CN205688264U - A kind of balloon structure for fire balloon - Google Patents
A kind of balloon structure for fire balloon Download PDFInfo
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- CN205688264U CN205688264U CN201620503927.1U CN201620503927U CN205688264U CN 205688264 U CN205688264 U CN 205688264U CN 201620503927 U CN201620503927 U CN 201620503927U CN 205688264 U CN205688264 U CN 205688264U
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Abstract
The utility model discloses a kind of balloon structure for fire balloon, this balloon structure includes sacculus substrate layer and the coating being attached on this sacculus substrate layer；The thickness of described sacculus substrate layer is 0.05mm～0.25mm；The thickness of described coating is 2 μm～50 μm.This utility model is improved by the Rotating fields crucial to balloon structure, the thickness etc. of every layer, compared with prior art can effectively solve the problem that the problem that the dissipation of sacculus heat is fast, and this sacculus uses the coating with titanium oxide or silicon oxide plus the structure of sacculus base material, intensity is high, it can be ensured that use this balloon structure to make the stability of fire balloon sacculus, the safety obtained.
Description
Technical field
This utility model belongs to fire balloon balloons technique field, ties more particularly, to a kind of sacculus for fire balloon
Structure, this balloon structure can be used for producing the fire balloon of thermal-collecting energy-saving.
Background technology
Fire balloon is made up of sacculus, hanging basket, heater three part, utilizes air heating in sacculus close to reduce air
Degree forms sacculus inner air and outer air pressure reduction and goes up to the air.Present people's many employings chinlon, the close fabric of terylene is progressively popularized along with fire balloon
Process as sacculus, but in fire balloon flight course, the heat in sacculus is constantly lost to outside diffusion, and thermal protection rate is not enough
60%, capacity usage ratio is relatively low, and for ensureing the flight time of fire balloon, generally requires the weight increasing carrying fuel, limit
Make the stroke of fire balloon.
Utility model content
For disadvantages described above or the Improvement requirement of prior art, the purpose of this utility model is to provide a kind of for steam
The balloon structure of ball, is wherein improved, with prior art phase by the Rotating fields crucial to balloon structure, the thickness etc. of every layer
Ratio can effectively solve the problem that sacculus heat dissipates fast problem, and this sacculus uses the coating with titanium oxide or silicon oxide to add
The structure of sacculus base material, intensity is high, it can be ensured that use this balloon structure to make the stability of fire balloon sacculus, the safety obtained
Property.
For achieving the above object, according to this utility model, it is provided that a kind of balloon structure for fire balloon, its feature exists
In, this balloon structure includes sacculus substrate layer and the coating being attached on this sacculus substrate layer；The thickness of described sacculus substrate layer
For 0.05mm～0.25mm；The thickness of described coating is 2 μm～50 μm.
As of the present utility model further preferably, described sacculus substrate layer is woven dacron or polyamide fabric.
As of the present utility model further preferably, described coating is titanium oxide layer or silicon oxide layer.
By the above technical scheme that this utility model is contemplated, compared with prior art, by existing sacculus fabric
The micro-nano titanium oxide of surface-coated of (i.e. sacculus base material) or silicon oxide form coating (i.e. heat build-up layer), utilize titanium oxide, oxidation
The heat reflection effect of silicon microcrystalline coating, makes sacculus have efficient heat build-up effect, improves heat utilization rate.This utility model is used
In the balloon structure of fire balloon, the thickness of its coating (such as titania coating or silica coating) is 2 μm～50 μm, sacculus base material
Thickness be 0.05mm～0.25mm；After tested, the balloon structure in this utility model is used can to make the sacculus heat of fire balloon
Lost rate is reduced to less than 15%, and the development for following fire balloon electroheat technology, distance flight manipulation technology has important
Meaning.
This utility model, by improving the structure of sacculus, utilizes the High Efficiency Thermal of crystallite titanium oxide/silicon oxide to reflect
Effect, makes conventional thermal balloon sacculus tight weave have the function of high-efficient heat accumulation, it is possible to increase the aloft heat energy utilization of fire balloon
Rate, reduces the aloft energy loss of fire balloon, improves flight time and the distance of fire balloon under the conditions of identical energy, has good
Good energy saving effect.
Accompanying drawing explanation
Fig. 1 is to use the fire balloon structural representation of balloon structure in this utility model；
Fig. 2 is the enlarged diagram of border circular areas in Fig. 1.
In figure, the implication of each reference is as follows: 1 is fire balloon sacculus, and 2 is tight weave (that is, sacculus base material), and 3 is heat build-up
Layer (that is, titania coating or silica coating).
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing and enforcement
Example, is further elaborated to this utility model.Should be appreciated that specific embodiment described herein is only in order to explain
This utility model, is not used to limit this utility model.Additionally, institute in each embodiment of this utility model disclosed below
Just can be mutually combined as long as the technical characteristic related to does not constitutes conflict each other.
Embodiment 1 uses titanium oxide layer as the coating being attached on sacculus substrate layer
For the balloon structure of fire balloon in the present embodiment, include sacculus substrate layer from bottom to top and be attached to this sacculus base
Coating in sheet material layers；The thickness of sacculus substrate layer is 0.05mm～0.25mm, can be woven dacron or polyamide fabric；The thickness of coating
Degree is 2 μm～50 μm, uses titanium oxide layer as coating in the present embodiment 1.Titania coating can be by by titanium oxide powder
Mix (can additionally add water) with conventional adhesive and form glue, and glue is coated in the surface of sacculus base material (such as woven dacron)
(by utilizing the existing coating methods such as spraying), i.e. obtains titania coating after solidification.
Titania coating in this embodiment 1 can also substitute with silica coating, and the thickness of coating can keep consistent.
Embodiment 2 uses the composite coating of titanium oxide/silicon oxide as the coating being attached on sacculus substrate layer
It is that 10:30:30:50 prepares compound prescription by polyurethane adhesive, titanium oxide powder, silica powder, propanol mass ratio
Glue, assists in preparation with supersonic oscillations, electromagnetic agitation heating function, makes composite glue solution mix homogeneously, and temperature controls 60
Preheat near DEG C.
In 100 DEG C～200 DEG C high-temperature services of temperature, nitrogen protection (nitrogen oxygen content 50ppm) under the conditions of with vertical oneself
Dynamic spray gun is cold dry to lowering the temperature after the terylene/chinlon tight weave even application 10 seconds after compound prescription glue cleaning being processed, spraying
After terylene/chinlon tight weave enter at temperature 20 DEG C～100 DEG C roller devices extruding, roller pressure be 0.1MPa～
0.6MPa.Terylene/chinlon tight weave is cooled to room temperature afterwards, and seam is made into fire balloon sacculus.
Composite glue solution in embodiment 2 can also use other proportionings, if polyurethane adhesive, titanium oxide, silicon oxide and third
The mass ratio of alcohol meets 10:(30～60): (30～60): (40～90)；The grain diameter of titanium oxide can be in 0.5 μm～20 μm
Distribution, the grain diameter of silicon oxide can be distributed in 0.1 μm～10 μm；The thickness of the composite coating of the titanium oxide/silicon oxide formed
Degree can be in 2 μm～50 μm, and accordingly, composite glue solution spray time under high temperature (i.e. 100 DEG C～200 DEG C) can also be flexible
Adjusting, spray time can be 5 seconds～50 seconds.
Through test analysis, the heat loss rate of above balloon structure more originally have dropped more than 25% and (surveyed under normal temperature and pressure
Trying certain former polyamide fabric thermal protection rate is about 55%, use same type, same thickness polyamide fabric as sacculus base material, through this reality
It is up to 85% by novel coating cloth heat build-up sacculus thermal protection rate), fire balloon heat utilization rate significantly improves.
As it will be easily appreciated by one skilled in the art that and the foregoing is only preferred embodiment of the present utility model, not
In order to limit this utility model, all any amendment, equivalents made within spirit of the present utility model and principle and changing
Enter, within should be included in protection domain of the present utility model.
Claims (2)
1. the balloon structure for fire balloon, it is characterised in that this balloon structure includes sacculus substrate layer and is attached to this
Coating on sacculus substrate layer；The thickness of described sacculus substrate layer is 0.05mm～0.25mm；The thickness of described coating be 2 μm～
50μm；
Described coating is titanium oxide layer or silicon oxide layer.
2. as claimed in claim 1 for the balloon structure of fire balloon, it is characterised in that described sacculus substrate layer be woven dacron or
Polyamide fabric.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620503927.1U CN205688264U (en) | 2016-05-27 | 2016-05-27 | A kind of balloon structure for fire balloon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620503927.1U CN205688264U (en) | 2016-05-27 | 2016-05-27 | A kind of balloon structure for fire balloon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205688264U true CN205688264U (en) | 2016-11-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620503927.1U Active CN205688264U (en) | 2016-05-27 | 2016-05-27 | A kind of balloon structure for fire balloon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205688264U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107419548A (en) * | 2017-09-18 | 2017-12-01 | 北京莱斯达电子科技股份有限公司 | A kind of ball lamp cloth |
-
2016
- 2016-05-27 CN CN201620503927.1U patent/CN205688264U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107419548A (en) * | 2017-09-18 | 2017-12-01 | 北京莱斯达电子科技股份有限公司 | A kind of ball lamp cloth |
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| GR01 | Patent grant |