CN217918427U - Fire control unmanned aerial vehicle - Google Patents

Fire control unmanned aerial vehicle Download PDF

Info

Publication number
CN217918427U
CN217918427U CN202222442679.2U CN202222442679U CN217918427U CN 217918427 U CN217918427 U CN 217918427U CN 202222442679 U CN202222442679 U CN 202222442679U CN 217918427 U CN217918427 U CN 217918427U
Authority
CN
China
Prior art keywords
organism
aerial vehicle
unmanned aerial
fire
camera
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
CN202222442679.2U
Other languages
Chinese (zh)
Inventor
邓永兵
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.)
Guogu Aviation Technology Hangzhou Co ltd
Original Assignee
Guogu Aviation Technology Hangzhou Co ltd
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 Guogu Aviation Technology Hangzhou Co ltd filed Critical Guogu Aviation Technology Hangzhou Co ltd
Priority to CN202222442679.2U priority Critical patent/CN217918427U/en
Application granted granted Critical
Publication of CN217918427U publication Critical patent/CN217918427U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Manipulator (AREA)

Abstract

The utility model discloses a fire control unmanned aerial vehicle, which comprises a bod, the outer surface mounting of organism has the screw, the mechanism of making a video recording is installed to the bottom of organism, the below of the mechanism of making a video recording is provided with the mechanism of putting out a fire, the lower surface bilateral symmetry of organism is connected with branch, the inboard of branch is provided with buffer gear. The utility model discloses a be provided with a series of structures for can be accurate carry out the water spray to the position of firing and put out a fire, have buffer gear simultaneously, can carry out the buffer protection to the organism when descending.

Description

Fire control unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a fire control unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, and can reach positions which cannot be reached by human beings, so that the unmanned aerial vehicle can play a very large auxiliary role in high-rise fire extinguishment, and the figure of the unmanned aerial vehicle can be often seen in the field of fire fighting.
But present fire control unmanned aerial vehicle is using because it is in the high altitude and is difficult to control, leads to the unable accurate alignment position of firing in spun water source, needs the fire fighter to carry out follow-up additional adjustment, and is more troublesome, and its organism itself lacks corresponding buffer gear simultaneously, leads to unable buffering impact force when descending.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a fire control unmanned aerial vehicle to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides a fire control unmanned aerial vehicle, includes the organism, the surface mounting of organism has the screw, the mechanism of making a video recording is installed to the bottom of organism, the below of the mechanism of making a video recording is provided with the mechanism of putting out a fire, the lower surface bilateral symmetry of organism is connected with branch, the inboard of branch is provided with buffer gear.
Preferably, the surfaces of the left end and the right end of the machine body are both connected with a convex plate, one side of the machine body is provided with a wind power detector, and the bottom end of the wind power detector is connected with the convex plate.
Preferably, the camera shooting mechanism comprises an adjusting block and a camera, the adjusting block is located at the bottom middle position of the machine body, the camera is installed on the lower surface of the adjusting block, one end surface of the adjusting block is connected with a driving wheel, the driving wheel is located inside the machine body, and one end surface of the driving wheel is connected with a motor.
Preferably, the mechanism of putting out a fire includes sleeve and gun sight, the sleeve is located the camera under, the gun sight is connected at telescopic top, the telescopic outside is provided with the connecting plate, telescopic one end runs through the connecting plate and is connected with from the driving wheel, the surface connection from the driving wheel has the drive belt, the other end and the action wheel of drive belt are connected.
Preferably, the position of the sighting telescope corresponds to the position of the camera.
Preferably, a hatch door is connected to a front end surface of the machine body, and the hatch door is located at a front side of the motor.
Preferably, buffer gear includes connecting rod, buffer beam, contact plate and spring, the lower surface at the flange is connected to the connecting rod, the bottom at the connecting rod is connected to the buffer beam, contact plate swing joint is in the bottom of buffer beam, the spring coupling is at the upper surface of buffer beam, and the spring is located the inside of connecting rod.
Compared with the prior art, the beneficial effects of the utility model are that:
1. this fire control unmanned aerial vehicle through setting up camera shooting mechanism and the mechanism of putting out a fire for when putting out a fire, can make a video recording to the position of getting on fire, make a video recording simultaneously and aim at through the gun sight between the mechanism of putting out a fire, thereby make the water of putting out a fire can be accurate spout to the camera position of shooing.
2. This fire control unmanned aerial vehicle, through setting up buffer gear, buffer gear makes this unmanned aerial vehicle when descending, and it receives the impact force on ground and can obtain the buffering to reduce the damage to the organism, safety more.
Drawings
Fig. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic view of the structure of the camera mechanism and the fire extinguishing mechanism of the utility model;
fig. 3 is a schematic view of the structure of the buffer mechanism of the present invention.
In the figure: 1. a body; 2. a propeller; 3. a convex plate; 4. a wind power detector; 5. a cabin door; 6. a regulating block; 7. a driving wheel; 8. a motor; 9. a transmission belt; 10. a driven wheel; 11. a connecting plate; 12. a sleeve; 13. a sighting telescope; 14. a camera; 15. a connecting rod; 16. a buffer rod; 17. a contact plate; 18. a spring; 19. a support rod.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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 all belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of the description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Example 1
As shown in fig. 1 and fig. 2, this embodiment fire control unmanned aerial vehicle, including organism 1, the surface mounting of organism 1 has screw 2, screw 2 is rotated at a high speed by relevant actuating mechanism's control, thereby it flies to drive organism 1, relevant actuating mechanism is relevant field prior art, not many explanations, camera shooting mechanism is installed to organism 1's bottom, camera shooting mechanism makes this unmanned aerial vehicle can make a video recording to relevant region when high altitude flight, camera shooting mechanism's below is provided with the mechanism of putting out a fire, it puts out a fire to put out a fire to the mechanism of putting out a fire, organism 1's lower surface bilateral symmetry is connected with branch 19, branch 19 supports organism 1, branch 19's inboard is provided with buffer gear, buffer gear makes this unmanned aerial vehicle can cushion organism 1 when descending.
Specifically, both ends surface all is connected with flange 3 about organism 1, and one side of organism 1 is provided with wind power detection instrument 4, and wind power detection instrument 4's bottom is connected with flange 3, and wind power detection instrument 4 is the technical product that has on the market, and its specific model chooses for use according to actual need, and its connected mode with flange 3 can be welding or bolt fastening, can survey wind-force at the in-process of this unmanned aerial vehicle flight through wind power detection instrument 4.
Further, the mechanism of making a video recording includes regulating block 6 and camera 14, regulating block 6 is located organism 1's bottom intermediate position, camera 14 installs the lower surface at regulating block 6, the one end surface connection of regulating block 6 has action wheel 7, action wheel 7 is located organism 1's inside, the one end surface connection of action wheel 7 has motor 8, motor 8 is common technical product on the market, its specific model chooses for use according to actual need, rotate through motor 8 control action wheel 7, action wheel 7 drives regulating block 6 and rotates, thereby make camera 14 can change the angle of making a video recording.
Further, the mechanism of putting out a fire includes sleeve 12 and gun sight 13, sleeve 12 is located camera 14 under, gun sight 13 is connected at sleeve 12's top, sleeve 12's the outside is provided with connecting plate 11, sleeve 12's one end runs through connecting plate 11 and is connected with from driving wheel 10, the surface connection from driving wheel 10 has drive belt 9, the other end and the action wheel 7 of drive belt 9 are connected, when needing this unmanned aerial vehicle to assist to put out a fire, insert the inside of sleeve 12 with the water pipe of fire gun and fix, this unmanned aerial vehicle takes off afterwards and drives the water pipe and remove in the high altitude, can drive near the source of a fire through unmanned aerial vehicle and spray water and put out a fire near this moment.
Furthermore, the position of the sighting telescope 13 corresponds to the position of the camera 14, so that the camera 14 can be aligned with the sighting telescope 13 during shooting when fire extinguishing is performed, and water sprayed from a water pipe can reach a preset position.
Further, the front end surface of the machine body 1 is connected with a cabin door 5, the cabin door 5 is located on the front side of the motor 8, and the motor 8 can be overhauled by opening the cabin door 5.
The using method of the embodiment comprises the following steps: at first insert the inside of sleeve 12 with the water pipe of fire gun and fix, control propeller 2 rotates afterwards and make this unmanned aerial vehicle take off, after taking off suitable position, carry out remote control to motor 8 through 1 inside wireless control module of organism, make action wheel 7 rotate, it rotates from driving wheel 10 this moment together, when action wheel 7 rotates, it will drive regulating block 6 and rotate, thereby make camera 14 rotate, carry out accurate the making a video recording to the position of firing, and simultaneously, because from the rotation of driving wheel 10, make sleeve 12 and gun sight 13 along with camera 14 rotate with the angle together, and then make the inside water pipe of sleeve 12 can be to camera 14 position of shining, thereby carry out accurate putting out a fire.
Example 2
This embodiment fire control unmanned aerial vehicle's structure is the same basically with embodiment 1 fire control unmanned aerial vehicle's structure, and its difference lies in: buffer gear includes connecting rod 15, buffer beam 16, contact plate 17 and spring 18, and connecting rod 15 is connected at the lower surface of flange 3, and buffer beam 16 is connected in the bottom of connecting rod 15, and contact plate 17 swing joint is in the bottom of buffer beam 16, and spring 18 is connected at the upper surface of buffer beam 16 to dispose the attenuator, and spring 18 is located the inside of connecting rod 15, and organism 1 when descending through spring 18, the impact force that it received will diminish (see fig. 3).
The using method of the embodiment comprises the following steps: when organism 1 descends, this moment because contact plate 17 is less than the bottom of branch 19 in its position of natural state, consequently contact plate 17 will contact with ground earlier, this moment is according to the roughness on ground, contact plate 17 rotates on buffer beam 16 and carries out the change of angle, with laminating ground, buffer beam 16 receives extrusion compression spring 18 simultaneously, spring 18 absorbs deformation with partial impact force, and then reduce the impact that organism 1 received, simultaneously because organism 1 dead weight itself, spring 18 will be in compression state always, the bounce-back can not appear.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (7)

1. The utility model provides a fire control unmanned aerial vehicle, includes organism (1), its characterized in that: the utility model discloses a fire fighting robot, including organism (1), the outer surface mounting of organism (1) has screw (2), the mechanism of making a video recording is installed to the bottom of organism (1), the below of the mechanism of making a video recording is provided with the mechanism of putting out a fire, the lower surface bilateral symmetry of organism (1) is connected with branch (19), the inboard of branch (19) is provided with buffer gear.
2. A fire fighting unmanned aerial vehicle as defined in claim 1, wherein: the wind power generation device is characterized in that the surfaces of the left end and the right end of the machine body (1) are connected with the convex plates (3), a wind power detector (4) is arranged on one side of the machine body (1), and the bottom end of the wind power detector (4) is connected with the convex plates (3).
3. A fire fighting unmanned aerial vehicle as defined in claim 1, wherein: camera shooting mechanism includes regulating block (6) and camera (14), regulating block (6) are located the bottom intermediate position of organism (1), the lower surface at regulating block (6) is installed in camera (14), the one end surface of regulating block (6) is connected with action wheel (7), action wheel (7) are located the inside of organism (1), the one end surface of action wheel (7) is connected with motor (8).
4. A fire fighting unmanned aerial vehicle as defined in claim 1, wherein: fire extinguishing mechanism includes sleeve (12) and gun sight (13), sleeve (12) are located camera (14) under, the top at sleeve (12) is connected in gun sight (13), the outside of sleeve (12) is provided with connecting plate (11), the one end of sleeve (12) is run through connecting plate (11) and is connected with from driving wheel (10), the surface connection from driving wheel (10) has drive belt (9), the other end and the action wheel (7) of drive belt (9) are connected.
5. A fire fighting unmanned aerial vehicle as defined in claim 4, wherein: the position of the sighting telescope (13) corresponds to the position of the camera (14).
6. A fire fighting unmanned aerial vehicle as defined in claim 1, wherein: the front end surface of the machine body (1) is connected with a cabin door (5), and the cabin door (5) is positioned on the front side of the motor (8).
7. A fire fighting unmanned aerial vehicle as defined in claim 1, wherein: buffer gear includes connecting rod (15), buffer beam (16), contact plate (17) and spring (18), the lower surface at flange (3) is connected in connecting rod (15), the bottom at connecting rod (15) is connected in buffer beam (16), contact plate (17) swing joint is in the bottom of buffer beam (16), the upper surface at buffer beam (16) is connected in spring (18), and spring (18) are located the inside of connecting rod (15).
CN202222442679.2U 2022-09-15 2022-09-15 Fire control unmanned aerial vehicle Active CN217918427U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202222442679.2U CN217918427U (en) 2022-09-15 2022-09-15 Fire control unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202222442679.2U CN217918427U (en) 2022-09-15 2022-09-15 Fire control unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN217918427U true CN217918427U (en) 2022-11-29

Family

ID=84173780

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202222442679.2U Active CN217918427U (en) 2022-09-15 2022-09-15 Fire control unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN217918427U (en)

Similar Documents

Publication Publication Date Title
US5426476A (en) Aircraft video camera mount
CN107315417A (en) A kind of Hydrophobicity of Composite Insulator detection means based on unmanned plane
CN217918427U (en) Fire control unmanned aerial vehicle
CN213948802U (en) A shoot device of making a video recording for disaster prevention unmanned aerial vehicle
CN213323689U (en) Unmanned aerial vehicle water ecology remote sensing monitoring system
CN210235335U (en) Automatic device that slowly falls of unmanned aerial vehicle based on HY-SRF05 ultrasonic wave module
CN114030629B (en) High-freedom-degree adjusting type security monitoring equipment for unmanned aerial vehicle
CN210882619U (en) Fire control unmanned aerial vehicle
CN216435111U (en) Warehouse fire initial stage fire alarm unmanned aerial vehicle
CN214112863U (en) Novel six-rotor unmanned reconnaissance helicopter induction system
CN219134498U (en) Unmanned aerial vehicle with waterlogging monitoring
CN220004551U (en) Unmanned aerial vehicle electric insulation spraying device with protection machanism
CN220221129U (en) Be applied to carrier-borne helicopter auxiliary landing's camera installing support
CN220996807U (en) Unmanned aerial vehicle of screw collision is prevented
CN211281460U (en) Unmanned aerial vehicle for environmental monitoring
CN212890983U (en) Unmanned aerial vehicle with monitoring function
CN205022851U (en) Undercarriage is fixed unmanned aerial vehicle
CN211076371U (en) Forest unmanned aerial vehicle camera and camera device
CN111114812A (en) Unmanned aerial vehicle convenient to direction with balance mechanism
CN215972164U (en) Ship cabin close-range detection unmanned aerial vehicle
CN212667648U (en) Plant protection unmanned aerial vehicle with stable landing
CN212556834U (en) Unmanned aerial vehicle patrols line nacelle
CN213323736U (en) Unmanned aerial vehicle patrols and examines that possesses monitoring alarm function
CN215323268U (en) Unmanned aerial vehicle carries AI nacelle
CN214729633U (en) Unmanned aerial vehicle flight anticollision protection architecture

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant