CN214729722U - Long service life's environmental monitoring unmanned aerial vehicle - Google Patents

Long service life's environmental monitoring unmanned aerial vehicle Download PDF

Info

Publication number
CN214729722U
CN214729722U CN202120151152.7U CN202120151152U CN214729722U CN 214729722 U CN214729722 U CN 214729722U CN 202120151152 U CN202120151152 U CN 202120151152U CN 214729722 U CN214729722 U CN 214729722U
Authority
CN
China
Prior art keywords
block
fixedly connected
aerial vehicle
unmanned aerial
environmental monitoring
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.)
Expired - Fee Related
Application number
CN202120151152.7U
Other languages
Chinese (zh)
Inventor
王赵明
谢洪波
杨岳华
章康勇
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.)
Zhejiang Jiaotou Expressway Construction Management Co ltd
Research Institute of Highway Ministry of Transport
Original Assignee
Zhejiang Jiaotou Expressway Construction Management Co ltd
Research Institute of Highway Ministry of Transport
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 Zhejiang Jiaotou Expressway Construction Management Co ltd, Research Institute of Highway Ministry of Transport filed Critical Zhejiang Jiaotou Expressway Construction Management Co ltd
Application granted granted Critical
Publication of CN214729722U publication Critical patent/CN214729722U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Forklifts And Lifting Vehicles (AREA)

Abstract

The utility model discloses an environment monitoring unmanned aerial vehicle with long service life, which comprises a flight assembly and a working assembly, wherein the working assembly is fixedly arranged inside the flight assembly; the flight subassembly includes the center block, the undercarriage is installed to the bottom of center block, the side-mounting of center block has the backup pad, flying motor is installed to the bottom of backup pad, the output shaft at flying motor top runs through the backup pad and extends to its top fixed mounting and has the flight blade. The utility model discloses a mutually supporting of flight subassembly and work subassembly has realized a long service life's environmental monitoring unmanned aerial vehicle, when not using, can protect the work main part well to, still promoted whole environmental monitoring unmanned aerial vehicle's shock resistance, effectively avoid the effort that external vibrations produced directly to use in the work main part, make whole environmental monitoring unmanned aerial vehicle have longer life, the practicality is high, is fit for using widely.

Description

Long service life's environmental monitoring unmanned aerial vehicle
Technical Field
The utility model relates to an environmental monitoring technical field specifically is a long service life's environmental monitoring unmanned aerial vehicle.
Background
At the in-process that carries out environmental monitoring, often need use environmental monitoring unmanned aerial vehicle, current environmental monitoring unmanned aerial vehicle can not protect operating mechanism well to current environmental monitoring unmanned aerial vehicle antidetonation effect is unsatisfactory, and when the user, operating mechanism takes place to damage easily, just at this moment influences whole unmanned aerial vehicle's life easily, and the practicality is low.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a long service life's environmental monitoring unmanned aerial vehicle to solve the problem that proposes in the background art.
In order to achieve the above object, the utility model provides a following technical scheme: an environment monitoring unmanned aerial vehicle with long service life comprises a flight assembly and a working assembly, wherein the working assembly is fixedly arranged in the flight assembly;
the flying assembly comprises a center block, the bottom of the center block is provided with an undercarriage, the side surface of the center block is provided with a support plate, the bottom of the support plate is provided with a flying motor, an output shaft at the top of the flying motor penetrates through the support plate and extends to the upper part of the support plate to be fixedly provided with a flying blade, and the bottom of the center block is provided with a hidden groove;
the working assembly comprises two slide rails, the tops of the slide rails are fixedly connected with the top of the inner wall of the hidden groove, the surfaces of the slide rails are connected with slide blocks in a sliding manner, the two slide blocks are fixedly connected through a movable plate, the left side and the right side of the bottom of the movable plate are fixedly connected with baffle plates, the two baffle plates are fixedly connected through a cross rod, the surface of the cross rod is connected with a transverse moving block in a sliding manner, transverse springs are sleeved on the surfaces of the cross rod and positioned on the left side and the right side of the transverse moving block, the baffle plates are fixedly connected with the transverse moving block through the transverse springs, the left side and the right side of the bottom of the transverse moving block are fixedly connected with telescopic rods, the bottom ends of the two telescopic rods are fixedly connected through an installation block, vertical springs are sleeved on the surface of the telescopic rods, the transverse moving block is fixedly connected with the installation block through the vertical springs, and the bottom of the installation block is provided with a working main body, the left and right sides of work main part all is provided with the cardboard, the cardboard is close to the first fixture block of top fixedly connected with of work main part one side, one side that first fixture block is close to the work main part runs through the slider and extends to its inside rather than swing joint, the cardboard is close to the bottom fixedly connected with second fixture block of work main part one side, one side fixedly connected with movable rod that the work main part was kept away from to the cardboard, spacing spring has been cup jointed on the surface of movable rod, the one end fixedly connected with that the cardboard was kept away from to the movable rod draws the piece.
Preferably, the bottom end of the sliding rail is fixedly connected with an anti-falling block.
Preferably, one end of the limiting spring, which is close to the working main body, is fixedly connected with the clamping plate, and one end of the limiting spring, which is far away from the clamping plate, is fixedly connected with the central block.
Preferably, the interlocking rod is movably connected with the central block.
Preferably, the bottom of the central block is provided with a cover plate matched with the hidden groove.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a mutually supporting of flight subassembly and work subassembly has realized a long service life's environmental monitoring unmanned aerial vehicle, when not using, can protect the work main part well to, still promoted whole environmental monitoring unmanned aerial vehicle's shock resistance, effectively avoid the effort that external vibrations produced directly to use in the work main part, make whole environmental monitoring unmanned aerial vehicle have longer life, the practicality is high, is fit for using widely.
2. The utility model discloses a set up the anticreep piece, avoid the slider to break away from with the surface from the slide rail, through setting up the apron, played the effect of protection work main part.
Drawings
FIG. 1 is a structural section view in elevation of the present invention;
fig. 2 is a schematic structural diagram of a top view of the present invention;
FIG. 3 is a structural section view of a front view of the working assembly of the present invention;
fig. 4 is a schematic structural diagram of the front view of the cover plate of the present invention.
In the figure: the flying assembly comprises a flying assembly 1, a center block 101, a landing gear 102, a supporting plate 103, a flying motor 104, a flying blade 105, a hidden groove 106, a working assembly 2, a sliding rail 201, a sliding block 202, a moving plate 203, a baffle 204, a cross bar 205, a transverse moving block 206, a transverse spring 207, a telescopic rod 208, an installation block 209, a vertical spring 210, a working body 211, a clamping plate 212, a first clamping block 213, a second clamping block 214, a movable rod 215, a limiting spring 216, a pulling block 217, an anti-dropping block 3 and a cover plate 4.
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. 1-4, an environmental monitoring unmanned aerial vehicle with long service life includes a flight assembly 1 and a working assembly 2, wherein the working assembly 2 is fixedly installed inside the flight assembly 1.
The flying assembly 1 comprises a center block 101, a landing gear 102 is mounted at the bottom of the center block 101, a support plate 103 is mounted on the side surface of the center block 101, a flying motor 104 is mounted at the bottom of the support plate 103, an output shaft at the top of the flying motor 104 penetrates through the support plate 103 and extends to the upper side of the support plate to be fixedly provided with flying blades 105, and a hidden groove 106 is formed in the bottom of the center block 101.
The working assembly 2 comprises two sliding rails 201, the top of the sliding rail 201 is fixedly connected with the top of the inner wall of the hidden groove 106, the surface of the sliding rail 201 is connected with a sliding block 202 in a sliding manner, the bottom end of the sliding rail 201 is fixedly connected with an anti-falling block 3, the sliding block 202 is prevented from being separated from the surface of the sliding rail 201 by arranging the anti-falling block 3, the two sliding blocks 202 are fixedly connected through a moving plate 203, the left side and the right side of the bottom of the moving plate 203 are fixedly connected with baffles 204, the two baffles 204 are fixedly connected through a cross rod 205, the surface of the cross rod 205 is connected with a transverse moving block 206 in a sliding manner, the transverse springs 207 are sleeved on the surface of the cross rod 205 and positioned on the left side and the right side of the transverse moving block 206, the baffles 204 are fixedly connected with the transverse moving block 206 through the transverse springs 207, the left side and the right side of the bottom of the transverse moving block 206 are fixedly connected with telescopic rods 208, the bottom ends of the two telescopic rods 208 are fixedly connected through an installation block 209, the surface of the telescopic rods 208 is sleeved with a vertical spring 210, the transverse moving block 206 is fixedly connected with the mounting block 209 through a vertical spring 210, a working main body 211 is mounted at the bottom of the mounting block 209, the working main body 211 can be a gas detector in the prior art, the specific model is not described in detail here, a cover plate 4 matched with the hidden groove 106 is arranged at the bottom of the central block 101, the function of protecting the working main body 211 is achieved by arranging the cover plate 4, as is apparent from the description drawing, a rubber block is arranged at the top of the cover plate 4 and is arranged for enabling the cover plate 4 to be connected with the central block 101 more firmly, clamping plates 212 are arranged at the left side and the right side of the working main body 211, a first clamping block 213 is fixedly connected at the top of one side of the clamping plate 212 close to the working main body 211, one side of the first clamping block 213 close to the working main body 211 penetrates through the sliding block 202 and extends to the inside to be movably connected with the sliding block, and a second clamping block 214 is fixedly connected at the bottom of one side of the clamping plate 212 close to the working main body 211, the first fixture block 213 and the second fixture block 214 are identical in size, a movable rod 215 is fixedly connected to one side of the clamping plate 212 far away from the working main body 211, the movable rod 215 is movably connected with the central block 101, the central block 101 cannot influence the movable rod 215 to move left and right, a limiting spring 216 is sleeved on the surface of the movable rod 215, one end, close to the working main body 211, of the limiting spring 216 is fixedly connected with the clamping plate 212, one end, far away from the clamping plate 212, of the limiting spring 216 is fixedly connected with the central block 101, one end, far away from the clamping plate 212, of the movable rod 215 is fixedly connected with a pull block 217, through the mutual matching of the flying component 1 and the working component 2, the environment monitoring unmanned aerial vehicle with long service life is realized, when the unmanned aerial vehicle is not used, the working main body 211 can be well protected, the anti-shock capability of the whole environment monitoring unmanned aerial vehicle is improved, and the direct action force generated by external shock is effectively avoided from acting on the working main body 211, make whole environmental monitoring unmanned aerial vehicle have longer life, the practicality is high, is fit for using widely.
When the unmanned aerial vehicle is used, when the unmanned aerial vehicle is in the state shown in the figure, the whole working main body 211 is positioned inside the central block 101, the cover plate 4 also shields the hidden groove 106, the working main body 211 is well protected, when the whole unmanned aerial vehicle is needed to be used, the cover plate 4 is taken down, the two pull blocks 217 are respectively pulled to two sides, the pull blocks 217 drive the first fixture block 213 and the second fixture block 214 to move through the fixture plates 212, the working main body 211 can fall due to gravity, the sliding block 202 slides downwards on the surface of the sliding rail 201, it needs to be noted that the falling process can be artificially controlled, namely before the pull blocks 217 are pulled, the whole unmanned aerial vehicle is firstly inclined, then the unmanned aerial vehicle is slowly erected, the erected direction is also the direction shown in the figure, therefore, the sliding block 202 slowly moves on the sliding rail 201, the bottom of the sliding block 202 is contacted with the top of the anti-off block 3, the pull blocks 217 are loosened, the limiting spring 216 drives the second fixture block 214 to move through the clamping plate 212, the second fixture block 214 can be inserted into the sliding block 202, in the using process, due to the relative motion principle of physics, the transverse moving block 206 can move on the surface of the cross rod 205, the transverse spring 207 can be stretched or compressed, the transverse moving block 206 and the mounting block 209 can move up and down relatively, and the vertical spring 210 can be compressed or stretched, so that the service life of the working main body 211 is well guaranteed.
In summary, the following steps: this long service life's environmental monitoring unmanned aerial vehicle through the mutually supporting of flight subassembly 1 and work subassembly 2, has solved the problem of proposing in the background art.
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 (5)

1. The utility model provides a long service life's environmental monitoring unmanned aerial vehicle, includes flight subassembly (1) and work subassembly (2), its characterized in that: the working assembly (2) is fixedly arranged in the flying assembly (1);
the flying assembly (1) comprises a center block (101), an undercarriage (102) is installed at the bottom of the center block (101), a support plate (103) is installed on the side face of the center block (101), a flying motor (104) is installed at the bottom of the support plate (103), an output shaft at the top of the flying motor (104) penetrates through the support plate (103) and extends to the upper side of the support plate to be fixedly provided with flying blades (105), and a hidden groove (106) is formed in the bottom of the center block (101);
the working assembly (2) comprises two sliding rails (201), the tops of the sliding rails (201) are fixedly connected with the top of the inner wall of the hidden groove (106), the sliding blocks (202) are connected to the surface of the sliding rails (201) in a sliding manner, the two sliding blocks (202) are fixedly connected with each other through a moving plate (203), the left side and the right side of the bottom of the moving plate (203) are fixedly connected with baffles (204), the two baffles (204) are fixedly connected with each other through a cross rod (205), the surface of the cross rod (205) is connected with a transverse moving block (206) in a sliding manner, transverse springs (207) are sleeved on the surface of the cross rod (205) and positioned on the left side and the right side of the transverse moving block (206), the baffles (204) are fixedly connected with the transverse moving block (206) through the transverse springs (207), the left side and the right side of the bottom of the transverse moving block (206) are fixedly connected with telescopic rods (208), and the bottom ends of the two telescopic rods (208) are fixedly connected through a mounting block (209), the surface of the telescopic rod (208) is sleeved with a vertical spring (210), the transverse moving block (206) is fixedly connected with the mounting block (209) through the vertical spring (210), the bottom of the mounting block (209) is provided with a working main body (211), clamping plates (212) are arranged on the left side and the right side of the working main body (211), the top of one side, close to the working main body (211), of each clamping plate (212) is fixedly connected with a first clamping block (213), one side, close to the working main body (211), of each first clamping block (213) penetrates through the sliding block (202) and extends to the inside of the sliding block (202) to be movably connected with the sliding block, the bottom of one side, close to the working main body (211), of each clamping plate (212) is fixedly connected with a second clamping block (214), one side, far away from the working main body (211), of each clamping plate (212) is fixedly connected with a movable rod (215), and the surface of each movable rod (215) is sleeved with a limiting spring (216), one end of the movable rod (215) far away from the clamping plate (212) is fixedly connected with a pulling block (217).
2. The long-life environmental monitoring unmanned aerial vehicle of claim 1, characterized in that: the bottom end of the sliding rail (201) is fixedly connected with an anti-falling block (3).
3. The long-life environmental monitoring unmanned aerial vehicle of claim 1, characterized in that: one end, close to the working main body (211), of the limiting spring (216) is fixedly connected with the clamping plate (212), and one end, far away from the clamping plate (212), of the limiting spring (216) is fixedly connected with the central block (101).
4. The long-life environmental monitoring unmanned aerial vehicle of claim 1, characterized in that: the movable rod (215) is movably connected with the central block (101).
5. The long-life environmental monitoring unmanned aerial vehicle of claim 1, characterized in that: the bottom of the central block (101) is provided with a cover plate (4) matched with the hidden groove (106).
CN202120151152.7U 2020-04-13 2021-01-20 Long service life's environmental monitoring unmanned aerial vehicle Expired - Fee Related CN214729722U (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202020534669 2020-04-13
CN202020534669X 2020-04-13

Publications (1)

Publication Number Publication Date
CN214729722U true CN214729722U (en) 2021-11-16

Family

ID=78643244

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120151152.7U Expired - Fee Related CN214729722U (en) 2020-04-13 2021-01-20 Long service life's environmental monitoring unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN214729722U (en)

Similar Documents

Publication Publication Date Title
CN213814222U (en) Camera adjusting device for electric cruise unmanned aerial vehicle
CN110350123B (en) Battery shock absorber of new energy automobile
CN211364927U (en) Support for unmanned aerial vehicle that anti-seismic performance is good for fire engine
CN112224431A (en) Unmanned aerial vehicle's take off and land platform device is patrolled and examined to electric power
CN214729722U (en) Long service life's environmental monitoring unmanned aerial vehicle
CN213974445U (en) Unmanned aerial vehicle with descending shock-absorbing function
CN211494442U (en) Aircraft ground frame that falls that possesses buffer function
CN212074449U (en) A device that is used for unmanned aerial vehicle intelligence to keep away barrier
CN208655600U (en) A kind of solar battery crystalline silicon inserting piece device
CN214248874U (en) Damping device for coal mine electromechanical equipment
CN114408169B (en) Ecological environment monitoring facilities based on unmanned aerial vehicle shoots usefulness
CN218022168U (en) Wing protector for multi-rotor unmanned aerial vehicle
CN115610643B (en) Unmanned aerial vehicle undercarriage that takes precautions against earthquakes
CN213342028U (en) Inverter with interface protection function
CN212968730U (en) Low-voltage control cabinet with shock-absorbing function
CN210495221U (en) Model airplane with emergency landing structure
CN215060516U (en) Wall-mounted touch monitor with high protection performance
CN214649005U (en) Damping buffer frame for fixed-wing unmanned aerial vehicle
CN218119636U (en) Operation screen
CN216253616U (en) Unmanned aerial vehicle flight controller
CN213521735U (en) Resistance to compression solar panel
CN216427120U (en) Safe efficient shock attenuation protection type glass-cutting machine
CN212928721U (en) Improved split gearbox body of compressor
CN212709967U (en) Electric power patrols line unmanned aerial vehicle
CN218703990U (en) Aerial photography unmanned aerial vehicle adopting square matrix for shooting

Legal Events

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: 20211116

CF01 Termination of patent right due to non-payment of annual fee