CN105757669A - Combustion panel for gas range and gas range - Google Patents
Combustion panel for gas range and gas range Download PDFInfo
- Publication number
- CN105757669A CN105757669A CN201610301858.0A CN201610301858A CN105757669A CN 105757669 A CN105757669 A CN 105757669A CN 201610301858 A CN201610301858 A CN 201610301858A CN 105757669 A CN105757669 A CN 105757669A
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- Prior art keywords
- bandlet
- bending
- gas
- protuberance
- flat
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- 238000002485 combustion reaction Methods 0.000 title claims abstract description 65
- 238000005452 bending Methods 0.000 claims abstract description 90
- 238000005520 cutting process Methods 0.000 claims abstract description 55
- 230000015572 biosynthetic process Effects 0.000 claims description 14
- 239000003054 catalyst Substances 0.000 claims description 7
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 6
- 150000002910 rare earth metals Chemical class 0.000 claims description 6
- 229910001256 stainless steel alloy Inorganic materials 0.000 claims description 3
- 238000000034 method Methods 0.000 description 13
- 239000000567 combustion gas Substances 0.000 description 10
- 229910002651 NO3 Inorganic materials 0.000 description 5
- 238000005496 tempering Methods 0.000 description 5
- 238000003466 welding Methods 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- 238000004134 energy conservation Methods 0.000 description 3
- 238000000465 moulding Methods 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 229910052593 corundum Inorganic materials 0.000 description 2
- 230000001186 cumulative effect Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000002737 fuel gas Substances 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910001845 yogo sapphire Inorganic materials 0.000 description 2
- OERNJTNJEZOPIA-UHFFFAOYSA-N zirconium nitrate Chemical compound [Zr+4].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O OERNJTNJEZOPIA-UHFFFAOYSA-N 0.000 description 2
- BNGXYYYYKUGPPF-UHFFFAOYSA-M (3-methylphenyl)methyl-triphenylphosphanium;chloride Chemical compound [Cl-].CC1=CC=CC(C[P+](C=2C=CC=CC=2)(C=2C=CC=CC=2)C=2C=CC=CC=2)=C1 BNGXYYYYKUGPPF-UHFFFAOYSA-M 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 230000003026 anti-oxygenic effect Effects 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000037237 body shape Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 238000005255 carburizing Methods 0.000 description 1
- 238000000975 co-precipitation Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000008367 deionised water Substances 0.000 description 1
- 229910021641 deionized water Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003203 everyday effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000002372 labelling Methods 0.000 description 1
- FYDKNKUEBJQCCN-UHFFFAOYSA-N lanthanum(3+);trinitrate Chemical compound [La+3].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O FYDKNKUEBJQCCN-UHFFFAOYSA-N 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- MIVBAHRSNUNMPP-UHFFFAOYSA-N manganese(2+);dinitrate Chemical compound [Mn+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O MIVBAHRSNUNMPP-UHFFFAOYSA-N 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- BXJPTTGFESFXJU-UHFFFAOYSA-N yttrium(3+);trinitrate Chemical compound [Y+3].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O BXJPTTGFESFXJU-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
- F23D14/82—Preventing flashback or blowback
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
- F23D14/76—Protecting flame and burner parts
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cookers (AREA)
- Gas Burners (AREA)
Abstract
The invention discloses a combustion panel for a gas range. The combustion panel is characterized by comprising flat bandlets and bent bandlets, wherein the flat bandlets and the bent bandlets are laminated at intervals to form a plurality of chuck bodies with combustion holes which are independent relatively, and the bent bandlets comprise raised parts which are formed by bending, and one or more first cutting parts of which the length direction is consistent with that of the bent bandlets are arranged at positions close to the lower ends on the side walls of the raised parts and are raised towards the direction opposite to the raised parts to form first raised parts.
Description
Technical field
The present invention relates to gas-cooker accessory, particularly to a kind of gas-cooker combustion panel and gas-cooker.
Background technology
Gas-cooker is and closely bound up everyday tools of living, and wherein, energy-conserving and environment-protective have become a kind of inexorable trend.At present, market has occurred the gas-cooker that a lot of type is energy-conservation.
A kind of energy focusing stove as disclosed in Chinese patent that notification number is CN203395955U, including combustor, tray for combustion, igniting chamber, cooker racks backing ring, wherein, tray for combustion adopts the form of positive and negative triangle arranged adjacent to constitute the position, multiple hole in tray for combustion, it is ensured that combustion gas and air fully burn after mixing and reach cumulative, energy-conservation purpose.Notification number be CN302151121S appearance patent disclosed in infrared combustion panel fall within same kind.But above-mentioned tray for combustion or combustion panel are in use susceptible to the phenomenon of tempering, burner port in tray for combustion is straight-through structure, when the moment being placed on by pot on cooker racks backing ring, can produce certain pressure at the upper surface of tray for combustion, flame can be taken advantage of a situation and is pressed downward against, and causes that tempering is extinguished.
At present, the Chinese patent that notification number is CN202024330U discloses a kind of infrared burner, combustion panel therein includes wire netting and web plate, as shown in Figure 2, web plate is made up of flat bandlet 1 and sine-shaped bending bandlet 2, web plate is provided with multiple relatively independent burner port, and wire netting is welded in the bottom surface of web plate by welding procedure.The hole order number of wire netting is more than the hole order number of web plate, and so, when the flame on web plate is subject to downward pressure, metal net layer and web plate layer can form certain pressure differential, and wire netting can play certain iris action, it is prevented that flame is altered back and extinguishes.But, above-mentioned wire netting is owing to being double-layer structure with web plate, both are welded to connect, it is known that the temperature produced during gas-cooker burning is significantly high, wire netting and web plate are in the state of high temperature for a long time, flame is easily by the comparatively fragile continuous damage of wire netting and web plate, causing that wire netting comes off inefficacy, even wire netting itself also produces to destroy, and greatly reduces the service life of combustion panel.
Summary of the invention
For the deficiency that prior art exists, the first object of the present invention is in that to provide the gas-cooker combustion panel of a kind of high life.
First technical purpose of the present invention has the technical scheme that a kind of gas-cooker combustion panel, including flat bandlet and bending bandlet, described flat bandlet and bending bandlet interval are built up multiple disk body with relatively independent burner port, described bending bandlet includes the lobe being bent to form, be provided with the first cutting part that at least one length direction is consistent with the length direction of bending bandlet on the sidewall of lobe near the position of lower end, the first cutting part protrudes formation the first protuberance to lobe opposite direction.
Pass through technique scheme, gas-cooker combustion panel is made up of flat bandlet and bending bandlet, flat bandlet and bending bandlet are only stacked and are rotated into annular dish by traditional combustion panel, and the upper and lower pore size of wherein independent burner port is consistent, is so susceptible to tempering phenomenon；
In this programme, one the first cutting part is equivalent to cut two equal lines of cut of length in lobe, deformation is protruded for the first cutting part, when being processed into disk body, in advance outwardly against the first cutting part and make its outwardly formation the first protuberance in lobe, so be equivalent to the partial amt of bending on bending bandlet double more, again flat bandlet and bending bandlet interval are built up disk body, the lobe peace bandlet bending bandlet on disk body forms multiple independent burner port, fuel gas taps through burner port, make fuel gas homogenous combustion on combustion panel；Here, first protruding parts is the position of close lower end on bending bandlet, combustion panel can be divided into upper and lower two-layer, the burner port of combustion panel lower floor is separated again by the first protuberance, burner port hole order number is made to be multiplied, the hole order number of such lower floor burner port is equivalent to the several times of burner port hole, upper strata order number, is equivalent to be formed a close web frame in the downside of combustion panel；
When using above-mentioned combustion panel, combustion gas passes in burner port burns, when the pressure being pressed downward against or air-flow, owing to the density of upper strata burner port is less than lower floor, therefore the upper and lower form pressure differential, when altering under flame, the closeer burner port of lower floor effectively blocks the trend altered under flame, compared to traditionally, it is necessary to the power more strengthened just can make the flame on upper strata alter to strile-back in gas kitchen, effectively avoid the generation of tempering phenomenon；Meanwhile, first protuberance is a part for bending bandlet, both are integrated, when using at high operating temperatures for a long time, without occurring damaging and coming off, more stable compared to the structure additionally welding stratum reticulare traditionally, longer service life, and do not need additionally to increase a stratum reticulare, be substantially reduced cost.
Preferably, the quantity of described first cutting part is several, and the length of each first cutting part does not wait and all protrudes formation the first protuberance to lobe opposite direction, and the first protuberance is that upper and lower interval is arranged.
Pass through technique scheme, form the often group line of cut of the first cutting part, length between group and group is all unequal, and combine between group in being arranged above and below, namely the first cutting part is in being spaced up and down, firmly make its outwardly formation the first protuberance outwardly against each first cutting part mid portion, here, the protrusion direction of the first protuberance is all consistent and all contrary with the protrusion direction of lobe, first protuberance in distribution up and down and the hole size that surrounds of the first protuberance not etc., look down combustion panel from upside, be equivalent to burner port is separated the aperture in more crypto set；Wherein, the dense degree of aperture can control according to the quantity of the first protuberance, and the first protuberance is more many, and aperture is more close, it is possible to meets the requirement to combustion panel under different condition.
Preferably, the sidewall of described first protuberance is provided with some second cutting parts that length direction is consistent with bending bandlet length direction, first protuberance is provided with from upper and lower both sides successively inwardly length and is gradually reduced and both sides length some lines of cut one to one up and down, first cutting part is made up of two lines of cut that length is equal, second cutting part forms cambered outwards second protuberance, and the protrusion direction of adjacent two second protuberances is contrary.
nullPass through technique scheme，Line of cut is inwardly divided into first group from the first upper and lower both sides of protuberance、Second group、3rd group etc.，Often group line of cut is second cutting part，Wherein two lines of cut in second group are in first group between two lines of cut，Between two lines of cut in second group of two lines of cut in 3rd group，By that analogy，Nested layer by layer，Be equivalent to second the second cutting part in first the second cutting part，3rd the second cutting part is in second the second cutting part，Former and later two second cutting parts are nest relation，First the second cutting part protrudes formation the second protuberance to the first protuberance opposite direction，Second the second cutting part then forms the second protuberance towards the direction identical with the first protuberance，By that analogy，The protrusion direction of adjacent two second protuberances is contrary，Thus burner port is carried out in various degree be separated to form close hole，Here，The quantity of the second cutting part can be configured as required，Therefore oneself can control the hole density size of burner port.
Preferably, the quantity of described flat bandlet and bending bandlet is one, and flat bandlet is superimposed with each other with bending bandlet and central rotation is folded into the disk body with multiple relatively independent burner ports.
By technique scheme, only needing a longer flat bandlet and a longer bending bandlet, two bandlets are superimposed, and the Tou Shiqi center rotary folding capturing bandlet can form a disk body, and here, the flat bandlet after molding and bending bandlet are in the shape of a spiral；This kind of structure combustion panel can use equipment time processing molding, convenient laborsaving, and simultaneously compact conformation, intensity are high.
Preferably, the quantity of described flat bandlet and bending bandlet is some, and some flat bandlets and bending bandlet are spaced and form the disk body with multiple relatively independent burner port.
By technique scheme, being undertaken being spaced formation combustion panel by flat bandlet and bending bandlet, then carried out fixing can the completing of welding machine again and make, processing technique is simple, it is not necessary to use the equipment of additional complexity to be processed.
Preferably, the quantity of described flat bandlet and bending bandlet is some, and flat bandlet and bending bandlet all individually surround ring-type and spaced concentric arrangement is formed and has multiple row disk body to independent burning hole.
By technique scheme, flat bandlet and bending bandlet are surrounded ring-type, and interval is nested layer by layer from inside to outside again, is finally welded and fixed, this kind of mode, and fixing between flat bandlet and bending bandlet is more firm.
Preferably, described bending bandlet is that waveform bending bandlet or triangle bending bandlet or isosceles trapezoid bend bandlet.
By technique scheme, the transition relative smooth between waveform bending its kink of bandlet, when being bent by bending bandlet, it is not susceptible to the fracture of bending bandlet；
The hole area more uniformly rule that triangle bending bandlet is divided into by the first protuberance and the second projection after shaping, is conducive to the homogenous combustion of combustion gas；
Isosceles trapezoid bending its upper base of bandlet fits in flat bandlet, and the junction point contact area between bending bandlet peace bandlet is big, and it is more stable that both connect；
To sum up, it is possible to select the bending bandlet being suitable for shape to be processed using according to different demands.
Preferably, generally circular in shape or the oval or polygon of described disk body.
By technique scheme, disk body is processed into different shapes, suitable disk body shape can be selected to use according to the difference of the kitchen range top, strong adaptability.
Preferably, described flat bandlet and bending bandlet are stainless steel alloy and make and surface scribbles rare earth catalyst.
By technique scheme, combustion gas is homogenous combustion in burner port, and burning can excite metal to produce infrared ray, and infrared ray is uniformly distributed in combustion panel upper surface and forms infrared thermal radiation, is greatly improved the efficiency of combustion of combustion gas, plays the effect of cumulative；Herein, what rare earth catalyst can promote combustion gas and air is sufficiently mixed burning, reduce the generation of CO, improve the efficiency of combustion of combustion gas, ignition temperature can be improved simultaneously, reach energy-conservation purpose, under the effect of this external rare earth catalyst, substantially increase the temperature of combustion panel, it is possible to prevent flame from extinguishing in the environment have wind.
The second object of the present invention is in that to provide the gas-cooker of a kind of high life.
Second technical purpose of the present invention has the technical scheme that a kind of gas-cooker, including the kitchen range top, equipped with above-mentioned gas-cooker combustion panel on the described kitchen range top.
A part in service life for gas-cooker depends on the quality of combustion panel, the high life of above-mentioned combustion panel, therefore can improve the service life of gas-cooker.
In sum, the present invention in contrast to the combustion panel having the beneficial effect that flat bandlet and bending bandlet book moulding of prior art and not only processes simply, and ensure the abundant burning of combustion gas, simultaneously, arranged by the structure of the first protuberance on bending bandlet and the second protuberance, the lower floor making combustion panel forms close web frame, not only solve the phenomenon of gas-cooker tempering, simultaneously because the first protuberance and the second protuberance are all wholely set with combustion panel, its bulk strength is high, long service life, and the first protuberance and the second protuberance instead of the extra stratum reticulare increased in prior art, it is substantially reduced cost.
Accompanying drawing explanation
Fig. 1 is the structural representation of flat bandlet and bending bandlet in prior art；
Fig. 2 is the structural representation of flat bandlet and bending bandlet in embodiment one；
Fig. 3 is the structural representation of flat bandlet and bending bandlet in embodiment two；
Fig. 4 is the structural representation of side, embodiment two protrusions portion, it is intended to represent the relation between the first cutting part；
Fig. 5 is the structural representation of flat bandlet and bending bandlet in embodiment three；
Fig. 6 is the structural representation of the first protuberance side in embodiment three, it is intended to represent the relation between the second cutting part；
Fig. 7 is the structural representation of flat bandlet and bending bandlet in embodiment four；
Fig. 8 is the structural representation of flat bandlet and bending bandlet in embodiment five；
Fig. 9 is the structural representation of disk body in embodiment one, it is intended to represent that flat bandlet and bending bandlet constitute the first shaped form of disk body；
Figure 10 is the structural representation of disk body in embodiment one, it is intended to represent that flat bandlet and bending bandlet constitute the second shaped form of disk body；
Figure 11 is the section structure schematic diagram of disk body in embodiment one；
Figure 12 is the structural representation of disk body in embodiment one, it is intended to represent that flat bandlet and bending bandlet constitute the third shaped form of disk body；
Figure 13 is the structural representation of embodiment six.
Accompanying drawing labelling: 1, flat bandlet；2, bending bandlet；3, burner port；4, disk body；5, lobe；6, the first cutting part；7, the second cutting part；8, the first protuberance；9, the second protuberance；10, the kitchen range top；11, line of cut.
Detailed description of the invention
Below in conjunction with accompanying drawing, the present invention is described in further detail.
Embodiment one, a kind of gas-cooker combustion panel:
The first shaped form that flat bandlet 1 and bending bandlet 2 constitute disk body 4 is as follows:
nullGas-cooker combustion panel as shown in accompanying drawing 2 and accompanying drawing 9 includes flat bandlet 1 and bending bandlet 2 is superimposed with each other and central rotation is folded into the annular dish 4 with multiple relatively independent burner port 3，Wherein，Bending bandlet 2 undulate，Bending bandlet 2 includes the lobe 5 being bent to form，The corrugated peaks or valleys that namely lobe 5 is bent to form，The sidewall of lobe 5 is provided with the first cutting part 6 that a length direction is consistent with the length direction of bending bandlet 2 near the position of lower end，Herein，One the first cutting part 6 is equivalent to cut two equal lines of cut of length 11 in lobe 5，Deformation is protruded for the first cutting part 6，First cutting part 6 protrudes formation the first protuberance 8 to lobe 5 opposite direction，The shape of the first protuberance 8 is the same with the shape of lobe 5，First protuberance 8 is preferably the 1/5 of whole bending bandlet 2 height apart from the bottom surface distance of annular dish 4,Burner port 3 is again separated by the first protuberance 8 in the lower floor of burner port 3，Be equivalent in lower floor, add one layer of close net.Wherein, flat bandlet 1 and bending bandlet 2 all adopt stainless steel alloy to make, herein, use Aludirome, ferrum-chromium-aluminum has superior thermostability, antioxygenic property, resistance to SO_2 and anti-carburizing, and there is light specific gravity, surface loading is high, resistivity is high, uses the advantages such as temperature height and long service life.Wherein, flat bandlet 1 and bending bandlet 2 are bound up by high temperature vacuum brazing, after flat bandlet 1 is disc-shaped with bending bandlet 2 rotation bending, then use nickel-based solder to weld under the high temperature of 1000 DEG C, and both are firmly welded together.Wherein, in order to allow combustion gas and air be sufficiently mixed burning, improving combustion panel temperature and prevent flame-out phenomenon, scribble rare earth catalyst on the surface of flat bandlet 1 and bending bandlet 2, catalyst improves the efficiency of combustion of combustion gas.
Here, rare earth catalyst composition can be Mn10Zr65La5Y5OX-La/Al2O3, its preparation method is as follows: by the aqueous solution 11.64g of manganese nitrate [Mn (NO3) 2] 50%, zirconium nitrate [Zr (NO3) 4`5H2O] 237.52g, Lanthanum (III) nitrate [La (NO3) 3`6H2O] 16.75g, Yttrium trinitrate [Y (NO3) 3`6H2O] 12.47g, aluminum nitrate [Al (NO3) 3`9H2O] 139.81g is dissolved in 300g deionized water, stirring is to dissolving, precipitant is done by also stream mode co-precipitation again with ammonia, after having precipitated at 90 DEG C ageing 4 hours, filter washing dry, carry out 600 DEG C of roastings again；Wherein, in above-mentioned Mn10Zr65La5Y5OX-La/Al2O3, X can be that 5-20, Mn can use Co, Fe, Ni, Ce to substitute.
Here, flat bandlet 1 is as follows with the second shaped form that bending bandlet 2 constitutes disk body 4:
Shown in accompanying drawing 2, accompanying drawing 10 and accompanying drawing 11, the quantity of flat bandlet 1 and bending bandlet 2 is some, and flat bandlet 1 and bending bandlet 2 all individually surround ring-type and spaced concentric arrangement is formed and has multiple row disk body 4 to independent burning hole 3.Flat bandlet 1 and bending bandlet 2 are surrounded ring-type, and interval is nested layer by layer from inside to outside again, is finally welded and fixed, this kind of mode, and fixing between flat bandlet 1 and bending bandlet 2 is more firm.
Here, flat bandlet 1 is as follows with the third shaped form that bending bandlet 2 constitutes disk body 4:
In conjunction with accompanying drawing 2 and 12, the quantity of flat bandlet 1 and bending bandlet 2 is some, and some flat bandlets 1 and bending bandlet 2 are spaced and form the disk body 4 with multiple relatively independent burner port 3.Being undertaken being spaced formation combustion panel by flat bandlet 1 and bending bandlet 2, then carried out fixing can the completing of welding machine again and make, processing technique is simple, it is not necessary to use the equipment of additional complexity to be processed.
Embodiment two, a kind of gas-cooker combustion panel:
Embodiment two and embodiment one are different in that the first protuberance 8 of bending bandlet 2 is different.As shown in accompanying drawing 3, accompanying drawing 4, the quantity of the first cutting part 6 is several, and the length of each first cutting part 6 does not wait and all protrudes formation the first protuberance 8 to lobe 5 opposite direction, and the first protuberance 8 is arranged in upper and lower interval.In other words, form the often group line of cut 11 of the first cutting part 6, length between group and group is all unequal, and combine between group in being arranged above and below, namely the first cutting part 6 is in being spaced up and down, firmly make its outwardly formation the first protuberance 8 outwardly against each first cutting part 6 mid portion, here, the protrusion direction of the first protuberance 8 is all consistent and all contrary with the protrusion direction of lobe 5, first protuberance 8 is in the hole size that distribution and the first protuberance 8 surround up and down not etc., look down combustion panel from upside, be equivalent to burner port 3 separates the aperture in more crypto set；Wherein, the dense degree of aperture can control according to the quantity of the first protuberance 8, and the first protuberance 8 is more many, and aperture is more close, it is possible to meet the requirement to combustion panel under different condition.
Embodiment three, a kind of gas-cooker combustion panel:
Embodiment three and embodiment one are different in that the first protuberance 8 of bending bandlet 2 and the second protuberance 9 are different.As depicted in figures 5 and 6, the sidewall of the first protuberance 8 is provided with some second cutting parts 7 that length direction is consistent with bending bandlet 2 length direction, first protuberance 8 is provided with from upper and lower both sides successively inwardly length and is gradually reduced and both sides length some lines of cut 11 one to one up and down, first cutting part 6 is made up of two lines of cut 11 that length is equal, second cutting part 7 forms cambered outwards second protuberance 9, and the protrusion direction of adjacent two second protuberances 9 is contrary.nullLine of cut 11 is inwardly divided into first group from the first protuberance about 8 both sides、Second group、3rd group etc.，Often group line of cut 11 is second cutting part 7，Wherein two lines of cut 11 in second group are in first group between two lines of cut 11，Between two lines of cut 11 in second group of two lines of cut 11 in 3rd group，By that analogy，Nested layer by layer，Be equivalent to second the second cutting part 7 and be arranged in first the second cutting part 7，3rd the second cutting part 7 is arranged in second the second cutting part 7，Former and later two second cutting parts 7 are nest relation，First the second cutting part 7 protrudes formation the second protuberance 9 to the first protuberance 8 opposite direction，Second the second cutting part 7 then forms the second protuberance 9 towards the direction identical with the first protuberance 8，By that analogy，The protrusion direction of adjacent two second protuberances 9 is contrary，Thus burner port 3 is carried out in various degree be separated to form close hole，Here，The quantity of the second cutting part 7 can be configured as required，Therefore oneself can control the hole density size of burner port 3.
Embodiment four, a kind of gas-cooker combustion panel:
Embodiment four is different in that with embodiment one shape of bending bandlet 2 lobe 5 is different.
As shown in Figure 7, bending bandlet 2 bends bandlet for triangle, and the first protuberance 8 therein is similarly the triangle contrary with protruding protrusion direction.
Embodiment five, a kind of gas-cooker combustion panel:
Embodiment five is different in that with embodiment one shape of bending bandlet 2 lobe 5 is different.
As shown in Figure 8, bending bandlet 2 bends bandlet for isosceles trapezoid, and the first protuberance 8 therein is similarly the isosceles trapezoid contrary with the first protuberance 8 protrusion direction.
Embodiment six, a kind of gas-cooker:
Gas-cooker as shown in Figure 13, including the kitchen range top 10, the kitchen range top 10 is provided with combustion panel bracket, and annular dish 4 is loaded on combustion panel bracket.
The above is only the exemplary embodiment of the present invention, and not for limiting the scope of the invention, protection scope of the present invention is determined by appended claim.
Claims (10)
1. a gas-cooker combustion panel, including flat bandlet (1) and bending bandlet (2), described flat bandlet (1) and bending bandlet (2) interval are built up multiple disk body (4) with relatively independent burner port (3), it is characterized in that: described bending bandlet (2) includes the lobe (5) being bent to form, the sidewall of lobe (5) is provided with the first cutting part (6) that at least one length direction is consistent with the length direction of bending bandlet (2) near the position of lower end, first cutting part (6) protrudes formation the first protuberance (8) to lobe (5) opposite direction.
2. gas-cooker combustion panel according to claim 1, it is characterized in that: the quantity of described first cutting part (6) is several, the length of each first cutting part (6) does not wait and all protrudes formation the first protuberance (8) to lobe (5) opposite direction, and the first protuberance (8) is arranged in upper and lower interval.
3. gas-cooker combustion panel according to claim 1, it is characterized in that: the sidewall of described first protuberance (8) is provided with some second cutting parts (7) that length direction is consistent with bending bandlet (2) length direction, first protuberance (8) is provided with from upper and lower both sides successively inwardly length and is gradually reduced and length some lines of cut (11) one to one, both sides up and down, second cutting part (7) is made up of two lines of cut (11) that length is equal, second cutting part (7) forms cambered outwards second protuberance (9), the protrusion direction of adjacent two second protuberances (9) is contrary.
4. gas-cooker combustion panel according to claim 1, it is characterized in that: the quantity of described flat bandlet (1) and bending bandlet (2) is one, flat bandlet (1) and bend bandlet (2) and be superimposed with each other and central rotation is folded into the disk body (4) with multiple relatively independent burner port (3).
5. gas-cooker combustion panel according to claim 1, it is characterized in that: the quantity of described flat bandlet (1) and bending bandlet (2) is some, some flat bandlets (1) and bending bandlet (2) are spaced formation and have the disk body (4) of multiple relatively independent burner port (3).
6. gas-cooker combustion panel according to claim 1, it is characterized in that: the quantity of described flat bandlet (1) and bending bandlet (2) is some, flat bandlet (1) and bending bandlet (2) all individually surround ring-type and spaced concentric arrangement is formed and has multiple row disk body (4) to independent burning hole (3).
7. the gas-cooker combustion panel according to claim 1 ~ 6 any one, is characterized in that: described bending bandlet (2) bends bandlet or triangle bending bandlet or isosceles trapezoid bending bandlet for waveform.
8. the gas-cooker combustion panel according to claim 1 ~ 6 any one, is characterized in that: generally circular in shape or the oval or polygon of described disk body (4).
9. the gas-cooker combustion panel according to claim 1 ~ 6 any one, is characterized in that: described flat bandlet (1) and bending bandlet (2) are stainless steel alloy and make and surface scribbles rare earth catalyst.
10. a gas-cooker, including the kitchen range top (10), is characterized in that: equipped with the gas-cooker combustion panel described in any one in the claims 1 ~ 6 on the described kitchen range top (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610301858.0A CN105757669B (en) | 2016-05-07 | 2016-05-07 | Gas-cooker combustion panel and gas-cooker |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610301858.0A CN105757669B (en) | 2016-05-07 | 2016-05-07 | Gas-cooker combustion panel and gas-cooker |
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| Publication Number | Publication Date |
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| CN105757669A true CN105757669A (en) | 2016-07-13 |
| CN105757669B CN105757669B (en) | 2017-09-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610301858.0A Expired - Fee Related CN105757669B (en) | 2016-05-07 | 2016-05-07 | Gas-cooker combustion panel and gas-cooker |
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| CN (1) | CN105757669B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110207121A (en) * | 2018-07-18 | 2019-09-06 | 华帝股份有限公司 | Infrared combustion plate and manufacturing method thereof |
| CN110440326A (en) * | 2019-08-08 | 2019-11-12 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454845A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454846A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas stove |
| CN110454844A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454843A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas stove |
| CN110454842A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas stove |
| CN110454847A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454847B (en) * | 2019-08-08 | 2024-05-28 | 华帝股份有限公司 | Metal honeycomb heating body for gas kitchen range |
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Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110207121A (en) * | 2018-07-18 | 2019-09-06 | 华帝股份有限公司 | Infrared combustion plate and manufacturing method thereof |
| CN110440326A (en) * | 2019-08-08 | 2019-11-12 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454845A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454846A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas stove |
| CN110454844A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454843A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas stove |
| CN110454842A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas stove |
| CN110454847A (en) * | 2019-08-08 | 2019-11-15 | 华帝股份有限公司 | Metal honeycomb heating body for gas cooker |
| CN110454847B (en) * | 2019-08-08 | 2024-05-28 | 华帝股份有限公司 | Metal honeycomb heating body for gas kitchen range |
| CN110454846B (en) * | 2019-08-08 | 2024-05-28 | 华帝股份有限公司 | Metal honeycomb heating body for gas kitchen ranges |
| CN110454844B (en) * | 2019-08-08 | 2024-05-28 | 华帝股份有限公司 | Metal honeycomb heating body for gas kitchen range |
| CN110454843B (en) * | 2019-08-08 | 2024-05-28 | 华帝股份有限公司 | Metal honeycomb heating body for gas kitchen ranges |
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| CN105757669B (en) | 2017-09-12 |
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Effective date of registration: 20210226 Address after: 237000 12 workshops of Lu'an Intelligent Manufacturing Industrial Park, Liandong u Valley, Lu'an economic and Technological Development Zone, Lu'an City, Anhui Province Patentee after: Lu'an flisberg Intelligent Equipment Co.,Ltd. Address before: 317500 No.11, Lane 148, Xiaoquan street, Taiping Street, Wenling City, Taizhou City, Zhejiang Province Patentee before: WENLING LIULING MACHINERY Co.,Ltd. |
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