A kind of fast cooling electric pressure cooking saucepanTechnical field
The present invention relates to electric pressure cooking saucepan technical field, specially a kind of fast cooling electric pressure cooking saucepan.
Background technology
Electric pressure cooking saucepan is the upgraded product of conventional high-tension pot and electric cooker, it combines the excellent of pressure cooker and electric cookerPoint thoroughly solves the safety problem of pressure cooker, relieves the security risk of general pressure cooker puzzlement consumer for many years；Its thermal effectRate is more than 80%, and time saving power saving, the performance value that electric pressure cooking saucepan product may refine has：Safety, energy saving, delicious health,Fashion is high-grade, automatic convenient, durable.It can be divided into traditional mechanically actuated and new-type according to the mode of operation of electric pressure cooking saucepanMicro computer operate two kinds.
Currently, existing electric pressure cooking saucepan is during use, since the inside of fuselage is in closed state, usage time mistakeWhen long, the temperature of fuselage interior can be increased gradually, and excessively high easily lead to of the internal temperature of fuselage damages electric pressure cooking saucepan, dropThe low safety used, while the service life of electric pressure cooking saucepan is also reduced, reduce use cost.In addition to this, existingElectric pressure cooking saucepan using being mostly to be cooled down using water cycle in the method that cools down, hot gas can not be made quickly to be discharged to outerPortion is difficult to realize and carries out fast cooling to the inside of fuselage, reduces the convenience to fuselage interior fast cooling, and rightWhen electric pressure cooking saucepan is used, to keeping the temperature and cooling is not easy to control.
Invention content
The purpose of the present invention is to provide a kind of fast cooling electric pressure cooking saucepans, solve asking proposed in background technologyTopic.
To achieve the above object, the present invention provides the following technical solutions：A kind of fast cooling electric pressure cooking saucepan, including fuselage,Engine base, upper cover and steam lid, the engine base are set to the lower part of the fuselage, and the upper cover is set to the upper of the fuselagePortion, the steam lid are set to the top of the upper cover, the fuselage, the engine base, the upper cover and steam lid successively intoRow is fixedly connected, and the side of the fuselage is equipped with controller, and the other side of the fuselage is equipped with radiator, the controller and instituteIt states radiator and is respectively embedded in the inside of the fuselage and be fixedly connected, the controller and the radiator are in parastateThe lower part of distribution, the controller and the radiator is equipped with the first air outlet, and first air outlet is embedded in the machineThe inside of body is annularly distributed, and convex block is equipped with outside first air outlet, the outside of the convex block is equipped with circular baffle plate, describedCircular baffle plate and fuselage are slidably connected by convex block and groove.
As a kind of preferred embodiment of the present invention, the fuselage includes shell, liner placing groove, fixing piece and hairHot plate, the shell are set to the outside of the liner placing groove, the liner placing groove and the shell using fixing piece intoRow connection, the inside that the heat-generating disc is set to the liner placing groove is fixedly connected.
As a kind of preferred embodiment of the present invention, the liner placing groove is internally provided with ventilation shaft, described logicalThe inside that wind pipeline is embedded in the liner placing groove is fixedly connected.
As a kind of preferred embodiment of the present invention, support plate is equipped between the shell and the liner placing groove,Support plate top is equipped with temperature sensor, and the support plate lower part is equipped with electric pushrod, and the electric pushrod lower part is equipped with partition board,The partition board and the electric pushrod are fixedly connected, and the partition board and the liner placing groove are carried out by the way of slidingConnection, the temperature sensor use DS18B20TO-92 models.
As a kind of preferred embodiment of the present invention, the engine base outer surface is equipped with power interface, the base innerEquipped with logical spool road, the inside that the power interface is embedded in the logical spool road is fixedly connected.
As a kind of preferred embodiment of the present invention, the engine base is internally provided with air-introduced machine, the air-introduced machine and instituteThe inner surface for stating engine base is fixedly connected, and the bottom of the engine base goes out Fen Kou equipped with second, and the logical spool road is set to instituteThe top of the second air outlet is stated, second air outlet and first air outlet are made of stainless steel.
As a kind of preferred embodiment of the present invention, the both sides of the radiator are respectively equipped with fastener, the fasteningPart is axisymmetricly distributed, and the fastener is connected with the fuselage using bolt type.
Compared with prior art, beneficial effects of the present invention are as follows：
1. by radiator being embedded in the inside of fuselage, and being equipped with temperature sense between shell and liner placing grooveDevice can measure the temperature in fuselage, and when temperature exceeds preset value, controller control electric pushrod makes partition board be moved upwardsDynamic, to open ventilation shaft, cooperation radiator makes gas circulate, easily achievees the effect that heat dissipation, effectively prevent because of machineThe internal temperature of body is excessively high to be caused to damage electric pressure cooking saucepan, improves the safety used, while also improving Voltage forceThe service life of pot, reduces use cost.
2. by being internally provided with air-introduced machine in engine base, being worked air-introduced machine using controller can be fuselage interiorHot gas release, be used cooperatively in combination with the first air outlet and the second air outlet, hot gas made quickly to be discharged to outside,Fast cooling is carried out to the inside of fuselage, improves the convenience to fuselage interior fast cooling.
3. can make to be fixedly connected between shell and liner placing groove by the fixing piece added, improving installation makesThe stability of used time, while making to be convenient for there are gap installation temperature inductor and electronic between shell and liner placing groovePush rod, convenient for being switched to ventilation shaft, convenient for being kept the temperature and being cooled down using partition board.
Description of the drawings
Fig. 1 is a kind of front view of fast cooling electric pressure cooking saucepan of the present invention,
Fig. 2 is a kind of side view of fast cooling electric pressure cooking saucepan of the present invention,
Fig. 3 is a kind of fuselage interior structural schematic diagram of fast cooling electric pressure cooking saucepan of the present invention,
Fig. 4 is a kind of part-structure connection diagram of fast cooling electric pressure cooking saucepan of the present invention,
Fig. 5 is a kind of base inner structural schematic diagram of fast cooling electric pressure cooking saucepan of the present invention.
In figure:Fuselage 1, engine base 2, upper cover 3, steam lid 4, controller 5, radiator 6, the first air outlet 7, convex block 8, circleBaffle 9, shell 10, liner placing groove 11, fixing piece 12, heat-generating disc 13, ventilation shaft 14, support plate 15, temperature sensor 16,Electric pushrod 17, partition board 18, power interface 19, logical spool road 20, air-introduced machine 21, the second air outlet 22, fastener 23.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, completeSite preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based onEmbodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every otherEmbodiment shall fall within the protection scope of the present invention.
- 5 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of fast cooling electric pressure cooking saucepan, including fuselage 1, machineSeat 2, upper cover 3 and steam lid 4, the engine base 2 are set to the lower part of the fuselage 1, and the upper cover 3 is set to the fuselage 1Top, the steam lid 4 is set to the top of the upper cover 3, the fuselage 1, the engine base 2, the upper cover 3 and steamLid 4 is fixedly connected successively, and the side of the fuselage 1 is equipped with controller 5, and the other side of the fuselage 1 is equipped with radiator 6,The inside that the controller 5 and the radiator 6 are respectively embedded in the fuselage 1 is fixedly connected, the controller 5 and instituteIt states radiator 6 to be distributed in parastate, the lower part of the controller 5 and the radiator 6 is equipped with the first air outlet 7, describedThe inside that first air outlet 7 is embedded in the fuselage 1 is annularly distributed, and first air outlet, 7 outside is equipped with convex block 8, describedThe outside of convex block 8 is equipped with circular baffle plate 9, and the circular baffle plate 9 and fuselage 1 are slidably connected by convex block 8 and groove.
Referring to Fig. 3, the fuselage 1 includes shell 10, liner placing groove 11, fixing piece 12 and heat-generating disc 13, it is describedShell 10 is set to the outside of the liner placing groove 11, the liner placing groove 11 and the shell 10 and is carried out using fixing pieceConnection, the inside that the heat-generating disc 13 is set to the liner placing groove 11 are fixedly connected, and pass through the fixing piece 12 addedIt can make to be fixedly connected between shell 10 and liner placing groove 11, improve stability, while also allow for shell 10 and interiorSupport plate 15 is installed between courage placing groove 11.
Referring to Fig. 4, the liner placing groove 11 is internally provided with ventilation shaft 14, the ventilation shaft 14 is embedded in instituteThe inside for stating liner placing groove 11 is fixedly connected, and the ventilation shaft 14 added can be such that the inside of liner placing groove 11 carries outCooling.
Referring to Fig. 4, being equipped with support plate 15 between the shell 10 and the liner placing groove 11,15 top of support plate is setThere are temperature sensor 16,15 lower part of the support plate to be equipped with electric pushrod 17,17 lower part of the electric pushrod is equipped with partition board 18, instituteIt states partition board 18 and the electric pushrod 17 is fixedly connected, the partition board 18 and the liner placing groove 11 are using the side slidedFormula is attached, and the temperature sensor 16 uses DS18B20TO-92 models, can be right by the temperature sensor 16 addedThe temperature on 11 surface of liner placing groove is incuded, and when 1 inside temperature of fuselage is excessively high convenient for timely radiating, is improvedThe convenience used, while the partition board 18 added can switch ventilation shaft 14.
It please refers to Fig.1 and Fig. 5,2 outer surface of the engine base is equipped with power interface 19, the engine base 2 is internally provided with logical spoolRoad 20, the inside that the power interface 19 is embedded in the logical spool road 20 are fixedly connected, are arranged convenient for fuselage interiorLine improves safety in use.
Referring to Fig. 5, the engine base 2 is internally provided with air-introduced machine 21, the inner surface of the air-introduced machine 21 and the engine base 2It is fixedly connected, the bottom of the engine base 2 goes out to divide mouth 22, the logical spool road 20 to be set to second outlet air equipped with secondThe top of mouth 22, second air outlet 22 and first air outlet 7 are made of stainless steel, pass through the air inducing addedThe hot gas that radiator 6 is produced by boasting can be guided to outside by machine 21, be convenient for rapid cooling, effectively prevented because in fuselage 1Portion's temperature is excessively high to cause danger.
Referring to Fig. 1, the both sides of the radiator 6 are respectively equipped with fastener 23, the fastener 23 is axisymmetricly distributed,The fastener 23 is connected with the fuselage 1 using bolt type, radiator 6 can be made to be fixed on machine by the fastener 23 addedThe outside of body improves stability in use.
A kind of controller 5 of fast cooling electric pressure cooking saucepan of the present invention changes main circuit or control according to predetermined orderResistance value enables device to control startup, speed governing, braking and reversely main of the electric pressure cooking saucepan in the wiring of circuit and change circuit.Controller is mainly made of program counter, command register, command decoder, clock generator and operation and control device, is coordinatedWith the operation for commanding entire electric pressure cooking saucepan, first with fixing piece 12 shell 10 and liner placing groove when actual use11 are fixed, and then utilizing can measure in fuselage 1 between shell 10 and liner placing groove 11 equipped with temperature inductor 16Temperature, when temperature exceeds 125 °, controller 5, which controls electric pushrod 17, makes partition board 18 be moved upwards, makes ventilation shaft 14In open state, then controls radiator 6 and work, radiate to the inside of fuselage 1,1 gas of fuselage is made to carry outCirculation, while it being internally provided with air-introduced machine 21 in engine base 2, being worked air-introduced machine 21 using controller 5 can be in fuselage 1The hot gas in portion is released, and is used cooperatively in combination with the first air outlet 7 and the second air outlet 22, and hot gas can go out by firstAir port 7 and the second air outlet 22 are quickly discharged to outside, realize and carry out fast cooling to the inside of fuselage 1.
The present invention fuselage 1, engine base 2, upper cover 3, steam lid 4, controller 5, radiator 6, the first air outlet 7, convex block 8,Circular baffle plate 9, shell 10, liner placing groove 11, fixing piece 12, heat-generating disc 13, ventilation shaft 14, support plate 15, temperature sensingDevice 16, electric pushrod 17, partition board 18, power interface 19, logical spool road 20, air-introduced machine 21, the second air outlet 22, fastener 23,Component is universal standard part or the component that those skilled in the art know, structure and principle, which are all this technology personnel, can lead toIt crosses technical manual to learn or by routine experiment method know, problems solved by the invention is that a kind of fast cooling electric pressure cooking saucepan is existingSome electric pressure cooking saucepans during use, due to fuselage inside be in closed state, when usage time is long, fuselage interiorTemperature can be increased gradually, and excessively high easily lead to of the internal temperature of fuselage damages electric pressure cooking saucepan, reduces the safety usedProperty, while the service life of electric pressure cooking saucepan is also reduced, reduce use cost.In addition to this, existing electric pressure cooking saucepan usesIt is mostly to be cooled down using water cycle in the method to cool down, hot gas can not be made quickly to be discharged to outside, be difficult to realize to machineThe inside of body carries out fast cooling, reduces the convenience to fuselage interior fast cooling, and to electric pressure cooking saucepan into enforcementWith when, to keeping the temperature and the problem of cooling is not easy to control.The present invention by radiator being embedded in the inside of fuselage,And temperature inductor is equipped between shell and liner placing groove can measure the temperature in fuselage, when temperature exceeds preset valueWhen, controller control electric pushrod makes partition board be moved upwards, and to open ventilation shaft, cooperation radiator makes gas carry outCirculation, easily achievees the effect that heat dissipation, effectively prevents from causing to damage electric pressure cooking saucepan because the internal temperature of fuselage is excessively high, carryThe high safety used, while the service life of electric pressure cooking saucepan is also improved, reduce use cost.By in engine basePortion is equipped with air-introduced machine, and air-introduced machine is worked and the hot gas of fuselage interior can be released using controller, in combination with theOne air outlet and the second air outlet are used cooperatively, and hot gas is made quickly to be discharged to outside, and fast prompt drop is carried out to the inside of fuselageTemperature improves the convenience to fuselage interior fast cooling.By the fixing piece added can make shell and liner placing groove itBetween be fixedly connected, improve stability when installing and using, while making between shell and liner placing groove that there are gaps, justIn carrying out installation temperature inductor and electric pushrod, convenient for being switched to ventilation shaft, convenient for using partition board carry out heat preservation andCooling.
Finally it should be noted that：The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention,Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be usedWith technical scheme described in the above embodiments is modified or equivalent replacement of some of the technical features.All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in the present invention'sWithin protection domain.