CN109506228A - A kind of biomass combustion furnace having more expects pipe - Google Patents

A kind of biomass combustion furnace having more expects pipe Download PDF

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Publication number
CN109506228A
CN109506228A CN201811631996.0A CN201811631996A CN109506228A CN 109506228 A CN109506228 A CN 109506228A CN 201811631996 A CN201811631996 A CN 201811631996A CN 109506228 A CN109506228 A CN 109506228A
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CN
China
Prior art keywords
cylinder
built
external heat
combustion
preservation cylinder
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Granted
Application number
CN201811631996.0A
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Chinese (zh)
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CN109506228B (en
Inventor
解正想
丁梦韦
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Hefei Yizheng Machinery Co Ltd
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Hefei Yizheng Machinery Co Ltd
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Priority to CN201811631996.0A priority Critical patent/CN109506228B/en
Publication of CN109506228A publication Critical patent/CN109506228A/en
Application granted granted Critical
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23BMETHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL
    • F23B90/00Combustion methods not related to a particular type of apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23JREMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J1/00Removing ash, clinker, or slag from combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23KFEEDING FUEL TO COMBUSTION APPARATUS
    • F23K1/00Preparation of lump or pulverulent fuel in readiness for delivery to combustion apparatus
    • F23K1/04Heating fuel prior to delivery to combustion apparatus

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Solid-Fuel Combustion (AREA)

Abstract

The present invention relates to a kind of biomass combustion furnaces for having more expects pipe.This has more the biomass combustion furnace of expects pipe, including fuselage cover, and built-in combustion cylinder is movably installed in the middle part of the fuselage cover, and the outer surface of the built-in combustion cylinder is arranged with external heat-preservation cylinder;The upper end of the fuselage cover is fixedly installed with tapered formula discharging wall, covers at the slot of the discharging wall and is equipped with outlet plate, the external heat-preservation cylinder top to discharging wall collection hot-zone formed below, and cover type is provided with collecting plate in the collection hot-zone;Feed box is provided with below the external heat-preservation cylinder, the lower end surface of the feed box offers the discharge nozzle of the funneling opening of several groups, and the lower end of the discharge nozzle is fixedly installed with collecting box;The side of the collecting box is provided with air inlet machine, and the output end of the air inlet machine is fixedly connected with air inlet pipe;This has more the biomass combustion furnace of expects pipe, facilitates fuel-flexible burning and uses, and is easy to operate, and ingenious in design, manufacturing cost is low, convenient for promoting the use of.

Description

A kind of biomass combustion furnace having more expects pipe
Technical field
The invention belongs to biomass combustion technical fields, and in particular to a kind of biomass combustion furnace for having more expects pipe.
Background technique
Biomass combustion is pyrolyzed the interest of the scientist of project depth, by biomass material integration or break process Afterwards, by inputting certain air or oxygen, in-furnace temperature is heated to exceed 500 DEG C, by thermal chemical reaction by biomass Macromolecular substances such as lignin etc. resolves into the thermochemical study technical method of the fuel material compared with small molecule, more existing In biomass pyrolytic combustion furnace, some built-in combustion barrels often only offer this four holes of charging, discharging, air inlet and outlet, The volume of cylinder is generally cylindrical type, and packing phenomenon is often generated after charging, is not easy full combustion, and after burning, burning The substances such as dust afterwards are not easy to be discharged, these all bring the influence being inconvenient to user.
Summary of the invention
The object of the invention is that solve the above-mentioned problems and to provide a kind of structure simple, design reasonably has more material The biomass combustion furnace of pipe.
The present invention through the following technical solutions to achieve the above objectives:
A kind of biomass combustion furnace having more expects pipe, including fuselage cover are movably installed in the middle part of the fuselage cover The outer surface of built-in combustion cylinder, the built-in combustion cylinder is arranged with external heat-preservation cylinder;
The upper end of the fuselage cover is fixedly installed with tapered formula discharging wall, covers and is equipped at the slot of the discharging wall Outlet plate, to discharging wall collection hot-zone formed below above the external heat-preservation cylinder, cover type is provided in the collection hot-zone Collecting plate;
Feed box is provided with below the external heat-preservation cylinder, it is funneling that the lower end surface of the feed box offers several groups The lower end of the discharge nozzle of opening, the discharge nozzle is fixedly installed with collecting box;
The side of the collecting box is provided with air inlet machine, and the output end of the air inlet machine is fixedly connected with air inlet pipe, described Air inlet pipe is and interior by being pierced by the outer surface from external heat-preservation cylinder rotation axis from the upper end of feed box inside feed box Burning tube inner chamber is set to communicate;
The built-in combustion cylinder is provided with pan feeding nozzle, the feeding pipe far from the side of air inlet pipe with external heat-preservation cylinder The outer surface of mouth is provided with classification rotary drive mechanism, and the classification rotary drive mechanism drives the built-in combustion cylinder individually to revolve Turn a fixing turn or rotates the built-in combustion cylinder and external heat-preservation cylinder simultaneously;
The outer surface of the built-in combustion cylinder and external heat-preservation cylinder offers ash output opening;
The feeding end of the pan feeding nozzle is provided with feeding mechanism, and the feeding mechanism includes feed inlet, is located at feed inlet The output port of the auger type feed pipe of lower section, the feed pipe is fixedly connected with the feeding end of pan feeding nozzle;
One side external surface of the fuselage cover is fixedly installed with manipulation electric box, the classification rotary drive mechanism with into Control port of the power input of mechanism of qi with the manipulation electric box is electrically connected.
As a further optimization solution of the present invention, the inner surface of the built-in combustion cylinder is set close to the position of pan feeding nozzle To be gradually wide funneling, it is slot at pan feeding nozzle, offers at gradual change through the built-in combustion cylinder and external heat preservation The venthole of cylinder.
As a further optimization solution of the present invention, the ash output opening aperture that the external heat-preservation cylinder surface opens up is greater than built-in When the ash output opening aperture that combustion barrel surface opens up, the external heat-preservation cylinder and built-in combustion cylinder rotate simultaneously, the external heat preservation Cylinder and the ash discharge hole site on built-in combustion cylinder surface are staggered.
As a further optimization solution of the present invention, the classification rotary drive mechanism includes being fixedly installed in fuselage cover The driving motor on surface, connects the output shaft of driving motor and the connection belt of turntable at the turntable for being placed on charging pipe surface rotation And the screw thread bull stick through turntable, one end of the screw thread bull stick are fixedly installed with fixture block, the pan feeding of the built-in combustion cylinder Nozzle is longer than the pan feeding nozzle of the external heat-preservation cylinder, and the pan feeding nozzle of the built-in combustion cylinder is longer than the external heat-preservation cylinder Pan feeding opening part is fixed with fixed ring, and the pan feeding nozzle of the external heat-preservation cylinder is fixed with bulge loop, the fixed ring with Bulge loop is provided with sliding slot, and the fixture block, which is inserted into the sliding slot of fixed ring and bulge loop, drives built-in combustion cylinder and external heat-preservation cylinder same Shi Xuanzhuan, the fixture block drive the rotation of built-in combustion cylinder after exiting bulge loop sliding slot.
As a further optimization solution of the present invention, the outer surface of the feed pipe is fixedly installed with charger, it is described into Material machine drives auger rotation in feed pipe, and the control output end of the power input and manipulation electric box of the charger electrically connects It connects.
As a further optimization solution of the present invention, the bottom end of the feed box is covered with discharge nozzle, the discharge nozzle into Material is provided with tip convex block between port.
As a further optimization solution of the present invention, deflation valve, discharging wall described in tapered formula are set at the outlet plate Preheating is set as between fuselage cover using case.
As a further optimization solution of the present invention, the collecting plate is heat storage, and the inner wall of the fuselage cover is sticked There is heat-insulated film layer.
The beneficial effects of the present invention are:
1) external heat-preservation cylinder and built-in combustion cylinder, Ke Yi are set in the way of rotational installation in fuselage cover of the present invention Entirety is rotated after charging, can solve the fuel accumulation problem of charging, and fuel combustion can be helped abundant, improves combustion Burn efficiency, the surface of built-in combustion cylinder and external heat-preservation cylinder offers ash output opening, and built-in ash output opening aperture is smaller, it is external go out Grey hole aperture is larger, when device enters discharge state, can individually rotate built-in combustion cylinder, i.e., in acceleration built-in combustion cylinder Fuel combustion may also help in the discharge such as dust particles in built-in combustion cylinder, and use is very convenient, operates scientific and flexible;
2) present invention is provided with feed box below external heat-preservation cylinder, and the bottom end setting of feed box has more expects pipe, assists Dust particles are discharged, and are additionally provided with tip convex block between multiple groups discharge nozzle, prevent dust and particulate matter from accumulating, air inlet pipe passes through Collecting box and discharge nozzle further utilize waste-heat internal gas, help gas to enter and are easier to burn in combustion barrel;
3) present invention is additionally provided with the convenient, flexible preheating application case used, can preheat some substances to be combusted, side Just it is used after feeding, single unit system facilitates fuel-flexible burning and uses, and easy to operate, and ingenious in design, manufacturing cost is low, just In popularization and use.
Detailed description of the invention
Fig. 1 is overall structure diagram of the invention;
Fig. 2 is the action schematic diagram when present invention enters discharge state;
Fig. 3 is the structural schematic diagram of the external heat-preservation cylinder of the present invention;
Fig. 4 is the structural schematic diagram of built-in combustion cylinder of the present invention;
Fig. 5 is the structural schematic diagram of fixed ring of the present invention;
Fig. 6 is the structural schematic diagram of bulge loop of the present invention.
In figure: 1, fuselage cover;11, electric box is manipulated;12, outlet plate;13, case is applied in preheating;21, built-in combustion cylinder; 22, external heat-preservation cylinder;23, venthole;3, feed inlet;31, feed pipe;32, charger;4, feed box;41, tip convex block;42, Discharge nozzle;43, collecting box;5, air inlet machine;51, air inlet pipe;6, collect hot-zone;61, collecting plate;62, discharging wall;71, driving motor; 72, belt is connected;73, turntable;74, screw thread bull stick;75, fixture block;76, fixed ring.
Specific embodiment
The application is described in further detail with reference to the accompanying drawing, it is necessary to it is indicated herein to be, implement in detail below Mode is served only for that the application is further detailed, and should not be understood as the limitation to the application protection scope, the field Technical staff can make some nonessential modifications and adaptations to the application according to above-mentioned application content.
Embodiment 1
As shown in Figure 1 and Figure 2, a kind of biomass combustion furnace having more expects pipe, including fuselage cover 1, in fuselage cover 1 Portion is movably installed with built-in combustion cylinder 21, and the outer surface of built-in combustion cylinder 21 is arranged with external heat-preservation cylinder 22;
The upper end of fuselage cover 1 is fixedly installed with tapered formula discharging wall 62, covers and is equipped with out at the slot of discharging wall 62 Gas plate 12, external 22 top to the collection hot-zone 6 formed below of discharging wall 62 of heat-preservation cylinder, collects cover type in hot-zone 6 and is provided with collecting plate 61;
The lower section of external heat-preservation cylinder 22 is provided with feed box 4, and the lower end surface of feed box 4 offers the funneling opening of several groups Discharge nozzle 42, the lower end of discharge nozzle 42 is fixedly installed with collecting box 43;
The side of collecting box 43 is provided with air inlet machine 5, and the output end of air inlet machine 5 is fixedly connected with air inlet pipe 51, air inlet pipe 51 by being pierced by the outer surface from external 22 rotation axis of heat-preservation cylinder from the upper end of feed box 4 inside feed boxes 4, and interior 21 inner cavity of combustion barrel is set to communicate;
Built-in combustion cylinder 21 is provided with pan feeding nozzle, pan feeding nozzle far from the side of air inlet pipe 51 with external heat-preservation cylinder 22 Outer surface be provided with classification rotary drive mechanism, the independent certain circle of rotation of classification rotary drive mechanism driving built-in combustion cylinder 21 Number rotates built-in combustion cylinder 21 and external heat-preservation cylinder 22 simultaneously;
The outer surface of built-in combustion cylinder 21 and external heat-preservation cylinder 22 offers ash output opening;
The feeding end of pan feeding nozzle is provided with feeding mechanism, and feeding mechanism includes feed inlet 3, positioned at 3 lower section of feed inlet The output port of auger type feed pipe 31, feed pipe 31 is fixedly connected with the feeding end of pan feeding nozzle;
One side external surface of fuselage cover 1 is fixedly installed with manipulation electric box 11, classification rotary drive mechanism and air inlet machine 5 Power input with manipulation electric box 11 control port be electrically connected.
The inner surface of built-in combustion cylinder 21 is set as gradually wide funneling close to the position of pan feeding nozzle, is at pan feeding nozzle Slot offers the venthole 23 through built-in combustion cylinder 21 and external heat-preservation cylinder 22 at gradual change;It is external as shown in Fig. 3 Fig. 4 The ash output opening aperture that 22 surface of heat-preservation cylinder opens up is greater than the ash output opening aperture that 21 surface of built-in combustion cylinder opens up, external heat-preservation cylinder 22 When rotating simultaneously with built-in combustion cylinder 21, external heat-preservation cylinder 22 and the ash discharge hole site on 21 surface of built-in combustion cylinder are staggered;Classification Rotary drive mechanism includes the driving motor 71 for being fixedly installed in 1 surface of fuselage cover, is placed on turning for 31 surface of feed pipe rotation Disk 73, the connection belt 72 of the output shaft for connecting driving motor 71 and turntable 73 and the screw thread bull stick 74 through turntable 73, spiral shell One end of line bull stick 74 is fixedly installed with fixture block 75, and the pan feeding nozzle of built-in combustion cylinder 21 is longer than the feeding pipe of external heat-preservation cylinder 22 Mouthful, as shown in Fig. 5 Fig. 6, the pan feeding opening part that the pan feeding nozzle of built-in combustion cylinder 21 is longer than external heat-preservation cylinder 22 is fixed with Fixed ring 76, the pan feeding nozzle of external heat-preservation cylinder 22 are fixed with bulge loop, and fixed ring 76 and bulge loop are provided with sliding slot, fixture block 75 Insertion fixed ring 76 drives built-in combustion cylinder 21 to rotate simultaneously with external heat-preservation cylinder 22 with the sliding slot of bulge loop, and fixture block 75 exits convex Built-in combustion cylinder 21 is driven to rotate after circular slide way;The outer surface of feed pipe 31 is fixedly installed with charger 32, and charger 32 drives Auger rotates in feed pipe 31, and the power input of charger 32 and the control output end of manipulation electric box 11 are electrically connected;Out The bottom end of hopper 4 is covered with discharge nozzle 42, and tip convex block 41 is provided between the charging port of discharge nozzle 42;It is set at outlet plate 12 Air valve is put, preheating is set as between tapered formula discharging wall 62 and fuselage cover 1 using case 13;Collecting plate 61 is heat storage, machine The inner wall of body shell 1, which is sticked, heat-insulated film layer.
It should be noted that when in use, charger 32 is controlled by manipulation electric box 11 first and is started, user can be with By 3 blowing of feed inlet, auger type feed pipe 31 can will burn in fuel transport to built-in combustion cylinder 21, at this point, built-in combustion The ash output opening that the ash output opening and external 22 surface of heat-preservation cylinder that 21 surfaces of cylinder open up open up is in the state that is staggered, at this time fuel and fuel The dust that burning generates is not easy to fall into from ash output opening in feed box 4, and external heat-preservation cylinder 22 is in keeping warm mode at this time;
In order to which the consumption of fuel can be accelerated, screw thread bull stick 74 can be rotated, fixture block 75 is stuck in fixed ring 76 and bulge loop Card slot in, control driving motor 71 export, by connection belt 72 drive turntable 73 rotate, while make screw thread bull stick 74 and card Block 75 drives built-in combustion cylinder 21 to rotate simultaneously with external heat-preservation cylinder 22, rotates fuel in built-in combustion barrel 21, accelerates combustion It burns, this state is heat preservation combustion state;After the high quality burning for ensuring certain time, stop driving motor 71, rotation screw thread turns After bar 74 drives fixture block 75 to exit the card slot of bulge loop, it is again started up driving motor 71, built-in combustion cylinder 21 rotates when independent, at this time Since the ash output opening of built-in combustion cylinder 21 is less than the ash output opening of external heat-preservation cylinder 22, the dust after burning can be from biggish external guarantor It is discharged into feed box 4 in the ash output opening of warm cylinder 22, this state is discharge state;
For full combustion, air inlet machine 5 is started by manipulation electric box 11, through air inlet pipe 51 into built-in combustion barrel 21 It is passed through air, it is ensured that oxygen is sufficient in built-in combustion cylinder 21, and in heat preservation combustion state, 23 position of venthole is constant, is burning When the flue gas that generates can be largely discharged by venthole 23 in collection hot-zone 6, another part passes through tiny between ash output opening Gap is dissipated to outside cylinder;When entering discharge state, built-in combustion cylinder 21 rotates, and ash output opening can be helped the dust after fuel combustion Row is arranged multiple groups discharge nozzle 42, is additionally provided with tip convex block 41 between multiple groups discharge nozzle 42 in feed box 4 in feed box 4, Tip convex block 41 can be it is coniform, the bottom plate of feed box 4 be substantially tip convex block 41 tip and funneling discharge nozzle 42 Funneling mouth, can effectively prevent dust accumulation, air inlet pipe 51 passes through collecting box 43 and feed pipe 31, dust residual temperature meeting The atmosphere temperature rising in air inlet pipe 51 is helped, auxiliary gas enters burning in built-in combustion cylinder 21;
Collection is provided with collecting plate 61 in hot-zone 6, for collecting heat, is formed between discharging wall 62 and fuselage cover 1 Preheating is further utilized and is dissipated using that can place the tools etc. for needing the incendiary material preheated or other needs to heat in case 13 The waste heat issued.
It should also be noted that, the output port of air inlet pipe 51 connects with the bitubular, surface can install high temperature resistant bearing, Or the output end of air inlet pipe 51 is set as smooth refractory metal.
The embodiments described above only express several embodiments of the present invention, and the description thereof is more specific and detailed, but simultaneously Limitations on the scope of the patent of the present invention therefore cannot be interpreted as.It should be pointed out that for those of ordinary skill in the art For, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to guarantor of the invention Protect range.

Claims (8)

1. a kind of biomass combustion furnace for having more expects pipe, it is characterised in that: including fuselage cover (1), the fuselage cover (1) Middle part is movably installed with built-in combustion cylinder (21), and the outer surface of the built-in combustion cylinder (21) is arranged with external heat-preservation cylinder (22);
The upper end of the fuselage cover (1) is fixedly installed with tapered formula discharging wall (62), covers at the slot of the discharging wall (62) Lid is equipped with outlet plate (12), to the discharging wall (62) collection hot-zone (6) formed below, institute above the external heat-preservation cylinder (22) It states collection hot-zone (6) interior cover type and is provided with collecting plate (61);
It is provided with feed box (4) below the external heat-preservation cylinder (22), the lower end surface of the feed box (4) offers several groups The lower end of the discharge nozzle (42) of funneling opening, the discharge nozzle (42) is fixedly installed with collecting box (43);
The side of the collecting box (43) is provided with air inlet machine (5), and the output end of the air inlet machine (5) is fixedly connected with air inlet pipe (51), the air inlet pipe (51) is internal by feed box (4), is pierced by from the upper end of feed box (4) through external heat-preservation cylinder (22) Outer surface at rotation axis is communicated with built-in combustion cylinder (21) inner cavity;
The side of the built-in combustion cylinder (21) and external heat-preservation cylinder (22) separate air inlet pipe (51) is provided with pan feeding nozzle, institute The outer surface for stating pan feeding nozzle is provided with classification rotary drive mechanism, and the classification rotary drive mechanism drives the built-in combustion Cylinder (21) individually rotates a fixing turn or rotates the built-in combustion cylinder (21) and external heat-preservation cylinder (22) simultaneously;
The outer surface of the built-in combustion cylinder (21) and external heat-preservation cylinder (22) offers ash output opening;
The feeding end of the pan feeding nozzle is provided with feeding mechanism, and the feeding mechanism includes feed inlet (3), is located at feed inlet (3) output port of the auger type feed pipe (31) below, the feed pipe (31) is fixedly connected with the feeding end of pan feeding nozzle;
One side external surface of the fuselage cover (1) is fixedly installed with manipulation electric box (11), the classification rotary drive mechanism It is electrically connected with the control port for manipulating electric box (11) with the power input of air inlet machine (5).
2. a kind of biomass combustion furnace for having more expects pipe according to claim 1, it is characterised in that: the built-in combustion cylinder (21) inner surface is set as gradually wide funneling close to the position of pan feeding nozzle, is slot at pan feeding nozzle, opens at gradual change Equipped with the venthole (23) for running through the built-in combustion cylinder (21) and external heat-preservation cylinder (22).
3. a kind of biomass combustion furnace for having more expects pipe according to claim 2, it is characterised in that: the external heat-preservation cylinder (22) the ash output opening aperture that surface opens up is greater than the ash output opening aperture that built-in combustion cylinder (21) surface opens up, the external heat-preservation cylinder (22) when being rotated simultaneously with built-in combustion cylinder (21), the ash output opening of the external heat-preservation cylinder (22) and built-in combustion cylinder (21) surface Position is staggered.
4. a kind of biomass combustion furnace for having more expects pipe according to claim 3, it is characterised in that: the classification rotation is driven Motivation structure includes the driving motor (71) for being fixedly installed in fuselage cover (1) surface, is placed on turning for feed pipe (31) surface rotation Disk (73), the connection belt (72) of the output shaft for connecting driving motor (71) and turntable (73) and the screw thread through turntable (73) One end of bull stick (74), the screw thread bull stick (74) is fixedly installed with fixture block (75), the feeding pipe of the built-in combustion cylinder (21) Mouth is longer than the pan feeding nozzle of the external heat-preservation cylinder (22), and the pan feeding nozzle of the built-in combustion cylinder (21) is longer than the external guarantor The pan feeding opening part of warm cylinder (22) is fixed with fixed ring (76), and the pan feeding nozzle of the external heat-preservation cylinder (22) is fixed with Bulge loop, the fixed ring (76) and bulge loop are provided with sliding slot, the sliding slot of fixture block (75) insertion fixed ring (76) and bulge loop Middle drive built-in combustion cylinder (21) rotates simultaneously with external heat-preservation cylinder (22), the fixture block (75) is exited after bulge loop sliding slot drive in Set combustion barrel (21) rotation.
5. a kind of biomass combustion furnace for having more expects pipe according to claim 1, it is characterised in that: the feed pipe (31) Outer surface be fixedly installed with charger (32), the interior auger rotation of the charger (32) driving feed pipe (31), the charging The power input of machine (32) and the control output end of manipulation electric box (11) are electrically connected.
6. a kind of biomass combustion furnace for having more expects pipe according to claim 1, it is characterised in that: the feed box (4) Bottom end be covered with discharge nozzle (42), be provided with tip convex block (41) between the charging port of the discharge nozzle (42).
7. a kind of biomass combustion furnace for having more expects pipe according to claim 1, it is characterised in that: the outlet plate (12) Deflation valve is arranged in place, is set as preheating described in tapered formula between discharging wall (62) and fuselage cover (1) using case (13).
8. a kind of biomass combustion furnace for having more expects pipe according to claim 1, it is characterised in that: the collecting plate (61) For heat storage, the inner wall of the fuselage cover (1) is sticked and has heat-insulated film layer.
CN201811631996.0A 2018-12-29 2018-12-29 Biomass combustion furnace with multiple discharging pipes Active CN109506228B (en)

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Application Number Priority Date Filing Date Title
CN201811631996.0A CN109506228B (en) 2018-12-29 2018-12-29 Biomass combustion furnace with multiple discharging pipes

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CN109506228A true CN109506228A (en) 2019-03-22
CN109506228B CN109506228B (en) 2020-02-18

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Cited By (2)

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Publication number Priority date Publication date Assignee Title
CN110560456A (en) * 2019-09-11 2019-12-13 合肥道正企智大数据有限公司 Waste salt residue harmless and resource utilization system based on Internet of things
CN114216134A (en) * 2021-12-17 2022-03-22 吴可清 Environment-friendly combustion system

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CN108800177A (en) * 2018-08-29 2018-11-13 湖北艾孚威环境能源科技有限公司 A kind of burning boiler fume extractor for being convenient for cleaning surface floating dust

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Publication number Priority date Publication date Assignee Title
JP2015140933A (en) * 2014-01-27 2015-08-03 長松院 泰久 Biomass rotating drier with small-sized steam power generator
CN205939107U (en) * 2016-08-11 2017-02-08 广东奥创新能源科技有限公司 Biomass gasification burner
CN106152168A (en) * 2016-08-29 2016-11-23 西安圣华农业科技股份有限公司 Inner cylinder rotating formula biomass particle burner
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110560456A (en) * 2019-09-11 2019-12-13 合肥道正企智大数据有限公司 Waste salt residue harmless and resource utilization system based on Internet of things
CN114216134A (en) * 2021-12-17 2022-03-22 吴可清 Environment-friendly combustion system

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