CN210101999U - Unmanned aerial vehicle high altitude drop protection device - Google Patents
Unmanned aerial vehicle high altitude drop protection device Download PDFInfo
- Publication number
- CN210101999U CN210101999U CN201920938876.9U CN201920938876U CN210101999U CN 210101999 U CN210101999 U CN 210101999U CN 201920938876 U CN201920938876 U CN 201920938876U CN 210101999 U CN210101999 U CN 210101999U
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- aerial vehicle
- unmanned aerial
- shell
- high altitude
- protection device
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Abstract
The utility model discloses a protection device is put in unmanned aerial vehicle high altitude, include the casing and put the thing cavity by what this casing surrounded, the casing includes the supporting layer outer wall parcel has outer buffer layer the supporting layer inner wall covers there is interior buffer layer be provided with the area on the casing and seal the putting of mechanism and put the thing mouth. Has the advantages that: the multilayer protective layer is arranged, so that the material put in the storage cavity is effectively protected. The collision deformation is little, and the buffering dynamics is big, sets up to different environment is reasonable, and the good reliability.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle high altitude transportation technique and specifically relates to an unmanned aerial vehicle high altitude is put in protection device.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle is applied to industries such as city management, agriculture, geology, meteorology, electric power, emergency rescue and disaster relief, video shooting, express delivery, military police and the like.
The system is widely used in the field of express delivery. For example for the administration of drugs or emergency supplies. When being attacked by the viper outdoors, when medicines such as serum need to be transported urgently, the unmanned aerial vehicle can be put in, the treatment time is shortened, and the harm to the patient is reduced. Because unmanned aerial vehicle is fit for flying in spacious space, to the space that the environment is complicated, can only take the high altitude to put in, however, put in the high altitude and cause the material to damage easily, cause the property loss. And objects falling from high altitude are liable to cause serious injury to people or animals. Extremely dangerous, factor of safety is low, can not satisfy people's demand.
SUMMERY OF THE UTILITY MODEL
In order to solve the problem, the utility model provides an unmanned aerial vehicle high altitude is put in protection device, safe, reliable carries out collision buffer protection to the high altitude whereabouts thing, effectively prevents to cause the injury to the whereabouts thing.
In order to achieve the above purpose, the utility model adopts the following specific technical scheme:
the utility model provides a protection device is put in unmanned aerial vehicle high altitude which the key lies in: the shell comprises a supporting layer, an outer buffer layer wraps the outer wall of the supporting layer, an inner buffer layer covers the inner wall of the supporting layer, and an object placing opening with a sealing mechanism is arranged on the shell.
Through above-mentioned design, set up the multilayer protection, at the in-process that falls, the shock attenuation is prevented falling, and when bumping, the casing realizes buffer protection. Unmanned aerial vehicle transportation reliability has been improved.
Further, the supporting layer is a frame structure;
the outer buffer layer is filled with gas or flexible materials or elastic materials;
the inner buffer layer is filled with gas or flexible materials or elastic materials.
By adopting the scheme, people can select different filling materials according to different putting sites, for example, the filling materials can be filled with gas in the outer protective layer and the inner protective layer on the sea, and when the putting is carried out on the sea, the whole shell can float on the sea. When the protective layer is thrown at a high altitude with hard geology, elastic materials or flexible materials can be adopted, so that the protective layer is prevented from being seriously deformed when collision occurs. Effectively protecting the materials.
Further, to protect the material to be fed, the thickness of the inner buffer layer is greater than the thickness of the outer buffer layer.
As described further below, the housing is divided into a first housing and a second housing by the storage opening, and the sealing mechanism is used to connect the first housing and the second housing.
According to the scheme, the shell is divided into two parts, so that the loading and the dismounting of the material are facilitated.
Further, when the outer protection layer is severely impacted, the support layer is a steel wire mesh woven by steel wires in order to protect the thrown materials. Form in the protective layer and prevent the deformation structure to the wire netting structure is firm, is difficult for taking place deformation, and the good reliability. And since the housing comprises a first housing and a second housing, the first housing and the second housing each comprise one support layer.
In a further description, at least one fixing hook is arranged on the cavity wall of the storage cavity, a fixing bandage is arranged on at least one fixing hook, and a fixing sleeve ring is arranged on the fixing bandage.
By adopting the scheme, the fixed hooks are matched with the fixed binding bands, so that the released materials can be fixed, and the released materials can be suspended. Fix and throw in the goods and materials, can prevent to throw in the goods and materials and roll in putting the thing cavity upset, cause to throw in the goods and materials damage. The suspended arrangement can reduce the collision force between the input materials and the wall of the storage cavity, thereby further protecting the input materials.
As described further, in order to prevent the fixing hook and the fixing band from damaging the thrown material, both the fixing hook and the fixing band are made of elastic materials.
As described further below, in order to facilitate transportation of the housing, at least one hanger is disposed on an outer surface of the housing.
Specifically, the shell is a spherical body or a square body.
As described further below, the surface of the housing is coated with a fluorescent layer.
By adopting the scheme, the materials thrown in high altitude are adopted, the throwing environment is complex, and the fluorescent layer is coated on the shell, so that the thrown materials can be searched at night.
The utility model has the advantages that: the multilayer protective layer is arranged, so that the material put in the storage cavity is effectively protected. Wherein prevent the deformation layer and can reduce the deformation degree that falls and collide the casing, further reduced the collision strength to the inner protective layer. Adopt fixed couple and fixing band to fix the input goods and materials in putting the thing cavity, increased the buffering dynamics of putting in the goods and materials, further protected again and put in the goods and materials. And aiming at different environments, the device is reasonably arranged and has good reliability.
Drawings
Fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a cross-sectional view of the spherical shell of the present invention;
FIG. 3 is a cross-sectional view of the square housing of the present invention;
FIG. 4 is a schematic view of the square structure of the present invention;
Detailed Description
The following provides a more detailed description of the embodiments and the operation of the present invention with reference to the accompanying drawings.
As can be seen from fig. 1, the high-altitude dropping protection device for the unmanned aerial vehicle comprises a shell 1 and a storage cavity 2 surrounded by the shell 1, wherein the shell 1 comprises a supporting layer 1a, an outer buffer layer 1b is wrapped on the outer wall of the supporting layer 1a, an inner buffer layer 1c is covered on the inner wall of the supporting layer 1a, and a storage opening with a sealing mechanism 3 is arranged on the shell 1.
Wherein the supporting layer 1a is a frame structure;
the outer buffer layer 1b is filled with gas or flexible materials or elastic materials;
the inner buffer layer 1c is filled with gas or flexible material or elastic material.
As can be seen from fig. 2 and 3, the outer buffer layer 1b is filled with a flexible material. And the inner buffer layer 1c is filled with a flexible material. The supporting layer 1a is of a steel frame structure and a steel wire mesh woven by steel wires.
In this embodiment, the thickness of the inner buffer layer 1c is greater than the thickness of the outer buffer layer 1 b.
As can be seen from fig. 2 and 3, 5 fixing hooks 4 are arranged on the cavity wall of the storage cavity 2, fixing bands 5 are arranged on the 2 fixing hooks 4, and fixing collars are arranged on the fixing bands 5. The fixing hook 4 and the fixing bandage 5 are made of elastic materials.
As can be seen from fig. 1-4, 2 hangers 6 are disposed on the outer surface of the housing 1.
As can be seen from fig. 1 and 2, the housing 1 is a spherical body
As can be seen from fig. 3 and 4, the housing 1 is a square body.
Preferably, the surface of the housing 1 is coated with a fluorescent layer.
The utility model discloses a theory of operation: put in the goods and materials and pack into putting the thing cavity 2 through sealing mechanism 3 to will put in the fixed even unsettled setting of goods and materials through fixed couple 4 and fixing bandage 5. After setting up, will put in goods and materials through sealing mechanism 3 and realize sealing to fix casing 1 on unmanned aerial vehicle through pendant 6, be convenient for put in.
Claims (10)
1. The utility model provides a protection device is put in unmanned aerial vehicle high altitude which characterized in that: the article placing cavity comprises a shell (1) and an article placing cavity (2) surrounded by the shell (1), wherein the shell (1) comprises a supporting layer (1a), an outer buffer layer (1b) wraps the outer wall of the supporting layer (1a), an inner buffer layer (1c) covers the inner wall of the supporting layer (1a), and an article placing opening with a sealing mechanism (3) is arranged on the shell (1).
2. The unmanned aerial vehicle high altitude drop protection device of claim 1, characterized in that:
the supporting layer (1a) is a frame structure;
the outer buffer layer (1b) is filled with gas or flexible materials or elastic materials;
the inner buffer layer (1c) is filled with gas or flexible materials or elastic materials.
3. The unmanned aerial vehicle high altitude drop protection device of claim 2, characterized in that: the thickness of the inner buffer layer (1c) is larger than that of the outer buffer layer (1 b).
4. The unmanned aerial vehicle high altitude drop protection device of claim 2, characterized in that: the shell (1) is divided into a first shell and a second shell by the object placing opening, and the sealing mechanism (3) is used for connecting the first shell and the second shell.
5. The unmanned aerial vehicle high altitude drop protection device of claim 4, characterized in that: the supporting layer (1a) is a steel wire mesh woven by steel wires.
6. The unmanned aerial vehicle high altitude drop protection device of claim 2, characterized in that: at least one fixing hook (4) is arranged on the cavity wall of the object placing cavity (2), a fixing binding band (5) is arranged on at least one fixing hook (4), and a fixing lantern ring is arranged on the fixing binding band (5).
7. The unmanned aerial vehicle high altitude drop protection device of claim 6, characterized in that: the fixing hook (4) and the fixing bandage (5) are made of elastic materials.
8. The unmanned aerial vehicle high altitude drop protection device of claim 1, characterized in that: at least one hanging piece (6) is arranged on the outer surface of the shell (1).
9. The unmanned aerial vehicle high altitude drop protection device of claim 1, characterized in that: the shell (1) is a spherical body or a square body.
10. The unmanned aerial vehicle high altitude drop protection device of claim 1, characterized in that: the surface of the shell (1) is coated with a fluorescent layer.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201920938876.9U CN210101999U (en) | 2019-06-21 | 2019-06-21 | Unmanned aerial vehicle high altitude drop protection device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201920938876.9U CN210101999U (en) | 2019-06-21 | 2019-06-21 | Unmanned aerial vehicle high altitude drop protection device |
Publications (1)
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CN210101999U true CN210101999U (en) | 2020-02-21 |
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CN201920938876.9U Expired - Fee Related CN210101999U (en) | 2019-06-21 | 2019-06-21 | Unmanned aerial vehicle high altitude drop protection device |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111731480A (en) * | 2020-08-06 | 2020-10-02 | 江西珉轩智能科技有限公司 | Environmental monitoring system based on big data |
CN111853143A (en) * | 2020-07-20 | 2020-10-30 | 长沙理工大学 | Gas-liquid-solid coupled air-drop carrier combined buffer device |
CN111846233A (en) * | 2020-07-20 | 2020-10-30 | 长沙理工大学 | Rigid-flexible coupled airborne cargo combined buffering device |
CN111853144A (en) * | 2020-07-20 | 2020-10-30 | 长沙理工大学 | Working method of air-liquid-solid coupled air-drop cargo combined buffer device |
CN111891360A (en) * | 2020-07-27 | 2020-11-06 | 赵昕 | Inflatable cabin capable of being thrown in |
CN117582622A (en) * | 2023-12-06 | 2024-02-23 | 广东锐捷安全技术股份有限公司 | Combined fire extinguishing system and method based on unmanned aerial vehicle platform |
-
2019
- 2019-06-21 CN CN201920938876.9U patent/CN210101999U/en not_active Expired - Fee Related
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111853143A (en) * | 2020-07-20 | 2020-10-30 | 长沙理工大学 | Gas-liquid-solid coupled air-drop carrier combined buffer device |
CN111846233A (en) * | 2020-07-20 | 2020-10-30 | 长沙理工大学 | Rigid-flexible coupled airborne cargo combined buffering device |
CN111853144A (en) * | 2020-07-20 | 2020-10-30 | 长沙理工大学 | Working method of air-liquid-solid coupled air-drop cargo combined buffer device |
CN111891360A (en) * | 2020-07-27 | 2020-11-06 | 赵昕 | Inflatable cabin capable of being thrown in |
CN111731480A (en) * | 2020-08-06 | 2020-10-02 | 江西珉轩智能科技有限公司 | Environmental monitoring system based on big data |
CN111731480B (en) * | 2020-08-06 | 2020-11-17 | 江西珉轩智能科技有限公司 | Environmental monitoring system based on big data |
CN117582622A (en) * | 2023-12-06 | 2024-02-23 | 广东锐捷安全技术股份有限公司 | Combined fire extinguishing system and method based on unmanned aerial vehicle platform |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200221 Termination date: 20200621 |
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CF01 | Termination of patent right due to non-payment of annual fee |