CN211167448U - Rescue unmanned aerial vehicle investigation mechanism of speedily carrying out rescue work with stronger protective structure - Google Patents
Rescue unmanned aerial vehicle investigation mechanism of speedily carrying out rescue work with stronger protective structure Download PDFInfo
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- CN211167448U CN211167448U CN201921178628.5U CN201921178628U CN211167448U CN 211167448 U CN211167448 U CN 211167448U CN 201921178628 U CN201921178628 U CN 201921178628U CN 211167448 U CN211167448 U CN 211167448U
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- aerial vehicle
- unmanned aerial
- protective structure
- control box
- bird
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Abstract
The utility model discloses an unmanned aerial vehicle investigation mechanism that speedily carries out rescue work in rescue with stronger protective structure, including protective structure and main part shell, protective structure's internally mounted has the camera, the mount is installed to protective structure's top, and installs the control box between the mount, both ends all are provided with the dust absorption cotton around the control box is inside, the louvre has been seted up to both sides wall around the control box, drive bird bee calling organ is all installed at both ends around the main part shell, and the main part shell is located the top of mount, drive the top of bird bee calling organ and install the photovoltaic board, the light is all installed to the left and right sides of main part shell. This unmanned aerial vehicle investigation mechanism that speedily carries out rescue work with stronger protective structure is provided with and drives bird bee calling organ, drives bird bee calling organ's effect under, can drive the bird function for unmanned aerial vehicle provides, avoids flying bird collision unmanned aerial vehicle, provides certain protection for unmanned aerial vehicle's flight.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle technical field that speedily carries out rescue work specifically is an unmanned aerial vehicle investigation mechanism that speedily carries out rescue work with stronger protective structure.
Background
When the accident happens, rescue personnel can not arrive at a proper place in time due to the influence of the place or the environment, at the moment, the unmanned aerial vehicle can be applied to the rescue and rescue process, the unmanned aerial vehicle is called as the unmanned aerial vehicle for short, and the unmanned aerial vehicle is an unmanned aerial vehicle controlled by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.
Current unmanned aerial vehicle investigation mechanism that speedily carries out rescue work provides good protection for unmanned aerial vehicle that can not be fine in the use to and when the barrier collided unmanned aerial vehicle, the damage that unmanned aerial vehicle produced was great, and can not be fine for unmanned aerial vehicle pass through the illumination and drive the bird function, external pencil is not convenient for bind or shelve in addition, the user demand who satisfies people that can not be fine, to above-mentioned condition, carry out technical innovation on current unmanned aerial vehicle investigation mechanism basis that speedily carries out rescue work.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a rescue unmanned aerial vehicle investigation mechanism that speedily carries out rescue work with stronger protective structure to it speedily carries out rescue work with current unmanned aerial vehicle investigation mechanism in the use to solve to provide among the above-mentioned background art, can not be fine provide good protection for unmanned aerial vehicle, and when the obstacle collided unmanned aerial vehicle, the damage that unmanned aerial vehicle produced is great, and can not be fine for unmanned aerial vehicle through the illumination and drive the bird function, external pencil is not convenient for bind or shelve moreover, can not be fine satisfy people's user demand problem.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a rescue unmanned aerial vehicle investigation mechanism of speedily carrying out rescue work with stronger protective structure, includes protective structure and main part shell, protective structure's internally mounted has the camera, the mount is installed to protective structure's top, and installs the control box between the mount, both ends all are provided with the dust absorption cotton around the control box is inside, the louvre has been seted up to both sides wall around the control box, both ends are all installed around the main part shell and are driven bird bee calling organ, and the main part shell is located the top of mount, drive the top of driving bird bee calling organ and install the photovoltaic board, the light is all installed to the left and right sides of main part shell.
Preferably, protective structure includes link, connecting rod, axostylus axostyle, sliding sleeve and spring, the axostylus axostyle has been run through to the inside of spring, and the sliding sleeve is all installed to the left and right sides of axostylus axostyle, the connecting rod is all installed to the upper and lower both sides of spring, and the upper and lower both ends of connecting rod respectively with link and sliding sleeve between be pin junction.
Preferably, an elastic structure is formed between the sliding sleeves through springs, and the shaft rod penetrates through the sliding sleeves and the springs respectively.
Preferably, threaded connection is adopted between the fixing frame and the control box, and the heat dissipation holes and the dust collection cotton are symmetrically distributed around the central axis of the control box.
Preferably, the bird repelling buzzers are in threaded connection with the main body shell, and the bird repelling buzzers are symmetrically distributed around the central axis of the main body shell.
Preferably, the photovoltaic panel and the illuminating lamp are in threaded connection with the main body shell, and the illuminating lamps are symmetrically distributed around the vertical center line of the main body shell.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model is provided with a protective structure, the collision force can be stably buffered through the spring, and the shaft lever can effectively control the moving track of the sliding sleeve, thereby effectively reducing the deflection or vibration generated by the unmanned aerial vehicle, leading the unmanned aerial vehicle to stably land or reducing the acting force of a barrier on the unmanned aerial vehicle;
2. the utility model discloses be provided with the control box, louvre and dust absorption cotton, can effectually provide the heat dissipation passageway for the control box through the louvre, and the symmetric distribution of louvre can make the gas circulate, thereby can effectually improve the radiating effect of air current to the inside subassembly of control box, when the gas flows through the dust absorption cotton, can effectually adsorb the dust in the gas, avoid the dust to adsorb on the surface of the inside subassembly of control box, influence the heat dissipation of subassembly, and the control box provides storage space for the pencil of the external subassembly of unmanned aerial vehicle, convenient to user dismantles or maintains, avoid dismantling the holistic step of unmanned aerial vehicle, can effectually improve the installation efficiency of user to the external subassembly;
3. the utility model discloses be provided with and drive bird bee calling organ, under the effect that drives bird bee calling organ, can drive the bird function for unmanned aerial vehicle provides, avoid flying bird collision unmanned aerial vehicle, provide certain protection for unmanned aerial vehicle's flight, be provided with photovoltaic board and light, can effectual absorption solar energy through the photovoltaic board, and the light can provide lighting service for unmanned aerial vehicle's flight at night to and can searchly the object of unmanned aerial vehicle below, the user of being convenient for seeks the inside object of unmanned aerial vehicle flight range or people.
Drawings
FIG. 1 is a schematic view of the structure of the present invention;
FIG. 2 is a schematic view of a partial enlarged structure at A in FIG. 1 according to the present invention;
fig. 3 is an external structural schematic diagram of the control box of the present invention.
In the figure: 1. a protective structure; 101. a connecting frame; 102. a connecting rod; 103. a shaft lever; 104. a sliding sleeve; 105. a spring; 2. a camera; 3. a fixed mount; 4. a control box; 5. a main body case; 6. a bird-repelling buzzer; 7. a photovoltaic panel; 8. an illuminating lamp; 9. heat dissipation holes; 10. dust-absorbing cotton.
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 work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a rescue and rescue unmanned aerial vehicle investigation mechanism with a strong protection structure comprises a protection structure 1 and a main body shell 5, wherein a camera 2 is arranged inside the protection structure 1, the protection structure 1 comprises a connecting frame 101, a connecting rod 102, a shaft rod 103, a sliding sleeve 104 and a spring 105, the shaft rod 103 penetrates through the spring 105, the sliding sleeves 104 are arranged on the left side and the right side of the shaft rod 103, the connecting rod 102 is arranged on the upper side and the lower side of the spring 105, the upper end and the lower end of the connecting rod 102 are respectively in pin connection with the connecting frame 101 and the sliding sleeve 104, the sliding sleeves 104 form an elastic structure through the spring 105, the shaft rod 103 penetrates through the sliding sleeve 104 and the spring 105 respectively, when an unmanned aerial vehicle lands or the bottom of the unmanned aerial vehicle touches an obstacle, at the moment, collision force acts on the connecting frame 101, so that the connecting frame 101 pushes the sliding sleeve 104 to stretch the spring 105 along the central, the shaft rod 103 can effectively control the moving track of the sliding sleeve 104, so that the spring 105 can stably buffer the collision force, the deflection or the vibration generated by the unmanned aerial vehicle can be effectively reduced, and the unmanned aerial vehicle can stably land or reduce the acting force of an obstacle on the unmanned aerial vehicle;
the fixing frame 3 is arranged above the protective structure 1, the control box 4 is arranged between the fixing frames 3, the front end and the rear end inside the control box 4 are respectively provided with the dust absorption cotton 10, the fixing frame 3 is in threaded connection with the control box 4, the heat dissipation holes 9 and the dust absorption cotton 10 are symmetrically distributed around the central axis of the control box 4, the heat dissipation channel can be effectively provided for the control box 4 through the heat dissipation holes 9, the air can be circulated due to the symmetrical distribution of the heat dissipation holes 9, the heat dissipation effect of air flow on components inside the control box 4 can be effectively improved, when air flows through the dust absorption cotton 10, dust in air can be effectively adsorbed, the dust is prevented from being adsorbed on the surface of the components inside the control box 4 to influence the heat dissipation of the components, the control box 4 provides a storage space for wiring harnesses of external components of the unmanned aerial vehicle, the unmanned aerial vehicle is, the mounting efficiency of a user on the external component can be effectively improved, heat dissipation holes 9 are formed in the front side wall and the rear side wall of the control box 4, bird repelling buzzers 6 are mounted at the front end and the rear end of the main body shell 5, the main body shell 5 is located above the fixing frame 3, the bird repelling buzzers 6 are in threaded connection with the main body shell 5, the bird repelling buzzers 6 are symmetrically distributed around the central axis of the main body shell 5, a bird repelling function can be provided for the unmanned aerial vehicle under the action of the bird repelling buzzers 6, the collision of flying birds with the unmanned aerial vehicle is avoided, and certain protection is provided for;
drive the top of bird bee calling organ 6 and install photovoltaic board 7, light 8 is all installed to the left and right sides of main part shell 5, be threaded connection between photovoltaic board 7 and light 8 and the main part shell 5, and about the vertical central line symmetric distribution of main part shell 5 between the light 8, can effectual absorption solar energy through photovoltaic board 7, and light 8 can provide lighting service for unmanned aerial vehicle's flight at night, and can searchlight unmanned aerial vehicle below the object, the user of being convenient for seeks the inside object of unmanned aerial vehicle flight range or people.
The working principle is as follows: when the rescue and emergency unmanned aerial vehicle detection mechanism with a strong protection structure is used, firstly, under the action of the bird repelling buzzer 6, a bird repelling function can be provided for the unmanned aerial vehicle, the bird is prevented from colliding with the unmanned aerial vehicle, wherein the bird repelling buzzer 6 is YD 4216;
secondly, solar energy can be effectively absorbed through the photovoltaic panel 7, the illuminating lamp 8 can provide illumination service for the flight of the unmanned aerial vehicle at night and can search objects below the unmanned aerial vehicle, then the control box 4 provides a storage space for a wiring harness of an external component of the unmanned aerial vehicle, the step of disassembling the whole unmanned aerial vehicle is avoided, and the installation efficiency of a user on the external component can be effectively improved;
finally, when unmanned aerial vehicle descends or unmanned aerial vehicle's bottom touches the barrier, this moment, the collision force is used in link 101 for link 101 promotes sliding sleeve 104 along the axis direction extension spring 105 of axostylus axostyle 103 through connecting rod 102, makes the buffering collision dynamics that spring 105 can be stable, thereby can effectually alleviate the skew or the vibrations that unmanned aerial vehicle produced, this is this rescue unmanned aerial vehicle investigation mechanism's that speedily carries out rescue work theory that has stronger protective structure.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a rescue unmanned aerial vehicle investigation mechanism of speedily carrying out rescue work with stronger protective structure, includes protective structure (1) and main part shell (5), its characterized in that: the utility model discloses a bird repelling device, including protective structure (1), mount (3), control box (4), both ends all are provided with dust absorption cotton (10) around control box (4), louvre (9) have been seted up to both sides wall around control box (4), bird repellent bee calling organ (6) are all installed at both ends around main part shell (5), and main part shell (5) are located the top of mount (3), drive the top of bird bee calling organ (6) and install photovoltaic board (7), light (8) are all installed to the left and right sides of main part shell (5), mount (3) are installed to the internally mounted of protective structure (1), mount (3) are installed to the top of protective structure (1), and install between mount (3) control box (4).
2. The unmanned aerial vehicle investigation mechanism that speedily carries out rescue work that has stronger protective structure of claim 1, its characterized in that: protective structure (1) is including link (101), connecting rod (102), axostylus axostyle (103), sliding sleeve (104) and spring (105), the inside of spring (105) is run through axostylus axostyle (103), and sliding sleeve (104) are all installed to the left and right sides of axostylus axostyle (103), connecting rod (102) are all installed to the upper and lower both sides of spring (105), and the upper and lower both ends of connecting rod (102) respectively with link (101) and sliding sleeve (104) between be pin junction.
3. The unmanned aerial vehicle investigation mechanism that speedily carries out rescue work that has stronger protective structure of claim 2, its characterized in that: an elastic structure is formed between the sliding sleeves (104) through springs (105), and the shaft rods (103) respectively penetrate through the sliding sleeves (104) and the springs (105).
4. The unmanned aerial vehicle investigation mechanism that speedily carries out rescue work that has stronger protective structure of claim 1, its characterized in that: the fixing frame (3) is in threaded connection with the control box (4), and the heat dissipation holes (9) and the dust collection cotton (10) are symmetrically distributed about the central axis of the control box (4).
5. The unmanned aerial vehicle investigation mechanism that speedily carries out rescue work that has stronger protective structure of claim 1, its characterized in that: the bird repelling buzzer (6) is in threaded connection with the main body shell (5), and the bird repelling buzzer (6) is symmetrically distributed about the central axis of the main body shell (5).
6. The unmanned aerial vehicle investigation mechanism that speedily carries out rescue work that has stronger protective structure of claim 1, its characterized in that: photovoltaic board (7) and light (8) all with be threaded connection between main body shell (5), and about the vertical central line symmetric distribution of main body shell (5) between light (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921178628.5U CN211167448U (en) | 2019-07-25 | 2019-07-25 | Rescue unmanned aerial vehicle investigation mechanism of speedily carrying out rescue work with stronger protective structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921178628.5U CN211167448U (en) | 2019-07-25 | 2019-07-25 | Rescue unmanned aerial vehicle investigation mechanism of speedily carrying out rescue work with stronger protective structure |
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| Publication Number | Publication Date |
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| CN211167448U true CN211167448U (en) | 2020-08-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921178628.5U Expired - Fee Related CN211167448U (en) | 2019-07-25 | 2019-07-25 | Rescue unmanned aerial vehicle investigation mechanism of speedily carrying out rescue work with stronger protective structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113022855A (en) * | 2021-04-14 | 2021-06-25 | 江苏航空职业技术学院 | Water intaking device based on many rotor unmanned aerial vehicle |
-
2019
- 2019-07-25 CN CN201921178628.5U patent/CN211167448U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113022855A (en) * | 2021-04-14 | 2021-06-25 | 江苏航空职业技术学院 | Water intaking device based on many rotor unmanned aerial vehicle |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200804 Termination date: 20210725 |
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| CF01 | Termination of patent right due to non-payment of annual fee |