CN207348970U - A kind of automated intelligent cooling device of gas turbine - Google Patents
A kind of automated intelligent cooling device of gas turbine Download PDFInfo
- Publication number
- CN207348970U CN207348970U CN201721465924.4U CN201721465924U CN207348970U CN 207348970 U CN207348970 U CN 207348970U CN 201721465924 U CN201721465924 U CN 201721465924U CN 207348970 U CN207348970 U CN 207348970U
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- CN
- China
- Prior art keywords
- gas turbine
- clearance layer
- cooling device
- condenser pipe
- casing
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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.)
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- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The utility model discloses a kind of automated intelligent cooling device of gas turbine, including body, the body is provided outside casing, formed with clearance layer between the body and the casing, refrigerant storage chamber and condenser pipe are provided with the clearance layer, the sensing valve being connected with the condenser pipe is provided with the refrigerant storage chamber, sensor device is additionally provided with the clearance layer；The blower system being connected with the clearance layer is provided with the outside of the casing.The utility model is simple in structure, and " thermal extremes " produced to gas turbine have good cooling effect, ensure that the normal work of gas turbine, extend the service life of gas turbine, meet actual operation requirements.
Description
Technical field
A kind of automated intelligent cooling device of gas turbine is the utility model is related to, belongs to Intelligent cooling device technology neck
Domain.
Background technology
Known technology like this is related to by gas generator and power turbine assembling gas turbine.Therefore, starting point is usual
It is so-called pure jet engine（That is, the aero-engine of fan is not bypassed）, wherein the gaseous-pressure before nozzle is
The overvoltage of 0.3-0.9bar.Nozzle is removed, and allows burning gases under stress in the single power of driving engine
Expanded in turbine.Thus, the jet engine for only producing propulsive force is successfully converted to electric generation gas turbine.It is such
Gas turbine is commonly referred to as aero-derived gas turbine, these many gas turbines have come into operation, and are particularly filled as backup power
Put.But gas turbine can produce very high temperature in real work（Also referred to as " thermal extremes "）, it is this " extreme high
Temperature " can directly the work efficiency of reduction gas turbine, oil consumption be very big and inner body loss is big, greatly shorten combustion gas
The service life of turbine.For this reason, it may be necessary to design a kind of new technical solution, the shortcomings of the prior art can be overcome.
The content of the invention
The utility model is exactly in view of the deficienciess of the prior art, providing a kind of automated intelligent cooling dress of gas turbine
Put, the cooling device is simple in structure, and " thermal extremes " produced to gas turbine have good cooling effect, ensure that
The normal work of gas turbine, extends the service life of gas turbine, meets actual operation requirements.
To solve the above problems, technical solution adopted in the utility model is as follows：
A kind of automated intelligent cooling device of gas turbine, including body, the body are provided outside casing, the body
Formed with clearance layer between the casing, refrigerant storage chamber and condenser pipe, the refrigerant are provided with the clearance layer
The sensing valve being connected with the condenser pipe is provided with storage chamber, sensor device is additionally provided with the clearance layer；
The blower system being connected with the clearance layer is provided with the outside of the casing.
As the improvement of above-mentioned technical proposal, the blower system includes temperature-compensating room, the temperature-compensating outside
Air inlet is provided with, temperature sense medium, Cycle Unit, energy transfer tube and flow valve are provided with the temperature-compensating room.
As the improvement of above-mentioned technical proposal, the condenser pipe is wound around on the madial wall of the clearance layer, and described
It is raised that reinforced partial condensation is provided with condenser pipe.
Compared with prior art, the implementation result of the utility model is as follows：
The automated intelligent cooling device of gas turbine described in the utility model, the cooling device is simple in structure, to combustion gas
" thermal extremes " that turbine produces have good cooling effect, ensure that the normal work of gas turbine, extend combustion
The service life of gas-turbine, meets actual operation requirements.
Brief description of the drawings
Fig. 1 is the automated intelligent cooling device structure diagram of gas turbine described in the utility model；
Fig. 2 is blower system internal structure schematic diagram described in the utility model；
Fig. 3 is condenser tube structure schematic diagram described in the utility model.
Embodiment
Illustrate the content of the utility model below in conjunction with specific embodiments.
As shown in figures 1 and 3, it is the automated intelligent cooling device structural representation of gas turbine described in the utility model
Figure.
The automated intelligent cooling device of gas turbine described in the utility model, including body 100, outside the body 100
Equipped with casing 200, clearance layer 300 is formed between the body 100 and casing 200, being equipped with refrigerant in the clearance layer 300 stores up
Chamber 310 and condenser pipe 320 are deposited, the refrigerant storage chamber 310 is equipped with the sensing valve 311 being connected with condenser pipe 320,
Sensor device 330 is additionally provided with clearance layer 300；The outside of casing 200 is equipped with the blower system being connected with clearance layer 300
400.The core of the utility model is liquid gas refrigeration system being combined, and coordinates corresponding inductor to realize to gas turbine
Intelligent cooling.Specifically, when sensor device 330, which senses gas turbine, produces " thermal extremes " or higher temperature（It is super
Cross predetermined temperature）, can voluntarily start sensing valve 311 and realize circulation temperature lowering effect of the refrigerant in clearance layer 300（This mistake
Journey, coordinates condenser pipe 320 further to realize and cools）, then coordinate blower system 400 to use, the height produced to gas turbine
Temperature realizes extraordinary cooling, cooling effect.
Further with improvement, the blower system 400 includes temperature-compensating room 410, and the outside of temperature-compensating room 410 is set
There is air inlet 420, temperature sense medium 411, Cycle Unit 412, energy transfer tube 413 are equipped with the temperature-compensating room 410
And flow valve 414, improve air-cooled effect and intelligence.
Specifically, the condenser pipe 320 is wound around on the madial wall of clearance layer 300, and condenser pipe 320 is equipped with and strengthens
Type partial condensation protrusion 321, realizes rapid cooling effect for the fuel oil of local boiling, avoids the loss of gas turbine.
Above content is the detailed description made in conjunction with specific embodiments to the utility model, it is impossible to assert that this practicality is new
Type specific implementation is only limitted to these explanations.For those skilled in the art of the present invention, this is not being departed from
On the premise of utility model is conceived, some simple deduction or replace can also be made, should all be considered as belonging to the utility model guarantor
The scope of shield.
Claims (3)
1. a kind of automated intelligent cooling device of gas turbine, including：Body（100）, it is characterised in that：The body（100）
It is provided outside casing（200）, the body（100）With the casing（200）Between formed with clearance layer（300）, the gap
Layer（300）It is interior to be equipped with refrigerant storage chamber（310）And condenser pipe（320）, the refrigerant storage chamber（310）On be provided with and institute
State condenser pipe（320）The sensing valve being connected（311）, in the clearance layer（300）Inside it is additionally provided with sensor device
（330）；
The casing（200）Outside is equipped with and the clearance layer（300）The blower system being connected（400）.
A kind of 2. automated intelligent cooling device of gas turbine according to claim 1, it is characterised in that：The blower system
（400）Including temperature-compensating room（410）, the temperature-compensating room（410）Outside is equipped with air inlet（420）, the temperature-compensating
Room（410）Inside it is provided with temperature sense medium（411）, Cycle Unit（412）, energy transfer tube（413）And flow valve（414）.
A kind of 3. automated intelligent cooling device of gas turbine according to claim 1, it is characterised in that：The condenser pipe
（320）It is wound around the clearance layer（300）Madial wall on, and the condenser pipe（320）It is equipped with reinforced partial condensation
It is raised（321）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721465924.4U CN207348970U (en) | 2017-11-07 | 2017-11-07 | A kind of automated intelligent cooling device of gas turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721465924.4U CN207348970U (en) | 2017-11-07 | 2017-11-07 | A kind of automated intelligent cooling device of gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207348970U true CN207348970U (en) | 2018-05-11 |
Family
ID=62353843
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721465924.4U Expired - Fee Related CN207348970U (en) | 2017-11-07 | 2017-11-07 | A kind of automated intelligent cooling device of gas turbine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207348970U (en) |
-
2017
- 2017-11-07 CN CN201721465924.4U patent/CN207348970U/en not_active Expired - Fee Related
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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: 20180511 Termination date: 20211107 |