CN113581629A - Aircraft anti-collision box based on air bag extrusion - Google Patents
Aircraft anti-collision box based on air bag extrusion Download PDFInfo
- Publication number
- CN113581629A CN113581629A CN202110736664.4A CN202110736664A CN113581629A CN 113581629 A CN113581629 A CN 113581629A CN 202110736664 A CN202110736664 A CN 202110736664A CN 113581629 A CN113581629 A CN 113581629A
- Authority
- CN
- China
- Prior art keywords
- anticollision
- gasbag
- aviation
- base
- case
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/20—External fittings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/38—Devices for discharging contents
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/02—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
- B65D81/05—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D81/00—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
- B65D81/18—Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents providing specific environment for contents, e.g. temperature above or below ambient
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D3/00—Devices using other cold materials; Devices using cold-storage bodies
- F25D3/02—Devices using other cold materials; Devices using cold-storage bodies using ice, e.g. ice-boxes
- F25D3/06—Movable containers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
Abstract
The invention discloses an aircraft anti-collision box based on air bag extrusion, and relates to the technical field of aircraft. This aircraft anticollision case based on gasbag extrusion carries out the aviation anticollision institution of anticollision including being used for the aviation, be used for utilizing the gasbag to carry out extruded gasbag extrusion mechanism and be used for water smoke to carry out the water smoke that gives off and give off the mechanism, aviation anticollision institution's inside is provided with the anticollision case, aviation anticollision institution is provided with gasbag extrusion mechanism through the anticollision incasement portion that sets up. This aircraft anticollision case based on gasbag extrusion when receiving outside extrusion through first gasbag, the air current velocity of flow through the bell is slower, so the air enters into the second gasbag after the compression, and after the air discharge of compression, compressed air gets back to the ordinary pressure after breaking away from high-pressure environment, can expand and externally do work and absorb heat simultaneously to make the inside cooling of second gasbag, thereby slowed down the speed that melts of ice-cube.
Description
Technical Field
The invention relates to the technical field of aircrafts, in particular to an aircraft anti-collision box based on air bag extrusion.
Background
The aviation case is a novel packaging product which is produced by replacing transportation and aims at solving the defects that the traditional simple wooden case packaging transportation can not solve the problems that high-tech products and materials can not be effectively protected in the long-distance transportation process and the maneuverability is poor; some materials require refrigerated storage during transport.
During transport, the ice pieces in the aircraft tank are constantly impacted due to the jolt of the aircraft, which accelerates the melting of the ice pieces and causes damage to the interior materials.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention provides the aircraft crash box based on air bag extrusion, which buffers the collision of ice blocks through the extrusion of the air bags, and ensures the preservation of the ice blocks.
In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides an airborne vehicle anticollision case based on gasbag extrusion, carries out the aviation anticollision institution of anticollision including being used for the aviation, is used for utilizing the gasbag to carry out extruded gasbag extrusion mechanism and is used for water smoke to carry out the water smoke that gives off and gives off the mechanism, aviation anticollision institution's inside is provided with the anticollision case, aviation anticollision institution is provided with gasbag extrusion mechanism through the anticollision incasement portion that sets up, aviation anticollision institution is provided with water smoke through the anticollision bottom of the case portion that sets up and gives off the mechanism.
Preferably, aviation anticollision institution's inside includes anticollision case, top cap and base, the top of anticollision case articulates there is the top cap, the bottom of anticollision case is provided with the base, the base level setting that the anticollision case passes through the setting.
Preferably, an interlayer is arranged around the inside of the anti-collision box, a groove is formed in the axis of the base, a plurality of vent holes are formed in the inside of the base, and the vent holes are communicated with the groove of the base.
Preferably, the inside of gasbag extrusion mechanism includes first gasbag, second gasbag and bell, four holes have been seted up on the four sides of anticollision case, second gasbag fixed connection is located the position in hole at the anticollision incasement wall, first gasbag fixed connection is located the position in hole at the anticollision incasement wall, in the anticollision incasement hole and be located fixedly connected with bell between first gasbag and the second gasbag.
Preferably, the inside that the water smoke distributes the mechanism includes leaking mouth, hob and chassis, anticollision bottom of the case portion and the position fixedly connected with chassis that is located the base top, the outer wall fixedly connected with hob on chassis, the bottom of hob and the top movable contact of base, a plurality of leaking mouth has been seted up to the outer lane that the chassis was kept away from to anticollision bottom of the case portion.
Preferably, the bottom of the chassis is fixedly connected with a rotating wheel, the chassis is in movable contact with the groove of the base through the rotating wheel, the bottom of the chassis is fixedly connected with a friction ball, the groove of the base is fixedly connected with a friction block, the friction ball is in movable contact with the friction block, and the friction ball and the friction block are made of friction heat generating materials.
The invention provides an aircraft crash box based on airbag extrusion. The method has the following beneficial effects:
1. this aircraft anticollision case based on gasbag extrusion, the air through first gasbag and second gasbag removes and elastic material's setting, can cushion the ice-cube to the damage of ice-cube has been avoided.
2. This aircraft anticollision case based on gasbag extrusion through the setting of leaking the mouth, can make the water droplet that drips on the ice-cube draw off to slow down the melting speed of ice-cube.
3. This aircraft anticollision case based on gasbag extrusion takes place rotatoryly after the inflation through the anticollision case to make the rise of anticollision case take the altitude under the elasticity of hob, the water evaporation of base inslot has been ensured to the friction striking dynamics of increase friction ball and clutch blocks, when steam removed the intermediate layer of anticollision case, ensured thermal sheltering from with inside heat dissipation.
4. This aircraft anticollision case based on gasbag extrusion when receiving outside extrusion through first gasbag, the air current velocity of flow through the bell is slower, so the air enters into the second gasbag after the compression, and after the air discharge of compression, compressed air gets back to the ordinary pressure after breaking away from high-pressure environment, can expand and externally do work and absorb heat simultaneously to make the inside cooling of second gasbag, thereby slowed down the speed that melts of ice-cube.
Drawings
FIG. 1 is a schematic axial side perspective view of the present invention;
FIG. 2 is a schematic cross-sectional view of FIG. 1 according to the present invention;
FIG. 3 is an enlarged view of portion A of FIG. 2 according to the present invention;
FIG. 4 is an enlarged view of the portion B of FIG. 2 according to the present invention.
In the figure: 1. an aviation anti-collision mechanism; 11. an anti-collision box; 12. a top cover; 13. a base; 14. a vent hole; 15. an interlayer; 2. an air bag extrusion mechanism; 21. a first air bag; 22. a second air bag; 23. a tapered mouth; 3. a water mist emission mechanism; 31. a water leakage port; 32. a screw rod; 33. a chassis; 34. a friction ball; 35. a friction block.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an aviation aircraft anticollision case based on gasbag extrusion, carries out crashproof aviation anticollision institution 1 including being used for the aviation, is used for utilizing the gasbag to carry out extruded gasbag extrusion mechanism 2 and is used for water smoke to carry out the water smoke that gives off and gives off mechanism 3, and aviation anticollision institution 1's inside is provided with crashproof case 11, and aviation anticollision institution 1 is provided with gasbag extrusion mechanism 2 through the crashproof case 11 inside that sets up, and aviation anticollision institution 1 is provided with water smoke through the crashproof case 11 bottom that sets up and gives off mechanism 3.
In this embodiment, the handle is mounted on the top of the top cover 12, so that the top cover 12 can be opened conveniently.
Specifically, aviation anticollision institution 1's inside includes anticollision case 11, top cap 12 and base 13, and the top of anticollision case 11 articulates there is top cap 12, and the bottom of anticollision case 11 is provided with base 13, and anticollision case 11 sets up through the base 13 level that sets up.
In this embodiment, the first airbag 21 performs cushion when colliding with another device.
Specifically, the interlayer 15 is arranged around the inside of the anti-collision box 11, the axis of the base 13 is provided with a groove, the inside of the base 13 is provided with a plurality of vent holes 14, and the vent holes 14 are communicated with the groove of the base 13.
In this embodiment, the ice cubes inside the crash box 11 are slightly smaller than the internal volume of the crash box 11.
Specifically, four holes have been seted up including first gasbag 21, second gasbag 22 and bell 23 in gasbag extrusion mechanism 2's inside, four sides of anticollision case 11, and second gasbag 22 fixed connection is located the position in hole at anticollision 11 inner walls, and first gasbag 21 fixed connection is located the position in hole at anticollision 11 outer walls, and anticollision 11 is downthehole and be located fixedly connected with bell 23 between first gasbag 21 and the second gasbag 22.
In this embodiment, the bottom of the base 13 is provided with a buckle, and the base can be mounted on an aircraft.
Specifically, the inside of mechanism 3 is gived off to water smoke includes leaking mouth 31, hob 32 and chassis 33, and the 11 bottoms of anticollision case just is located the position fixedly connected with chassis 33 at 13 tops of base, and the outer wall fixedly connected with hob 32 of chassis 33, the bottom of hob 32 and the top movable contact of base 13, and a plurality of leaks mouth 31 has been seted up to the outer lane of chassis 33 is kept away from to 11 bottoms of anticollision case.
In this embodiment, the second bladder 22 cushions the ice cubes that are shaken.
Specifically, the bottom of the chassis 33 is fixedly connected with a rotating wheel, the chassis 33 is in movable contact with the groove of the base 13 through the rotating wheel, the bottom of the chassis 33 is fixedly connected with a friction ball 34, the groove of the base 13 is fixedly connected with a friction block 35, and the friction ball 34 is in movable contact with the friction block 35.
In this embodiment, the friction ball 34 and the friction block 35 are made of friction heat generating material.
When in use, the top cover 12 on the crash box 11 is opened, the frozen material is put into the crash box 11, when bumping is encountered in the transportation process of the aircraft, the crash box 11 drives the crash box 11 to shake under the inertia of the internal material and ice cubes, when the first air bag 21 on the crash box 11 collides with other devices, the first air bag 21 performs buffering collision, the internal ice cubes and the material perform buffering on the collision of the second air bag 22, when the first air bag 21 is collided, the hole facing the cone-shaped opening 23 is small, so that the air flow passes slowly, the first air bag 21 extrudes the air in the first air bag 21, the air flow generates heat in the extrusion process, after passing through the cone-shaped opening 23, the second air bag 22 is expanded to enter the compressed air in the second air bag 22, after the compressed air is discharged, the compressed air returns to the normal pressure after being separated from the high-pressure environment, will expand to do work externally and absorb heat at the same time, thereby reducing the temperature inside the second air bag 22, making the ice blocks not easy to melt, when the second airbag 22 is compressed by the ice inside the crash box 11, the hole of the tapered mouth 23 on the side of the second airbag 22 is large, the air flow easily passes, the ice cubes inside the crash box 11 drop water drops after melting, the water drops flow into the groove of the base 13 through the drain opening 31, when the first air bag 21 is collided, the crash box 11 can rotate under the action of the rotating wheels at the bottom of the chassis 33, the crash box 11 drives the screw rod 32 to rotate, so that the crash box 11 is jacked up by the screw rod 32 with certain elasticity, the friction ball 34 continuously strikes and rubs against the friction block 35, the bottom of the base 13 is contacted with the aircraft, so that heat is transferred to evaporate water in the groove of the base 13, and the evaporated water vapor is sent into the interlayer 15 through the vent holes 14, thereby having heat insulation and heat absorption effects on the crash box 11.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.
Claims (6)
1. The utility model provides an aircraft anticollision case based on gasbag extrusion, is including aviation anticollision institution (1) that is used for the aviation to carry out the anticollision, is used for utilizing the gasbag to carry out the gasbag extrusion mechanism (2) that extrudees and is used for the water smoke to carry out the water smoke that gives off and gives off mechanism (3), its characterized in that: the aviation anticollision institution is characterized in that an anticollision box (11) is arranged inside the aviation anticollision institution (1), an airbag extrusion mechanism (2) is arranged inside the aviation anticollision institution (1) through the arranged anticollision box (11), and a water mist emission mechanism (3) is arranged at the bottom of the aviation anticollision institution (1) through the arranged anticollision box (11).
2. An air bag crash box based aircraft according to claim 1, characterised in that: the aviation anticollision institution (1) is characterized in that the interior of the aviation anticollision institution (1) comprises an anticollision box (11), a top cover (12) and a base (13), the top of the anticollision box (11) is hinged to the top cover (12), the base (13) is arranged at the bottom of the anticollision box (11), and the anticollision box (11) is horizontally arranged through the base (13).
3. An air bag crash box based aircraft crash box according to claim 2, characterized in that: interlayer (15) have been seted up around the inside of anticollision case (11), the axle center department of base (13) has seted up slottedly, a plurality of air vent (14) have been seted up to the inside of base (13), air vent (14) all communicate with each other with the groove of base (13).
4. An air bag crash box based aircraft according to claim 1, characterised in that: the inside of gasbag extrusion mechanism (2) includes first gasbag (21), second gasbag (22) and bell (23), four holes have been seted up on the four sides of anticollision case (11), second gasbag (22) fixed connection is located the position in hole at anticollision case (11) inner wall, first gasbag (21) fixed connection is located the position in hole at anticollision case (11) outer wall, anticollision case (11) are downthehole and be located fixedly connected with bell (23) between first gasbag (21) and second gasbag (22).
5. An air bag crash box based aircraft crash box according to claim 2, characterized in that: the inside of water smoke emission mechanism (3) is including leaking mouth (31), hob (32) and chassis (33), crashproof case (11) bottom and the position fixedly connected with chassis (33) that is located base (13) top, the outer wall fixedly connected with hob (32) on chassis (33), the bottom of hob (32) and the top movable contact of base (13), a plurality of leaks mouth (31) have been seted up to the outer lane of chassis (33) is kept away from to crashproof case (11) bottom.
6. An air bag crash box based aircraft according to claim 5, characterised in that: the bottom fixedly connected with of chassis (33) rotates the wheel, chassis (33) are through the rotation wheel that sets up and the inslot swing joint of base (13), the bottom fixedly connected with friction ball (34) on chassis (33), the inslot fixedly connected with friction block (35) of base (13), friction ball (34) and friction block (35) swing joint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110736664.4A CN113581629A (en) | 2021-06-30 | 2021-06-30 | Aircraft anti-collision box based on air bag extrusion |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110736664.4A CN113581629A (en) | 2021-06-30 | 2021-06-30 | Aircraft anti-collision box based on air bag extrusion |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113581629A true CN113581629A (en) | 2021-11-02 |
Family
ID=78245350
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110736664.4A Withdrawn CN113581629A (en) | 2021-06-30 | 2021-06-30 | Aircraft anti-collision box based on air bag extrusion |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113581629A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114859741A (en) * | 2022-04-26 | 2022-08-05 | 海安方好家具有限公司 | Control device for micro-heating efficient demisting smart home |
| CN116130863A (en) * | 2022-12-28 | 2023-05-16 | 江苏河马自动化设备有限公司 | Low-power consumption battery box fire alarm controller |
-
2021
- 2021-06-30 CN CN202110736664.4A patent/CN113581629A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114859741A (en) * | 2022-04-26 | 2022-08-05 | 海安方好家具有限公司 | Control device for micro-heating efficient demisting smart home |
| CN114859741B (en) * | 2022-04-26 | 2024-01-12 | 杭州绿城橱柜有限公司 | Control device of micro-heating efficient demisting intelligent home |
| CN116130863A (en) * | 2022-12-28 | 2023-05-16 | 江苏河马自动化设备有限公司 | Low-power consumption battery box fire alarm controller |
| CN116130863B (en) * | 2022-12-28 | 2024-03-26 | 南京睿实智能安全科技有限公司 | Low-power consumption battery box fire alarm controller |
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| PB01 | Publication | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20211102 |
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| WW01 | Invention patent application withdrawn after publication |