CN217969923U - Emergency rescue unmanned aerial vehicle - Google Patents
Emergency rescue unmanned aerial vehicle Download PDFInfo
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- CN217969923U CN217969923U CN202221911060.5U CN202221911060U CN217969923U CN 217969923 U CN217969923 U CN 217969923U CN 202221911060 U CN202221911060 U CN 202221911060U CN 217969923 U CN217969923 U CN 217969923U
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Abstract
The utility model belongs to the field of unmanned aerial vehicle that speedily carries out rescue work, specific unmanned aerial vehicle that speedily carries out rescue work that says so, including the unmanned aerial vehicle body, the top fixedly connected with base of unmanned aerial vehicle body, the top fixedly connected with protecting crust of base, the front fixedly connected with hinge of protecting crust, the outer wall fixedly connected with door that opens and shuts of hinge, the bottom fixedly connected with buffer gear of unmanned aerial vehicle body, the bottom fixedly connected with support of buffer gear; carry out the protection work through using the base to fix the protecting crust at the top of unmanned aerial vehicle body when using, use the rotatory door that opens and shuts of hinge when need using the unmanned aerial vehicle body in the protection process, open the protecting crust after the rotation finishes, open afterwards and operate the unmanned aerial vehicle body, use the hinge to reclose the door that opens and shuts after the operation finishes, buffer gear also provides the buffering work when emergency unmanned aerial vehicle body promptly compels to land when using.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field of speedily carrying out rescue work specifically is an unmanned aerial vehicle of speedily carrying out rescue work in emergency.
Background
Unmanned aircraft is called unmanned aerial vehicle for short, and is called UAV in short in English, and is an unmanned aircraft operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, compared with the unmanned aircraft, the unmanned aircraft is more suitable for tasks too 'fool, dirty or dangerous', the unmanned aircraft can be divided into military and civil according to the application field, and the unmanned aircraft can be divided into reconnaissance aircraft and target aircraft in the military, and the unmanned aircraft can be applied to the industry in the civil field, and is really just needed by the unmanned aircraft; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.
Along with the progress of science and technology, more and more unmanned aerial vehicle appears in the scene of speedily carrying out emergency rescue, can effectually carry out the toxic gas detection when using, survey three-dimensional reconstruction (including range finding), emergent material is put in, emergency lighting and communication command, atmospheric environment monitoring and full zone temperature monitoring, all have effectual guarantee to the stability of developing and the security of speedily carrying out rescue work.
When the existing emergency rescue unmanned aerial vehicle is used, the working surface is complex, the protection effect is not comprehensive enough, the unmanned aerial vehicle is easy to lose the working capacity due to collision or sundries falling when the existing emergency rescue unmanned aerial vehicle works, and the comprehensiveness and the stability of information collection are not effectively guaranteed when the existing emergency rescue unmanned aerial vehicle is used;
therefore, an emergency rescue unmanned aerial vehicle is provided to the above problem.
SUMMERY OF THE UTILITY MODEL
In order to compensate prior art's not enough, solve current emergency rescue unmanned aerial vehicle when using because the working face is comparatively complicated, the protective effect is comprehensive not enough again, appears colliding with or debris drop and lets unmanned aerial vehicle lose the operational capability easily when carrying out work, does not have the problem of effectual guarantee to information collection comprehensiveness and stability when using, the utility model provides an emergency rescue unmanned aerial vehicle.
The utility model provides a technical scheme that its technical problem adopted is: an unmanned aerial vehicle emergently speedily carries out rescue work, including the unmanned aerial vehicle body, the top fixedly connected with base of unmanned aerial vehicle body, the top fixedly connected with protecting crust of base, the positive fixedly connected with hinge of protecting crust.
The outer wall fixedly connected with door that opens and shuts of hinge, the bottom fixedly connected with buffer gear of unmanned aerial vehicle body, buffer gear's bottom fixedly connected with support.
Preferably, the positive fixedly connected with glass board of the door that opens and shuts, and constitute between the door that opens and shuts and the glass board and run through the structure, and through adhesive bonding between door that opens and shuts and the glass board, let the linkage effect and the connection stability of equipment all have effectual guarantee through adhesive bonding, the structural safety nature and the structural condition of lifting means that can be more stable when using.
Preferably, the positive fixedly connected with pivot of protecting crust, and the outer wall swing joint of pivot has the buckle, and constitutes between pivot and the buckle and run through the structure, and the buckle constitutes revolution mechanic through pivot and protecting crust, lets the butt joint effect and the butt joint stability of equipment all have effectual promotion through revolution mechanic, lets the limit state of equipment have effectual guarantee when using.
Preferably, the openly fixedly connected with limit buckle that opens and shuts the door, and open and shut and pass through welded connection between door and the limit buckle, let the connection status and the connection stability of equipment all have effectual guarantee through welded connection, let the operation effect of equipment also have effectual promotion when using.
Preferably, buffer gear includes shell, spring and support, and the interior diapire fixed connection spring of shell, and the bottom fixed connection support of spring, and support and shell constitution run through the structure, and the support passes through the spring and constitutes elevation structure with the shell, lets the structural stability and the security of equipment all have effectual promotion through elevation structure, lets the connection effect and the connection stability of equipment all have effectual promotion when using.
Preferably, the inside wall fixed connection of shell has a limit head, and the shell passes through limit head and support constitution limit structure, lets the fixed effect of equipment and flexible stable all have effectual guarantee through limit structure.
Preferably, the support includes joint and slide bar, and the bottom fixed connection slide bar of joint, and the axis coincidence setting of the axis of joint and slide bar, and pass through welded connection between joint and the slide bar, let the connection effect and the connection security of equipment all have effectual promotion through welded connection, all have effectual guarantee to the operational effect and the operating stability of equipment.
Preferably, the bottom fixedly connected with base of slide bar, and the axis coincidence setting of the axis of slide bar and base let the butt joint state and the equilibrium of equipment all have effectual promotion through the axis coincidence setting.
The utility model discloses an useful part lies in:
the utility model discloses an unmanned aerial vehicle body, a pedestal, the protecting crust, the hinge, the door opens and shuts, cooperation work between support and the buffer gear can effectual guarantee equipment's structural stability and security, let the protective effect of unmanned aerial vehicle body have more comprehensive promotion when using, can effectually let unmanned aerial vehicle have better guarantee in stability when working under the complex emergency environment when using, all there is effectual promotion to operating condition and operating stability, use the protecting crust to fix the top at the unmanned aerial vehicle body and carry out protection work when using, use the rotatory door that opens and shuts of hinge when needing to use the unmanned aerial vehicle body in the protection process, open the protecting crust after the rotation finishes, operate the unmanned aerial vehicle body afterwards, use the hinge to reclose the door after finishing the operation, carry out continuation protection work to the unmanned aerial vehicle body after closing, buffer gear also provides buffering work when emergency unmanned aerial vehicle body takes place to force to descend when using, can effectual reduction of impact force, there is effectual promotion to the protective effect of unmanned aerial vehicle body.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without inventive exercise.
Fig. 1 is a schematic view of the structure of the present invention;
FIG. 2 is a schematic view of the buffering mechanism of the present invention;
FIG. 3 is a schematic view of the support structure of the present invention;
fig. 4 is an enlarged view of the structure at a in fig. 1 of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a base; 3. a protective shell; 4. a hinge; 5. opening and closing the door; 6. a glass plate; 7. a support; 8. a buffer mechanism; 801. a housing; 802. a spring; 803. a limiting head; 9. a support; 901. a snap head; 902. a slide bar; 903. a base; 10. a rotating shaft; 11. a limit buckle; 12. and (5) buckling.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
Please refer to fig. 1-4, an emergency unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a base 2 fixedly connected to the top of the unmanned aerial vehicle body 1, a protective shell 3 fixedly connected to the top of the base 2, and a hinge 4 fixedly connected to the front of the protective shell 3.
The outer wall fixedly connected with door 5 that opens and shuts of hinge 4, the bottom fixedly connected with buffer gear 8 of unmanned aerial vehicle body 1, the bottom fixedly connected with support 7 of buffer gear 8.
In the embodiment, the front surface of the opening and closing door 5 is fixedly connected with the glass plate 6, a penetrating structure is formed between the opening and closing door 5 and the glass plate 6, and the opening and closing door 5 is connected with the glass plate 6 through gluing; during operation, can effectually let the staff see through glass board 6 in real time and come to inspect the running state of unmanned aerial vehicle body 1.
In this embodiment, the front surface of the protective shell 3 is fixedly connected with a rotating shaft 10, the outer wall of the rotating shaft 10 is movably connected with a buckle 12, a penetrating structure is formed between the rotating shaft 10 and the buckle 12, and the buckle 12 and the protective shell 3 form a rotating structure through the rotating shaft 10; during operation, the limiting effect of the opening and closing door 5 can be effectively guaranteed, and the structural stability and the protection safety of the equipment are effectively guaranteed.
In this embodiment, the front surface of the opening and closing door 5 is fixedly connected with a limit buckle 11, and the opening and closing door 5 is connected with the limit buckle 11 by welding; during operation, the limiting stability of the equipment can be effectively guaranteed, and the limiting stability is effectively improved.
In this embodiment, the buffering mechanism 8 includes a housing 801, a spring 802 and a support 9, the inner bottom wall of the housing 801 is fixedly connected to the spring 802, the bottom of the spring 802 is fixedly connected to the support 9, the support 9 and the housing 801 form a penetrating structure, and the support 9 and the housing 801 form a lifting structure through the spring 802; during operation, the buffering effect of the equipment can be effectively guaranteed, and the impact force can be effectively reduced when the condition of forced landing is required.
In this embodiment, the inner side wall of the housing 801 is fixedly connected to the limiting head 803, and the housing 801 and the support 9 form a limiting structure through the limiting head 803; the during operation can effectual guarantee support 9's structural stability, lets the buffering stability and the security of equipment all have effectual promotion when using, all has effectual promotion to the structural security and the stability of equipment.
In this embodiment, the support 9 includes a clamping head 901 and a sliding rod 902, the bottom of the clamping head 901 is fixedly connected to the sliding rod 902, a central axis of the clamping head 901 is overlapped with a central axis of the sliding rod 902, and the clamping head 901 is connected to the sliding rod 902 by welding; the during operation, structural stability and the connection security that can effectual guarantee equipment let the structural symmetry of equipment also have effectual guarantee when using, and lifting stability has effectual promotion.
In this embodiment, the bottom of the sliding rod 902 is fixedly connected with a base 903, and a central axis of the sliding rod 902 is overlapped with a central axis of the base 903; during operation, the stress balance of the equipment can be effectively guaranteed, and the structural stability of the equipment is effectively improved when the equipment is used.
Theory of operation, carry out protection work at unmanned aerial vehicle body 1's top through using base 2 to fix protecting crust 3 when using, use hinge 4 rotation opening and shutting door 5 when need use unmanned aerial vehicle body 1 in the protection course, open protecting crust 3 after the rotation finishes, operate unmanned aerial vehicle body 1 afterwards, use hinge 4 reclosing opening and shutting door 5 after the operation finishes, carry out continuation protection work to unmanned aerial vehicle body 1 after closing, use pivot 10 rotatory buckle 12 to come to dock with spacing knot 11 simultaneously, carry out spacing fixed work to opening and shutting door 5 among the butt joint process, buffer gear 8 also provides buffer work when emergency unmanned aerial vehicle body 1 carries out urgent compelling to land appearing in the use.
In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention.
Claims (8)
1. The utility model provides an emergent unmanned aerial vehicle that speedily carries out rescue work which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein the top of the unmanned aerial vehicle body (1) is fixedly connected with a base (2), the top of the base (2) is fixedly connected with a protective shell (3), and the front of the protective shell (3) is fixedly connected with a hinge (4);
the outer wall fixedly connected with of hinge (4) opens and shuts door (5), the bottom fixedly connected with buffer gear (8) of unmanned aerial vehicle body (1), the bottom fixedly connected with support (7) of buffer gear (8).
2. The emergency rescue unmanned aerial vehicle of claim 1, characterized in that: the front face of the opening and closing door (5) is fixedly connected with a glass plate (6), a penetrating structure is formed between the opening and closing door (5) and the glass plate (6), and the opening and closing door (5) is connected with the glass plate (6) through gluing.
3. The emergency rescue unmanned aerial vehicle of claim 1, characterized in that: the front face of the protective shell (3) is fixedly connected with a rotating shaft (10), the outer wall of the rotating shaft (10) is movably connected with a buckle (12), a penetrating structure is formed between the rotating shaft (10) and the buckle (12), and the buckle (12) and the protective shell (3) form a rotating structure through the rotating shaft (10).
4. The emergency rescue unmanned aerial vehicle of claim 1, characterized in that: the front side of the opening and closing door (5) is fixedly connected with a limit buckle (11), and the opening and closing door (5) is connected with the limit buckle (11) through welding.
5. The unmanned aerial vehicle of claim 1, wherein: buffer gear (8) include shell (801), spring (802) and support (9), and the interior diapire fixed connection spring (802) of shell (801), and the bottom fixed connection support (9) of spring (802), and support (9) and shell (801) constitute and run through the structure, and support (9) pass through spring (802) and shell (801) constitution elevation structure.
6. The emergency rescue unmanned aerial vehicle of claim 5, characterized in that: the inner side wall of the shell (801) is fixedly connected with a limiting head (803), and the shell (801) and the support (9) form a limiting structure through the limiting head (803).
7. The emergency rescue unmanned aerial vehicle of claim 5, characterized in that: the support (9) comprises a clamping head (901) and a sliding rod (902), the bottom of the clamping head (901) is fixedly connected with the sliding rod (902), the central axis of the clamping head (901) is overlapped with the central axis of the sliding rod (902), and the clamping head (901) is connected with the sliding rod (902) through welding.
8. The emergency rescue unmanned aerial vehicle of claim 7, characterized in that: the bottom of slide bar (902) is fixedly connected with base (903), and the axis of slide bar (902) and the axis coincidence setting of base (903).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221911060.5U CN217969923U (en) | 2022-07-22 | 2022-07-22 | Emergency rescue unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221911060.5U CN217969923U (en) | 2022-07-22 | 2022-07-22 | Emergency rescue unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217969923U true CN217969923U (en) | 2022-12-06 |
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ID=84279730
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221911060.5U Active CN217969923U (en) | 2022-07-22 | 2022-07-22 | Emergency rescue unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217969923U (en) |
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2022
- 2022-07-22 CN CN202221911060.5U patent/CN217969923U/en active Active
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