CN204851654U - Totally enclosed integral turbine - Google Patents
Totally enclosed integral turbine Download PDFInfo
- Publication number
- CN204851654U CN204851654U CN201520415234.2U CN201520415234U CN204851654U CN 204851654 U CN204851654 U CN 204851654U CN 201520415234 U CN201520415234 U CN 201520415234U CN 204851654 U CN204851654 U CN 204851654U
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- turbine
- blade
- shell
- turbine blade
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Abstract
The utility model discloses a totally enclosed integral turbine, including turbine shaft, turbine blade, the turbine shell links together becomes a whole. The shell of turbine one end is fixed the shell that circles the other end in the bearing and is fixed and circle in another bearing, and the outer lane of two bearings is fixed on equipment, and the power transmission rotates for the turbine casing. The utility model discloses a technique is the physics field. Main technique is exactly that turbine shell and turbine blade and turbine shaft link together and become a whole. Solved traditional turbine, gas or liquid will be from the backward flows of the gap between blade and the shell, between blade and the blade when pressure, like this the product will the generate pressure phenomenon of poor and turbine blade deformation. The utility model discloses the turbine is used for automobile engine's turbocharged machine, the suction pump, and gas compressor, the fluid pressure pump, the turbine engine and the screw of car and aircraft still are used for the domestic appliance and the product for civilian use etc..
Description
Technical field
The utility model belongs to the physical technique field of the power transmission of gas and liquid, compression, motion, is specifically related to a kind of hermetically sealed integrated type turbo machine.
Background technique
Along with the sharply development of society industry, the various industrial products of 21 century rise, such as the band such as automobile, electrical equipment, the product for civilian use gives us quick, comfortable life style, but these products all will use turbo machine, due to traditional turbine design defect, cause the waste of the energy and the lower powered using effect of product.And the utility model just completely solves these corresponding problems, reach the performance of energy saving and high power products.
Model utility content
The technical problems to be solved in the utility model is exactly existing conventional turbine because turbine blade is not connected with turbine case, turbine blade does not carry out overlap, and gas or liquid will from the phenomenons of the gap backflow between blade and shell, between blade and blade and deformable blade when there being pressure to cause turbo machine.The power pressure of such product using effect is just very poor, wastes energy again.
In order to solve the problems of the technologies described above, the utility model provides a kind of hermetically sealed integrated type turbo machine, comprise turbine blade, turbine shaft and turbine case, the shell two ends of turbo machine are fixed on the inner ring of two bearings, the outer ring of bearing is fixed on equipment, and power transmission is rotated to turbine casing.
Further, the outer end of turbine case and turbine blade connects together, and the inner and the turbine shaft of turbine blade connect together into as a whole.
Further, the blade of turbine is spirality, the tail end of turbine blade will overlap below the front end of turbine blade, or the tail end of turbine blade will overlap below the front end of another turbine blade, but have certain space length to come propellant gas or liquid between lap, blade has one chip or multidisc.
Further, the shape of turbine blade between turbine case and turbine shaft is arc, the resistance that when can reduce turbine rotation, gas or liquid produce blade.
This programme is by turbine shaft welding or is cast in turbine blade the inner, and then the outer end of turbine blade is welded or is cast in turbine case, makes these parts become as a whole.On the inner ring that the shell of turbo machine one end is fixed on bearing, the shell of the other end is fixed on the inner ring of another bearing, and the outer ring of two bearings is fixed on equipment, and power transmission is rotated to turbine casing.The shell of turbo machine is that motor or driving engine power drive.And Design Turbine Blade growth blade, the blade between turbine casing and turbine shaft is arc.The blade of turbine is spirality, the tail end of turbine blade will overlap below the front end of turbine blade, or the tail end of turbine blade will overlap below the front end of another turbine blade, but have certain space length to come propellant gas or liquid between lap, blade has one chip or multidisc.So often open that blade is overlapping layer by layer ensures air-flow or the liquid condition without backflow.The size of turbine blade and monolithic, multi-disc are determined by space size, reaches the object that pressure is good.The technical field of the hermetically sealed integral type turbo machine of the utility model is the physical technique field belonging to the power transmission of gas and liquid, compression, motion.Main technology is exactly that turbine case links together into as a whole with turbine blade and turbine shaft.Solve conventional turbine, when there being pressure, gas or liquid will from the gap backflows between blade and shell, between blade and blade, and such product will produce the very poor phenomenon of being out of shape with turbine blade of pressure.The utility model is used for the turbocharger of motor car engine, and suction pump, gas compressor, liquid pressure pump, the turbogenerator of automobile and aircraft and propeller cavitation, also for household electric appliance and the product for civilian use etc.For the degree of difficulty of processing technology and the consideration of manufacturing cost, material used in the utility model, can adopt steel, plastics, PX material, glass, pottery etc., the material etc. involved by whole scheme can find in common market.
Accompanying drawing explanation
Fig. 1 is the utility model hermetically sealed integrated type turbo machine front end elevational part-structure schematic diagram.
1. turbine shaft, 2. turbine bucket, 3. turbine casing, 4. bearing, 5. arc shaped blade front end, 6. blade tail end, 7. turbine case drive unit (illustrating in fig. 2).
Fig. 2 is the structure principle chart of the utility model hermetically sealed integrated type turbo machine lateral parts.
3. turbine casing, 4. bearing, 7. turbine case drive unit.
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail:
Embodiment
Embodiment one: as shown in Figure 1, the utility model hermetically sealed integrated type turbo machine front end elevational part-structure, comprising 1. turbine shafts links together into as a whole with 2. turbine buckets with 3. turbine casings, 3. turbine casings are fixed in the inner ring of 4. bearings, again the outer ring of 4. bearings is fixed on equipment, during rotating turbine, turbine 5. arc shaped blade front end is compressed into turbine 6. blade tail end gas or liquid and is gone out.
In technique scheme, first 3 turbine casings are given by power transmission, then drive 1. turbine shafts and 2. turbine buckets and 3. turbine casings to link together into as a wholely to rotate in the inner ring of 4. bearings, the air inlet head of turbo machine is connected in the space of gas or liquid, other end be connected to need gas or liquid water-tight equipment and space in, then during rotating turbine, turbine 5. arc shaped blade front end is compressed into turbine 6. blade tail end gas or liquid and is entered in water-tight equipment or space.For the degree of difficulty of processing technology and the consideration of manufacturing cost, material used in the utility model, can adopt steel, plastics, PX material, glass, pottery etc., the material etc. involved by whole scheme can find in common market.
Embodiment two: if Fig. 2 is the structure of the utility model hermetically sealed integrated type turbo machine lateral parts, 3 shell two ends of turbo machine are fixed on the inner ring of two 4 bearings, then the outer ring of 4 bearings is fixed on equipment, again 7. turbine case drive units are fixed on 3. turbine casings, such power transmission rotates to 3 turbine casings.
In technique scheme, turbo machine is fixed on the inner ring of two 4 bearings, then the outer ring of 4 bearings is fixed on equipment, power 7. turbine case drive unit is rotated whole turbo machine drive by 3. turbine casings, and gas or liquid are compressed in water-tight equipment or space.
Above-described is only preferred implementation of the present utility model and principle, should be understood that for a person skilled in the art, under the prerequisite not departing from the utility model principle and structure, can also make some distortion and improvement, these all can not affect the effect of the utility model enforcement and the model utility of patent.
Claims (4)
1. hermetically sealed integrated type turbo machine, it is characterized in that: comprise turbine blade, turbine shaft and turbine case, turbine case two ends are fixed on the inner ring of two bearings, the outer ring of bearing is fixed on pedestal, and power transmission is rotated to turbine casing.
2. hermetically sealed integrated type turbo machine according to claim 1, is characterized in that: the outer end of turbine case and turbine blade connects together, and the inner and the turbine shaft of turbine blade connect together into as a whole.
3. hermetically sealed integrated type turbo machine according to claim 1, it is characterized in that: described turbine blade is spirality, the tail end of turbine blade overlaps below the front end of turbine blade, or the tail end of turbine blade overlaps below the front end of another turbine blade, have gap between lap, described turbine blade has one chip or multidisc.
4. hermetically sealed integrated type turbo machine according to claim 1, is characterized in that: the shape of turbine blade between turbine case and turbine shaft is arc.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520415234.2U CN204851654U (en) | 2015-06-16 | 2015-06-16 | Totally enclosed integral turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520415234.2U CN204851654U (en) | 2015-06-16 | 2015-06-16 | Totally enclosed integral turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204851654U true CN204851654U (en) | 2015-12-09 |
Family
ID=54742208
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520415234.2U Expired - Fee Related CN204851654U (en) | 2015-06-16 | 2015-06-16 | Totally enclosed integral turbine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204851654U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106321449A (en) * | 2015-06-16 | 2017-01-11 | 周先明 | Totally-sealed integral turbine |
-
2015
- 2015-06-16 CN CN201520415234.2U patent/CN204851654U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106321449A (en) * | 2015-06-16 | 2017-01-11 | 周先明 | Totally-sealed integral turbine |
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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: 20151209 Termination date: 20200616 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |