CN208073622U - A kind of gas oil separation structure - Google Patents
A kind of gas oil separation structure Download PDFInfo
- Publication number
- CN208073622U CN208073622U CN201820309568.5U CN201820309568U CN208073622U CN 208073622 U CN208073622 U CN 208073622U CN 201820309568 U CN201820309568 U CN 201820309568U CN 208073622 U CN208073622 U CN 208073622U
- Authority
- CN
- China
- Prior art keywords
- oil
- guide sleeve
- turbine wheel
- wheel shaft
- gas
- 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.)
- Expired - Fee Related
Links
- 238000000926 separation method Methods 0.000 title claims abstract description 21
- 238000010276 construction Methods 0.000 claims abstract description 7
- 239000003921 oil Substances 0.000 description 48
- 239000010687 lubricating oil Substances 0.000 description 7
- 230000005540 biological transmission Effects 0.000 description 3
- 238000005461 lubrication Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
Abstract
The utility model is related to a kind of gas oil separation structures, including engine spindle, oil gas guide sleeve, engine spindle is hollow-core construction, it is formed by connecting by compressorshaft and turbine wheel shaft, equipped with the oil gas guide sleeve for extending radially through main shaft on the compressorshaft positioned at fore bearing chamber, oil gas guide sleeve is being provided with venthole positioned at main-shaft core position, turbine wheel shaft is radially provided with 2 the first uniformly distributed oil circuit holes, it is additionally provided with internal diameter on the inner wall near exhaust pipe in turbine wheel shaft and is more than the annular oil trap of inner wall surface, and is provided with the second oil circuit hole on oil trap.The utility model utilizes existing high-speed rotating engine spindle structure, does not need individual separating mechanism, while realizing Oil-gas Separation, can not only subtract low power consumption, the air of separation is burnt up through exhaust section, reduces the pollution to extraneous atmospheric environment.
Description
Technical field
The utility model is related to a kind of gas oil separation structures.
Background technology
Because of the rotation of the components such as bearing, gear and oil lubrication splash when aero-engine works, cause to exist in bearing bore
A large amount of mist of oils blend to form oil gas with bearing chamber air, and oil gas is unfavorable for lubrication and the cooling of system, it is therefore desirable to by oil gas
Discharge.If the oil gas in bearing bore, which is expelled directly out, will cause a large amount of consumption of lubricating oil, and pollute environment, therefore must will be in bearing bore
The lubricating oil contained in air is separated, to reduce lube use rate.Generally use centrifuge formula ventilator realizes oil gas at present
Separation, centrifuge formula ventilator are that the separation of liquid phase oil droplet in oil gas is carried out using centrifugal principle.Structure is mainly by rotor, shell
And the compositions such as bearing support, it is a complete attachment, is driven by special transmission mechanism.Rotor is to realize Oil-gas Separation
Core carries the impeller of 6~8 disc, and center is the central shaft of supporting rotor, and venthole is typically recessed on axis.It is mingled with sliding
After the oil gas of the small oil droplet of oil enters centrifuge formula ventilator, wheel rotation keeps air outwardly radial by one with the small oil droplet of lubricating oil
Power, i.e. centrifugal force.Since lubricating oil is different from the density of air, lubricating oil is thrown to inner walls by centrifugal force, by wall
Aperture flows back to casing inner cavity or bearing bore, and the gas after being detached is discharged from centre bore, to realize the function of Oil-gas Separation.It is existing
Some gas oil separation structures is complicated, need to design special transmission mechanism to drive, and the power of consumption of engine carries out when work
Oil-gas Separation reduces the output power of engine.
Invention content
The purpose of this utility model is to provide a kind of gas oil separation structure, need not be special while realizing Oil-gas Separation
The transmission mechanism of door drives, simple in structure, and reduces the power consumption of engine.
The technical solution of the utility model is that the gas oil separation structure includes engine spindle, oil gas guide sleeve, is started
Owner's axis is hollow-core construction, is formed by connecting by compressorshaft and turbine wheel shaft, and diameter is housed on the compressorshaft positioned at fore bearing chamber
To the oil gas guide sleeve through main shaft, oil gas guide sleeve is being provided with venthole positioned at main-shaft core position, and turbine wheel shaft is radially provided with 2
The first uniformly distributed oil circuit hole is additionally provided with annular collection of the internal diameter more than inner wall surface in turbine wheel shaft on the inner wall near exhaust pipe
Oil groove, and the second oil circuit hole is provided on oil trap, the first oil circuit hole is mutually with the second oil circuit hole along engine spindle axis
90 ° of angles, the hollow-core construction of the engine spindle extend to exhaust pipe.
When the utility model is used, since fore bearing is to use pressure seal, the air pressure in bearing bore is more than extraneous gas
Pressure, therefore the oil gas of fore bearing intracavitary enters compressor spindle axis under the action of bearing bore chamber pressure by oil gas guide sleeve.
Oil gas into spindle axis is rotated with main axis, and enters the turbine wheel shaft axle center being connected with compressor main shaft.Oil gas exists
Oil-gas Separation is carried out due to centrifugal force in rotary course, small lubricating oil oil droplet hits the condensed on inner walls in spindle axis into oil
Pearl.After oil droplet is expelled directly out from the first oil circuit hole or is collected on oil trap, it is discharged by the second oil circuit hole, the lubricating oil of discharge can
The air for utilizing, and separating again is discharged into air after entering exhaust section burn-up by exhaust pipe along turbine wheel shaft.This practicality is new
Type utilizes existing high-speed rotating engine spindle structure, does not need individual separating mechanism, is realizing the same of Oil-gas Separation
When, it can not only subtract low power consumption, the air of separation is burnt up through exhaust section, reduces the pollution to extraneous atmospheric environment.
Description of the drawings
Fig. 1 the utility model is related to gas oil separation structure schematic diagram.
Specific implementation mode
As shown, gas oil separation structure includes engine spindle, oil gas guide sleeve 7, engine spindle is hollow-core construction, by
Compressorshaft 1 and turbine wheel shaft 2 are formed by connecting, equipped with the oil gas for extending radially through main shaft on the compressorshaft 1 positioned at fore bearing chamber
Guide sleeve 7, oil gas guide sleeve 7 are being provided with venthole positioned at main-shaft core position, and turbine wheel shaft 2 is radially provided with 2 the first uniformly distributed oil
Road hole 3 is additionally provided with the annular oil trap 4 that internal diameter is more than inner wall surface in turbine wheel shaft 2 on the inner wall near exhaust pipe 6, and
The second oil circuit hole 5 is provided on oil trap, the first oil circuit hole 3 is mutually in 90 ° along engine spindle axis with the second oil circuit hole 5
The hollow-core construction at angle, the engine spindle extends to exhaust pipe 6.
Claims (1)
1. a kind of gas oil separation structure, which is characterized in that the structure includes engine spindle, oil gas guide sleeve (7), engine
Main shaft is hollow-core construction, is formed by connecting by compressorshaft (1) and turbine wheel shaft (2), on the compressorshaft of fore bearing chamber (1)
Equipped with the oil gas guide sleeve (7) for extending radially through main shaft, oil gas guide sleeve (7) is being provided with venthole, turbine wheel shaft positioned at main-shaft core position
(2) be radially provided with two the first uniformly distributed oil circuit holes (3), also set on the inner wall of exhaust pipe (6) nearby in turbine wheel shaft (2)
There is internal diameter to be more than the annular oil trap (4) of inner wall surface, and is provided with the second oil circuit hole (5), the first oil circuit hole on oil trap
(3) with the second oil circuit hole (5) along engine spindle axis mutually at an angle of 90, the hollow-core construction of the engine spindle extends to
Exhaust pipe (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820309568.5U CN208073622U (en) | 2018-03-06 | 2018-03-06 | A kind of gas oil separation structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820309568.5U CN208073622U (en) | 2018-03-06 | 2018-03-06 | A kind of gas oil separation structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208073622U true CN208073622U (en) | 2018-11-09 |
Family
ID=64038613
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820309568.5U Expired - Fee Related CN208073622U (en) | 2018-03-06 | 2018-03-06 | A kind of gas oil separation structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208073622U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108361111A (en) * | 2018-03-06 | 2018-08-03 | 中国航发哈尔滨东安发动机有限公司 | A kind of gas oil separation structure |
| CN110917734A (en) * | 2019-12-05 | 2020-03-27 | 中国航发四川燃气涡轮研究院 | Centrifugal impeller type ventilator and gear box |
-
2018
- 2018-03-06 CN CN201820309568.5U patent/CN208073622U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108361111A (en) * | 2018-03-06 | 2018-08-03 | 中国航发哈尔滨东安发动机有限公司 | A kind of gas oil separation structure |
| CN110917734A (en) * | 2019-12-05 | 2020-03-27 | 中国航发四川燃气涡轮研究院 | Centrifugal impeller type ventilator and gear box |
| CN110917734B (en) * | 2019-12-05 | 2021-10-22 | 中国航发四川燃气涡轮研究院 | Centrifugal impeller type ventilator and gear box |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181109 |