CN211352492U - Upper capsule heating plate of electric heating space capsule - Google Patents
Upper capsule heating plate of electric heating space capsule Download PDFInfo
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- CN211352492U CN211352492U CN201921853354.5U CN201921853354U CN211352492U CN 211352492 U CN211352492 U CN 211352492U CN 201921853354 U CN201921853354 U CN 201921853354U CN 211352492 U CN211352492 U CN 211352492U
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Abstract
The utility model provides an upper part cabin hot plate of electrical heating space cabin comprises heat preservation (1), gum cotton flannel (2), zone of heating (3), casing board (4), reflection stratum (5), far infrared radiation layer (6), temperature sensor (7), DC power supply (8), and the position of each component part in the upper part cabin hot plate is: the heat preservation layer (1) is arranged on the uppermost layer of the heating plate of the upper cabin, the back adhesive lint (2) -the heating layer (3) -the shell plate (4) -the reflection layer (5) -the far infrared radiation layer (6) is arranged on the lowest layer and faces the interior of the space cabin, the temperature sensor (7) is arranged between the back adhesive lint (2) and the heat preservation layer (1), and the direct current power supply (8) is connected with the heating layer (3). After the heating plate is manufactured, the heating plate can be bent into various shapes such as an arc shape, a semi-circle shape, a trapezoid shape and the like which are matched with the shape of the interior of the upper cabin of the space cabin according to the shape of the interior of the upper cabin of the space cabin.
Description
Technical Field
The utility model relates to a by safe voltage (18-36v) power supply, electric heating element is the upper part cabin hot plate heating source of space capsule, and an upper part cabin hot plate surface of electric heating space capsule has the function of heating and radiation far infrared, and this technique belongs to far infrared heating technical field.
Background
With the continuous improvement of the life quality of people and the accelerated aging speed of the population in China, the requirements of middle-aged and elderly people on self health care are higher and higher; people pay more attention to self maintenance and conditioning, the two factors promote the appearance of a plurality of similar infrared space capsules, beauty space capsules, sweat steaming space capsules, aroma space capsules and the like in the market, and the upper chamber heating mode of the products has the following defects: 1. the driving voltage of the heating source in the cabin is alternating current 220 v; 2. the infrared radiation source of the upper capsule of the space capsule is two infrared radiation tubes, so that the far infrared radiation area is very low and the far infrared radiation is not uniform; 3. the surface working temperature of the conventional capsule infrared heating pipe is about above 300 ℃, and the safety cannot be guaranteed; the first defect is that the danger of electric shock of a user is increased, the second defect is that the effect of far infrared rays radiated by the space capsule on a human body is not obvious, the user only feels that the physical therapy effect is exerted on the local part of the body, the physical therapy and health care effects of the whole body cannot be achieved, and the third defect is that the user is easily scalded.
Disclosure of Invention
In order to overcome the problem that exists in the use of various capsule in the market, the utility model provides an upper capsule hot plate of electrical heating capsule, the heating source of an upper capsule hot plate (hereinafter referred to as hot plate) of electrical heating capsule is by safe voltage (being less than or equal to 36v) driven, the highest operating temperature in hot plate surface is less than or equal to 80 ℃, the hot plate has the dual function of heating and surface radiation far infrared, the hot plate still radiates 5-20 microns far infrared to the object when heating the inside object of capsule. After the heating plate is manufactured, the shape can be bent into various shapes such as arc, semicircle, trapezoid and the like which are matched with the shape of the interior of the upper cabin of the space capsule according to the shape of the interior of the upper cabin of the space capsule.
The utility model provides a technical scheme that its technical problem adopted is: the hot plate mainly comprises heat preservation, gum flannelette, zone of heating, casing board, reflection stratum, far infrared radiation layer, temperature sensor, DC power supply, and the position of each component part in the hot plate is: the heat insulating layer is arranged on the uppermost layer of the heating plate, and the back adhesive flannelette, the heating layer, the shell plate, the reflecting layer and the far infrared radiation layer are arranged on the second layer of the heating plate and face the interior of the space capsule, the temperature sensor is arranged between the back adhesive flannelette and the heat insulating layer, and the direct current power supply is connected with the heating layer. The installation sequence of all components in the heating plate is as follows:
1. a heating layer is arranged on the upper surface of the shell plate;
2. sticking a piece of gum flannelette on the surface of the heating layer;
3. mounting a heat-insulating layer on the surface of the back adhesive flannelette;
4. manufacturing a reflecting layer on the lower surface of the shell plate;
5. manufacturing a far infrared radiation layer on the surface of the reflecting layer;
6. the direct current power supply is connected with the heating layer;
7. the temperature sensor is arranged between the adhesive-backed flannelette and the heat-insulating layer.
After the heating plate is manufactured, the heating plate can be bent into various shapes such as an arc shape, a semi-circle shape, a trapezoid shape and the like which are matched with the shape of the interior of the upper cabin of the space cabin according to the shape of the interior of the upper cabin of the space cabin.
The shape of the heating plate before bending is rectangular or other geometric shapes such as square, trapezoid and the like.
When the output voltage of the direct current power supply is loaded on the heating layer of the heating plate, the heating layer starts to generate heat, the heat is transmitted to the far infrared radiation layer through the shell plate and the reflecting layer, the far infrared radiation layer can complete the conversion of heat and far infrared rays after being heated, the far infrared radiation layer can radiate the far infrared rays into the space capsule, and the working temperature of the surface of the far infrared radiation layer is 45-80 ℃.
The thickness of the heat-insulating layer is 2-10mm, and the heat-insulating layer can be made of polystyrene foam plastics or polyurethane foam plastics.
The thickness of the back adhesive flannelette is between 0.5 and 1 mm.
The thickness of the shell plate is 0.3-1mm, the shell plate is made of high-temperature resistant and insulating epoxy resin plates, phenolic resin plates, silicon rubber plates and the like, and the shell plate has certain bending performance and can be bent into an arc shape, a semicircular shape and the like.
The heating layer can be made of an electric heating film or a metal heating wire, for example, the electric heating film can be made of a graphene heating film or a graphite heating film, and the metal heating wire can be made of a nickel-chromium heating wire.
The thickness of the reflecting layer is between 0.05 and 0.2mm, the reflecting layer is manufactured by two methods, a metal film is stuck on the surface of the shell plate, and the metal film can be an aluminum film or a copper film or other metal films with the function of reflecting far infrared rays; b. and coating silver paint or copper paint on the surface of the shell plate, and forming a metal film reflecting layer on the surface of the shell plate after a solvent contained in the silver paint or the copper paint is volatilized.
The thickness of the far infrared radiation layer is between 0.1 and 0.3mm, the far infrared radiation layer is manufactured by two methods, a far infrared radiation film is pasted on the surface of the reflecting layer, which can be a graphene film or other films with far infrared radiation performance; b. coating with far infrared radiation function on the surface of the shell plate, and forming a far infrared radiation layer on the surface of the reflecting layer after the solvent contained in the coating is volatilized.
The temperature sensor is mainly used for detecting the working temperature of the heating plate, and the temperature sensor can be a thermocouple or a thermal resistance sensor.
The heating source is an AC-DC converter, and the maximum working voltage of the AC-DC converter is less than or equal to 36 v.
The utility model has the advantages that: compared with the capsule with health care function which is generally used in the market at present, the capsule manufactured by the technology has the following advantages: 1. the original heating element is replaced by an alternating current 220v heating mode, and a heating element is replaced by a heating mode with the safe voltage less than or equal to 36 v; 2. the safety of the upper cabin of the original space capsule during heating is improved; 3. the range of far infrared radiation in the space capsule is improved.
Drawings
The present invention will be further explained with reference to the drawings and examples.
Fig. 1 is a schematic configuration diagram of a heating plate.
Fig. 2 is a schematic view showing that the heating panel is trapezoidal in shape before being bent.
Fig. 3 is a schematic view showing the heating plate bent in an arc shape.
Description of the figure numbers: 1. the heat-insulating layer, 2, the back adhesive flannelette, 3, the heating layer, 4, the shell plate, 5, the reflecting layer, 6, the far infrared radiation layer, 7, the temperature sensor and 8, the direct-current power supply.
Detailed Description
Example 1: referring to fig. 1, 2, and 3, the heating plate mainly comprises a heat preservation layer 1, a piece of adhesive-backed flannelette 2, a heating layer 3, a shell plate 4, a reflecting layer 5, a far infrared radiation layer 6, a temperature sensor 7, and a direct current power supply 8, and the positions of the components in the heating plate are as follows: the heat preservation layer 1 is arranged on the uppermost layer of the heating plate, the back adhesive lint 2, the heating layer 3, the shell plate 4, the reflection layer 5 and the far infrared radiation layer 6 are arranged on the lowest layer and face the interior of the space capsule, the direct current power supply 8 is connected with the heating layer 3, and the temperature sensor 7 is arranged between the heat preservation layer 1 and the back adhesive lint 2.
The heat preservation 1 chooses 3 mm's expanded polystyrene heated board for use, and 0.5 mm's epoxy board preparation is chosen to casing board 4, and the nichrome metal heater strip preparation of 0.5mm of diameter is chosen to zone of heating 3, and self-adhesion black cotton flannel is chosen for use to gum cotton flannel 2, and self-adhesion aluminium membrane is chosen for use to reflecting layer 5, and graphite alkene radiation film preparation is chosen for use to far infrared radiation layer 6, and temperature sensor 7 chooses the thermistor preparation.
The shell plate 4 is trapezoidal, and the appearance of the heat preservation layer 1, the adhesive-backed flannelette 2, the reflecting layer 5 and the far infrared radiation layer 6 is the same as that of the shell plate 4.
The processing sequence of each part in the heating plate is as follows:
1. a heating layer 3 is arranged on the upper surface of the shell plate 4;
2. sticking a back adhesive flannelette 2 on the surface of the heating layer 3;
3. the surface of the back adhesive flannelette 2 is provided with an insulating layer 1;
4. a reflecting layer 5 is adhered to the lower surface of the shell plate 4;
5. a far infrared radiation layer 6 is adhered on the surface of the reflecting layer 5;
6. the direct current power supply 8 is connected with the heating layer 3;
7. the temperature sensor 7 is arranged between the adhesive-backed flannelette 2 and the heat-insulating layer 1
When the output end of the direct current power supply 8 is connected to the heating layer 3 of the heating plate, the heating layer 3 starts to generate heat, the heat is transmitted to the far infrared radiation layer 6 through the shell plate 4 and the reflecting layer 5, the far infrared radiation layer 6 can complete the heat-far infrared conversion after being heated, the far infrared radiation layer 6 can radiate far infrared rays into the space capsule, and the surface working temperature of the far infrared radiation layer 6 is 45-80 ℃.
Example 2: referring to fig. 1, 2, and 3, the heating plate mainly comprises a heat preservation layer 1, a piece of adhesive-backed flannelette 2, a heating layer 3, a shell plate 4, a reflecting layer 5, a far infrared radiation layer 6, a temperature sensor 7, and a direct current power supply 8, and the positions of the components in the heating plate are as follows: the heat preservation layer 1 is arranged on the uppermost layer of the heating plate, the adhesive-backed flannelette 2, the heating layer 3, the shell plate 4, the reflecting layer 5 and the far infrared radiation layer 6 are arranged on the second layer, the lowest layer of the far infrared radiation layer 6 faces the interior of the space capsule, the direct current power supply 8 is connected with the heating layer 3, and the temperature sensor 7 is arranged between the heat preservation layer 1 and the adhesive-backed flannelette 2.
The heat preservation layer 1 selects a 3mm expanded polystyrene heat preservation plate, the shell plate 4 selects a 0.5mm epoxy resin plate to make, the heating layer 3 selects a 0.5mm nickel-chromium metal heating wire to make, the gum flannelette 2 selects a self-adhesive black flannelette, the reflecting layer 5 selects water-based silver powder paint, the far infrared radiation layer 6 selects far infrared coating, and the temperature sensor 7 selects a thermocouple to make.
The shell plate 4 is rectangular, and the heat preservation layer 1 and the adhesive-backed flannelette 2 are identical to the shell plate 4 in appearance.
The processing sequence of each part in the heating plate is as follows:
8. a heating layer 3 is arranged on the upper surface of the shell plate 4;
9. sticking a back adhesive flannelette 2 on the surface of the heating layer 3;
10. the surface of the back adhesive flannelette 2 is provided with an insulating layer 1;
11. coating a reflecting layer 5 on the lower surface of the shell plate 4;
12. coating a far infrared radiation layer 6 on the surface of the reflecting layer 5;
13. the direct current power supply 8 is connected with the heating layer 3;
14. the temperature sensor 7 is arranged between the adhesive-backed flannelette 2 and the heat-insulating layer 1
When the output end of the direct current power supply 8 is connected to the heating layer 3 of the heating plate, the heating layer 3 starts to generate heat, the heat is transmitted to the far infrared radiation layer 6 through the shell plate 4 and the reflecting layer 5, the far infrared radiation layer 6 can complete the heat-far infrared conversion after being heated, the far infrared radiation layer 6 can radiate far infrared rays into the space capsule, and the surface working temperature of the far infrared radiation layer 6 is 45-80 ℃.
Claims (8)
1. The utility model provides an upper part cabin hot plate of electrical heating space cabin, comprises heat preservation (1), gum cotton flannel (2), zone of heating (3), casing board (4), reflection stratum (5), far infrared radiation layer (6), temperature sensor (7), DC power supply (8), and the position of each component part in the upper part cabin hot plate of an electrical heating space cabin is: the heat preservation layer (1) is arranged on the uppermost layer of an upper cabin heating plate of an electric heating space cabin, and then the back adhesive lint (2) -the heating layer (3) -the shell plate (4) -the reflection layer (5) -the far infrared radiation layer (6) is arranged on the lowest layer and faces to the inside of the space cabin, the temperature sensor (7) is arranged between the back adhesive lint (2) and the heat preservation layer (1), and the direct current power supply (8) is connected with the heating layer (3).
2. The upper heating plate for an electrically heated space capsule as claimed in claim 1, wherein: an upper heating plate of an electrically heated space capsule is rectangular or square or trapezoidal in shape before it is bent.
3. The upper heating plate for an electrically heated space capsule as claimed in claim 1, wherein: the shape of the upper cabin heating plate of the electric heating capsule can be bent into an arc shape, a semicircular shape and a trapezoidal shape according to the shape of the inner part of the upper cabin of the capsule.
4. The upper heating plate for an electrically heated space capsule as claimed in claim 1, wherein: the thickness of the heat-insulating layer (1) is 2-10mm, and the heat-insulating layer (1) can be made of polystyrene foam plastic or polyurethane foam plastic plate.
5. The upper heating plate for an electrically heated space capsule as claimed in claim 1, wherein: the thickness of the back adhesive flannelette (2) is between 0.5 and 1 mm.
6. The upper heating plate for an electrically heated space capsule as claimed in claim 1, wherein: the thickness of the shell plate (4) is 0.3-1mm, and the shell plate (4) is made of high-temperature-resistant and insulating epoxy resin plates, phenolic resin plates and silicone rubber plates.
7. The upper heating plate for an electrically heated space capsule as claimed in claim 1, wherein: the thickness of the far infrared radiation layer (6) is between 0.1 mm and 0.3 mm.
8. The upper heating plate for an electrically heated space capsule as claimed in claim 1, wherein: the thickness of the reflecting layer (5) is between 0.05 and 0.2 mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921853354.5U CN211352492U (en) | 2019-10-25 | 2019-10-25 | Upper capsule heating plate of electric heating space capsule |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921853354.5U CN211352492U (en) | 2019-10-25 | 2019-10-25 | Upper capsule heating plate of electric heating space capsule |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211352492U true CN211352492U (en) | 2020-08-25 |
Family
ID=72103070
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921853354.5U Expired - Fee Related CN211352492U (en) | 2019-10-25 | 2019-10-25 | Upper capsule heating plate of electric heating space capsule |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211352492U (en) |
-
2019
- 2019-10-25 CN CN201921853354.5U patent/CN211352492U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200825 Termination date: 20211025 |
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| CF01 | Termination of patent right due to non-payment of annual fee |