CN214887382U - Gas turbine unit cabin with monitoring function - Google Patents
Gas turbine unit cabin with monitoring function Download PDFInfo
- Publication number
- CN214887382U CN214887382U CN202120331243.9U CN202120331243U CN214887382U CN 214887382 U CN214887382 U CN 214887382U CN 202120331243 U CN202120331243 U CN 202120331243U CN 214887382 U CN214887382 U CN 214887382U
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- CN
- China
- Prior art keywords
- gas turbine
- cabin
- generator
- monitor
- control terminal
- 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
- 238000012544 monitoring process Methods 0.000 title claims abstract description 17
- 230000002159 abnormal effect Effects 0.000 abstract description 5
- 238000013024 troubleshooting Methods 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 abstract description 2
- 208000033999 Device damage Diseases 0.000 abstract 1
- 238000013480 data collection Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 36
- 238000007689 inspection Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
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- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The utility model discloses a gas turbine set cabin with monitoring function, which comprises a gas turbine, an engine, a generator cabin, a gas turbine cabin, a guide rail, a monitor, a data collector, an alarm, a display and a control terminal; the generator chamber and the gas turbine chamber are arranged side by side; the engine and the gas turbine are respectively arranged in the generator cabin and the gas turbine cabin and are connected through a rotating shaft; the monitor is installed on the guide rail, and the guide rail sets up respectively and is fixed in generator cabin, gas turbine cabin top, and control terminal passes through the cable and is connected with data collection station, monitor and siren respectively, and the control terminal output is connected with the display. The utility model processes and judges the data collected by the data collector through the control terminal, and gives an alarm when finding abnormal data, thereby being beneficial to the fault analysis and the troubleshooting of the gas turbine unit; through portable watch-dog, under the unable accurate condition of judging the device damage of tour personnel, the backstage is accurately tourd.
Description
Technical Field
The utility model relates to a gas turbine unit cabin safety technical field especially relates to a take monitor function's gas turbine unit cabin.
Background
During the normal operation of the gas turbine unit, the generator cabin and the turbine cabin need to be ventilated and cooled by the fan, and natural gas leaked from the turbine cabin is prevented from leaking to the generator cabin, so that the turbine cabin is under negative pressure and the generator cabin is under positive pressure. Because of the cabin environment is abominable, tour personnel can't get into the cabin and inspect and the window monitoring range on the cabin door is limited and because of the cabin environment reason the window monitoring on the cabin door is vague after operation or taking place abnormal alarm, be very unfavorable for tour personnel to the operation of gas turbine and the tour inspection when taking place abnormal alarm, threaten the operation safety of gas turbine and seriously lead to the equipment to damage, cause great loss.
In a test system of a gas turbine test bed disclosed in the published patent application number (CN201620426302. X), the analysis and troubleshooting speed of equipment faults is improved by measuring the external atmospheric pressure and gas pressure, temperature, flow, rotating speed and vibration parameters of each component of the gas turbine in real time and monitoring the running state of the equipment. The scheme is only used for monitoring the internal parameters of the gas turbine, but if the cabin finds that a lot of oil is accumulated after the shutdown every time, the oil leakage point cannot be judged; or during the normal operation of the gas turbine, the parameters of the vibration measuring points are abnormal, and whether the reasons are problems such as looseness of the vibration measuring points or not cannot be accurately judged in an auxiliary mode.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to overcome prior art not enough, provide a take monitor function's gas turbine unit cabin, install the watch-dog according to the guide rail route removal additional in gas turbine unit generator cabin and turbine cabin, tour personnel can carry out the accurate tour to the generator and the gas turbine body in cabin inside in real time at the background, and after taking place unusual the warning, can carry out accurate supplementary judgement.
The purpose of the utility model is realized through the following technical scheme:
a gas turbine engine unit cabin with a monitoring function comprises a gas turbine, an engine, a generator cabin, a gas turbine cabin, a guide rail and a monitor; the generator chamber and the gas turbine chamber are arranged side by side; the engine and the gas turbine are respectively arranged in the generator cabin and the gas turbine cabin and are connected through a rotating shaft; the guide rail sets up respectively and is fixed in generator cabin, gas turbine cabin top, and the watch-dog is installed on the guide rail.
The guide rails are distributed on the walls of the top ends of the rooms of the generator cabin and the gas turbine cabin in an I shape.
The monitor is an omnidirectional monitor, and a camera of the monitor can rotate by 360 degrees.
The gas turbine unit cabin with the monitoring function further comprises a data acquisition unit, an alarm, a display and a control terminal, wherein the control terminal is connected with the data acquisition unit, the monitor and the alarm through cables, and the output end of the control terminal is connected with the display. The data acquisition unit is arranged in the gas turbine unit and comprises an air pressure sensor, a temperature sensor, a vibration sensor and a flow sensor.
The utility model has the advantages that:
1. the utility model transmits the real-time data of the operation of the gas turbine unit to the control terminal through the data acquisition unit, processes and judges the data by the control terminal, and sends out an alarm to the staff if abnormal data is found, thereby being beneficial to the fault analysis and the troubleshooting of the gas turbine unit;
2. the utility model discloses an equip portable watch-dog, can pass through cabin window and can't accurately judge under the condition that the device damaged patrolling personnel, the backstage carries out real-time accurate inspection.
Drawings
Fig. 1 is a connection diagram of the present invention.
Detailed Description
In order to clearly understand the technical features, objects, and effects of the present invention, embodiments of the present invention will be described with reference to the accompanying drawings.
In the present embodiment, as shown in fig. 1, a gas turbine engine compartment with a monitoring function includes a gas turbine, an engine, a generator compartment, a gas turbine compartment, a guide rail, and a monitor; the generator chamber and the gas turbine chamber are arranged side by side; the engine and the gas turbine are respectively arranged in the generator cabin and the gas turbine cabin and are connected through a rotating shaft; the guide rail sets up respectively and is fixed in generator cabin, gas turbine cabin top, and the watch-dog is installed on the guide rail.
The guide rails are distributed on the walls of the top ends of the rooms of the generator cabin and the gas turbine cabin in an I shape. On the basis of not influencing the normal operation of the unit, corresponding adjustment and arrangement can be carried out according to the part which is actually required to be monitored in the cabin.
The monitor is an omnidirectional monitor, and a camera of the monitor can rotate by 360 degrees. The monitor model can be flexibly selected according to the monitoring precision requirement, and can flexibly slide on the guide rail after being installed.
The gas turbine unit cabin with the monitoring function further comprises a data acquisition unit, an alarm, a display and a control terminal, wherein the control terminal is connected with the data acquisition unit, the monitor and the alarm through cables, and the output end of the control terminal is connected with the display. The data acquisition unit is arranged in the gas turbine unit and comprises an air pressure sensor, a temperature sensor, a vibration sensor and a flow sensor.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, and it should be understood by those skilled in the art that the present invention is not limited by the above embodiments, but only by the description of the above embodiments and the description, without departing from the spirit and scope of the present invention, the present invention can also have various changes and modifications, and these changes and modifications all fall within the scope of the claimed invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. A gas turbine engine unit cabin with a monitoring function is characterized by comprising a gas turbine, an engine, a generator cabin, a gas turbine cabin, a guide rail and a monitor; the generator chamber and the gas turbine chamber are arranged side by side; the engine and the gas turbine are respectively arranged in the generator cabin and the gas turbine cabin and are connected through a rotating shaft; the guide rail sets up respectively and is fixed in generator cabin, gas turbine cabin top, and the watch-dog is installed on the guide rail.
2. Gas turbine engine compartment with monitoring according to claim 1, characterized in that the guide rails are distributed in an i-shape on the generator compartment and the top wall of the gas turbine compartment room.
3. The gas turbine nacelle with monitoring function of claim 1, wherein the monitor is an omnidirectional monitor, and the camera of the omnidirectional monitor can rotate 360 °.
4. The gas turbine engine compartment with monitoring function of claim 1, further comprising a data collector, an alarm, a display and a control terminal, wherein the control terminal is connected with the data collector, the monitor and the alarm through cables, and the output end of the control terminal is connected with the display.
5. The gas turbine nacelle with monitoring function of claim 4, wherein the data collector is disposed in the gas turbine, and comprises a pressure sensor, a temperature sensor, a vibration sensor, and a flow sensor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120331243.9U CN214887382U (en) | 2021-02-05 | 2021-02-05 | Gas turbine unit cabin with monitoring function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120331243.9U CN214887382U (en) | 2021-02-05 | 2021-02-05 | Gas turbine unit cabin with monitoring function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214887382U true CN214887382U (en) | 2021-11-26 |
Family
ID=78857952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120331243.9U Expired - Fee Related CN214887382U (en) | 2021-02-05 | 2021-02-05 | Gas turbine unit cabin with monitoring function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214887382U (en) |
-
2021
- 2021-02-05 CN CN202120331243.9U patent/CN214887382U/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: 20211126 |