CN214875643U - Detector for monitoring homeland resources - Google Patents

Detector for monitoring homeland resources Download PDF

Info

Publication number
CN214875643U
CN214875643U CN202121394927.XU CN202121394927U CN214875643U CN 214875643 U CN214875643 U CN 214875643U CN 202121394927 U CN202121394927 U CN 202121394927U CN 214875643 U CN214875643 U CN 214875643U
Authority
CN
China
Prior art keywords
aerial vehicle
unmanned aerial
wall
vehicle body
terminal
Prior art date
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.)
Active
Application number
CN202121394927.XU
Other languages
Chinese (zh)
Inventor
代国强
丁丽丽
窦林
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN202121394927.XU priority Critical patent/CN214875643U/en
Application granted granted Critical
Publication of CN214875643U publication Critical patent/CN214875643U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Studio Devices (AREA)

Abstract

The utility model discloses a detection instrument for territory resource monitoring, including unmanned aerial vehicle body, camera body and coupling mechanism, coupling mechanism is inside to be provided with terminal and terminal seat, and coupling mechanism is assembled and is used for making camera body and unmanned aerial vehicle body keep fixed to make terminal and terminal seat intercommunication form closed series circuit. The utility model provides a detection instrument for national soil resource control, install camera body and unmanned aerial vehicle body fast and dismantle through coupling mechanism, can guarantee the power supply and the outage of camera body when connecting, can make things convenient for the staff to change the camera body, can reduce staff's work load, thereby can improve staff's work efficiency, come the rotor of protection unmanned aerial vehicle body through the anticollision support arm, when the unmanned aerial vehicle body receives the collision, can reduce the impact force that unmanned aerial vehicle body rotor received, can improve the life of unmanned aerial vehicle body, reduce economic loss.

Description

Detector for monitoring homeland resources
Technical Field
The utility model relates to a device technical field that takes photo by plane relates to a detection instrument for territory resource monitoring particularly.
Background
Aerial photography, also known as aerial photography, aerial photography or aerial photography, refers to the process of shooting the earth landform from the air to obtain a top view.
According to the patent number: CN212022955U discloses a detection instrument for territory resource control, including the device main part, the equal fixed mounting in four corners in outer end of device main part has first connecting seat, inside one side of first connecting seat all is provided with the linking arm, the equal fixed mounting in outer end one side of linking arm has the screw, bottom one side of linking arm all is provided with the bracing piece, bottom one side fixed mounting of device main part has the base support, one side that the bottom of device main part is close to the base support is provided with the camera of taking photo by plane, top one side fixed mounting of camera of taking photo by plane has the axis of rotation, and the axis of rotation runs through inside one side of device main part, top one side fixed mounting of axis of rotation has first bevel gear, one side fixed mounting that the inside of device main part is close to first bevel gear has servo motor. The main technical effects are as follows: through the arranged first connecting seat, when a user needs to store the device main body for use, the user can push the button, then push the clamping rod out of the first connecting seat through the ejector rod, push the limiting rod through the first spring, reset the ejector rod for use, thereby being capable of adjusting the connecting block arranged on the rotating rod, and after the connecting arm is folded on one side of the outer wall of the device main body, the user can conveniently store or carry the device for use, otherwise, when the user needs to use the device, the user can push the clamping rod into the first connecting seat through the second spring arranged in the placing groove in the connecting block, thereby realizing the clamping connection between the first connecting seat and the connecting block for use, the user can take off through the screw propeller, in order to improve the stability of the connecting arm during use, the supporting rod arranged on the second connecting seat can be pulled to the seat bracket, inhale mutually through first magnet and second magnet, then can increase stability through the bracing piece, convenient to use personnel use, better for traditional mode, axis of rotation through setting up, the many snap-on of current aerial photography camera of device of taking photo by plane, need the device main part to change the position and just can realize the multi-angle and shoot, it rotates to drive second bevel gear through servo motor, cooperation through first bevel gear and second bevel gear, the aerial photography camera that drives the axis of rotation bottom setting carries out horizontal rotation, thereby can realize changing the visual angle and shoot, improve the device's practicality, the user of being convenient for uses, better for traditional mode.
In the process of monitoring and shooting by the homeland resources, different lenses are frequently required to be replaced to obtain better shooting effect, most of the cameras of the existing unmanned aerial vehicle are fixedly connected on the unmanned aerial vehicle body and cannot be detached, which brings inconvenience to shooting work, meanwhile, when flying, the unmanned aerial vehicle mainly depends on the lifting force caused by the rotation of the rotor wing to fly, during the flight of the unmanned aerial vehicle, the unmanned aerial vehicle can collide with some obstacles (such as branches and the like), can damage the rotor wing of the unmanned aerial vehicle, thereby make unmanned aerial vehicle damage, for this reason, provide a detection instrument for homeland resource control, the camera that aims at solving unmanned aerial vehicle is fixed connection mostly on the unmanned aerial vehicle body, and unable dismantlement has brought inconvenience and has collided some barriers (for example branch etc.) for shooting work, can cause the damage to unmanned aerial vehicle's rotor to make the problem of unmanned aerial vehicle damage.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a detection instrument for territory resource monitoring, the camera that aims at solving unmanned aerial vehicle is fixed connection mostly on the unmanned aerial vehicle body, can't dismantle, has brought inconvenience and has collided some barriers (for example branch etc.) for shooting work, can cause the damage to unmanned aerial vehicle's rotor to make the problem of unmanned aerial vehicle damage.
In order to achieve the above object, the present invention provides the following technical solutions:
the utility model provides a detection instrument for homeland resource control, includes unmanned aerial vehicle body and camera body, its characterized in that still includes coupling mechanism, coupling mechanism is inside to be provided with terminal and terminal seat, coupling mechanism is assembled and is used for making the camera body with the unmanned aerial vehicle body keeps fixed, so that terminal and terminal seat intercommunication form closed series circuit.
As preferred, the support department fixed mounting of unmanned aerial vehicle body has the anticollision support arm, the anticollision support arm is assembled and is used for reducing the external impact force that unmanned aerial vehicle body rotor received.
Preferably, the fixing rod is fixedly installed on an outer wall of one side of the camera body, the rotating rod is connected to one end of the fixing rod away from the camera body in a shaft-to-shaft manner, the outer wall of the fixing ring is symmetrically and slidably connected with sliding rods, one end of each sliding rod penetrates through and extends to the inner wall of one side of the fixing ring, a limiting piece is fixedly arranged at one end of the sliding rod positioned in the fixing ring, a compression spring is arranged between the sliding rod and the fixing ring, the sliding seat is connected with the outer wall of the top of the fixed rod in a sliding way, the outer wall of one side of the rotating rod is provided with a threaded sleeve, the sliding seat is in threaded connection with the inner wall of the threaded sleeve, the rotating rod is in threaded connection with the fixed ring through the threaded sleeve, the terminal seat is fixedly arranged on the outer wall of one side of the fixed seat, and the terminals are symmetrically arranged on the outer wall of one side of the sliding rod.
As preferred, the anticollision support arm includes extension arm, crashproof board and elastic plate, extension arm fixed mounting in the outer wall of unmanned aerial vehicle body support one side, the one end fixed mounting of extension arm has the arc, the support column is installed to the outer wall symmetry of arc, crashproof board sliding connection in the outer wall of support column, the elastic plate fixed set up in the arc with between the crashproof board, the elastic plate sets up along the arc array.
In the technical scheme, the utility model provides a pair of a detection instrument for territorial resource control has following beneficial effect:
1. the utility model discloses a, install camera body and unmanned aerial vehicle body fast and dismantle through coupling mechanism, can guarantee the power supply and the outage of camera body simultaneously when connecting, can make things convenient for the staff to change the camera body, can reduce staff's work load to can improve staff's work efficiency.
2. The utility model discloses a, protect the rotor of unmanned aerial vehicle body through the anticollision support arm, when the unmanned aerial vehicle body received the collision, can reduce the impact force that unmanned aerial vehicle body rotor received to can prevent that the rotor from receiving the damage when receiving the striking, can improve the life of unmanned aerial vehicle body, reduce economic loss.
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 perspective view of an embodiment of the present invention;
fig. 2 is a schematic view of a mounting position structure of a camera body according to an embodiment of the present invention;
fig. 3 is a schematic view of a mounting position structure of a terminal block according to an embodiment of the present invention;
fig. 4 is a schematic structural view of a connection mechanism according to an embodiment of the present invention;
fig. 5 is a schematic view of a connection relationship of a connection mechanism according to an embodiment of the present invention;
fig. 6 is a schematic structural view of the anti-collision support arm provided by the embodiment of the present invention.
Description of reference numerals:
1. an unmanned aerial vehicle body; 2. a camera body; 3. a connecting mechanism; 31. a terminal; 32. a terminal block; 33. a fixed seat; 34. a fixing ring; 341. a slide bar; 342. a limiting sheet; 35. a sliding seat; 36. fixing the rod; 37. rotating the rod; 371. a threaded sleeve; 4. an anti-collision support arm; 41. an extension arm; 42. an anti-collision plate; 43. an elastic plate; 44. an arc-shaped plate; 45. and (4) a support column.
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.
Referring to fig. 1-6, a detecting instrument for monitoring homeland resources comprises an unmanned aerial vehicle body 1 and a camera body 2, and further comprises a connecting mechanism 3, wherein a terminal 31 and a terminal seat 32 are arranged inside the connecting mechanism 3, and the connecting mechanism 3 is assembled to keep the camera body 2 and the unmanned aerial vehicle body 1 fixed, so that the terminal 31 is communicated with the terminal seat 32 to form a closed series circuit. Install camera body 2 and unmanned aerial vehicle body 1 fast and dismantle through coupling mechanism 3, can guarantee the power supply and the outage of camera body 2 simultaneously when connecting, can make things convenient for the staff to change camera body 2, can reduce staff's work load to staff's work efficiency can be improved.
As shown in fig. 1 and 6, the support department fixed mounting of unmanned aerial vehicle body 1 has anticollision support arm 4, and anticollision support arm 4 is assembled and is used for reducing the external impact force that unmanned aerial vehicle body 1 rotor received. Protect the rotor of unmanned aerial vehicle body 1 through crashproof support arm 4, when unmanned aerial vehicle body 1 receives the collision, can reduce the impact force that 1 rotor of unmanned aerial vehicle body received to can prevent that the rotor from receiving the damage when receiving the striking, can improve unmanned aerial vehicle body 1's life, reduce economic loss. )
As shown in fig. 2, fig. 3, fig. 4 and fig. 5, in order to realize the rapid installation and detachment of the camera body 2 through the connecting mechanism 3, a fixing base 33 is fixedly installed on the outer wall of one side of the unmanned aerial vehicle body 1, a terminal base 32 is fixedly installed on the outer wall of one end of the fixing base 33, and the terminal base 32 and the battery pack of the unmanned aerial vehicle body 1 are electrically connected, so that after the terminal 31 and the terminal base 32 are fixed, the camera body 2 can be supplied with power, so that the camera body 2 can work normally, a fixing ring 34 is fixedly installed on the outer wall of the fixing base 33, a fixing rod 36 is fixedly installed on the outer wall of the camera body 2, the fixing rod 36 is divided into an upper end and a lower end, a rotating rod 37 is rotatably connected to the outer wall of the lower end of the fixing rod 36, a sliding base 35 is slidably connected to the outer wall of the upper end of the fixing rod 36, two terminals 31 are fixedly installed on the outer wall of one end of the sliding base 35, used for matching with the terminal seat 32 to form a closed series circuit, a thread bush 371 is fixedly arranged on one end of the rotating rod 37, threads are arranged on the outer wall and the inner wall of the thread bush 371, the inner wall of the thread bush 35 and the thread bush 371 are in threaded connection, the outer wall of the thread bush 371 is in connection with the inner wall of the fixing ring 34, in order to ensure that the terminal 31 can accurately fall into the terminal seat 32 when in use, a sliding rod 341 is connected on the outer wall of the fixing ring 34 in a sliding way, a limiting sheet 342 is fixedly arranged at one end of the sliding rod 341 positioned in the fixing ring 34, the limiting sheet 342 is always in contact with the outer wall of the fixing seat 33 through a compression spring between the sliding rod 341 and the fixing ring 34, thereby when the terminal 31 moves inwards, the terminal 31 is limited, when in use, a user holds the camera body 2 by hand, and determines the installation direction of the camera body 2, aim at solid fixed ring 34 with thread bush 371, will rotate dwang 37, make the outer wall of thread bush 371 rotatory to solid fixed ring 34 inner wall, when thread bush 371 rotated, make threaded connection slide at the sliding seat 35 of thread bush 371 inner wall, make terminal 31 move to terminal seat 32 in, form closed series circuit, make camera body 2 circular telegram begin work.
As shown in fig. 6, in order to protect the rotor, an anti-collision support arm 4 is fixedly installed on a bracket portion of the main body 1 of the unmanned aerial vehicle, wherein an extension arm 41 is directly and fixedly installed on the bracket of the main body 1 of the unmanned aerial vehicle, an arc-shaped plate 44 is fixedly installed on one end of the extension arm 41 away from the main body 1 of the unmanned aerial vehicle, the arc-shaped plate 44 is used for matching the shape of the rotating rotor to prevent the rotor from colliding with the arc-shaped plate 44 when rotating and damaging the rotor, support posts 45 are symmetrically installed on the outer wall of the arc-shaped plate 44, an anti-collision plate 42 is slidably connected between the two support posts 45, the anti-collision plate 42 is used for receiving external impact, an elastic plate 43 is arranged between the anti-collision plate 42 and the arc-shaped plate 44, the elastic plate 43 is of an arc-shaped structure, when the impact is received, the anti-collision plate 42 slides inwards to press the elastic plate 43, so that the elastic plate 43 is elastically deformed, reducing the impact force and thus reducing the impact strength.
The electrical components presented in the document are all electrically connected with an external master controller and a 12V lithium battery, and the master controller can be a conventional known device controlled by a computer and the like.
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 (5)

1. The utility model provides a detection instrument for homeland resource control, includes unmanned aerial vehicle body (1) and camera body (2), its characterized in that still includes coupling mechanism (3), coupling mechanism (3) inside is provided with terminal (31) and terminal seat (32), coupling mechanism (3) are assembled and are used for making camera body (2) with unmanned aerial vehicle body (1) keeps fixed, so that terminal (31) and terminal seat (32) intercommunication form closed series circuit.
2. A detection instrument for territorial resource control according to claim 1, characterized in that the support of unmanned aerial vehicle body (1) is fixedly provided with an anti-collision support arm (4), and the anti-collision support arm (4) is assembled to reduce the external impact force to which the rotor of unmanned aerial vehicle body (1) is subjected.
3. The detecting instrument for monitoring the territorial resources according to claim 1, wherein the connecting mechanism (3) comprises a fixed seat (33), a fixed ring (34), a sliding seat (35), a fixed rod (36) and a rotating rod (37), the fixed seat (33) is fixedly installed on the outer wall of one side of the bottom of the unmanned aerial vehicle body (1), the fixed ring (34) is fixedly installed on the outer wall of the fixed seat (33), the terminal seat (32) is fixedly installed in the fixed seat (33), the terminal seat (32) is electrically connected with a battery pack inside the unmanned aerial vehicle body (1), and the terminal (31) is electrically connected with the camera body (2).
4. The detecting instrument for monitoring the national resources as claimed in claim 3, wherein the fixing rod (36) is fixedly installed on the outer wall of one side of the camera body (2), the rotating rod (37) is coupled to one end of the fixing rod (36) far away from the camera body (2), the outer wall of the fixing ring (34) is symmetrically and slidably connected with a sliding rod (341), one end of the sliding rod (341) penetrates through and extends to the inner wall of one side of the fixing ring (34), one end of the sliding rod (341) located in the fixing ring (34) is fixedly installed with a limiting piece (342), a compression spring is arranged between the sliding rod (341) and the fixing ring (34), the sliding seat (35) is slidably connected to the outer wall of the top of the fixing rod (36), and the outer wall of one side of the rotating rod (37) is provided with a threaded sleeve (371), sliding seat (35) threaded connection in the inner wall of thread bush (371), dwang (37) through thread bush (371) with solid fixed ring (34) keep threaded connection, terminal seat (32) fixed mounting in the outer wall of fixing base (33) one side, terminal (31) symmetry install in the outer wall of sliding rod (341) one side.
5. The detector for monitoring the national resources as claimed in claim 2, wherein the anti-collision support arm (4) comprises an extension arm (41), an anti-collision plate (42) and an elastic plate (43), the extension arm (41) is fixedly mounted on the outer wall of one side of the bracket of the unmanned aerial vehicle body (1), an arc plate (44) is fixedly mounted at one end of the extension arm (41), support columns (45) are symmetrically mounted on the outer wall of the arc plate (44), the anti-collision plate (42) is slidably connected to the outer wall of the support columns (45), the elastic plate (43) is fixedly arranged between the arc plate (44) and the anti-collision plate (42), and the elastic plate (43) is arranged along an arc array.
CN202121394927.XU 2021-06-22 2021-06-22 Detector for monitoring homeland resources Active CN214875643U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202121394927.XU CN214875643U (en) 2021-06-22 2021-06-22 Detector for monitoring homeland resources

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202121394927.XU CN214875643U (en) 2021-06-22 2021-06-22 Detector for monitoring homeland resources

Publications (1)

Publication Number Publication Date
CN214875643U true CN214875643U (en) 2021-11-26

Family

ID=78929747

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202121394927.XU Active CN214875643U (en) 2021-06-22 2021-06-22 Detector for monitoring homeland resources

Country Status (1)

Country Link
CN (1) CN214875643U (en)

Similar Documents

Publication Publication Date Title
CN204916210U (en) Cloud platform overhead electric power patrols line unmanned aerial vehicle
CN112744104B (en) Unmanned aerial vehicle descending charging device and unmanned aerial vehicle system
CN111439143A (en) Unmanned aerial vehicle recovery system and recovery method thereof
CN210708463U (en) Storage device for aerospace model
CN214875643U (en) Detector for monitoring homeland resources
CN209538633U (en) It is a kind of that formula lifting device is gone along with sb. to guard him from construction based on civil engineering house
CN107352023B (en) Aircraft with a flight control device
CN212099369U (en) Multi-angle engineering three-dimensional model information acquisition device based on unmanned aerial vehicle
CN216241104U (en) Intelligent aerogenerator wind vane device
CN216509142U (en) Rotatable positioning device for aerial survey unmanned aerial vehicle camera
CN215361883U (en) Be used for surveying and mapping unmanned aerial vehicle that takes photo by plane
CN211063481U (en) Double-motor device capable of rotating clockwise and anticlockwise synchronously
CN107176289B (en) Aircraft with a flight control device
CN212556753U (en) Unmanned aerial vehicle that sponge city quality of water environmental monitoring used
CN207809770U (en) Smart city unmanned plane
CN220616199U (en) Photovoltaic power plant inspection device
CN220616198U (en) Unmanned aerial vehicle with strike unit
CN116119063B (en) Mapping unmanned aerial vehicle energy supplementing relay platform and application method
CN212148450U (en) Unmanned aerial vehicle recovery system
CN215245531U (en) Environment monitoring unmanned aerial vehicle
CN217533234U (en) Self-locking anti-collision device for cluster type unmanned aerial vehicle low-altitude photography
CN216301453U (en) Novel infrared waterproof unmanned aerial vehicle of patrolling
CN218949526U (en) Unmanned aerial vehicle is patrolled and examined to electric power
CN217064261U (en) Protective structure's control security protection equipment
CN214875527U (en) Structure suitable for connecting tail wing to fuselage

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant