CN210568433U - Deflagration generator - Google Patents

Deflagration generator Download PDF

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Publication number
CN210568433U
CN210568433U CN201921033811.6U CN201921033811U CN210568433U CN 210568433 U CN210568433 U CN 210568433U CN 201921033811 U CN201921033811 U CN 201921033811U CN 210568433 U CN210568433 U CN 210568433U
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CN
China
Prior art keywords
mixing chamber
taken over
deflagration
gas
air
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Active
Application number
CN201921033811.6U
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Chinese (zh)
Inventor
王逢
赵亮
赵奔逸
佘娟霞
张保堂
李乐
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.)
Shanxi Wiser Technology Institute Co ltd
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Shanxi Wiser Technology Institute Co ltd
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Priority to CN201921033811.6U priority Critical patent/CN210568433U/en
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Abstract

The utility model relates to a deflagration generator belongs to petrochemical industry tail gas treatment technical field, specifically install the gas including the front end of mixing chamber pipe and take over, deflagration gas export is installed to the rear end of mixing chamber pipe, the gas is taken over and is set up with deflagration gas export is concentric, the air is taken over and is installed to the anterior top of mixing chamber pipe and take over, the air is taken over and is extended to the mixing chamber intraductally, and the bottom that the air was taken over is sealed, still is provided with a plurality of mixed flow holes on the circumference that the air was taken over, the rear portion top of mixing chamber pipe is installed the firing bar and is taken over, install the firing bar in the firing bar is taken over, the firing head of firing bar is located the mixing chamber intraductally, the.

Description

Deflagration generator
Technical Field
The utility model relates to a deflagration generator belongs to petrochemical trade tail gas treatment technical field.
Background
The existing torch ground transfer combustion type igniter has the following principle: the instrument air and fuel gas for ignition enter the mixing chamber through respective pipelines and a flow-limiting orifice plate (or a pressure reducing valve), when the concentration of the instrument air and the fuel gas reaches a chemical concentration range, the instrument air and the fuel gas are ignited by electric sparks generated by high-voltage discharge of a high-energy semiconductor electric nozzle and are detonated, and generated flames are transmitted to the pilot burner along the pipelines and ignite the pilot burner.
The existing ground transfer combustion type ignition mode of the torch is characterized in that: firstly, air and fuel gas are respectively connected into a mixing chamber to be naturally mixed, and the mixing effect is poor under the influence of respective gas flow and pressure of an air pipeline and a fuel gas pipeline; secondly, the concentration of the mixed gas is only between the upper explosion limit and the lower explosion limit, the mixer can deflagrate when sparks exist, the propagation of flame after deflagration is also influenced by the concentration of the mixed gas in the pipeline, and the deflagration success rate of the mixer is only 50 percent generally.
SUMMERY OF THE UTILITY MODEL
For solving the technical problem that prior art exists, the utility model provides a simple structure, reasonable in design can effectively improve the detonation generator of detonation success rate and reliability.
For realizing above-mentioned mesh, the utility model discloses the technical scheme who adopts is a detonation generator, take over and the ignition pole including mixing chamber pipe, gas, the gas is taken over, the ignition pole, the gas is taken over to the front end of mixing chamber pipe is installed, deflagration gas export is installed to the rear end of mixing chamber pipe, gas are taken over and deflagration gas export sets up with one heart, the air is taken over to be installed to the anterior top of mixing chamber pipe, it is intraductal that the air is taken over and is extended to the mixing chamber, and the bottom that the air was taken over seals, still be provided with a plurality of mixing holes on the circumference that the air was taken over, the ignition pole is installed to the rear portion top of mixing chamber pipe, install the ignition pole in the ignition pole is taken over, the ignition head of ignition pole.
Preferably, the air connecting pipe is vertically arranged, and the bottom of the air connecting pipe is positioned below the axis of the gas connecting pipe.
Preferably, the outer wall of the mixing chamber pipe is further provided with an observation hole and explosion-proof glass arranged on the observation hole, and the axis of the observation hole and the axis of the ignition rod are in the same plane.
Preferably, the connection end of the mixing chamber pipe and the gas connection pipe is provided with an abrupt cross section.
Preferably, the deflagration gas outlet is of a conical structure.
Compared with the prior art, the utility model discloses following technological effect has: the utility model improves the circulation contact surface of the air pipeline, so that the air pipeline and the fuel gas entering the mixing chamber are fully and uniformly mixed, and the deflagration success rate is increased; by changing the structural form of the gas inlet and the air inlet, shock waves generated when deflagration occurs can be effectively coped, so that upstream equipment and instruments are prevented from being damaged, the safety of a deflagration system is ensured, and the service life of the deflagration system is prolonged; the ignition condition is effectively monitored through the observation hole, and the detonation reliability is enhanced.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Detailed Description
In order to make the technical problem, technical solution and advantageous effects to be solved by the present invention more clearly understood, the following description is given in conjunction with the accompanying drawings and embodiments to illustrate the present invention in further detail. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
As shown in fig. 1, a detonation generator, including mixing chamber pipe 1, gas takeover 2, air takeover 3, the igniter rod takeover 4 and igniter rod 5, gas takeover 2 is installed to the front end of mixing chamber pipe 1, deflagration gas export 6 is installed to the rear end of mixing chamber pipe 1, deflagration gas export 6 is the toper structure, mixing chamber pipe 1, gas takeover 2 and deflagration gas export 6 set up with one heart, air takeover 3 is installed to the front portion top of mixing chamber pipe 1, air takeover 3 extends to in the mixing chamber pipe 1, and the bottom of air takeover 3 is sealed, still be provided with a plurality of mixing hole 7 on the circumference of air takeover 3, igniter rod takeover 4 is installed to the rear portion top of mixing chamber pipe 1, igniter rod 5 is installed in igniter rod takeover 4, the igniter head of igniter rod 5 is located mixing chamber pipe 1.
The utility model discloses well air is taken over 3 and is stretched into 1 intraductal bottom in mixing chamber pipe, and 3 vertical settings are taken over to the air, and the bottom that 3 were taken over to the air is located the axis below that 2 were taken over to the gas, 3 lower extremes are taken over to the air and is sealed, stretch into some pipe lateral wall border and open if dry mixing orifice, make the flow direction variety of air admission mixing chamber pipe 1, and with the gas contact surface greatly increased who gets into mixing chamber pipe 1, the speed and the homogeneity of gas mixing obtain obvious enhancement, thereby reach the purpose that gas and air intensive mixing reach deflagration concentration rapidly, the effectual success rate that has improved system deflagration.
Wherein, the outer wall of the mixing chamber pipe 1 is also provided with an observation hole 8 and an explosion-proof glass 9 arranged on the observation hole, and the axis of the observation hole 8 and the axis of the ignition rod 5 are in the same plane. The ignition rod 5 is connected through the ignition rod connecting pipe 4 in a threaded mode and inserted into the mixing chamber pipe 1, the observation hole 8 is arranged at the same cross section horizontal position, the situation after ignition and deflagration is effectively monitored, rapid processing can be carried out when deflagration is observed not to occur, the reliability of deflagration is improved, and the deflagration ignition efficiency is also improved.
Furthermore, the connection end of the mixing chamber pipe 1 to the gas connection pipe 2 is provided with an abrupt cross section 10. The sudden change cross section structure of the gas inlet and the mixed flow hole structure of the air inlet can also effectively block shock waves generated when the deflagration occurs, avoid damaging upstream equipment instruments, and indirectly prolong the service life of the deflagration system. The deflagration gas outlet 6 adopts a structure with a gradually-reduced cross section, which is also beneficial to the conduction of flame and improves the safety of deflagration ignition.
To sum up, the utility model discloses detonation generator can effectively improve system detonation success rate, reliability, security and life through the optimal design to the structure.
The foregoing is considered as illustrative and not restrictive of the preferred embodiments of the invention, and any modifications, equivalents and improvements made within the spirit and principles of the invention are intended to be included within the scope of the invention.

Claims (5)

1. A detonation generator, characterized by: take over, the igniter is taken over and the igniter is taken over including mixing chamber pipe, gas, the gas is installed at the front end of mixing chamber pipe and is taken over, deflagration gas export is installed to the rear end of mixing chamber pipe, gas are taken over and are exported the concentric setting with deflagration, the air is taken over to install the anterior top of mixing chamber pipe, it is intraductal that the air is taken over to extend to the mixing chamber, and the bottom that the air was taken over seals, still be provided with a plurality of mixed flow holes on the circumference that the air was taken over, the igniter is taken over to install above the rear portion of mixing chamber pipe, install the igniter in the igniter is taken over, the igniter of igniter is located the mixing chamber intraductally.
2. A deflagration generator according to claim 1, characterized in that: the air connecting pipe is vertically arranged, and the bottom of the air connecting pipe is positioned below the axis of the gas connecting pipe.
3. A deflagration generator according to claim 1, characterized in that: the outer wall of the mixing chamber pipe is also provided with an observation hole and explosion-proof glass arranged on the observation hole, and the axis of the observation hole and the axis of the ignition rod are in the same plane.
4. A deflagration generator according to claim 1, characterized in that: and the connecting end of the mixing chamber pipe and the gas connecting pipe is provided with an abrupt cross section.
5. A deflagration generator according to claim 1, characterized in that: the explosion gas outlet is of a conical structure.
CN201921033811.6U 2019-07-04 2019-07-04 Deflagration generator Active CN210568433U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921033811.6U CN210568433U (en) 2019-07-04 2019-07-04 Deflagration generator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921033811.6U CN210568433U (en) 2019-07-04 2019-07-04 Deflagration generator

Publications (1)

Publication Number Publication Date
CN210568433U true CN210568433U (en) 2020-05-19

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921033811.6U Active CN210568433U (en) 2019-07-04 2019-07-04 Deflagration generator

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CN (1) CN210568433U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112361378A (en) * 2020-11-15 2021-02-12 西安长峰机电研究所 Miniaturized safety mechanism

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112361378A (en) * 2020-11-15 2021-02-12 西安长峰机电研究所 Miniaturized safety mechanism

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