CN208350747U - A kind of gas-monitoring unmanned plane - Google Patents
A kind of gas-monitoring unmanned plane Download PDFInfo
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- CN208350747U CN208350747U CN201820846801.3U CN201820846801U CN208350747U CN 208350747 U CN208350747 U CN 208350747U CN 201820846801 U CN201820846801 U CN 201820846801U CN 208350747 U CN208350747 U CN 208350747U
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Abstract
The utility model discloses a kind of gas-monitoring unmanned planes, including drone body, the surface of drone body offers thermovent, and dust-proof web plate is connected in thermovent, the sidewall symmetry of dust-proof web plate is fixedly connected there are four fixture block, the surface of drone body offers the card slot to match with fixture block, the lower end four corners of drone body are fixedly connected to support tube, the inside of support tube is fixed with buffer spring, the lower end of buffer spring is fixedly connected with support rod, the lower end of support rod is fixedly connected with support plate, the lower end of support plate is by there is multiple buffer gears to be connected with buffer board.The utility model makes drone body have the function of preferable dustproof and rainproof, and drone body is made to have the function of preferable bumper and absorbing shock when falling.
Description
Technical field
The utility model relates to air vehicle technique field more particularly to a kind of gas-monitoring unmanned planes.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle.Unmanned plane is actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition: nobody
This several major class of helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol.With manned aircraft phase
Than it has many advantages, such as that small in size, low cost, easy to use, low to operational environment requirement, battlefield survival is stronger.Due to
UAV has great significance to Future Air Combat, and each main military country of the world all is stepping up to carry out unmanned fly
The development work of machine.
It is proposed a kind of gas-monitoring unmanned plane, but its cushion effect when falling between stabilizer blade and ground in the prior art
Not enough, it influences collision to be easy to damage unmanned plane, and in order to make the electrical component inside unmanned plane in working long hours
It is able to carry out effective rapid cooling, often opens up heat release hole on the casing surface of unmanned plane, but be easy in heat release hole into ash
And then it influences the electrical component inside unmanned plane and works normally.
Utility model content
Purpose of the utility model is to solve the cushion effects in the prior art when falling between stabilizer blade and ground not
It is enough, it influences collision and is easy to damage unmanned plane, and in order to make the energy in working long hours of the electrical component inside unmanned plane
Enough carry out effective rapid cooling, often open up heat release hole on the casing surface of unmanned plane, but be easy in heat release hole into ash into
And a kind of gas-monitoring unmanned plane for influencing the problem of electrical component inside unmanned plane works normally, and proposing.
To achieve the goals above, the utility model adopts the technical scheme that
A kind of gas-monitoring unmanned plane, including drone body, the surface of the drone body offer thermovent, and
Dust-proof web plate is connected in the thermovent, the upper end side wall of the dust-proof web plate is fixedly connected with the lid that keeps off the rain being obliquely installed,
The sidewall symmetry of the dust-proof web plate is fixedly connected there are four fixture block, and the surface of the drone body offers and fixture block phase
The card slot matched, the side wall of the fixture block offer cylinder groove, and the cylinder groove is interior to be fixedly connected with gag lever post by reset spring,
The side wall of the card slot offers limiting slot corresponding with gag lever post, and the surface of the fixture block offers reseting groove, the limit
One end that bar is located in cylinder groove is fixedly connected with release link, and the release link is protruded into reseting groove by through-hole, and fixed company
It is connected to pull rod, the lower end four corners of the drone body are fixedly connected to support tube, and the inside fixation of the support tube is set
There is buffer spring, the lower end of the buffer spring is fixedly connected with support rod, and the lower end of the support rod is fixedly connected with support
Plate, the lower end of the support plate is by there is multiple buffer gears to be connected with buffer board.
Preferably, the bar wall of the gag lever post is symmetrically fixedly connected there are two the first position limiting slide block, the cylinder groove it is interior
Wall offers the first limit sliding chutes to match with the first position limiting slide block.
Preferably, the upper side pole wall of the support rod is symmetrically fixedly connected there are two the second position limiting slide block, the support tube
Inner wall offer the second limit sliding chutes to match with the second position limiting slide block.
Preferably, the lower end four corners of the support plate with the upper end four corners of buffer board are corresponding is fixedly connected with limit
Telescopic rod.
Preferably, the buffer gear is hinged with support plate lower end including two, and the decoupling rods being distributed in splayed, and two
Same root tension spring is fixedly connected between decoupling rod described in root, the lower end of the decoupling rod is rotatably connected to damping sliding block,
The upper end of the buffer board offers the damping sliding slot to match with damping sliding block.
Preferably, the upper end of the damping sliding block is fixedly connected with U-shaped snap-gauge, the opposite two side walls of the U-shaped snap-gauge
It is connected with same root shaft by ball bearing rotational, the axial wall of the shaft and the lower end of decoupling rod are fixedly attached.
Compared with prior art, the utility model provides a kind of gas-monitoring unmanned plane, have it is following the utility model has the advantages that
1, the gas-monitoring unmanned plane can help the electrical component in drone body to carry out by the thermovent being equipped with
Heat dissipation, and dust-proof web plate is connected in thermovent, preferable dustproof effect can be played, dust is preferably avoided and enters nobody
In machine ontology and then the problem of electrical component inside unmanned plane works normally is influenced, and is connected by the way that the side of dust-proof web plate is fixed
The lid that keeps off the rain connect can preferably avoid the problem that rainwater is entered by thermovent and cause to damage it in drone body, make nothing
Man-machine ontology has the function of preferable dustproof and rainproof, and reset spring releases gag lever post outside cylinder groove, makes gag lever post and limit
Slot engaging can make fixture block is firm to be connected in card slot, and then can be fixed on what dust-proof web plate consolidated in thermovent, and
When needing to remove dust-proof web plate progress maintenance and cleaning, pull rod is pulled, and then drive gag lever post mobile by release link, will limited
Bar pulls out in limiting slot, can unlock, convenient for the dismounting to dust-proof web plate.
2, the gas-monitoring unmanned plane, in unmanned plane landing, buffer board and ground face contact, decoupling rod stress are squeezed, benefit
It is slided in damping sliding slot with damping sliding block, tension spring provides a pull-back forces for two decoupling rods, and it is slow can to play level-one
Cushioning effect is rushed, then buffer spring is squeezed by support rod, buffer spring plays a level 2 buffering shock-absorbing function, can make nothing
Man-machine ontology has the function of preferable bumper and absorbing shock when falling, and avoids when drone body falls and is easy by rigid collision
The problem of causing drone body to be damaged.
And be not directed to part in the device and be the same as those in the prior art or can be realized by using the prior art, this is practical
It is novel that drone body is made to have the function of preferable dustproof and rainproof, make drone body that there is preferable bumper and absorbing shock when falling
Function.
Detailed description of the invention
Fig. 1 be the utility model proposes a kind of gas-monitoring unmanned plane structural schematic diagram；
Fig. 2 be the utility model proposes a kind of gas-monitoring unmanned plane part A structural schematic diagram；
Fig. 3 be the utility model proposes a kind of gas-monitoring unmanned plane part B structural schematic diagram；
Fig. 4 be the utility model proposes a kind of gas-monitoring unmanned plane dust-proof web plate with keep off the rain lid connect structure show
It is intended to.
In figure: 1 drone body, 2 thermovents, 3 dust-proof web plates, 4 keep off the rain lid, 5 fixture blocks, 6 card slots, 7 cylinder grooves, 8 reset
Spring, 9 gag lever posts, 10 limiting slots, 11 reseting grooves, 12 release links, 13 pull rods, 14 support tubes, 15 buffer springs, 16 support rods,
17 support plates, 18 buffer boards, 19 damping sliding slots, 20 decoupling rods, 21 tension springs, 22 damping sliding blocks.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
In the description of the present invention, it should be understood that term " on ", "lower", "front", "rear", "left", "right",
The orientation or positional relationship of the instructions such as "top", "bottom", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
For ease of description the utility model and simplify description, rather than the device or element of indication or suggestion meaning must have it is specific
Orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
Referring to Fig.1-4, a kind of gas-monitoring unmanned plane, including drone body 1, the surface of drone body 1 offer
Thermovent 2, and dust-proof web plate 3 is connected in thermovent 2, the upper end side wall of dust-proof web plate 3 is fixedly connected with the gear being obliquely installed
Rain lid 4, the sidewall symmetry of dust-proof web plate 3 are fixedly connected there are four fixture block 5, and the surface of drone body 1 offers and 5 phase of fixture block
Matched card slot 6, the side wall of fixture block 5 offer cylinder groove 7, pass through reset spring 8 in cylinder groove 7 and be fixedly connected with gag lever post 9,
The side wall of card slot 6 offers limiting slot 10 corresponding with gag lever post 9, and the surface of fixture block 5 offers reseting groove 11, and gag lever post 9
It is fixedly connected with release link 12 in one end in cylinder groove 7, release link 12 is protruded into reseting groove 11 by through-hole, and is fixedly connected
There is pull rod 13, the lower end four corners of drone body 1 are fixedly connected to support tube 14, and the inside of support tube 14 is fixed with slow
Spring 15 is rushed, the lower end of buffer spring 15 is fixedly connected with support rod 16, and the lower end of support rod 16 is fixedly connected with support plate 17,
The lower end of support plate 17 is by there is multiple buffer gears to be connected with buffer board 18.
The bar wall of gag lever post 9 is symmetrically fixedly connected there are two the first position limiting slide block, and the inner wall of cylinder groove 7 offers and first
The first limit sliding chutes that position limiting slide block matches.
The upper side pole wall of support rod 16 is symmetrically fixedly connected there are two the second position limiting slide block, and the inner wall of support tube 14 offers
The second limit sliding chutes to match with the second position limiting slide block.
The lower end four corners of support plate 17 with the upper end four corners of buffer board 18 are corresponding is fixedly connected with limit telescopic bar.
Buffer gear includes two hinged with 17 lower end of support plate, and in the decoupling rod 20 of splayed distribution, two dampings
Same root tension spring 21 is fixedly connected between bar 20, the lower end of decoupling rod 20 is rotatably connected to damping sliding block 22, buffer board
18 upper end offers the damping sliding slot 19 to match with damping sliding block 22.
The upper end of damping sliding block 22 is fixedly connected with U-shaped snap-gauge, and the opposite two side walls of U-shaped snap-gauge are turned by ball bearing
Dynamic to be connected with same root shaft, the lower end of the axial wall and decoupling rod 20 of shaft is fixedly attached.
In the utility model, in use, the electrical component in drone body 1 can be helped by the thermovent 2 being equipped with
Radiate, and be connected with dust-proof web plate 3 in thermovent 2, preferable dustproof effect can be played, preferably avoid dust into
Enter in drone body 1 and then influence the problem of electrical component inside unmanned plane works normally, and passes through the one of dust-proof web plate 3
What side was fixedly connected keep off the rain, and lid 4 can preferably avoid rainwater from entering in drone body 1 by thermovent 2 causes to damage it
The problem of, so that drone body 1 is had the function of preferable dustproof and rainproof, and reset spring 8 releases gag lever post 9 outside cylinder groove 7,
Engage gag lever post 9 with limiting slot 10, can make fixture block 5 is firm to be connected in card slot 6, and then can be steady by dust-proof web plate 3
Solid be fixed in thermovent 2, and when needing to remove dust-proof web plate 3 and carrying out maintenance and cleaning, pull pull rod 13, and then by multiple
Position bar 12 drives gag lever post 9 mobile, and gag lever post 9 is pulled out in limiting slot 10, can be unlocked, convenient for dust-proof web plate 3
Dismounting, in unmanned plane landing, buffer board 18 and ground face contact, 20 stress of decoupling rod is squeezed, using damping sliding block 22 in damping
Sliding in sliding slot 19, tension spring 21 are that two decoupling rods 20 provide a pull-back forces, can play first-level buffer cushioning effect,
Buffer spring 15 is squeezed by support rod 16 again, buffer spring 15 plays a level 2 buffering shock-absorbing function, can make unmanned plane
Ontology 1 has the function of preferable bumper and absorbing shock when falling, and avoids when drone body 1 falls and is easy to lead by rigid collision
The problem of causing drone body 1 to damage.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not
It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
1. a kind of gas-monitoring unmanned plane, including drone body (1), which is characterized in that the surface of the drone body (1)
It offers thermovent (2), and is connected with dust-proof web plate (3) in the thermovent (2), the upper end side wall of the dust-proof web plate (3)
It is fixedly connected with keeping off the rain lid (4) of being obliquely installed, the sidewall symmetry of the dust-proof web plate (3) is fixedly connected there are four fixture block (5),
The surface of the drone body (1) offers the card slot (6) to match with fixture block (5), and the side wall of the fixture block (5) offers
Cylinder groove (7), the cylinder groove (7) is interior to be fixedly connected with gag lever post (9) by reset spring (8), the side wall of the card slot (6)
Limiting slot (10) corresponding with gag lever post (9) is offered, the surface of the fixture block (5) offers reseting groove (11), the limit
One end that bar (9) is located in cylinder groove (7) is fixedly connected with release link (12), and the release link (12) protrudes into reset by through-hole
In slot (11), and pull rod (13) are fixedly connected with, the lower end four corners of the drone body (1) are fixedly connected to support tube
(14), the inside of the support tube (14) is fixed with buffer spring (15), and the lower end of the buffer spring (15) is fixedly connected
Have support rod (16), the lower end of the support rod (16) is fixedly connected with support plate (17), and the lower end of the support plate (17) is logical
It has crossed multiple buffer gears and has been connected with buffer board (18).
2. a kind of gas-monitoring unmanned plane according to claim 1, which is characterized in that the bar wall pair of the gag lever post (9)
Title is fixedly connected there are two the first position limiting slide block, and the inner wall of the cylinder groove (7) is offered to match with the first position limiting slide block
First limit sliding chutes.
3. a kind of gas-monitoring unmanned plane according to claim 1, which is characterized in that the upper side pole of the support rod (16)
Wall is symmetrically fixedly connected there are two the second position limiting slide block, and the inner wall of the support tube (14) offers and the second position limiting slide block phase
The second limit sliding chutes matched.
4. a kind of gas-monitoring unmanned plane according to claim 1, which is characterized in that the lower end four of the support plate (17)
At angle with the upper end four corners of buffer board (18) are corresponding is fixedly connected with limit telescopic bar.
5. a kind of gas-monitoring unmanned plane according to claim 1, which is characterized in that the buffer gear include two with
Support plate (17) lower end is hinged, and the decoupling rod (20) being distributed in splayed, is fixedly connected between two decoupling rods (20)
Have same root tension spring (21), the lower end of the decoupling rod (20) is rotatably connected to damping sliding block (22), the buffer board
(18) upper end offers the damping sliding slot (19) to match with damping sliding block (22).
6. a kind of gas-monitoring unmanned plane according to claim 5, which is characterized in that the upper end of the damping sliding block (22)
It is fixedly connected with U-shaped snap-gauge, the opposite two side walls of the U-shaped snap-gauge are connected with same root shaft by ball bearing rotational,
The axial wall of the shaft and the lower end of decoupling rod (20) are fixedly attached.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820846801.3U CN208350747U (en) | 2018-06-02 | 2018-06-02 | A kind of gas-monitoring unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820846801.3U CN208350747U (en) | 2018-06-02 | 2018-06-02 | A kind of gas-monitoring unmanned plane |
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| Publication Number | Publication Date |
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| CN208350747U true CN208350747U (en) | 2019-01-08 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110831390A (en) * | 2019-12-13 | 2020-02-21 | 江苏久胜电气科技有限公司 | Large-wheelbase multi-rotor unmanned aerial vehicle flight controller |
| CN110879056A (en) * | 2019-12-04 | 2020-03-13 | 山东省国土测绘院 | Unmanned aerial vehicle mapping system |
| CN112693599A (en) * | 2021-01-22 | 2021-04-23 | 宁夏翼航智控科技有限公司 | Unmanned aerial vehicle with rapid diagnosis, identification and early warning functions |
| CN113168776A (en) * | 2019-10-09 | 2021-07-23 | 乐天集团股份有限公司 | Processing system, unmanned aerial vehicle and flight path determination method |
-
2018
- 2018-06-02 CN CN201820846801.3U patent/CN208350747U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113168776A (en) * | 2019-10-09 | 2021-07-23 | 乐天集团股份有限公司 | Processing system, unmanned aerial vehicle and flight path determination method |
| CN113168776B (en) * | 2019-10-09 | 2023-04-18 | 乐天集团股份有限公司 | Processing system, unmanned aerial vehicle and flight path determination method |
| CN110879056A (en) * | 2019-12-04 | 2020-03-13 | 山东省国土测绘院 | Unmanned aerial vehicle mapping system |
| CN110879056B (en) * | 2019-12-04 | 2022-01-07 | 山东省国土测绘院 | Unmanned aerial vehicle mapping system |
| CN110831390A (en) * | 2019-12-13 | 2020-02-21 | 江苏久胜电气科技有限公司 | Large-wheelbase multi-rotor unmanned aerial vehicle flight controller |
| CN112693599A (en) * | 2021-01-22 | 2021-04-23 | 宁夏翼航智控科技有限公司 | Unmanned aerial vehicle with rapid diagnosis, identification and early warning functions |
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