CN212074418U - Unmanned aerial vehicle for geographic exploration - Google Patents
Unmanned aerial vehicle for geographic exploration Download PDFInfo
- Publication number
- CN212074418U CN212074418U CN202020283392.8U CN202020283392U CN212074418U CN 212074418 U CN212074418 U CN 212074418U CN 202020283392 U CN202020283392 U CN 202020283392U CN 212074418 U CN212074418 U CN 212074418U
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- baffle
- branch
- fixed connection
- connecting rod
- camera
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Abstract
The utility model discloses an unmanned aerial vehicle for geographic exploration, which comprises a body, body bottom fixedly connected with base, the base outside is provided with protection machanism, the body bottom is provided with the camera, protection machanism includes branch, first baffle, second baffle, connecting rod and sleeve, branch fixed connection is in the base outside, the quantity of branch sets up to a plurality ofly, first baffle fixed connection is between a plurality of branches, second baffle sliding connection is between a plurality of branches. The utility model discloses a drive the second baffle and rotate, make it pass logical groove and cooperate with the bar groove of first branch one side, utilize the cooperation of first baffle and second baffle, can protect the camera, can improve its stability of placing subaerial before unmanned aerial vehicle takes off through this structure to can carry out good protection to the camera of installing on it, be favorable to improving its life.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle is used in geographic exploration.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated 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.
The bottom of the unmanned aerial vehicle for the geographic survey is often provided with a camera, and the camera is generally exposed outside and is not well protected, so that the camera is easily damaged in the using and transporting processes.
Therefore, it is necessary to invent a unmanned aerial vehicle for geographic exploration to solve the above problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle for geophysical prospecting, place unmanned aerial vehicle subaerial during the use, can adjust the distance that the inner tube stretches out the urceolus through rotatory inner tube, thereby adjust the height of each branch, can steadily place unmanned aerial vehicle, be favorable to it to take off stably, be favorable to increasing the area of contact on inner tube and ground through stabilizing the piece, stability when placing unmanned aerial vehicle can be improved, can rotate the sleeve and drive the connecting rod rotation after the use, thereby it rotates to drive the second baffle, can pass logical groove and cooperate with the bar groove of first branch one side, cooperation through first baffle and second baffle, can protect the camera, can carry out good protection to the camera of installing on the unmanned aerial vehicle through this structure, be favorable to improving its life, with the above-mentioned weak point in the solution technique.
In order to achieve the above object, the present invention provides the following technical solutions: an unmanned aerial vehicle for geographic detection comprises a body, wherein the bottom of the body is fixedly connected with a base, a protection mechanism is arranged on the outer side of the base, and a camera is arranged at the bottom of the body;
protection machanism includes branch, first baffle, second baffle, connecting rod and sleeve, branch fixed connection is in the base outside, the quantity of branch sets up to a plurality ofly, first baffle fixed connection is between a plurality of branches, second baffle sliding connection is between a plurality of branches, first baffle sets up in the second baffle outside, connecting rod and second baffle fixed connection, the one end and the sleeve fixed connection of second baffle are kept away from to the connecting rod, fixedly connected with montant between body and the camera, sleeve threaded connection is in the montant outside.
Preferably, the body outside fixedly connected with diaphragm, the diaphragm top is kept away from body one side and is provided with the flabellum.
Preferably, the bottom of the supporting rod is provided with an adjusting component, the adjusting component comprises an outer barrel, an inner barrel and a stabilizing block, the stabilizing block is fixedly connected to the bottom of the inner barrel, and the inner barrel is in threaded connection with the bottom of the outer barrel.
Preferably, the bottom of the outer barrel is provided with a blind hole, an internal thread is arranged in the blind hole, an external thread is arranged on the outer side of the inner barrel, and the external thread is meshed with the internal thread.
Preferably, the supporting rods comprise first supporting rods and second supporting rods, the first supporting rods and the second supporting rods are distributed in a staggered mode, a through groove penetrating through the supporting rods is formed in one side of the second supporting rods, and the second baffle is connected with the through groove in a sliding mode.
Preferably, first bracing piece both sides all are provided with the bar groove, the second baffle cooperatees with the bar groove.
Preferably, first baffle fixed connection is between first branch and second branch, the quantity of connecting rod sets up to a plurality ofly, and is a plurality of the connecting rod is the annular array and distributes in the base outside.
In the technical scheme, the utility model provides a technological effect and advantage:
place unmanned aerial vehicle subaerial during the use, can adjust the distance that the urceolus stretches out the inner tube through rotatory inner tube, thereby adjust the height of each branch, can steadily place unmanned aerial vehicle, be favorable to it to take off steadily, be favorable to increasing the area of contact of inner tube with ground through stabilizing the piece, stability when placing unmanned aerial vehicle can be improved, can rotate the sleeve and drive the connecting rod rotation after the use, thereby drive the second baffle and rotate, can pass through logical groove and cooperate with the bar groove of first branch one side, cooperation through first baffle and second baffle, can protect the camera, can improve its stability of placing subaerial before unmanned aerial vehicle takes off through this structure, and can carry out good protection to the camera of installing on it, be favorable to improving its life.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments described in the present invention, and other drawings can be obtained by those skilled in the art according to these drawings.
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a distribution diagram of the support rods of the present invention;
fig. 3 is a top view of the present invention;
FIG. 4 is a connecting rod distribution diagram of the present invention;
fig. 5 is an enlarged view of the structure of the portion a of fig. 1 according to the present invention.
Description of reference numerals:
the camera comprises a body 1, a base 2, a camera 3, a supporting rod 4, a first supporting rod 401, a second supporting rod 402, a first baffle 5, a second baffle 6, a connecting rod 7, a sleeve 8, a transverse plate 9, fan blades 10, an outer barrel 11, an inner barrel 12, a stabilizing block 13 and a through groove 14.
Detailed Description
In order to make the technical solution of the present invention better understood by those skilled in the art, the present invention will be further described in detail with reference to the accompanying drawings.
The utility model provides an unmanned aerial vehicle for geographic exploration, as shown in figures 1-5, which comprises a body 1, wherein the bottom of the body 1 is fixedly connected with a base 2, a protection mechanism is arranged outside the base 2, and a camera 3 is arranged at the bottom of the body 1;
the protection mechanism comprises support rods 4, a first baffle 5, a second baffle 6, a connecting rod 7 and a sleeve 8, wherein the support rods 4 are fixedly connected to the outer side of the base 2, the number of the support rods 4 is multiple, the first baffle 5 is fixedly connected among the support rods 4, the second baffle 6 is slidably connected among the support rods 4, the first baffle 5 is arranged on the outer side of the second baffle 6, the connecting rod 7 is fixedly connected with the second baffle 6, one end, far away from the second baffle 6, of the connecting rod 7 is fixedly connected with the sleeve 8, a vertical rod is fixedly connected between the body 1 and the camera 3, and the sleeve 8 is in threaded connection with the outer side of the vertical rod;
further, in the above technical solution, a transverse plate 9 is fixedly connected to the outer side of the body 1, and a fan blade 10 is arranged on one side of the top of the transverse plate 9, which is far away from the body 1;
further, in the above technical solution, an adjusting assembly is arranged at the bottom of the supporting rod 4, the adjusting assembly includes an outer cylinder 11, an inner cylinder 12 and a stabilizing block 13, the stabilizing block 13 is fixedly connected to the bottom of the inner cylinder 12, the inner cylinder 12 is in threaded connection with the bottom of the outer cylinder 11, and the stabilizing block 13 is beneficial to stable placement of the body 1;
further, in the above technical solution, the bottom of the outer cylinder 11 is provided with a blind hole, an internal thread is arranged inside the blind hole, an external thread is arranged outside the inner cylinder 12, and the external thread is engaged with the internal thread;
further, in the above technical solution, the supporting rods 4 include first supporting rods 401 and second supporting rods 402, the first supporting rods 401 and the second supporting rods 402 are distributed in a staggered manner, through grooves 14 penetrating through the supporting rods are formed in one side of the second supporting rods 402, the second baffle 6 is slidably connected with the through grooves 14, and the through grooves 14 are beneficial to the sliding connection between the second baffle 6 and the second supporting rods 402;
further, in the above technical solution, strip-shaped grooves are formed in both sides of the first support rod 401, the second baffle 6 is matched with the strip-shaped grooves, and the strip-shaped grooves are beneficial to stable connection between the second baffle 6 and the first support rod 401;
further, in the above technical solution, the first baffle 5 is fixedly connected between the first support rod 401 and the second support rod 402, the number of the connecting rods 7 is multiple, and the connecting rods 7 are distributed on the outer side of the base 2 in an annular array;
the implementation mode is specifically as follows: by arranging the adjusting component at the bottom of the supporting rod 4, the unmanned aerial vehicle is placed on the ground when in use, because the inner cylinder 12 is in threaded connection with the outer cylinder 11, the distance that the inner cylinder 12 extends out of the outer cylinder 11 can be adjusted by rotating the inner cylinder 12, so that the height of each supporting rod 4 can be adjusted, the unmanned aerial vehicle can be stably placed and can stably take off, the contact area between the inner cylinder 12 and the ground can be increased by the stabilizing block 13, the stability when the unmanned aerial vehicle is placed can be improved, the first supporting rod 401 and the second supporting rod 402 are distributed on the outer side of the base 2 in an annular array manner, the stability of the body 1 when in placement can be further improved, after use, the sleeve 8 can be rotated, the sleeve 8 can drive the connecting rod 7 to rotate, the connecting rod 7 can drive the second baffle 6 to rotate, the second baffle 6 is in sliding connection with the through groove 14 on the second supporting rod 402, so that the second baffle 6 can pass through the, thereby make second baffle 6 rotate to between second branch 402 and the first branch 401, cooperation through first baffle 5 and second baffle 6, can protect camera 3, prevent to cause the damage to camera 3 in the use, can take off before unmanned aerial vehicle through this structure, improve its stability of placing subaerial, and can carry out good protection to camera 3 of installing on it, be favorable to improving its life, the problem of protecting camera 3 on unmanned aerial vehicle among the prior art has specifically been solved to this embodiment.
This practical theory of operation:
referring to the attached drawings 1-5 of the specification, when in use, an unmanned aerial vehicle is placed on the ground, because the inner cylinder 12 is in threaded connection with the outer cylinder 11, the distance that the inner cylinder 12 extends out of the outer cylinder 11 can be adjusted by rotating the inner cylinder 12, so that the height of each supporting rod 4 can be adjusted, the unmanned aerial vehicle can be stably placed, the contact area between the inner cylinder 12 and the ground can be increased through the stabilizing block 13, the stability when the unmanned aerial vehicle is placed is improved, after the unmanned aerial vehicle is used, the sleeve 8 can be rotated to drive the connecting rod 7 to rotate, the connecting rod 7 can drive the second baffle 6 to rotate, the second baffle 6 is in sliding connection with the through groove 14 on the second supporting rod 402, so that the second baffle 6 can pass through the through groove 14 and be matched with the strip-shaped groove on one side of the first supporting rod 401, so that the second baffle 6 can be rotated between the second supporting rod 402 and the first supporting rod, can protect camera 3, prevent to cause the damage to camera 3 in the use.
While certain exemplary embodiments of the present invention have been described above by way of illustration only, it will be apparent to those of ordinary skill in the art that the described embodiments may be modified in various different ways without departing from the spirit and scope of the present invention. Accordingly, the drawings and description are illustrative in nature and should not be construed as limiting the scope of the invention.
Claims (7)
1. The utility model provides an unmanned aerial vehicle for geographical survey, includes body (1), its characterized in that: the bottom of the body (1) is fixedly connected with a base (2), a protection mechanism is arranged on the outer side of the base (2), and a camera (3) is arranged at the bottom of the body (1);
protection machanism includes branch (4), first baffle (5), second baffle (6), connecting rod (7) and sleeve (8), branch (4) fixed connection is in the base (2) outside, the quantity of branch (4) sets up to a plurality ofly, first baffle (5) fixed connection is between a plurality of branch (4), second baffle (6) sliding connection is between a plurality of branch (4), first baffle (5) set up in the second baffle (6) outside, connecting rod (7) and second baffle (6) fixed connection, the one end and sleeve (8) fixed connection of second baffle (6) are kept away from in connecting rod (7), fixedly connected with montant between body (1) and camera (3), sleeve (8) threaded connection is in the montant outside.
2. A geo-based drone according to claim 1, characterized in that: the fan blade is characterized in that a transverse plate (9) is fixedly connected to the outer side of the body (1), and fan blades (10) are arranged on one side, away from the body (1), of the top of the transverse plate (9).
3. A geo-based drone according to claim 1, characterized in that: the utility model discloses a bearing support, including branch (4), branch (4) bottom is provided with adjusting part, adjusting part includes urceolus (11), inner tube (12) and stabilizing block (13), stabilizing block (13) fixed connection is in inner tube (12) bottom, inner tube (12) threaded connection is in urceolus (11) bottom.
4. A geo-based drone according to claim 3, characterized in that: the bottom of the outer barrel (11) is provided with a blind hole, an internal thread is arranged in the blind hole, an external thread is arranged on the outer side of the inner barrel (12), and the external thread is meshed with the internal thread.
5. A geo-based drone according to claim 1, characterized in that: branch (4) include first branch (401) and second branch (402), first branch (401) and second branch (402) crisscross the distribution, second branch (402) one side is provided with logical groove (14) that run through, second baffle (6) and logical groove (14) sliding connection.
6. A geo-based drone according to claim 5, characterized in that: the two sides of the first supporting rod (401) are provided with strip-shaped grooves, and the second baffle (6) is matched with the strip-shaped grooves.
7. A geo-based drone according to claim 5, characterized in that: first baffle (5) fixed connection is between first branch (401) and second branch (402), the quantity of connecting rod (7) sets up to a plurality ofly, and is a plurality of connecting rod (7) are ring array and distribute in the base (2) outside.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020283392.8U CN212074418U (en) | 2020-03-10 | 2020-03-10 | Unmanned aerial vehicle for geographic exploration |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020283392.8U CN212074418U (en) | 2020-03-10 | 2020-03-10 | Unmanned aerial vehicle for geographic exploration |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212074418U true CN212074418U (en) | 2020-12-04 |
Family
ID=73560212
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020283392.8U Expired - Fee Related CN212074418U (en) | 2020-03-10 | 2020-03-10 | Unmanned aerial vehicle for geographic exploration |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212074418U (en) |
-
2020
- 2020-03-10 CN CN202020283392.8U patent/CN212074418U/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: 20201204 |
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| CF01 | Termination of patent right due to non-payment of annual fee |