CN213841913U - Non-combustion gasification expanded propelling device - Google Patents
Non-combustion gasification expanded propelling device Download PDFInfo
- Publication number
- CN213841913U CN213841913U CN202022488929.7U CN202022488929U CN213841913U CN 213841913 U CN213841913 U CN 213841913U CN 202022488929 U CN202022488929 U CN 202022488929U CN 213841913 U CN213841913 U CN 213841913U
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- CN
- China
- Prior art keywords
- propeller main
- main part
- basket
- trigger
- reaction
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- 238000002309 gasification Methods 0.000 title claims abstract description 26
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 14
- 238000006243 chemical reaction Methods 0.000 claims abstract description 40
- 238000005422 blasting Methods 0.000 claims abstract description 27
- 238000007789 sealing Methods 0.000 claims abstract description 6
- 239000003153 chemical reaction reagent Substances 0.000 claims description 16
- 239000012528 membrane Substances 0.000 claims description 14
- 239000000376 reactant Substances 0.000 claims description 5
- 230000001960 triggered effect Effects 0.000 claims description 3
- 238000004880 explosion Methods 0.000 abstract description 5
- 235000014171 carbonated beverage Nutrition 0.000 description 11
- 239000007938 effervescent tablet Substances 0.000 description 9
- 239000007789 gas Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 6
- 239000002994 raw material Substances 0.000 description 5
- 239000000843 powder Substances 0.000 description 4
- 238000003860 storage Methods 0.000 description 4
- BVKZGUZCCUSVTD-UHFFFAOYSA-N carbonic acid Chemical compound OC(O)=O BVKZGUZCCUSVTD-UHFFFAOYSA-N 0.000 description 3
- KRKNYBCHXYNGOX-UHFFFAOYSA-N citric acid Chemical compound OC(=O)CC(O)(C(O)=O)CC(O)=O KRKNYBCHXYNGOX-UHFFFAOYSA-N 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- BVKZGUZCCUSVTD-UHFFFAOYSA-M Bicarbonate Chemical compound OC([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-M 0.000 description 2
- UIIMBOGNXHQVGW-UHFFFAOYSA-M Sodium bicarbonate Chemical compound [Na+].OC([O-])=O UIIMBOGNXHQVGW-UHFFFAOYSA-M 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 235000013305 food Nutrition 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 241000220479 Acacia Species 0.000 description 1
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 1
- 235000010643 Leucaena leucocephala Nutrition 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000008213 purified water Substances 0.000 description 1
- 238000006479 redox reaction Methods 0.000 description 1
- 229910000030 sodium bicarbonate Inorganic materials 0.000 description 1
- 235000017557 sodium bicarbonate Nutrition 0.000 description 1
- 230000003019 stabilising effect Effects 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 239000002912 waste gas Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Abstract
The utility model discloses a propelling device for non-combustion gasification expansion, which comprises a propeller main body and a triggering explosion device, wherein the propeller main body is connected with the triggering explosion device, a slidable triggering reaction device is arranged on the propeller main body, and the outer wall of the triggering explosion device is provided with an empennage; parameters of different use scenes can be optimized, and the pressure during blasting can be quantitatively controlled to prevent danger; the reaction propulsion efficiency can be increased on the premise of sealing, and the reaction device is convenient to store.
Description
Technical Field
The utility model relates to a advancing device especially relates to a non-combustion gasification expanded advancing device.
Background
The rocket is a propelling device which utilizes the reaction force of high-speed backward jet hot air generated by violent oxidation-reduction reaction to move forward; the initial rocket is mainly used for military use, so that various warheads are carried by the rocket, and the stability of the flight attitude of the rocket is controlled by a tail fin stabilizing device; because the rocket is cheap and has a long range, the limitation of the terrain is easily overcome. In the existing rocket, a combustion chamber is replaced by a gasification chamber filled with non-combustible gas, and the purpose of propulsion is achieved by utilizing high-pressure gas to do work through expansion; however, the adopted reaction raw materials are difficult to obtain, the reaction emission causes pollution to the environment, the gas pressure can not be changed according to scenes, the pressure during blasting can not be controlled during gasification, danger can be generated sometimes, and the storage is inconvenient.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to solve the technical problem who exists among the prior art, provide an expanding advancing device of non-combustion gasification.
In order to achieve the above purpose, the utility model provides a technical scheme is: the utility model provides a non-combustion gasification expanded advancing device, includes propeller main part and triggers the blasting unit, be provided with the reaction unit that triggers in the propeller main part, propeller main part upper end is provided with sealed lid, propeller main part lower extreme is provided with the rubber membrane, it includes gasification adjusting module to trigger the blasting unit, propeller main part lower extreme passes through rubber membrane and gasification adjusting module interval, it is provided with the fin to trigger the blasting unit outer wall.
Preferably, the triggered reaction device comprises a reagent basket, the reagent basket is coaxial with the thruster main body, an inner permanent magnet is arranged at the inner side of the wall of the reagent basket, and an outer permanent magnet matched with the inner permanent magnet is arranged outside the wall of the thruster main body.
Preferably, the reagent basket is annular, and the diameter of the reagent basket is smaller than that of the inner wall of the propeller main body.
Preferably, the triggering explosion device comprises a cylinder shell, the gasification adjusting module comprises a cross support bottom, the cross support bottom is connected with the cylinder shell, a buckle is arranged on the outer wall of an upper port of the cylinder shell and matched with a clamping sleeve on the propeller main body to connect the triggering explosion device with the propeller main body, and a support leg is fixed on a lower port of the cylinder shell.
Preferably, a threaded hole is formed in the center of the cross support bottom, a screw needle is arranged on the threaded hole, a spring clamping groove is formed in the center of the cross support bottom, one end of the spring is connected with the spring clamping groove, and the other end of the spring is connected with the central perforated plate.
Preferably, the sealing cover is in a spiral bullet shape.
The utility model discloses beneficial effect: the adopted reaction raw materials are easy to obtain, common foods in life such as carbonated beverages, effervescent tablets, mantou and the like can be selected, and the reaction effluent hardly pollutes the environment, so that the method has the advantages of simplicity, environmental protection, low maintenance cost, low material requirement, high safety and the like; meanwhile, the gasification adjusting module can adjust the pressure through the needle position so as to optimize parameters of different use scenes, and the rubber film can quantitatively control the pressure during blasting to prevent danger; the reaction propulsion efficiency can be increased on the premise of sealing, and the reaction device is convenient to store.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic cross-sectional view of a trigger reaction device according to the present invention;
fig. 3 is a schematic view of the triggered blasting device of the present invention;
fig. 4 is a schematic plan view of the cross-shaped bottom support of the present invention.
Description of the reference numerals
1-propeller main body 2-trigger reaction device 3-trigger blasting device 4-empennage 5-sealing cover 6-working medium injection opening 7-rubber membrane 8-snap ring 9-cutting ferrule 10-reactant basket 11-inner permanent magnet 12-outer permanent magnet 13-snap ring 14-center perforated plate 15-spring 16-cross support bottom 17-screw rod needle 18-cylinder shell 19-support leg 20-threaded hole 21-spring clamping groove.
Detailed Description
This section will describe in detail the embodiments of the present invention, preferred embodiments of the present invention are shown in the attached drawings, which are used to supplement the description of the text part of the specification with figures, so that one can intuitively and vividly understand each technical feature and the whole technical solution of the present invention, but they cannot be understood as the limitation of the protection scope of the present invention.
In the description of the present invention, it should be understood that the orientation or positional relationship indicated with respect to the orientation description, such as up, down, front, rear, left, right, etc., is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
In the description of the present invention, a plurality of means are one or more, a plurality of means are two or more, and the terms greater than, less than, exceeding, etc. are understood as not including the number, and the terms greater than, less than, within, etc. are understood as including the number. If the first and second are described for the purpose of distinguishing technical features, they are not to be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated or implicitly indicating the precedence of the technical features indicated.
In the description of the present invention, unless there is an explicit limitation, the words such as setting, installation, connection, etc. should be understood in a broad sense, and those skilled in the art can reasonably determine the specific meanings of the above words in combination with the specific contents of the technical solution.
Referring to fig. 1-4, the preferred embodiment of the utility model, a non-combustion gasification expanded advancing device, including propeller main part 1 and trigger blasting unit 3, propeller main part 1 with trigger blasting unit 3 and pass through cutting ferrule 9 and buckle 8 and be connected, be provided with on the propeller main part 1 and trigger reaction unit 2, 1 upper end of propeller main part is provided with working medium filling opening 6, working medium filling opening 6 is provided with sealed lid 5, 1 lower extreme of propeller main part is provided with rubber membrane 7, trigger blasting unit 3 and include gasification adjusting module, 1 lower extreme of propeller main part passes through rubber membrane 7 and gasification adjusting module interval, it is provided with fin 4 to trigger 3 outer walls of blasting unit.
The reaction raw materials adopted in the utility model are easy to obtain, common foods in life such as carbonated beverage, effervescent tablets, Mantussi and the like can be selected, and the reaction discharge hardly pollutes the environment, thus having the advantages of simplicity, environmental protection, low maintenance cost, low requirement on materials, high safety and the like; meanwhile, the gasification adjusting module can adjust the pressure through the needle position so as to optimize parameters of different use scenes, and the rubber film 7 at the lower end of the propeller main body 1 can quantitatively control the pressure during blasting to prevent danger; the utility model discloses raw materials in well triggering formula reaction unit 2 can increase reaction propulsion efficiency under sealed lid 5 is sealed, also convenient storage, fin 4 can also be the stability of stabilising arrangement control flight gesture
In this embodiment, the triggering reaction apparatus 2 includes a reagent basket 10, the reagent basket 10 is coaxial with the propeller main body 1, an inner permanent magnet 11 is disposed at an inner side of a wall of the reagent basket 10, an outer permanent magnet 12 matched with the inner permanent magnet 11 is disposed outside a wall of the propeller main body 1, after the reagent basket 10 is placed in the reaction material, a position of the reagent basket 10 can be controlled by controlling the outer permanent magnet 12 outside the wall of the propeller main body 1, so as to facilitate control of a reaction for generating gas, carbonated beverage reaction materials generally disposed in the propeller main body 1 generally adopt effervescent tablet powder and mantou fragment, and when the carbonated beverage reaction materials are required to be used, the outer permanent magnet 12 controls the reagent basket 10 to be immersed in the carbonated beverage with the powder, so as to trigger the reaction. When the effervescent tablet is put into water, the following reaction occurs due to the main components of the effervescent tablet, namely citric acid and baking soda:
H++CO3 2-＝＝HCO3 2-
H++HCO3 2-＝＝H2CO3
H2CO3＝＝CO2(g)+H2O
carbonated beverage, effervescent tablet, mantoux and the like, and reaction discharge almost has no pollution to the environment, is concise and environment-friendly, has low requirements on materials, and has higher safety; the carbonated beverage contains certain amount of carbonic acid and other acids, and can promote reaction, and the Mantussi contains acacia, etc., and can reduce surface tension of liquid and CO2DissolutionAnd the reaction is accelerated to compress the gas in the closed container.
In this embodiment, the reagent basket 10 is annular, and the diameter of the reagent basket 10 is smaller than the diameter of the inner wall of the thruster main body 1, so that the reagent basket 10 can slide in the thruster main body 1, and the reaction can be controlled more conveniently.
In this embodiment, trigger blasting unit 3 still includes drum shell 18, 16 is held in the palm at the bottom of the gasification governing module includes the cross, 16 with 16 are connected at the bottom of the cross support, the last port outer wall of drum shell 18 is equipped with buckle 13, the lower port of drum shell 18 is fixed with stabilizer blade 19, the inside fluid of propeller main part 1 is under huge pressure, through triggering 3 bottom blowout of blasting unit, the reaction force that triggers blasting unit 3 is used for providing the power of propeller main part 1, makes propeller main part 1 impel forward, trigger blasting unit 3 pass through buckle 13 with propeller main part 1 is connected, makes the device dismantle convenient, succinct practical.
In this embodiment, a threaded hole 20 is formed in the center of the cross support base 16, a screw pin 17 is arranged on the threaded hole 20, a spring clamping groove 21 is formed in the center of the cross support base 16, one end of the spring 15 is connected with the spring clamping groove 21, the other end of the spring 15 is connected with the central perforated plate 14, the spring 15 is compressed, the pressure of the spring 15 is in direct proportion to the compression length of the spring 15, and the spring can be used for controlling the pressure during blasting in a fixed amount. Meanwhile, the pressure can be adjusted through the needle position of the screw needle 17 so as to optimize the parameters of different use scenes.
In this embodiment, sealed lid 5 is spiral warhead form, can reduce the resistance when flying, sealed lid 5 passes through threaded connection on propeller main part 1, can guarantee that the gas that the reaction produced does not leak, can increase reaction propulsion efficiency, convenient storage under the sealed condition simultaneously. On the premise of ensuring sealing, attention is paid that liquid cannot contact with the powder, the aim of long-term storage can be achieved, even if gas in the carbonated beverage is lost to a certain extent, the excessive effervescent tablet powder can sufficiently support gas generation, so that if the carbonated beverage needs to be stored for a long time, the carbonated beverage can be replaced by purified water and the excessive effervescent tablets are matched.
The utility model discloses a theory of operation: put the required raw materials of reaction in advance in propeller main part 1 and the reactant basket 10, through going on of outer permanent magnet 12 control reaction, along with the reaction goes on, the atmospheric pressure crescent in the trigger formula reaction unit 2, and the pressure of placing the rubber membrane 7 upper surface in propeller main part 1 bottom is showing to be greater than atmospheric pressure, and rubber membrane 7 expands downwards. Because a spring 15 is connected below the rubber membrane 7 through a central perforated plate 14, after the rubber membrane 7 expands, the spring 15 compresses, the pressure of the spring 15 is in direct proportion to the compression length of the spring 15, and the method can be used for quantitatively controlling the pressure during blasting. When the pressure reaches a certain value, the spring 15 is compressed below the height of the tip of the screw needle 17, the tip punctures the rubber membrane 7 through the central perforated plate 14, and the rubber membrane 7 is broken. The internal fluid is sprayed out from the bottom of the triggering blasting device 3 under huge pressure, and the reaction force of the triggering blasting device 3 provides the power of the propeller main body 1, so that the propeller main body 1 is sprayed out for a certain distance forwards.
The utility model discloses a propulsion calculation of concrete implementation case as follows: because the utility model discloses the example has adopted the mixture commonly used in the life, is difficult to obtain the proportion of its specific each component, through the actual measurement, adopts a certain brand effervescent tablet of 720g, and 100g mantoux reacts with 17L carbonated beverage, and the atmospheric pressure of production is about 5atm in 3L cavity. Under the condition, the total mass of the waste gas and the waste liquid in the used model is about 17.8kg, the mass of the other parts is about 200g, and the cross section area of a working medium outlet wrapped by the rubber membrane in the used model is about 32cm through calculation2And 1600N thrust can be generated at the moment of blasting. In an ideal state, the temperature of the working medium is almost unchanged before and after injection, and if the compressed gas expands to apply work and completely provides kinetic energy of the propeller and the fluid, the small heat engine can theoretically propel about 14m upwards vertically and fly farther in the horizontal direction under the condition of neglecting the air resistance effect. The actual propulsion is about 10 m.
The above additional technical features can be freely combined and used in superposition by those skilled in the art without conflict.
The above is only the preferred embodiment of the present invention, as long as the technical solution of the purpose of the present invention is realized by the substantially same means, all belong to the protection scope of the present invention.
Claims (6)
1. A non-combustion gasification expanded propulsion device, characterized in that: including propeller main part (1) and trigger blasting unit (3), propeller main part (1) with trigger blasting unit (3) are connected, be provided with on propeller main part (1) and trigger reaction unit (2), propeller main part (1) upper end is provided with sealed lid (5), propeller main part (1) lower extreme is provided with rubber membrane (7), trigger blasting unit (3) are including gasification adjusting module, propeller main part (1) lower extreme passes through rubber membrane (7) and gasification adjusting module interval, trigger blasting unit (3) outer wall is provided with fin (4).
2. A non-combustion gasification expansion propulsion device according to claim 1, characterized in that: the triggering reaction device (2) comprises a reactant basket (10), wherein the reactant basket (10) is coaxial with the propeller main body (1), an inner permanent magnet (11) is arranged on the inner side of the wall of the reactant basket (10), and an outer permanent magnet (12) matched with the inner permanent magnet is arranged outside the wall of the propeller main body (1).
3. A non-combustion gasification expansion propulsion device according to claim 2, characterized in that: the reagent basket (10) is annular, and the diameter of the reagent basket (10) is smaller than that of the inner wall of the propeller main body (1).
4. A non-combustion gasification expansion propulsion device according to claim 1, characterized in that: the triggered blasting device (3) further comprises a cylinder shell (18), the gasification adjusting module comprises a cross support bottom (16), the cross support bottom (16) is connected with the cylinder shell (18), a buckle (13) is arranged on the outer wall of an upper port of the cylinder shell (18), and a support leg (19) is fixed on a lower port of the cylinder shell (18).
5. A non-combustion gasification expansion propulsion device according to claim 4, characterized in that: the cross support base (16) is provided with a threaded hole (20) in the center, a screw needle (17) is arranged on the threaded hole (20), a spring clamping groove (21) is formed in the center of the cross support base (16), one end of a spring (15) is connected with the spring clamping groove (21), and the other end of the spring (15) is connected with a central perforated plate (14).
6. A non-combustion gasification expansion propulsion device according to claim 1, characterized in that: the sealing cover (5) is in a spiral bullet shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022488929.7U CN213841913U (en) | 2020-11-02 | 2020-11-02 | Non-combustion gasification expanded propelling device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022488929.7U CN213841913U (en) | 2020-11-02 | 2020-11-02 | Non-combustion gasification expanded propelling device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213841913U true CN213841913U (en) | 2021-07-30 |
Family
ID=77012876
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022488929.7U Expired - Fee Related CN213841913U (en) | 2020-11-02 | 2020-11-02 | Non-combustion gasification expanded propelling device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213841913U (en) |
-
2020
- 2020-11-02 CN CN202022488929.7U patent/CN213841913U/en not_active Expired - Fee Related
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| 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: 20210730 |