CN205351387U - Ground ignition - Google Patents

Ground ignition Download PDF

Info

Publication number
CN205351387U
CN205351387U CN201620137671.7U CN201620137671U CN205351387U CN 205351387 U CN205351387 U CN 205351387U CN 201620137671 U CN201620137671 U CN 201620137671U CN 205351387 U CN205351387 U CN 205351387U
Authority
CN
China
Prior art keywords
combustible gas
ignition
gas pipeline
detonation
pipeline
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
Application number
CN201620137671.7U
Other languages
Chinese (zh)
Inventor
郭红普
冯养伟
王光辉
马振朋
毕殿磊
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.)
Puyang Puruide Combustion Control Equipment Engineering Co Ltd
Original Assignee
Puyang Puruide Combustion Control Equipment Engineering 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 Puyang Puruide Combustion Control Equipment Engineering Co Ltd filed Critical Puyang Puruide Combustion Control Equipment Engineering Co Ltd
Priority to CN201620137671.7U priority Critical patent/CN205351387U/en
Application granted granted Critical
Publication of CN205351387U publication Critical patent/CN205351387U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

Ground ignition is the ignition technology of petroleum chemical enterprise's torch, boiler, and its structural relation is that first stop valve, first filter, spark arrester, first manometer, first check valve are being installed to the order on the combustible gas pipeline, second stop valve, second filter, second manometer, second check valve are being installed to the order on compressed air pipeline, be connected in the detonation indoorly after the combustible gas pipeline joins with compressed air pipeline's terminal, installing the ball valve on the pipeline of detonation room and altar lamp, installing the high voltage generator in the one end on high -pressure ignition wire way, installing aviation semiconductor ignition electric nozzle at the other end on high -pressure ignition wire way, aviation semiconductor ignition electric nozzle's the other end is connected indoorly in the detonation, the first flow regulator of deciding is being installed to first manometer and first check valve centre at the combustible gas pipeline, install the second at compressed air pipeline's second manometer with the centre of second check valve and deciding flow regulator, be provided with fire observation hole on the detonation room.

Description

Ground igniter
Technical field: this utility model relates to the firing technique of petroleum chemical enterprise's torch, boiler, especially ground igniter.
Background technology: at present, petroleum chemical enterprise's torch, boiler ground igniter be mainly made up of combustible gas, compression air and igniter, due to design and technical defect, combustible gas, compressed-air actuated mixing ratio are wayward, often repeated multiple times and be lot more time to light, ignition success rate is low, makes device discharge gas empty in a large number or enter boiler furnace, there is Environmental Safety hidden danger.
Summary of the invention: the purpose of this utility model is to provide the ground igniter that ignition success rate is higher, the duration of ignition is shorter and safe and reliable, the shortcoming which overcoming other technology at present, the purpose of this utility model is realized in, it is to be formed by connecting by combustible gas pipeline, compressed-air line, high-tension ignition circuit, and on combustible gas pipeline, order is installed with the first stop valve, the first filter, spark arrester, the first Pressure gauge, the first check-valves;On compressed-air line, order is installed with the second stop valve, the second filter, the second Pressure gauge, the second check-valves;The terminal of combustible gas pipeline and compressed-air line is connected to detonation indoor after converging;The detonation room pipeline with altar lamp is installed with ball valve (leading pouring effect).
Being installed with high tension generator in one end of high-tension ignition circuit, the other end at high-tension ignition circuit is installed with aviation quasiconductor ignition electric nozzle, and the other end of aviation quasiconductor ignition electric nozzle is connected to detonation indoor.
In the middle of first Pressure gauge and the first check-valves of combustible gas pipeline, the first constant flow control device is installed;At the second Pressure gauge of compressed-air line and the centre of the second check-valves, the second constant flow control device is installed.
Detonation room is provided with flame-observing hole.
Application process of the present utility model is: open the certain aperture of front end valve, compression air or combustible gas are through filter (combustible gas pipeline is equipped with spark arrester), check-valves, constant flow control device, enter mixing chamber, open high tension generator simultaneously, aviation quasiconductor ignition electric nozzle sends spark initiation gaseous mixture, and detonation fireball ignites altar lamp.
Meaning of the present utility model is: owing to being respectively mounted constant flow regulating valve on combustible gas pipeline and compressed-air line, can disposable setting igniting time desired gas flow (when combustible gas component changes, can set separately at the scene), igniting need not regulate flow proportional more frequently every time later, have only to open the first and second certain apertures of stop valve, press button ignition switch and namely can light.Make ignition success rate greatly improve, shorten the duration of ignition greatly;Safety and environmental protection hidden danger are broken off.
Accompanying drawing illustrates: Fig. 1 is the structural representation of ground igniter, in figure 1, combustible gas pipeline 2, compressed-air line 3, high-tension ignition circuit the 4, first stop valve the 5, first filter 6, spark arrester the 7, first Pressure gauge the 8, first check-valves the 9, first constant flow control device the 10, second stop valve the 11, second filter the 12, second Pressure gauge the 13, second check-valves the 14, second constant flow control device 15, aviation quasiconductor ignition electric nozzle 16, detonation room 17, flame-observing hole 18, ball valve 19, high tension generator
Detailed description of the invention: embodiment 1. this utility model is to be formed by connecting by combustible gas pipeline 1, compressed-air line 2, high-tension ignition circuit 3, on combustible gas pipeline 1, order is installed with first stop valve the 4, first filter 5, spark arrester the 6, first Pressure gauge the 7, first check-valves 8;On compressed-air line 2, order is installed with second stop valve the 10, second filter the 11, second Pressure gauge the 12, second check-valves 13;The terminal of combustible gas pipeline 1 and compressed-air line 2 is connected in detonation room 16 after converging;The pipeline of detonation room 16 and altar lamp is installed with ball valve 18.
Embodiment 2, being installed with high tension generator 19 in one end of high-tension ignition circuit 3, the other end at high-tension ignition circuit 3 is installed with aviation quasiconductor ignition electric nozzle 15, and the other end of aviation quasiconductor ignition electric nozzle 15 is connected in detonation room 16.
Embodiment 3, in the middle of the first Pressure gauge 7 of combustible gas pipeline 1 and the first check-valves 8, first constant flow control device 9 is installed;At the second Pressure gauge 12 of compressed-air line 2 and the centre of the second check-valves 13, second constant flow control device 14 is installed.
Embodiment 4, on detonation room 16, it is provided with flame-observing hole 17.

Claims (4)

1. ground igniter, it is to be formed by connecting by combustible gas pipeline (1), compressed-air line (2), high-tension ignition circuit (3), it is characterized in that: be installed with the first stop valve (4), the first filter (5), spark arrester (6), the first Pressure gauge (7), the first check-valves (8) in the upper order of combustible gas pipeline (1);In the upper order of compressed-air line (2), the second stop valve (10), the second filter (11), the second Pressure gauge (12), the second check-valves (13) are installed;The terminal of combustible gas pipeline (1) and compressed-air line (2) is connected in detonation room (16) after converging;Detonation room (16) pipeline with altar lamp is installed with ball valve (18).
2. ground according to claim 1 igniter, it is characterized in that: in one end of high-tension ignition circuit (3), high tension generator (19) is installed, the other end at high-tension ignition circuit (3) is installed with aviation quasiconductor ignition electric nozzle (15), and the other end of aviation quasiconductor ignition electric nozzle (15) is connected in detonation room (16).
3. ground according to claim 1 igniter, is characterized in that: be installed with the first constant flow control device (9) in the middle of first Pressure gauge (7) and the first check-valves (8) of combustible gas pipeline (1);In second Pressure gauge (12) of compressed-air line (2) and the centre of the second check-valves (13), the second constant flow control device (14) is installed.
4. ground according to claim 1 igniter, is characterized in that: be provided with flame-observing hole (17) on detonation room (16).
CN201620137671.7U 2016-02-24 2016-02-24 Ground ignition Active CN205351387U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620137671.7U CN205351387U (en) 2016-02-24 2016-02-24 Ground ignition

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620137671.7U CN205351387U (en) 2016-02-24 2016-02-24 Ground ignition

Publications (1)

Publication Number Publication Date
CN205351387U true CN205351387U (en) 2016-06-29

Family

ID=56179992

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620137671.7U Active CN205351387U (en) 2016-02-24 2016-02-24 Ground ignition

Country Status (1)

Country Link
CN (1) CN205351387U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106823593A (en) * 2017-03-20 2017-06-13 濮阳普瑞德燃控设备工程有限公司 Torch gas Special filtering device and application process

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106823593A (en) * 2017-03-20 2017-06-13 濮阳普瑞德燃控设备工程有限公司 Torch gas Special filtering device and application process

Similar Documents

Publication Publication Date Title
CN200993369Y (en) Igniter for drilling fluid-gas separator
CN205351387U (en) Ground ignition
CN201137969Y (en) Automatic detonation igniting apparatus on earth for flare
CN100545516C (en) Remote explosion ignition device
CN208983349U (en) A kind of spare igniter of overhead torch
CN104748132A (en) Lifting micro-positive pressure energy concentration maintenance type torch burner
CN103615740B (en) Torch detonation ignition safety system
CN201363757Y (en) Self-ignition device of blowing air combustion furnace
CN212618261U (en) Well blowout ignition simulation gas distribution device
CN205560840U (en) Long -range flame jet formula ignition
CN211119484U (en) Solar ground explosion igniter
CN207849421U (en) A kind of detonation ignitor
CN103807875A (en) Ground detonation type ignition device
CN205746964U (en) Training simulation fire point firearm
CN203744297U (en) Ground deflagration type ignition device
CN204125166U (en) Hydrochloric acid synthetic furnace automatic firing mechanism
CN208332325U (en) Igniter for the website that recovers the oil
CN205332268U (en) Novel open flow pond torch manufacturing equipment device
CN206540131U (en) Low NOXDischarge band automatic ignition, the integrated altar lamp of band fire inspection
CN101614397B (en) Combined mechanical pressure release anti-backfire device
CN211060148U (en) Open type torch ignition system of refuse landfill
CN206386962U (en) A kind of two sections of ignition combustion systems of small-power hot air type
CN204684501U (en) A kind of hydrogen and oxygen gas mixture spark arrester
CN2221693Y (en) Gas safety valve
CN221005126U (en) Deflagration ignition device

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant