CN106482135B - The ground flare of combustion air is provided by gas source energy - Google Patents
The ground flare of combustion air is provided by gas source energy Download PDFInfo
- Publication number
- CN106482135B CN106482135B CN201611142250.4A CN201611142250A CN106482135B CN 106482135 B CN106482135 B CN 106482135B CN 201611142250 A CN201611142250 A CN 201611142250A CN 106482135 B CN106482135 B CN 106482135B
- Authority
- CN
- China
- Prior art keywords
- turbine
- compressor
- gas
- air
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G7/00—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
- F23G7/06—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2209/00—Specific waste
- F23G2209/14—Gaseous waste or fumes
Abstract
It is a kind of to provide the ground flare of combustion air by gas source energy, including burner and turbo compressor, the burner includes air intake and fuel gas inlet, the air intake participates in the compressed air of burning to receive, the turbo compressor includes shaft and the turbine and compressor that are fixed in the shaft, the turbine has turbine inlet portion and turbine outlet portion, the turbine inlet portion to receive high-pressure gas make the high-pressure gas in the turbine expansion work to drive the turbine to rotate, the turbine outlet portion is connected to the fuel gas inlet, the compressor includes compressor inlet portion and blower outlet portion, the compressor inlet portion is to receive surrounding air, the blower outlet portion is connected to the air intake.
Description
Technical field
It is the present invention relates to a kind of ground flare, in particular to a kind of to provide the ground fire of combustion air by gas source energy
Torch.
Background technique
There are two types of air needed for existing ground flare burning, and one is gas source injection air is utilized, another kind is benefit
With dynamic power machine air blast.The former needs that the nozzle of torch and ejecting port are exposed in atmospheric environment and cannot be closed, and noise is big,
Gas source and flow amount is small when torch starting and closing, injection lack of air, insufficient, variable parameter operation bad adaptability of burning.Using dynamic
Power machinery air blast can avoid these problems.However, the supply arrangement of traditional ground flare combustion air mostly uses greatly prime mover,
And well site needs the prime mover being equipped with for torch to provide electric power, or cleaning generally in remote districts using traditional ground flare
Fossil fuel.Well site goods and materials in remote districts transport inconvenient, power tense, the necessary resources that when traditional torch use consumes
(motor, internal combustion engine, cable, the energy, transport installation etc.) is more, this undoubtedly needs to increase many cost inputs.
High-pressure air source to be treated has very high pressure energy in oil well or gas well, directlys adopt high pressure relief equipment not only
Cost is increased, and causes the wasting of resources of high-pressure air source pressure energy.Therefore, high pressure gas to be treated how is efficiently used
The pressure energy in source is those skilled in the art's urgent problem to be solved.
Summary of the invention
In view of this, the present invention proposes a kind of ground flare by gas source energy offer combustion air.
It is a kind of to provide the ground flare of combustion air, including burner and turbo compressor by gas source energy, it is described
Burner includes air intake and fuel gas inlet, and the air intake participates in the compressed air of burning to receive, described
Concora crush mechanism of qi includes shaft and the turbine and compressor that are fixed in the shaft, and the turbine is with turbine inlet portion and thoroughly
Clear oral area, the turbine inlet portion to receive high-pressure gas make the high-pressure gas in the turbine expansion work from
And the turbine is driven to rotate, the turbine outlet portion is connected to the fuel gas inlet, and the compressor includes compressor inlet
Portion and blower outlet portion, the compressor inlet portion is to receive surrounding air, the blower outlet portion and the air
Entrance connection.
In one embodiment, the turbo compressor includes casing, and the turbo compressor is mounted on structure in the casing
At a modular unit.
In one embodiment, the turbine is axial flow type or radial type turbine turbine.
In one embodiment, the compressor is axial flow type or radial type compressor.
In one embodiment, the turbo compressor is arranged at the air source inlet of the torch.
In one embodiment, the high-pressure gas is well head high-pressure natural gas.
In conclusion the present invention provides the pressures that one kind can efficiently use high-pressure air source to be treated in oil well or gas well
The ground flare of energy.One turbo compressor is set at burner air source inlet, and high-pressure air source is by turbine turbine to turbine
Workmanship, the high-pressure air source of pressure reduction are passed through torch burning room.Turbine rotation drives coaxial compressor, and compression impellor is from atmosphere
Middle draw air is delivered to torch burning room through compression, so that gas source and air are sufficiently mixed burning in a combustion chamber.The present invention
As a source of power with gas source pressure energy, high-pressure air source is passed through turbine reduces the pressure of gas source, reduces high pressure relief equipment
Investment, save the cost, turbine driving compressor compressed air is delivered to burner, replaces prime mover, possessing traditionally
Under the premise of the torch advantage of face, the investment and material supply of power-equipment are reduced.
Detailed description of the invention
Fig. 1 is the operational flow diagram of ground flare of the present invention.
Specific embodiment
Before describing the embodiments in more detail, it should be understood that the present invention is not limited to institutes hereafter or in attached drawing in the application
The detailed construction or arrangement of elements of description.The embodiment that the present invention can realize for other way.Furthermore, it is to be understood that this paper institute
The wording and term used is solely for description purposes, should not be interpreted in a limited way."include", "comprise" used herein,
The similar wording such as " having " is meant comprising items listed thereafter, its equivalent and other additional things.In particular, when description
When " certain element ", it also may include multiple that the present invention, which does not limit the quantity of the element as one,.
As shown in Figure 1, the present invention proposes a kind of ground flare by gas source energy offer combustion air, the ground flare
Including burner 10 and turbo compressor 12, in the present embodiment, in order to facilitate the installation of, the setting of turbo compressor 12 is filled in burning
It sets at 10 air source inlet, in other embodiments, according to actual installation needs, turbo compressor 12, which also can be set, to burn
The other positions of device 10.Burner 10 includes air intake 14 and fuel gas inlet 16.
Turbo compressor 12 includes shaft 18 and the turbine 20 and compressor 22 that are fixedly mounted in shaft 18.Wherein,
Turbine 20 can be axial flow type or radial type, and compressor 22 can be axial flow type or radial type.In the present embodiment, turbine 20 and pressure
Mechanism of qi 22 is all made of axial flow type, and collectively constitutes axial-flow turbine compressor.
Turbine 20 includes turbine inlet portion 24 and turbine outlet portion 26, and turbine inlet portion 24 is to receive high-pressure gas, example
Tathagata is connected to from the high pressure natural gas in well site, turbine outlet portion 26 with the fuel gas inlet 16 of burner 10, high-pressure natural gas into
Enter turbine 20 and drive the rotation of turbine turbine, high-pressure natural gas pressure reduction, the natural gas being depressured through turbine 20 is through turbine outlet portion
26 and fuel gas inlet 16 enter burner 10 combustion chamber.
Compressor 22 includes compressor inlet portion 28 and blower outlet portion 30, blower outlet portion 30 and burner 10
Air intake 14 be connected to.The rotation of turbine turbine drives shaft 18, and shaft 18 drives the compression impellor rotation of compressor 22, calms the anger
Wheel rotation makes surrounding air be sucked into compressor 22 from compressor inlet portion 28, and air passes through pressure after the compression of compressor 22
Mechanism of qi outlet portion 30 and air intake 14, which enter in the combustion chamber of burner 10, is sufficiently mixed burning with natural gas.
In an illustrated embodiment, turbo compressor 12 further includes shell (not shown go out), turbine 20, compressor 22 and is turned
Axis 18, which is installed in the casing, constitutes a modular unit, installs, maintains easily convenient for the modularization of ground flare in this way.
As a source of power with the high-pressure natural gas in well site, effective use gas source pressure energy is burning dress to turbo compressor 12
10 offers decompression natural gas and sufficient compressed air are provided, torch burning is promoted, greatly reduce field well site dynamic power machine,
The investment of high pressure relief equipment and its necessary resources reduces cost, energy conservation and environmental protection.
In conclusion the present invention provides the pressures that one kind can efficiently use high-pressure air source to be treated in oil well or gas well
The ground flare of energy.One turbo compressor is set at torch air source inlet, high-pressure air source does manual work to turbine by turbine turbine,
The high-pressure air source of pressure reduction is passed through torch burning room.Turbine rotation drives coaxial compressor, and compression impellor is inhaled from atmosphere
Air is taken to be delivered to torch burning room through compression, so that gas source and air are sufficiently mixed burning in a combustion chamber.The present invention is with gas
As a source of power, high-pressure air source is passed through turbine reduces the pressure of gas source to source pressure energy, reduces the throwing of high pressure relief equipment
Enter, save the cost, turbine driving compressor compressed air is delivered to torch, replaces prime mover, traditional ground flare is excellent possessing
Under the premise of gesture, the investment and material supply of power-equipment are reduced.
Concepts described herein may be embodied to other forms without departing from its spirit and characteristics.It is disclosed
The specific embodiments are to be considered as illustrative and not restrictive.Therefore, the scope of the present invention be by the attached claims,
Instead of making decisions based on these previous descriptions.Any change within the literal meaning and equivalent scope of the claims is all
It should belong to these the scope of the claims.
Claims (6)
1. a kind of provide the ground flare of combustion air by gas source energy, which is characterized in that including burner and turbine pressure
Mechanism of qi, the burner include air intake and fuel gas inlet, and the air intake participates in the compression sky of burning to receive
Gas, the turbo compressor include shaft and the turbine and compressor that are fixed in the shaft, and the turbine has turbine
Inlet portion and turbine outlet portion, the turbine inlet portion make the high-pressure gas in the turbine to receive high-pressure gas
Expansion work is to drive the turbine to rotate, and the turbine outlet portion is connected to the fuel gas inlet, and the compressor includes
Compressor inlet portion and blower outlet portion, the compressor inlet portion is to receive surrounding air, the blower outlet portion
It is connected to the air intake.
2. providing the ground flare of combustion air by gas source energy as described in claim 1, which is characterized in that the turbine
Compressor includes casing, and the turbo compressor, which is mounted in the casing, constitutes a modular unit.
3. providing the ground flare of combustion air by gas source energy as described in claim 1, which is characterized in that the turbine
For axial flow type or radial type turbine turbine.
4. providing the ground flare of combustion air by gas source energy as described in claim 1, which is characterized in that described to calm the anger
Machine is axial flow type or radial type compressor.
5. providing the ground flare of combustion air by gas source energy as described in claim 1, which is characterized in that the turbine
Compressor is arranged at the air source inlet of the torch.
6. providing the ground flare of combustion air by gas source energy as described in claim 1, which is characterized in that the high pressure
Combustion gas is well head high-pressure natural gas.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611142250.4A CN106482135B (en) | 2016-12-12 | 2016-12-12 | The ground flare of combustion air is provided by gas source energy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611142250.4A CN106482135B (en) | 2016-12-12 | 2016-12-12 | The ground flare of combustion air is provided by gas source energy |
Publications (2)
Publication Number | Publication Date |
---|---|
CN106482135A CN106482135A (en) | 2017-03-08 |
CN106482135B true CN106482135B (en) | 2019-03-01 |
Family
ID=58284727
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201611142250.4A Active CN106482135B (en) | 2016-12-12 | 2016-12-12 | The ground flare of combustion air is provided by gas source energy |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106482135B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018107334A1 (en) * | 2016-12-12 | 2018-06-21 | 深圳智慧能源技术有限公司 | Ground torch for supplying combustion air by using air source energy |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101280723A (en) * | 2008-05-29 | 2008-10-08 | 华北电力大学 | Method and device for reutilization of natural gas pipe network pressure energy in gas turbine working domain |
CN102330573A (en) * | 2010-10-22 | 2012-01-25 | 靳北彪 | Pressure gas turbine booster system |
CN205261590U (en) * | 2016-01-06 | 2016-05-25 | 山东恒能环保能源设备有限公司 | Ground torch |
CN206247353U (en) * | 2016-12-12 | 2017-06-13 | 深圳智慧能源技术有限公司 | The ground flare of combustion air is provided by source of the gas energy |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2119891B1 (en) * | 2008-05-15 | 2023-09-13 | Mitsubishi Heavy Industries, Ltd. | Control of working fluid flow of a two-shaft gas turbine |
-
2016
- 2016-12-12 CN CN201611142250.4A patent/CN106482135B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101280723A (en) * | 2008-05-29 | 2008-10-08 | 华北电力大学 | Method and device for reutilization of natural gas pipe network pressure energy in gas turbine working domain |
CN102330573A (en) * | 2010-10-22 | 2012-01-25 | 靳北彪 | Pressure gas turbine booster system |
CN205261590U (en) * | 2016-01-06 | 2016-05-25 | 山东恒能环保能源设备有限公司 | Ground torch |
CN206247353U (en) * | 2016-12-12 | 2017-06-13 | 深圳智慧能源技术有限公司 | The ground flare of combustion air is provided by source of the gas energy |
Also Published As
Publication number | Publication date |
---|---|
CN106482135A (en) | 2017-03-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11008938B2 (en) | Gas turbine blower/pump | |
CN206247353U (en) | The ground flare of combustion air is provided by source of the gas energy | |
US9470150B2 (en) | Gas turbine power augmentation system | |
JP2013513072A (en) | Modification of a simple cycle gas turbine to utilize a compressed air energy storage room with an expander for additional power generation | |
EP2597274A3 (en) | Gas turbine engine lockout-time reduction | |
EP1939437A3 (en) | Turbine engine with modulated flow fan and method of operation | |
CN103104350A (en) | Twin-shaft gas turbine | |
CN105986894A (en) | Power generation system having compressor creating excess air flow and ejector augmenting the excess air flow | |
CN105888878A (en) | Turbineless jet engines | |
US10907640B2 (en) | Gas turbine blower/pump | |
CN106482135B (en) | The ground flare of combustion air is provided by gas source energy | |
US20170096936A1 (en) | Gas turbine assembly | |
CN102588143B (en) | Minitype turbofan engine | |
CN203463307U (en) | Spray type environment-friendly energy-saving explosion-proof fan based on underground water bin water source | |
CN103362637A (en) | Fluid drive mechanism for turbocharger | |
CN209053693U (en) | Gas turbine | |
CN104847480B (en) | The exhaust-driven turbo-charger exhaust-gas turbo charger of two-stage supercharging | |
KR102566355B1 (en) | Gas Turbine Blower/Pump | |
CA2921053C (en) | Gas turbine blower/pump | |
CN112160835A (en) | Combustion chamber of turbofan aircraft engine | |
CN204691895U (en) | The exhaust-gas turbocharger of two-stage supercharging | |
CN101655032A (en) | Single screw-rod engine and energy converting method thereof | |
CN105089784A (en) | Energy-efficient turbine fan | |
WO2018107334A1 (en) | Ground torch for supplying combustion air by using air source energy | |
CN104500215B (en) | Gaseous fuel piston engine and its gas handling system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |