CN106014644A - Gas turbine intake heating control system - Google Patents

Gas turbine intake heating control system Download PDF

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Publication number
CN106014644A
CN106014644A CN201610540894.2A CN201610540894A CN106014644A CN 106014644 A CN106014644 A CN 106014644A CN 201610540894 A CN201610540894 A CN 201610540894A CN 106014644 A CN106014644 A CN 106014644A
Authority
CN
China
Prior art keywords
hot water
heat exchanger
control system
heating control
air heat
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.)
Pending
Application number
CN201610540894.2A
Other languages
Chinese (zh)
Inventor
王小鹏
李剑斌
邵帅
仲恒
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.)
Nanjing Leaguer-United Top Holdings Power Energy-Saving Co Ltd
Original Assignee
Nanjing Leaguer-United Top Holdings Power Energy-Saving 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.)
Filing date
Publication date
Application filed by Nanjing Leaguer-United Top Holdings Power Energy-Saving Co Ltd filed Critical Nanjing Leaguer-United Top Holdings Power Energy-Saving Co Ltd
Priority to CN201610540894.2A priority Critical patent/CN106014644A/en
Publication of CN106014644A publication Critical patent/CN106014644A/en
Pending legal-status Critical Current

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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
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Pump Type And Storage Water Heaters (AREA)

Abstract

The invention discloses a gas turbine intake heating control system which comprises a heat exchanger, a hot water circulation pump, a water feed tank and an air heat exchanger. The heat exchanger, the hot water circulation pump, the water feed tank and the air heat exchanger are sequentially connected through hot water supply pipes. An electric adjusting valve is further installed between the water feed tank and the air heat exchanger. The air heat exchanger is further connected with the heat exchanger through a hot water return pipe. The gas turbine intake heating control system further comprises a control cabinet. The control cabinet is connected with the hot water supply pipes, the hot water return pipe and the air heat exchanger. The water flow in the hot water supply pipes and the hot water return pipe is controlled. The gas turbine intake heating control system is high in safety; once a problem or a breakdown happens to a certain position, alarming is started through the corresponding alarming function, the system is cut off at the same time, and the safety of the whole is ensured; the automation degree is high, and automatic control is achieved through the control cabinet; and the hot water flow of a pipeline is adjusted by monitoring the temperature of an air outlet of the surface type air heat exchanger, and therefore it is ensured that a unit runs in an interval with the optimal performance.

Description

A kind of combustion engine inlet air heating control system
Technical field
The present invention relates to a kind of combustion engine inlet air heating control system.
Background technology
When gas turbine unit is in part load condition, because intake air temperature is low, need to consume substantial amounts of heat when burning, Cause fuel engine power generation efficiency and reduction of exerting oneself.For improving the generating efficiency of combustion engine and exerting oneself, install inlet air heating control additional to unit System, to heat compressor air inlet machine, improves exerting oneself and efficiency of combustion engine.
Summary of the invention
It is an object of the invention to be to overcome above-mentioned the deficiencies in the prior art, solve the technological deficiency that presently, there are, this Bright provide a kind of combustion engine inlet air heating control system, it is achieved automatically control the heating of combustion engine air inlet, it is ensured that unit is in optimality Can section operation.
The technical solution adopted in the present invention is:
A kind of combustion engine inlet air heating control system, including heat exchanger, hot water circulating pump, feed-tank and air heat exchanger, described Heat exchanger, hot water circulating pump, feed-tank and air heat exchanger are linked in sequence by hot water feeding pipe, described feed-tank and air It is also equipped with electric control valve between heat exchanger, is connected also by hot water return pipe between described air heat exchanger and heat exchanger; Also include that switch board, described switch board are all connected with hot water feeding pipe, hot water return pipe and air heat exchanger, control hot water Discharge in feed pipe, hot water return pipe.
Further, described hot water feeding pipe is also associated with filling pipe, and described filling pipe is provided with constant pressure arrangement.
Further, described filling pipe is expansion tube.
Further, described hot water feeding pipe and hot water return pipe are mounted on flange butterfly, flange check valve and self-operated type Temperature control valve (TCV).
The invention has the beneficial effects as follows: a kind of combustion engine inlet air heating control system disclosed by the invention,
1. safety is high: once having somewhere to go wrong or fault, such as superpressure, overtemperature, discharge is low, temperature is the most high, right The warning function answered just starts warning, simultaneously cutting system, thus can guarantee that the safety of entirety.
2. automaticity is high, realizes automatically controlling by switch board, reduces labor intensity.
3. regulate pipeline hot water flow by the air exit temp of monitoring surface-type air heat exchanger, to ensure that unit is Best performance section operation.
Below in conjunction with the accompanying drawings the present invention is described in further detail.
Accompanying drawing explanation
Fig. 1 is the schematic flow sheet of combustion engine inlet air heating control system of the present invention.
In figure, 1, heat exchanger 2, hot water circulating pump 3, feed-tank 4, air heat exchanger 5, hot water feeding pipe 6, Hot water return pipe 7, switch board 8, filling pipe 9, constant pressure arrangement 10, electric control valve.
Detailed description of the invention
In order to deepen the understanding of the present invention, the present invention is further detailed explanation with embodiment below in conjunction with the accompanying drawings.With Lower embodiment is only used for clearly illustrating technical scheme, and can not limit the scope of the invention with this.
As it is shown in figure 1, combustion engine inlet air heating control system of the present invention, change including heat exchanger, hot water circulating pump, feed-tank and air Hot device, heat exchanger, hot water circulating pump, feed-tank and air heat exchanger be linked in sequence by hot water feeding pipe, feed-tank and air It is also equipped with electric control valve between heat exchanger, is connected also by hot water return pipe between air heat exchanger and heat exchanger;Also wrap Including switch board, switch board is all connected with hot water feeding pipe, hot water return pipe and air heat exchanger, controls hot water feeding pipe, heat Discharge in water return pipe.
Further, hot water feeding pipe is also associated with filling pipe, and described filling pipe is provided with constant pressure arrangement, the pressure of control piper Power, it is ensured that the safety of pipeline.
Further, filling pipe is expansion tube.
Further, hot water feeding pipe and hot water return pipe are mounted on flange butterfly, flange check valve and self-operated type temperature tune Joint valve, is monitored controlling to the pressure on system pipeline, flow, temperature, occurs abnormal, can open and close pipeline.
Combustion engine inlet air heating control system workflow:
When Gas Generator Set is in part load condition, for improving exerting oneself and efficiency of unit, startup inlet air heating control system: Hot water generator is arranged on waste heat boiler afterbody, utilizes the waste heat of flue gas to carry out the recirculated water in heating generator, and the hot water of generation leads to Superheated water circulating pump is re-fed into the surface-type air heat exchanger being positioned at combustion engine air inlet, will enter the air heating of combustion engine, thus Improve the efficiency of whole Gas Generator Set.
Feed-tank in Fig. 1 is used for regulating the discharge of hot-water heating system.
The advantage of combustion engine inlet air heating control system of the present invention:
1. safety is high: once having somewhere to go wrong or fault, such as superpressure, overtemperature, discharge is low, temperature is the most high, right The warning function answered just starts warning, simultaneously cutting system, thus can guarantee that the safety of entirety.
2. automaticity is high, realizes automatically controlling by switch board, reduces labor intensity.
3. regulate pipeline hot water flow by the air exit temp of monitoring surface-type air heat exchanger, to ensure that unit is Best performance section operation.
Being noted that embodiment described above is illustrative not limiting to technical solution of the present invention, art is common The equivalent of technical staff or other amendments made according to prior art, as long as not exceeding the thinking of technical solution of the present invention And scope, within should be included in interest field of the presently claimed invention.

Claims (4)

1. a combustion engine inlet air heating control system, it is characterised in that: include heat exchanger, hot water circulating pump, feed-tank and sky Gas heat exchanger, described heat exchanger, hot water circulating pump, feed-tank and air heat exchanger be linked in sequence by hot water feeding pipe, institute State and between feed-tank and air heat exchanger, be also equipped with electric control valve, also by heat between described air heat exchanger and heat exchanger Water return pipe is connected;Also including switch board, described switch board is equal with hot water feeding pipe, hot water return pipe and air heat exchanger It is connected, controls the discharge in hot water feeding pipe, hot water return pipe.
A kind of combustion engine inlet air heating control system the most according to claim 1, it is characterised in that: described hot water feeding pipe It is also associated with filling pipe, described filling pipe is provided with constant pressure arrangement.
A kind of combustion engine inlet air heating control system the most according to claim 1, it is characterised in that: described filling pipe is swollen Tube expansion.
A kind of combustion engine inlet air heating control system the most according to claim 1, it is characterised in that: described hot water feeding pipe Be mounted on flange butterfly, flange check valve and self force type temperature regulating valve on hot water return pipe.
CN201610540894.2A 2016-07-11 2016-07-11 Gas turbine intake heating control system Pending CN106014644A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610540894.2A CN106014644A (en) 2016-07-11 2016-07-11 Gas turbine intake heating control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610540894.2A CN106014644A (en) 2016-07-11 2016-07-11 Gas turbine intake heating control system

Publications (1)

Publication Number Publication Date
CN106014644A true CN106014644A (en) 2016-10-12

Family

ID=57109200

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610540894.2A Pending CN106014644A (en) 2016-07-11 2016-07-11 Gas turbine intake heating control system

Country Status (1)

Country Link
CN (1) CN106014644A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003161164A (en) * 2001-11-26 2003-06-06 Hitachi Ltd Combined-cycle power generation plant
CN1456795A (en) * 1995-12-28 2003-11-19 株式会社日立制作所 Gas turbine, integrated circulating device and droplet injector of gas turbine
US20100089023A1 (en) * 2008-10-09 2010-04-15 Mitsubishi Heavy Industries, Ltd. Intake air heating system of combined cycle plant
EP2778368A1 (en) * 2013-03-12 2014-09-17 Ansaldo Energia S.p.A. Combined-cycle power plant with control of the inlet air temperature and method for controlling a combined-cycle power plant
CN105484815A (en) * 2015-12-31 2016-04-13 中国能源建设集团广东省电力设计研究院有限公司 Fuel gas and steam combination system and running control method thereof
CN205977420U (en) * 2016-07-11 2017-02-22 南京力合联升电力节能科技有限公司 Combustion engine heating control system that admits air

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1456795A (en) * 1995-12-28 2003-11-19 株式会社日立制作所 Gas turbine, integrated circulating device and droplet injector of gas turbine
JP2003161164A (en) * 2001-11-26 2003-06-06 Hitachi Ltd Combined-cycle power generation plant
US20100089023A1 (en) * 2008-10-09 2010-04-15 Mitsubishi Heavy Industries, Ltd. Intake air heating system of combined cycle plant
EP2778368A1 (en) * 2013-03-12 2014-09-17 Ansaldo Energia S.p.A. Combined-cycle power plant with control of the inlet air temperature and method for controlling a combined-cycle power plant
CN105484815A (en) * 2015-12-31 2016-04-13 中国能源建设集团广东省电力设计研究院有限公司 Fuel gas and steam combination system and running control method thereof
CN205977420U (en) * 2016-07-11 2017-02-22 南京力合联升电力节能科技有限公司 Combustion engine heating control system that admits air

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Application publication date: 20161012

RJ01 Rejection of invention patent application after publication