CN107269394A - A kind of filter for gas turbine inlet - Google Patents

A kind of filter for gas turbine inlet Download PDF

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Publication number
CN107269394A
CN107269394A CN201710467587.0A CN201710467587A CN107269394A CN 107269394 A CN107269394 A CN 107269394A CN 201710467587 A CN201710467587 A CN 201710467587A CN 107269394 A CN107269394 A CN 107269394A
Authority
CN
China
Prior art keywords
filter
gas turbine
air
air inlet
turbine inlet
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.)
Granted
Application number
CN201710467587.0A
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Chinese (zh)
Other versions
CN107269394B (en
Inventor
何利锋
欧阳明辉
陆元彬
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JIANGSU RENHE ENVIRONMENTAL EQUIPMENTS CO Ltd
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JIANGSU RENHE ENVIRONMENTAL EQUIPMENTS CO Ltd
Priority date (The priority date 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 date listed.)
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Priority to CN201710467587.0A priority Critical patent/CN107269394B/en
Publication of CN107269394A publication Critical patent/CN107269394A/en
Application granted granted Critical
Publication of CN107269394B publication Critical patent/CN107269394B/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/055Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with intake grids, screens or guards
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D46/00Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
    • B01D46/02Particle separators, e.g. dust precipitators, having hollow filters made of flexible material
    • B01D46/023Pockets filters, i.e. multiple bag filters mounted on a common frame
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D46/00Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
    • B01D46/10Particle separators, e.g. dust precipitators, using filter plates, sheets or pads having plane surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D46/00Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
    • B01D46/24Particle separators, e.g. dust precipitators, using rigid hollow filter bodies
    • B01D46/2403Particle separators, e.g. dust precipitators, using rigid hollow filter bodies characterised by the physical shape or structure of the filtering element
    • B01D46/2411Filter cartridges
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D46/00Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
    • B01D46/56Filters or filtering processes specially modified for separating dispersed particles from gases or vapours with multiple filtering elements, characterised by their mutual disposition
    • B01D46/62Filters or filtering processes specially modified for separating dispersed particles from gases or vapours with multiple filtering elements, characterised by their mutual disposition connected in series
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing

Abstract

The present invention relates to filter technology field, more particularly to a kind of filter for gas turbine inlet, it includes the anti-catkin net in air inlet front end, rain cover, the anti-icing equipment being connected with combustion engine system heat sources, filter module, the filter outlet pipeline for connecting combustion engine compressor air inlet machine mouthful set gradually according to outlet side of the air filtration direction from filter air inlet side to filter.Instant invention overcomes the surface of filter medium of filter can be caused to block and the drawbacks of freeze when being used under the conventional filter in the winter time adverse circumstances such as low temperature and high humidity, the reliability and service life of filter are improved.

Description

A kind of filter for gas turbine inlet
Technical field
The present invention relates to filter technology field, more particularly to a kind of filter for gas turbine inlet.
Background technology
With the reinforcement of China environmental protection consciousness, the adjustment of domestic electrical energy resource structure, the particularly domestic north Electric power and the adjustment of heat supply in winter mode, no longer directly use coal unit, but use IGCC gas turbine coal gasifications substantially Generate electricity and generated electricity with Natural Gas turbine and thermal power plant unit, using centralized power generation heat supply, hot pipe network conveying thermal source.Therefore, combustion gas Turbine need to extract the air in thermo-power plant environment;In order to control the air quality into gas turbine, to ensure unit Normal work is, it is necessary to supporting combustion engine air intake filter.
Unit typically uses import brand combustion engine, and supporting combustion engine inlet air filtration is according to external design, in north of china in winter Under low temperature and high humidity and haze, ice and snow, rime, the ambient condition for the catkin that floats, because temperature drastically changes, air humidity tends to Saturation, when the filter cylinder is crossed air filtering, through filter material throttle effect, damp atmosphere is blocked in the space of filter cartridge with dust In, negative-pressure ward when compressor works accelerates flow velocity during through small holes, spreads reduction of speed when flowing through filter material again, slowly block filter material The solidification shape crystal ice granule thing of highly humid air formation half cut, makes filter material by Partial Blocking, charge flow rate is reduced, on filter differential pressure Rise, while ambient temperature and humidity changes again, filter operation is in negative-feedback state.Filter differential pressure is raised extremely, combustion gas compressor The air of suction is reduced, and influence combustion engine burning, load declines, and power output declines, and causes combustion engine load down to run or air inlet Filter High Pressure Difference chaser.
Therefore, using the supporting filter of the combustion engine gas handling system of prior art, in north of China winter low temperature high humility Etc. the surface of filter medium of filter can be caused to block when using under adverse circumstances and freezing, filter differential pressure rises extremely, fault rate Height so that filter can not long-term operation well, had a strong impact on the normal operation of whole unit.
The content of the invention
In order to overcome drawbacks described above present in existing combustion engine air intake filter technology, make in the adaptation of combustion engine air intake filter Combustion engine factory of state local environment requirement, the present invention proposes a kind of filter for gas turbine inlet, and its technical scheme is as follows:
A kind of filter for gas turbine inlet, including according to air filtration direction from filter air inlet side to filtering The anti-catkin net in air inlet front end that the outlet side of device is set gradually, rain cover, the anti-icing equipment being connected with combustion engine system heat sources, mistake Strainer modules, the filter outlet pipeline for connecting combustion engine compressor air inlet machine mouthful.
In such scheme, anti-catkin net is increased to air intake filter, when catkin waves, catkin is intercepted at filter most The stainless steel wire of outer layer is online;When catkin intercepts many, by clearing up net, it is ensured that anti-catkin net is reusable.Catkin Rain cover is installed behind net additional, to stop the entrance of rainwater.
In addition in such scheme, also directed to filter element in filter module when environment temperature is low, air humidity is high Easily there is freezing phenomena, anti-icing equipment is devised on the filter, i.e., introduce thermal source on air intake filter air intake end face, adjust The intake air temperature of high-pass filter, makes the air of convergence moisture-saturated, and original text, relative humidity reduction so that filtering are risen with intake air temperature The air of device air inlet is in unsaturated vapor phase by filter element, and filter differential pressure does not rise.
The above-mentioned anti-icing equipment being connected with combustion engine system heat sources can be the inlet air heating system (IBH) for connecting gas turbine High Temperature Gas jet pipe, it would however also be possible to employ pipe heat exchanger.
It is blower outlet IBH pipelines leading to coarse filtration element filter bag when introducing thermal source using IBH High Temperature Gas jet pipe Before, (general 390 DEG C or so) Zuo You of high temperature airs of IBH, mixed, raised with the high humidity cold air sucked using jet pipe The temperature of filter air inlet;Filter sets high temperature air jet pipe when manufacturing and designing.
It is (general 65 DEG C or so) works of hot water using fuel engine power generation waste heat boiler when obtaining thermal source using pipe heat exchanger For thermal source, exchanged heat using pipe heat exchanger, improve the temperature of inlet air, abolish the saturation state of highly humid air, realize dehumidifying Deicing purpose;Pipe heat exchanger device is set when filter manufactures and designs.
Filter module in the present invention includes modular casing and the mistake filtering element in the modular casing Part.It is that can be combined into the filter of different filtration capacities using modular organization benefit so that design is more flexible, has simultaneously Beneficial to the shortening production cycle.
Wherein, filter element includes coarse filtration element and smart filter element, and the coarse filtration element is pre-filtering cloth bag mistake Filter, the smart filter element is filtering cartridge filter, and the pre-filtering cloth envelop collector is arranged on according to air filtration direction Before filtering cartridge filter.
Above scheme is to be directed to north of China dust storm, and the situation of the high dustiness of haze air adds the filtering of filter Series, i.e., be combined, coarse filtration uses filtering accuracy for G4-M5 cloth envelop collector using coarse filtration with essence filtering, essence filtering Using the filtering cartridge filter of F9 ratings above.Filter bag intercepts bulky grain degree dust, and filter cylinder intercepts small particle size dust, makes filter cylinder Filter dust containing capacity to reduce, while auxiliary in pulse of compressed air.Increase the filter cylinder life-span, due to cheap, the filter cylinder valency of coarse filtration bag Lattice are expensive, combustion engine is run the reduction of filter element consumptive material consumption.The whole service pressure difference reduction of filter, improves combustion engine unit Generating and heating load, also improve economic benefit.
The filter for gas turbine inlet of the present invention also includes bottom steel structure support, the filter module peace On the bottom steel structure support.Using bottom steel structure support filter can be caused to be arranged on certain height, just In obtaining relatively clean air-source, air inlet/outlet pipeline is easy to the air inlet position with compressor mutually to coordinate.
Specifically, the filter module includes the modular casing of multiple connections of overlapping up and down, its bottom one layer of mould Block formula casing is arranged on the bottom steel structure support.
As a further improvement on the present invention, the structure of rain cover, is anti-from air inlet front end according to air filtration direction Catkin net is to labyrinth passage is formed between anti-icing equipment, moisture and moisture can be stopped by being provided with the labyrinth passage What is entered removes wet plate.Due to being provided with dash in the labyrinth passage of rain cover except wet plate, rainwater did not entered with some moisture Inside filter, it is blocked.
Preferably, the anti-catkin net in air inlet front end is stainless steel steel wire.
The beneficial effects of the invention are as follows:
First, the air inlet band anti-catkin net of stainless steel can prevent northern catkin from waving under situation, and catkin suede is intercepted at anti- The surface of catkin net, filter interior is not entered and blocks filter.
Second, air inlet front end has inside rain cover, rain cover, and there is labyrinth-like to remove wet plate, be easy to rainy state to rain Water does not enter in the case of filter interior, high humility, and part steam is standby to be blocked in addition to wet plate, so as to reduce into filtering The humidity of device inner air.
3rd, the anti-icing equipment in filter effectively can prevent filter element from being blocked because of icing, so as to reduce Pressure difference when filter is run, improves combustion engine unit operation reliability.
4th, filter capability is improved using increase filter filtering series.Pre-filtering Bag filter in filter Device, is blocked except the dust coarse granule in air, the dust containing capacity of reduction filter refined filtration cylinder, the service life of extension refined filtration cylinder;Filtering Efficient filter cylinder in device, makes the air into combustion engine compressor reach regulation cleanliness factor, it is ensured that combustion engine compressor blade and cavity Not because of air purity problem ash.
5th, filter module is modular body structure, can be combined into the filter of different filtration capacities so that set Meter is more flexible, while being conducive to shortening the production cycle.
6th, bottom steel structure support is provided with filter, filter is arranged on certain height, is easy to obtain phase To clean air-source, air inlet/outlet pipeline is easy to the air inlet position with compressor mutually to coordinate.
Brief description of the drawings
Fig. 1 is a kind of structural representation of filter for gas turbine inlet of the present invention;
Fig. 2 be in Fig. 1 on air inlet rain cover labyrinth passage structure division partial enlarged drawing.
In figure:1st, the anti-catkin net in air inlet front end, 2, rain cover, 2-1, except wet plate, 3, anti-icing equipment, 4, coarse filtration element (pre-filtering cloth envelop collector), 5, smart filter element (filtering cartridge filter), 6, modular casing, 6-1, first layer modular case Body, 6-2, second layer modular casing, 6-3, third layer modular casing, 6-4, the 4th layer of modular casing, 6-5, layer 5 Modular casing, 7, filter outlet pipeline, 8, filter thermal source utilize import piping, 9, bottom steel structure support, 10, passage Door.
In figure:A, filter air inlet side, B, the outlet side of filter, C, the labyrinth passage (air stream of rain cover To).
Embodiment
With reference to the accompanying drawings and examples, the embodiment to the present invention is further described.Following examples are only For clearly illustrating technical scheme, and it can not be limited the scope of the invention with this.
Such as Fig. 1 to 2 is a kind of filter for gas turbine inlet, including is entered according to air filtration direction from filter Gas side is connected to the anti-catkin net 1 in the air inlet front end that the outlet side of filter is set gradually, rain cover 2, with combustion engine system heat sources Anti-icing equipment 3, filter module, the filter outlet pipeline 7 for connecting combustion engine compressor air inlet machine mouthful.
In the present embodiment, filter module includes modular casing 6 and the filtering in the modular casing 6 Element.
Wherein, filter element includes coarse filtration element 4 and smart filter element 5, and the coarse filtration element is pre-filtering cloth bag Filter, the smart filter element is efficient filtering cartridge filter, and the pre-filtering cloth envelop collector is according to air filtration direction It is arranged on before efficient filtering cartridge filter.
The filter for gas turbine inlet of the present embodiment also includes bottom steel structure support 9, the filter mould Block is arranged on the bottom steel structure support 9.
Specifically, the filter module includes the modular casing of multiple connections of overlapping up and down, and it is bottom one layer Modular casing is arranged on the bottom steel structure support.In the present embodiment, there is provided first layer modular casing 6-1, Two layers of modular casing 6-2, third layer modular casing 6-3, the 4th layer of modular casing 6-4, layer 5 modular casing 6- 5, its nethermost first layer modular casing 6-1 are arranged on the bottom steel structure support 9.
In order to strengthen rain-proof and damp proof effect, rain cover 2 according to air filtration direction from the anti-catkin net 1 in air inlet front end to Labyrinth passage C is formed between anti-icing equipment 3, being provided with the labyrinth passage can stop what moisture and moisture entered Except wet plate 2-1.In the present embodiment, multiple labyrinth passages, and the labyrinth type on rain cover are arranged with rain cover 2 from bottom to up Passage is by formed by a bending (first rise and decline again).Certain labyrinth passage can also be designed to other structures shape Shape, such as by multiple bending or turn back and form labyrinth passage.In addition, set in the present embodiment on labyrinth passage Except wet plate.Preferably, except wet plate can use the cellular board breathed freely or the PVC board with loose structure, when air-flow is by except wet plate, Moisture is isolated because air impact removes wet plate, is formed after water droplet by the outside that rain cover is fallen under deadweight, serves stop The effect that some moisture enters.
In the present embodiment, anti-icing equipment 3 is connection IBH High Temperature Gas jet pipe or pipe heat exchanger.In figure, external heat source leads to Filter thermal source is crossed to introduce using import piping 8.
In the present embodiment, the anti-catkin net 1 in air inlet front end is preferably stainless steel steel wire.
In the present embodiment, pre-filtering cloth envelop collector uses filtering accuracy for G4-M5 cloth envelop collector, the high-efficient filter Cylinder filter uses filtering accuracy for the filtering cartridge filter of F9 ratings above.
For convenience of installing and overhauling, access door 10 is additionally provided with the filter of the present embodiment.
Described above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art For member, without departing from the technical principles of the invention, some improvements and modifications can also be made, these improvements and modifications Also it should be regarded as protection scope of the present invention.

Claims (8)

1. a kind of filter for gas turbine inlet, including according to air filtration direction from filter air inlet side to filter Outlet side set gradually the anti-catkin net in air inlet front end, rain cover, the anti-icing equipment being connected with combustion engine system heat sources, filtering Device module, the filter outlet pipeline for connecting combustion engine compressor air inlet machine mouthful.
2. a kind of filter for gas turbine inlet according to claim 1, it is characterized in that:The filter module Filter element including modular casing and in the modular casing.
3. a kind of filter for gas turbine inlet according to claim 2, it is characterized in that:The filter element bag Coarse filtration element and smart filter element are included, the coarse filtration element is pre-filtering cloth envelop collector, and the smart filter element is filter Cylinder filter, and the pre-filtering cloth envelop collector is arranged on before filtering cartridge filter according to air filtration direction.
4. a kind of filter for gas turbine inlet according to claim 1,2 or 3, it is characterized in that:Also include bottom Portion's steel structure support, the filter module is arranged on the bottom steel structure support.
5. a kind of filter for gas turbine inlet according to claim 4, it is characterized in that:The filter module Include the modular casing of multiple connections of overlapping up and down, its bottom one layer of modular casing is arranged on the bottom steel construction branch On frame.
6. a kind of filter for gas turbine inlet according to claim 1, it is characterized in that:The rain cover according to Air filtration direction is from the anti-catkin net in air inlet front end to labyrinth passage is formed anti-icing equipment, in the labyrinth passage Inside being provided with can stop that what moisture and moisture entered removes wet plate.
7. a kind of filter for gas turbine inlet according to claim 1, it is characterized in that:The anti-icing equipment is Connect the High Temperature Gas jet pipe or pipe heat exchanger of the inlet air heating system of gas turbine.
8. a kind of filter for gas turbine inlet according to claim 1, it is characterized in that:The air inlet front end Anti- catkin net is stainless steel steel wire.
CN201710467587.0A 2017-06-20 2017-06-20 Filter for gas turbine inlet Active CN107269394B (en)

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Application Number Priority Date Filing Date Title
CN201710467587.0A CN107269394B (en) 2017-06-20 2017-06-20 Filter for gas turbine inlet

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CN107269394B CN107269394B (en) 2024-01-19

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107842424A (en) * 2017-11-28 2018-03-27 华电电力科学研究院 The anti-willow catkins flying in the air device of gas turbine inlet air system
CN108223134A (en) * 2017-12-29 2018-06-29 中国舰船研究设计中心 Gas turbine inlet air grid and naval vessel
CN110671207A (en) * 2019-09-27 2020-01-10 江苏欧瑞特新材料有限公司 Box fine filter of gas turbine air intake system
CN111042926A (en) * 2020-01-02 2020-04-21 江苏科技大学 Gas turbine air intake system
CN111412067A (en) * 2020-04-09 2020-07-14 江苏华强新能源科技有限公司 Back-flushing type high-efficiency filter for gas turbine air inlet system
CN112302799A (en) * 2020-11-12 2021-02-02 无锡华南钢结构环保有限公司 Deicing and temperature regulating mechanism of air inlet system for gas turbine

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11311131A (en) * 1998-04-28 1999-11-09 Toshiba Corp Gas turbine inlet system installation
US20080298957A1 (en) * 2006-06-21 2008-12-04 General Electric Company Inlet air conditioning system
CN202417715U (en) * 2011-11-11 2012-09-05 中国海洋石油总公司 Air inlet purifying system for offshore turbine
CN104061075A (en) * 2014-05-09 2014-09-24 江苏东泽环保科技有限公司 Inlet air filter device of gas turbine
CN204212859U (en) * 2014-11-13 2015-03-18 九江七所精密机电科技有限公司 A kind of gas turbine pulse self-cleaning type air intake filter
CN204543835U (en) * 2015-04-20 2015-08-12 北京京能未来燃气热电有限公司 The smart filter cylinder dust exhaust apparatus of combustion engine inlet air filter system
CN104895677A (en) * 2015-06-01 2015-09-09 江苏华强新能源科技有限公司 Air intake system and method for gas turbine
CN205216420U (en) * 2015-11-09 2016-05-11 九江七所精密机电科技有限公司 Absorbent composite module formula air filtration system of secondary is prevented to online deashing
CN207064075U (en) * 2017-06-20 2018-03-02 江苏人和环保设备有限公司 A kind of filter for gas turbine inlet

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11311131A (en) * 1998-04-28 1999-11-09 Toshiba Corp Gas turbine inlet system installation
US20080298957A1 (en) * 2006-06-21 2008-12-04 General Electric Company Inlet air conditioning system
CN202417715U (en) * 2011-11-11 2012-09-05 中国海洋石油总公司 Air inlet purifying system for offshore turbine
CN104061075A (en) * 2014-05-09 2014-09-24 江苏东泽环保科技有限公司 Inlet air filter device of gas turbine
CN204212859U (en) * 2014-11-13 2015-03-18 九江七所精密机电科技有限公司 A kind of gas turbine pulse self-cleaning type air intake filter
CN204543835U (en) * 2015-04-20 2015-08-12 北京京能未来燃气热电有限公司 The smart filter cylinder dust exhaust apparatus of combustion engine inlet air filter system
CN104895677A (en) * 2015-06-01 2015-09-09 江苏华强新能源科技有限公司 Air intake system and method for gas turbine
CN205216420U (en) * 2015-11-09 2016-05-11 九江七所精密机电科技有限公司 Absorbent composite module formula air filtration system of secondary is prevented to online deashing
CN207064075U (en) * 2017-06-20 2018-03-02 江苏人和环保设备有限公司 A kind of filter for gas turbine inlet

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107842424A (en) * 2017-11-28 2018-03-27 华电电力科学研究院 The anti-willow catkins flying in the air device of gas turbine inlet air system
CN108223134A (en) * 2017-12-29 2018-06-29 中国舰船研究设计中心 Gas turbine inlet air grid and naval vessel
CN110671207A (en) * 2019-09-27 2020-01-10 江苏欧瑞特新材料有限公司 Box fine filter of gas turbine air intake system
CN111042926A (en) * 2020-01-02 2020-04-21 江苏科技大学 Gas turbine air intake system
CN111042926B (en) * 2020-01-02 2023-06-20 江苏科技大学 Gas turbine air inlet system
CN111412067A (en) * 2020-04-09 2020-07-14 江苏华强新能源科技有限公司 Back-flushing type high-efficiency filter for gas turbine air inlet system
CN111412067B (en) * 2020-04-09 2022-05-24 江苏华强新能源科技有限公司 Back-flushing type high-efficiency filter for gas turbine air inlet system
CN112302799A (en) * 2020-11-12 2021-02-02 无锡华南钢结构环保有限公司 Deicing and temperature regulating mechanism of air inlet system for gas turbine

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