CN203527426U - Turn-over platform for disassembling and assembling novel gas turbine module - Google Patents
Turn-over platform for disassembling and assembling novel gas turbine module Download PDFInfo
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- CN203527426U CN203527426U CN201320715100.3U CN201320715100U CN203527426U CN 203527426 U CN203527426 U CN 203527426U CN 201320715100 U CN201320715100 U CN 201320715100U CN 203527426 U CN203527426 U CN 203527426U
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- combustion machine
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Abstract
The utility model relates to a turn-over platform for disassembling and assembling a novel gas turbine module. According to the technical scheme of the turn-over platform, the turn-over platform for disassembling and assembling the novel gas turbine module comprises an original platform and a switching platform, wherein the original platform is a turn-over platform for disassembling and assembling an old gas turbine module, the switching platform comprises a disk and a rigid reinforcing shaft, a positioning bolt penetrates a matching hole and a positioning hole to connect the switching platform to the original platform, and an assembling bolt penetrates an installing hole and an assembling hole to connect the novel gas turbine module to the switching platform. According to the turn-over platform for disassembling and assembling the novel gas turbine module, the existing turn-over platform for disassembling and assembling the old gas turbine module is redesigned and remanufactured for disassembling and assembling the novel gas turbine module.
Description
Technical field
The utility model relates to a kind of overturn platform, particularly relates to a kind of overturn platform that decomposes and assemble for novel combustion machine turbine unit body.
Background technology
In the decomposition of combustion machine turbine unit body and assembling process, need repeatedly to overturn, need to require design frock to meet the demands according to decomposition, assembly technology.Combustion machine turbine unit body decomposes, general assembly state is that turbine wheel shaft is perpendicular to the ground, and lifting, transportation and laying state are that turbine wheel shaft is parallel to the ground, therefore requires overturn platform to turn over and turn 90 degrees, the two drop hanger traction control speed and the angle that during upset, adopt row to hang.Turbine unit body completes on overturn platform surface and decomposes and assembling, and then overturn platform turns over to turn 90 degrees and lifts, and enters next procedure.
The series of products of present various combustion machines are many, each series needs to design and produce corresponding assembly tooling, and versatility is not strong, the decomposition of the turbine unit body of making and assembling overturn platform are very many, easily be eliminated soon and leave unused in a large number, cause and take substantial contribution and take large quantity space.
Utility model content
The purpose of this utility model is to provide a kind of overturn platform that decomposes and assemble for novel combustion machine turbine unit body, adopt existing old type combustion machine turbine unit body to decompose and assembling overturn platform, through redesigning after manufacture, for carrying out decomposition and the assembly work of novel combustion machine turbine unit body.
The technical solution of the utility model is:
An overturn platform that decomposes and assemble for novel combustion machine turbine unit body, described novel combustion machine turbine unit body comprises rotor and stator, and axis hole is worn in described rotor setting, and described overturn platform comprises original platform and transfer platform; Described original platform is the overturn platform that decomposes and assemble for old type combustion machine turbine unit body, the decomposition of described original platform, assembling load and overturn platform diameter can meet the specification requirement of described novel combustion machine turbine unit body decomposition and general assembly, described original platform is provided with frock stand, described tooling platform has set up round mouth one, locating hole and dead axle hole, and described round mouth one and locating hole and described novel combustion machine turbine unit body size are mismatched; Described transfer platform comprises disk and rigidity reinforced shaft, seam is set below described disk to be coordinated with described round mouth one, it is corresponding with described position of positioning hole that described disk arranges mating holes, and described transfer platform penetrates described mating holes by bolt and is connected with described original platform with described locating hole; Round mouth two with described novel combustion machine turbine unit body dimensional fits is set above described disk, the pilot hole that described disk setting coordinates with the installing hole of described novel combustion machine turbine unit body, for being connected by assembling bolt described novel combustion machine turbine unit body with described transfer platform; Described rigidity reinforced shaft is fixedly installed on described disc centre, and the lower end of described rigidity reinforced shaft is used for penetrating described dead axle hole, described in the upper end of described rigidity reinforced shaft is used for penetrating, wears axis hole.
The described overturn platform that decomposes and assemble for novel combustion machine turbine unit body, preferred version is: described bolt, described mating holes and described locating hole quantity are 18, and described bolt is M20.
The described overturn platform that decomposes and assemble for novel combustion machine turbine unit body, preferred version is: described assembling bolt, described installing hole and described pilot hole quantity are 100, and described assembling bolt is M8.
The beneficial effects of the utility model:
1, the utility model is in design philosophy, in line with the principle of saving time, saving funds, the overturn platform that has utilized original combustion machine turbine unit body to decompose and assemble, on the basis of not destroying former overturn platform frock stand, improve dexterously design, adopt the method that increases transfer platform, overturn platform is had adapt to multiple combustion machine turbine unit body to overturn, decompose and assemble, fix and the function of the work such as lifting, in the situation that improving capacity utilization, saved funds and manufactured and designed the time, and having saved the space in workshop.
2, in the rigidity reinforced shaft at transfer platform center, go deep into the rotor center of turbine unit body, its effect one is when decomposition/general assembly turbine unit body rotor, to carry out accurate axle location; Effect two is to locate rotor in upset turbine unit body process, reduces turbine unit body upset inertia, guarantees the rigidity of bolt.
Accompanying drawing explanation
Fig. 1 is original platform structure schematic front view;
Fig. 2 is original platform structure diagrammatic top view;
Fig. 3 is the location drawing that original platform overturns after 90 °;
Fig. 4 is transfer platform structural representation front view;
Fig. 5 is transfer platform structural representation top view;
Fig. 6 is that novel combustion machine turbine unit body is arranged on the schematic diagram on new overturn platform;
Fig. 7 is the location drawing that new overturn platform overturns after 90 °;
In figure: 1 is disk, 2 is rigidity reinforced shaft, and 3 is original platform, and 4 is novel combustion machine turbine unit body, and 5 is dead axle hole.
The specific embodiment
As shown in Fig. 1～7, a kind of overturn platform that decomposes and assemble for novel combustion machine turbine unit body 4, described novel combustion machine turbine unit body 4 comprises rotor and stator, and axis hole is worn in described rotor setting, and described overturn platform comprises original platform 3 and transfer platform; Described original platform 3 is the overturn platform that decomposes and assemble for old type combustion machine turbine unit body, the decomposition of described original platform 3, assembling load are 22T, overturn platform diameter is 3m, the decomposition of described novel combustion machine turbine unit body 4, assembling load are 3T, overturn platform diameter is 1m, can meet the specification requirement of decomposition and general assembly; Described original platform 3 is provided with frock stand, and described tooling platform has set up round mouth one, 18 locating holes and dead axle holes 5, and described round mouth one and locating hole and described novel combustion machine turbine unit body size are mismatched; Described transfer platform comprises disk 1 and rigidity reinforced shaft 2, described disk 1 arranges seam below and coordinates with described round mouth one, it is corresponding with described 18 position of positioning hole that described disk 1 arranges mating holes, and described transfer platform penetrates described 18 mating holes by 18 M20 bolts and is connected with described original platform 3 with described 18 locating holes; Described disk 1 arranges the round mouth two with described novel combustion machine turbine unit body dimensional fits above, described disk 1 arranges 100 pilot holes that installing hole coordinates with described novel combustion machine turbine unit body, and described novel combustion machine turbine unit body 4 penetrates described 100 installing holes by 100 M8 assembling bolts and is connected with described transfer platform with described 100 pilot holes; Described rigidity reinforced shaft 2 is fixedly installed on described disk 1 center, and the lower end of described rigidity reinforced shaft 2 penetrates described dead axle hole, described in the upper end of described rigidity reinforced shaft 2 penetrates, wears axis hole.After installing, can overturn, decompose and assemble, the work such as fixing and lifting.
Claims (3)
1. an overturn platform that decomposes and assemble for novel combustion machine turbine unit body, is characterized in that, described novel combustion machine turbine unit body comprises rotor and stator, and axis hole is worn in described rotor setting, and described overturn platform comprises original platform and transfer platform; Described original platform is the overturn platform that decomposes and assemble for old type combustion machine turbine unit body, the decomposition of described original platform, assembling load and overturn platform diameter can meet the specification requirement of described novel combustion machine turbine unit body decomposition and general assembly, described original platform is provided with frock stand, described tooling platform has set up round mouth one, locating hole and dead axle hole, and described round mouth one and locating hole and described novel combustion machine turbine unit body size are mismatched; Described transfer platform comprises disk and rigidity reinforced shaft, seam is set below described disk to be coordinated with described round mouth one, it is corresponding with described position of positioning hole that described disk arranges mating holes, and described transfer platform penetrates described mating holes by bolt and is connected with described original platform with described locating hole; Round mouth two with described novel combustion machine turbine unit body dimensional fits is set above described disk, the pilot hole that described disk setting coordinates with the installing hole of described novel combustion machine turbine unit body, for being connected by assembling bolt described novel combustion machine turbine unit body with described transfer platform; Described rigidity reinforced shaft is fixedly installed on described disc centre, and the lower end of described rigidity reinforced shaft is used for penetrating described dead axle hole, described in the upper end of described rigidity reinforced shaft is used for penetrating, wears axis hole.
2. the overturn platform that decomposes and assemble for novel combustion machine turbine unit body according to claim 1, is characterized in that, described bolt, described mating holes and described locating hole quantity are 18, and described bolt is M20.
3. the overturn platform that decomposes and assemble for novel combustion machine turbine unit body according to claim 1 and 2, is characterized in that, described assembling bolt, described installing hole and described pilot hole quantity are 100, and described assembling bolt is M8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320715100.3U CN203527426U (en) | 2013-11-11 | 2013-11-11 | Turn-over platform for disassembling and assembling novel gas turbine module |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320715100.3U CN203527426U (en) | 2013-11-11 | 2013-11-11 | Turn-over platform for disassembling and assembling novel gas turbine module |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203527426U true CN203527426U (en) | 2014-04-09 |
Family
ID=50413686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320715100.3U Expired - Fee Related CN203527426U (en) | 2013-11-11 | 2013-11-11 | Turn-over platform for disassembling and assembling novel gas turbine module |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203527426U (en) |
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2013
- 2013-11-11 CN CN201320715100.3U patent/CN203527426U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140409 Termination date: 20171111 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |