installation structure for locking turbines Download PDFInfo
- Publication number
- CN103831758A CN103831758A CN201210471360.0A CN201210471360A CN103831758A CN 103831758 A CN103831758 A CN 103831758A CN 201210471360 A CN201210471360 A CN 201210471360A CN 103831758 A CN103831758 A CN 103831758A
- Authority
- CN
- China
- Prior art keywords
- locked
- base
- turbine
- turbines
- chuck 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
- B25B11/02—Assembly jigs
Abstract
The invention provides an auxiliary installation structure for locking turbines. No matter whether shafts of the turbines to be locked are long or not, the auxiliary installation structure is suitable for the turbines. The auxiliary installation structure is good in university and comprises a head clamping board. Clamping openings matched with turbine heads in shape and size are formed in the head clamping board. The bottom of the head clamping board is supported by the upper surface of a base. The auxiliary installation structure for locking the turbines is characterized in that an air cylinder base of an air cylinder is installed on a transverse guide rail on the upper surface of the base, an air cylinder arm of the air cylinder is tightly fixed to the bottom face of a supporting block, the air cylinder moves perpendicularly, the turbine heads of the turbines to be locked are clamped to the corresponding clamping openings, the middle shaft end of each turbine to be locked is supported by the supporting block, the end to be locked of each turbine to be locked is exposed out of the supporting block, the bottom of the head clamping board is clamped to a longitudinal linear rail of the base, and the longitudinal linear rail is perpendicular to the vertical face of the head clamping board and protrudes out of the upper surface of the base.
Description
Technical field
The present invention relates to booster turbine components fixing device, be specially the auxiliary mounting structure of turbine locking.
Background technology
In the installation process of booster turbine, for locking nut, must fix turbine head, shape due to turbine head when installation is different, adopt a kind of custom-designed chuck plate on the ground horizontal fix, the bayonet socket that has the multiple turbine head shape and size such as circle, triangle, hexagon on chuck plate, like this for different turbine heads, does not need replacing instrument.But practical operation is sometimes not too convenient, this just need to adopt turbine exemplar horizontal installation, for this reason, we have designed base, support, support, chuck plate are installed on to base side by side, on support, be provided with the brace table corresponding with bayonet socket, to solve horizontally-mounted problem, but, the problem that this structure exists is that it is only that sub-fraction rides over the brace table on support that turbine exemplar needs one end of locking nut, because the distance between existing support, chuck plate is fixed, inapplicable in short-term when the axle of worm gear to be locked, cause its versatility poor.
Summary of the invention
For above-mentioned situation, the invention provides the auxiliary mounting structure of turbine locking, no matter the axial length of its worm gear to be locked is short, all can be suitable for this structure, the versatility of this structure is good.
The auxiliary mounting structure of turbine locking, its technical scheme is such, it comprises chuck plate, on described chuck plate, be provided with the bayonet socket matching with the shape and size of turbine head, described chuck plate bottom supporting is in the upper surface of base, it is characterized in that: the cylinder block of cylinder is installed on the upper surface cross track of described base, the bottom surface of the fastening described rest pad of cylinder arm of described cylinder, described cylinder moves in vertical direction, the turbine head of worm gear to be locked is installed in corresponding described bayonet socket, the middle part axle head of worm gear described to be locked is supported on described rest pad, the locking end for the treatment of of worm gear described to be locked exposes to described rest pad, the bottom of described chuck plate is installed in longitudinal rectilinear orbit of described base, described longitudinal rectilinear orbit is perpendicular to the facade of described chuck plate, described rectilinear orbit evagination is in the upper surface of described base.
The present invention adopts after said structure, the turbine head of worm gear to be locked is installed in corresponding bayonet socket, the middle part axle head of worm gear to be locked is supported on rest pad, the locking end for the treatment of of worm gear to be locked exposes to described rest pad, and cylinder up-down adjustment makes rest pad can adapt to the worm gear to be locked of the position of differing heights, and cross track guarantees that rest pad position is accurate, chuck plate moves along rectilinear orbit, no matter the axial length of worm gear to be locked is short, all can be suitable for this structure, the versatility of this structure is good.
Accompanying drawing explanation
Fig. 1 is main TV structure schematic diagram of the present invention;
Fig. 2 is that the A of this Fig. 1 is to view structure schematic diagram;
Fig. 3 is the top view structural representation of Fig. 1.
The specific embodiment
See Fig. 1, Fig. 2, Fig. 3, it comprises chuck plate 1, on chuck plate 1, be provided with the bayonet socket 2 matching with the shape and size of turbine head, chuck plate 1 bottom supporting is in the upper surface of base 3, it is characterized in that: the cylinder block of cylinder 4 is installed on the upper surface cross track 5 of base 3, the bottom surface of the fastening rest pad 6 of cylinder arm of cylinder 4, cylinder 4 moves in vertical direction, the turbine head of worm gear to be locked is installed in corresponding bayonet socket 2, the middle part axle head of worm gear to be locked is supported on rest pad 6, the locking end for the treatment of of worm gear to be locked exposes to rest pad 6, the bottom of chuck plate 1 is installed in longitudinal rectilinear orbit 7 of base, longitudinally rectilinear orbit 7 is perpendicular to the facade of chuck plate 1, rectilinear orbit 7 evaginations are in the upper surface of base 3.
Claims (1)
1. the auxiliary mounting structure of turbine locking, it comprises chuck plate, on described chuck plate, be provided with the bayonet socket matching with the shape and size of turbine head, described chuck plate bottom supporting is in the upper surface of base, it is characterized in that: the cylinder block of cylinder is installed on the upper surface cross track of described base, the bottom surface of the fastening described rest pad of cylinder arm of described cylinder, described cylinder moves in vertical direction, the turbine head of worm gear to be locked is installed in corresponding described bayonet socket, the middle part axle head of worm gear described to be locked is supported on described rest pad, the locking end for the treatment of of worm gear described to be locked exposes to described rest pad, the bottom of described chuck plate is installed in longitudinal rectilinear orbit of described base, described longitudinal rectilinear orbit is perpendicular to the facade of described chuck plate, described rectilinear orbit evagination is in the upper surface of described base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210471360.0A CN103831758A (en) | 2012-11-20 | 2012-11-20 | Auxiliary installation structure for locking turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210471360.0A CN103831758A (en) | 2012-11-20 | 2012-11-20 | Auxiliary installation structure for locking turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103831758A true CN103831758A (en) | 2014-06-04 |
Family
ID=50795819
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210471360.0A Pending CN103831758A (en) | 2012-11-20 | 2012-11-20 | Auxiliary installation structure for locking turbines |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103831758A (en) |
-
2012
- 2012-11-20 CN CN201210471360.0A patent/CN103831758A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140604 |