CN206801710U - A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas - Google Patents

A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas Download PDF

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Publication number
CN206801710U
CN206801710U CN201720657801.4U CN201720657801U CN206801710U CN 206801710 U CN206801710 U CN 206801710U CN 201720657801 U CN201720657801 U CN 201720657801U CN 206801710 U CN206801710 U CN 206801710U
Authority
CN
China
Prior art keywords
natural gas
air
refrigerating module
inlet
pipe
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
Application number
CN201720657801.4U
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Chinese (zh)
Inventor
宋勇
朱涛
徐钟宇
吴剑
王松浩
许昊煜
邵飞
胡中强
任磊
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.)
China Datang Corp Science and Technology Research Institute Co Ltd East China Branch
Original Assignee
China Datang Corp Science and Technology Research Institute Co Ltd East China Branch
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.)
Filing date
Publication date
Application filed by China Datang Corp Science and Technology Research Institute Co Ltd East China Branch filed Critical China Datang Corp Science and Technology Research Institute Co Ltd East China Branch
Priority to CN201720657801.4U priority Critical patent/CN206801710U/en
Application granted granted Critical
Publication of CN206801710U publication Critical patent/CN206801710U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a kind of cooling system that gas turbine inlet air cooling is carried out using natural gas, including inlet plenum;Described inlet plenum one end and atmosphere, the other end and combustion chamber;The inlet plenum is disposed with shutter, filter, refrigerating module, muffler from one end to the other end with atmosphere;The inlet plenum is additionally provided with natural gas air inlet pipe and natural gas escape pipe;The natural gas air inlet pipe connects with refrigerating module;Natural gas is stood out by natural gas air inlet pipe from pressure regulation, and into after refrigerating module, voltage regulating station is returned from natural gas escape pipe.Compared with prior art, the utility model refrigerating module low-temperature receiver is directly taken to voltage regulating station natural gas, simple in construction without extra low-temperature receiver, is easy to safeguard.Natural gas temperature rise by heat exchange reduces the heat exchange amount of Dual-tube heat exchanger, improves the thermal efficiency;Air themperature reduces, and improves the air mass of air.

Description

A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas
Technical field
The technical field of gas turbine is the utility model is related to, it is specifically a kind of to carry out gas turbine using natural gas The cooling system of inlet gas cooling.
Background technology
Because summer temperature is high, when air themperature is high, combustion engine plenum chamber suction air quality is reduced, and combustion engine, which is contributed, to drop It is low.Combustion engine output is improved, on the one hand improves combustion engine technology, researches and develops new material, improves combustion engine charge combustion temperature;The opposing party Face can increase air-mass flow, increase turbine output work.
Utility model content
The purpose of this utility model is the combustion engine plenum chamber suction air in order to solve in the prior art when air themperature is high Mass lost, combustion engine are contributed the defects of reduction, there is provided a kind of cooling system that gas turbine inlet air cooling is carried out using natural gas To solve the above problems.
To achieve these goals, the technical solution of the utility model is as follows:
A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas, including inlet plenum;The inlet plenum one End and atmosphere, the other end and combustion chamber;The inlet plenum is set gradually from one end to the other end with atmosphere There are shutter, filter, refrigerating module, muffler;The inlet plenum is additionally provided with natural gas air inlet pipe and natural gas escape pipe; The natural gas air inlet pipe connects with refrigerating module;Natural gas is stood out into natural gas air inlet pipe from pressure regulation, through supercooling mould After block, voltage regulating station is returned from natural gas escape pipe.
Preferably, it is provided with flow control valve in the natural gas air inlet pipe.
Preferably, it is provided with outlet valve on the natural gas escape pipe.
Preferably,:The refrigerating module is coil pipe.
Preferably, there is fin on the coil pipe.
The utility model compared with prior art, has the advantages that:
(1) the utility model refrigerating module low-temperature receiver is directly taken to voltage regulating station natural gas, simple in construction without extra low-temperature receiver, It is easy to safeguard.
(2) the natural gas temperature rise Jing Guo heat exchange reduces the heat exchange amount of Dual-tube heat exchanger, improves the thermal efficiency;It is empty Temperature degree reduces, and improves the air mass of air, improves combustion engine and contributes.
Brief description of the drawings
Fig. 1 is overall structure diagram of the present utility model.
Embodiment
The effect of to make to architectural feature of the present utility model and being reached, has a better understanding and awareness, to compared with Good embodiment and accompanying drawing coordinate detailed description, are described as follows:
As shown in figure 1, a kind of cooling system that gas turbine inlet air cooling is carried out using natural gas, including inlet plenum 1;Institute State the one end of inlet plenum 1 and atmosphere, the other end and combustion chamber;Inlet plenum 1 is from one end with atmosphere to the other end It is disposed with shutter 11, filter 12, refrigerating module 13, muffler 14;Inlet plenum 1 is additionally provided with natural gas air inlet pipe 15 With natural gas escape pipe 16;Natural gas air inlet pipe 15 connects with refrigerating module 13;Natural gas is stood out into natural gas from pressure regulation Air inlet pipe 15, after refrigerating module 13, voltage regulating station is returned to from natural gas escape pipe 16.
Flow control valve 151 is provided with natural gas air inlet pipe 15.Outlet valve is provided with natural gas escape pipe 16 161.Refrigerating module 13 is coil pipe.There is fin on coil pipe.
The operation principle of the present embodiment begins, and voltage regulating station inlet natural gas temperature stabilization is maintained at less than 20 DEG C, and summer Temperature then reaches more than 30 DEG C, increases by a branch road after voltage regulating station fire shut-off valve, draws the relatively low natural gas of temperature and enters combustion After machine inlet gas cooling module 13 discharges cold energy, before returning to voltage regulating station Dual-tube heat exchanger by natural gas escape pipe 16.Air is from entering The import of air chamber 1 is successively by filter 12, refrigerating module 13.Air is carrying out heat exchange by refrigerating module 13 and natural gas Enter combustion chamber from the port of export of inlet plenum 1 afterwards.After natural gas carries out heat exchange with air, natural gas temperature rise reduces double The heat exchange amount of heat exchange of heat pipe, improves the thermal efficiency;Air themperature reduces, and improves the air mass of air.Refrigerating module 13 enters Air pipe is buried, and whole process is using the possibility that natural gas leakage is reduced with welding.
The advantages of general principle of the present utility model, principal character and the utility model has been shown and described above.One's own profession The technical staff of industry is it should be appreciated that the utility model is not restricted to the described embodiments, described in above-described embodiment and specification Simply principle of the present utility model, the utility model also has respectively on the premise of the spirit and scope of the utility model is not departed from Kind changes and improvements, these changes and improvements are both fallen within claimed the scope of the utility model.The requires of the utility model Protection domain defined by appended claims and its equivalent.

Claims (5)

  1. A kind of 1. cooling system that gas turbine inlet air cooling is carried out using natural gas, it is characterised in that:Including inlet plenum (1); Described inlet plenum (1) one end and atmosphere, the other end and combustion chamber;The inlet plenum (1) from atmosphere one End to the other end is disposed with shutter (11), filter (12), refrigerating module (13), muffler (14);The inlet plenum (1) natural gas air inlet pipe (15) and natural gas escape pipe (16) are additionally provided with;The natural gas air inlet pipe (15) and refrigerating module (13) connect;Natural gas is stood out by natural gas air inlet pipe (15) from pressure regulation, into after refrigerating module (13), is gone out from natural gas Tracheae (16) returns to voltage regulating station.
  2. 2. a kind of cooling system that gas turbine inlet air cooling is carried out using natural gas according to claim 1, its feature It is:Flow control valve (151) is provided with the natural gas air inlet pipe (15).
  3. 3. a kind of cooling system that gas turbine inlet air cooling is carried out using natural gas according to claim 1, its feature It is:Outlet valve (161) is provided with the natural gas escape pipe (16).
  4. 4. a kind of cooling system that gas turbine inlet air cooling is carried out using natural gas according to claim 1, its feature It is:The refrigerating module (13) is coil pipe.
  5. 5. a kind of cooling system that gas turbine inlet air cooling is carried out using natural gas according to claim 4, its feature It is:There is fin on the coil pipe.
CN201720657801.4U 2017-06-07 2017-06-07 A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas Expired - Fee Related CN206801710U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720657801.4U CN206801710U (en) 2017-06-07 2017-06-07 A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720657801.4U CN206801710U (en) 2017-06-07 2017-06-07 A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas

Publications (1)

Publication Number Publication Date
CN206801710U true CN206801710U (en) 2017-12-26

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720657801.4U Expired - Fee Related CN206801710U (en) 2017-06-07 2017-06-07 A kind of cooling system that gas turbine inlet air cooling is carried out using natural gas

Country Status (1)

Country Link
CN (1) CN206801710U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110439689A (en) * 2019-08-06 2019-11-12 四川村田机械制造股份有限公司 A kind of air inlet device for gas turbine
CN110469406A (en) * 2019-08-06 2019-11-19 四川村田机械制造股份有限公司 A kind of manufacturing method of air inlet device for gas turbine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110439689A (en) * 2019-08-06 2019-11-12 四川村田机械制造股份有限公司 A kind of air inlet device for gas turbine
CN110469406A (en) * 2019-08-06 2019-11-19 四川村田机械制造股份有限公司 A kind of manufacturing method of air inlet device for gas turbine
CN110439689B (en) * 2019-08-06 2021-03-30 四川村田机械制造股份有限公司 Gas turbine air inlet unit
CN110469406B (en) * 2019-08-06 2021-06-29 四川村田机械制造股份有限公司 Manufacturing method of gas inlet device of gas turbine

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20171226

Termination date: 20180607

CF01 Termination of patent right due to non-payment of annual fee