CN209258399U - A kind of unmanned plane for having comprehensive radar and being able to detect air quality - Google Patents
A kind of unmanned plane for having comprehensive radar and being able to detect air quality Download PDFInfo
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- CN209258399U CN209258399U CN201821854809.0U CN201821854809U CN209258399U CN 209258399 U CN209258399 U CN 209258399U CN 201821854809 U CN201821854809 U CN 201821854809U CN 209258399 U CN209258399 U CN 209258399U
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- bottom case
- radar
- unmanned plane
- upper casing
- air quality
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Abstract
The utility model discloses a kind of unmanned planes for having comprehensive radar and being able to detect air quality, including bottom case, ventilation opening and convex block, the inside of the bottom case is equipped with detection device, and bottom case is internally provided with the first fixture block, and the outer wall of the bottom case is internally provided with air inlet.The setting that the utility model passes through permeable structures between detection device and upper casing, so that the gas around the unmanned plane can be sucked into its inside by detection device by air inlet, and the inside air substance is detected by relative other component, probe radar and the setting for detecting position between device, so that the air particles molecule that probe radar can suck air inlet is photographed, and radar of popping one's head in equidistantly uniformly is distributed in the surrounding of upper casing outer wall, its number is arranged so that the unmanned plane can meet the demand for having comprehensive radar, therefore pass through cooperation mutual between above-mentioned part, it is provided convenience for the unmanned plane to what Detection of Air Quality worked.
Description
Technical field
The utility model relates to Detection of Air Quality air vehicle technique field, specially one kind have comprehensive radar can
Detect the unmanned plane of air quality.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned vehicle of presetting apparatus manipulation;Unmanned plane is actually the general designation of unmanned vehicle, with scientific skill
The application field of the continuous unmanned plane of art is also constantly expanding, thus to the unmanned plane of Detection of Air Quality carry out innovation with
Setting, plays a part of promotion to its development.
The unmanned plane of existing Detection of Air Quality, since it cannot be comprehensive to the region progress detected
Detections of radar, to be impacted to the authenticity of the regional air quality measurements, and since the unmanned plane is in lifting
Buffering effect between ground is bad, larger so as to cause local pressure between ground and the contact surface of the fuselage, thus right
A degree of damage is caused at this, and then influence is caused on the service life of the unmanned plane, for this purpose, it is proposed that one kind has entirely
Orientation radar is able to detect the unmanned plane of air quality.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane for having comprehensive radar and being able to detect air quality, with
The unmanned plane for solving existing Detection of Air Quality mentioned above in the background art, since it cannot be to detecting
Region carry out comprehensive detections of radar, to be impacted to the authenticity of the regional air quality measurements, and due to
Buffering effect of the unmanned plane in lifting between ground is bad, so as to cause part between ground and the contact surface of the fuselage
Stress is larger, thus to a degree of damage is caused at this, and then the problem of cause influence to the service life of the unmanned plane.
To achieve the above object, the utility model provides the following technical solutions: one kind having comprehensive radar and is able to detect
The unmanned plane of air quality, including bottom case, ventilation opening and convex block, the inside of the bottom case are equipped with detection device, and bottom case
It is internally provided with the first fixture block, the outer wall of the bottom case is internally provided with air inlet, and upper casing is provided with above bottom case, described
Upper casing is internally provided with the second fixture block, and pars intramuralis is respectively and fixedly provided with probe radar outside the left and right ends of upper casing, the upper casing
Top is fixed with bracket, and the top of bracket is equipped with wing, and the center bottom of the bracket is connected with supporting block, the upper casing
Middle part above be provided with fixed plate, and the top end surface of fixed plate is fixed with bolt, and the center bottom surface of the bottom case connects
It is connected to bearing plate, and the bottom end of bearing plate is provided with traveller, nave boss frame is provided with immediately below the traveller, and nave boss frame is interior
Portion is provided with limited block, and the outer wall surface of the limited block is connected with spring, and the ventilation opening is set to bottom case bottom end surface, institute
The outer wall surface that convex block is set to probe radar is stated, and the outside connection of convex block is fluted.
Preferably, first fixture block matches with the size between the second fixture block, and bottom case passes through the first fixture block and the
Detachable structure is constituted between the cooperation and upper casing of two fixture blocks.
Preferably, the probe radar is equidistantly uniformly distributed in the edge of upper casing surrounding, and in the level of detection device
Heart line is vertical with the probe vertical centerline of radar, and detects device by constituting permeable structures between air inlet and upper casing.
Preferably, the bracket is equidistantly uniformly distributed in the top end surface of upper casing, and supporting block is set as triangular shape knot
Structure, and supporting block is by integrally changing structure between welding and bracket.
Preferably, the traveller is slidably connected with limited block, and nave boss frame passes through cooperation and the bottom case of traveller and limited block
Between constitute slide construction.
Preferably, it is fitted closely between the top end surface of the spring and the bottom end surface of bottom case, and nave boss frame passes through bullet
Stretching structure is constituted between spring and bottom case.
Compared with prior art, the beneficial effects of the utility model are as follows:
1. the utility model is by the setting of size between the first fixture block and the second fixture block, so that it can be to bottom case and upper casing
Between positioned and fixed, to reduce since the secured performance between it is bad, cause the unmanned plane by the external world
When the influence of power, cause to generate loosening between it, so that a degree of damage is caused to the connector between it, thus to nothing
Man-machine normal work cause influence, and by the combination between the first fixture block and the second fixture block, can for bottom case with it is upper
It dismounts work between shell provide convenience, and then service work provide between the unmanned plane inner body
It is convenient;
2. the utility model by detection device and upper casing between permeable structures setting so that detection device can by into
Gas around the unmanned plane is sucked into its inside by port, and by relative other component to the inside air object
Quality detection, probe radar and the setting for detecting position between device, so that the air particles that probe radar can suck air inlet
Molecule is photographed, to provide convenience for the unmanned plane to what Detection of Air Quality worked;
3. the utility model by between traveller and bottom case slide construction setting so that its can to it is flexible when spring carry out
Limit, avoids impacting the structure of itself inside, since its collapsing length is longer or too short so as to shorten making for its
With the service life, therefore the setting of the slide construction, so that the progress of telescopic spring work is more smooth, to improve the unmanned plane
The compactedness and harmony connected between internal part.
Detailed description of the invention
Fig. 1 is that the utility model faces schematic diagram of internal structure;
Fig. 2 is the utility model overlooking structure diagram;
Fig. 3 is the utility model present invention looks up structural representation.
In figure: 1, bottom case;2, device is detected;3, the first fixture block;4, air inlet;5, upper casing;6, the second fixture block;7, probe thunder
It reaches;8, bracket;9, wing;10, supporting block;11, fixed plate;12, bearing plate;13, traveller;14, limited block;15, nave boss frame;
16, spring;17, bolt;18, ventilation opening;19, convex block;20, groove.
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.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: one kind having comprehensive radar and is able to detect air
The unmanned plane of quality, including bottom case 1, ventilation opening 18 and convex block 19, the inside of bottom case 1, which is equipped with, detects device 2, and bottom case 1
It is internally provided with the first fixture block 3, the size between the first fixture block 3 and the second fixture block 6 matches, and bottom case 1 passes through the first fixture block 3
Detachable structure is constituted between the cooperation and upper casing 5 of the second fixture block 6, size sets between the first fixture block 3 and the second fixture block 6
It sets, so that it can be to being positioned between bottom case 1 and upper casing 5 and being fixed, to reduce due to the secured performance between it not
It is good, cause the unmanned plane in the influence by external force, causes to generate loosening between it, to make the connector between it
At a degree of damage, to cause influence to what unmanned plane worked normally, and pass through the first fixture block 3 and the second card
Combination between block 6 can dismount work between bottom case 1 and upper casing 5 and provide convenience, and then for inside the unmanned plane
Service work provide convenience between part, and the outer wall of bottom case 1 is internally provided with air inlet 4, and the top of bottom case 1 is set
It is equipped with upper casing 5, upper casing 5 is internally provided with the second fixture block 6, and pars intramuralis is respectively and fixedly provided with probe thunder outside the left and right ends of upper casing 5
Up to 7, probe radar 7 is equidistantly uniformly distributed in the edge of 5 surrounding of upper casing, and detects the horizontal center line and probe thunder of device 2
Vertical centerline up to 7 is vertical, and detects device 2 by constituting permeable structures between air inlet 4 and upper casing 5, detection device 2 with
The setting of permeable structures between upper casing 5, so that the gas around the unmanned plane can be sucked by detection device 2 by air inlet 4
Its inside, and by relative other component to the inside air substance detect, probe radar 7 and detection device 2 it
Between position setting so that the air particles molecule that probe radar 7 can suck air inlet 4 be photographed, and the radar 7 etc. of popping one's head in
Away from the surrounding for being uniformly distributed in 5 outer wall of upper casing, number is arranged so that the unmanned plane can be to the need for having comprehensive radar
It asks and is met, to be provided convenience for the unmanned plane to what Detection of Air Quality worked;
The top of upper casing 5 is fixed with bracket 8, and the top of bracket 8 is equipped with wing 9, and bracket 8 is equidistantly uniformly distributed in
The top end surface of upper casing 5, and supporting block 10 is set as triangular shape structure, and supporting block 10 by between welding and bracket 8 at
Integral structure, 8 several settings of bracket so that wing 9 can the multi-faceted stability to the unmanned plane maintain, from
And reduce since bracket 8 is arranged that number is less, cause the unmanned plane in flight by the influence of extraneous factor, to its
The probability that phenomena such as stability impacts generates, the shape of supporting block 10 and its welded between bracket 8 set
It sets, effectively raises the secured performance between bracket 8 and upper casing 5 and bracket 8 and supporting block 10, and then improve this nobody
The stability of machine, the center bottom of bracket 8 are connected with supporting block 10, fixed plate 11 are provided with above the middle part of upper casing 5, and solid
The top end surface of fixed board 11 is fixed with bolt 17;
The center bottom surface of bottom case 1 is connected with bearing plate 12, and the bottom end of bearing plate 12 is provided with traveller 13, traveller 13
It is slidably connected with limited block 14, and nave boss frame 15 passes through composition sliding knot between traveller 13 and the cooperation and bottom case 1 of limited block 14
Structure, the setting of slide construction between traveller 13 and bottom case 1 so that its can to it is flexible when spring 16 limit, avoid due to it
Collapsing length is longer or too short, impacts to the structure of itself inside, so as to shorten its service life, therefore the sliding
The setting of structure, so that spring 16 stretches, the progress of work is more smooth, to improve between the unmanned plane internal part
The compactedness and harmony of connection, the underface of traveller 13 be provided with nave boss frame 15, and nave boss frame 15 is internally provided with limit
Block 14, the outer wall surface of limited block 14 are connected with spring 16, close between the top end surface of spring 16 and the bottom end surface of bottom case 1
Fitting, and nave boss frame 15 is by constituting stretching structure between spring 16 and bottom case 1, the deformation generated by spring 16, so that its
A buffering is carried out between fuselage and nave boss frame 15 when can be to lifting, so as to avoid since buffering effect is not between said two devices
Good, the harmony between fuselage and nave boss frame 15 when to lifting impacts, and then causes certain journey to connector between it
The damage of degree, ventilation opening 18 are set to 1 bottom end surface of bottom case, and convex block 19 is set to the outer wall surface of probe radar 7, and convex block 19
Outside connection fluted 20.
Working principle: for this kind of unmanned plane for having comprehensive radar and being able to detect air quality, when use first
The unmanned plane is risen by control device, and allows its flight to area to be tested, secondly by detection device 2 into
Gas around port 4 is adsorbed, and by pop one's head in radar 7 air is imaged, secondly by detection device 2 and
The inside air substance is detected between relative other component, and by information display module to the testing result
It is shown;
The unmanned plane at work, can be radiated by part of the ventilation opening 18 to its inside, avoid due to this nobody
Machine causes its internal local temperature higher under prolonged work, so that the security performance assembly of the unmanned plane is influenced, and
It, can by cooperation mutual between stretching structure between slide construction and spring 16 and bottom case 1 between traveller 13 and limited block 14
Buffered between unmanned plane and ground when for landing, when radar 7 of popping one's head in generates damage, can by convex block 19 and groove 20 it
Between mutual cooperation, work can be dismounted for the probe and provide convenience, and then provide just for its service work
Benefit just completes the use process of the unmanned plane in this way.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane for having comprehensive radar and being able to detect air quality, including bottom case (1), ventilation opening (18) and convex block
(19), it is characterised in that: the inside of the bottom case (1) is equipped with detection device (2), and bottom case (1) is internally provided with first
The outer wall of fixture block (3), the bottom case (1) is internally provided with air inlet (4), and upper casing (5), institute are provided with above bottom case (1)
Being internally provided with the second fixture block (6) for upper casing (5) is stated, and pars intramuralis is respectively and fixedly provided with probe radar outside the left and right ends of upper casing (5)
(7), the top of the upper casing (5) is fixed with bracket (8), and the top of bracket (8) is equipped with wing (9), the bracket (8)
Center bottom is connected with supporting block (10), is provided with fixed plate (11) above the middle part of the upper casing (5), and fixed plate (11)
Top end surface is fixed with bolt (17), and the center bottom surface of the bottom case (1) is connected with bearing plate (12), and bearing plate (12)
Bottom end be provided with traveller (13), be provided with nave boss frame (15) immediately below the traveller (13), and the inside of nave boss frame (15)
It is provided with limited block (14), the outer wall surface of the limited block (14) is connected with spring (16), and the ventilation opening (18) is set to
Bottom case (1) bottom end surface, the convex block (19) are set to the outer wall surface of probe radar (7), and the outside connection of convex block (19)
Fluted (20).
2. a kind of unmanned plane for having comprehensive radar and being able to detect air quality according to claim 1, feature exist
In: first fixture block (3) matches with the size between the second fixture block (6), and bottom case (1) passes through the first fixture block (3) and the
Detachable structure is constituted between the cooperation and upper casing (5) of two fixture blocks (6).
3. a kind of unmanned plane for having comprehensive radar and being able to detect air quality according to claim 1, feature exist
In: probe radar (7) is equidistantly uniformly distributed in the edge of upper casing (5) surrounding, and detects the horizontal center line of device (2)
It is vertical with the probe vertical centerline of radar (7), and it is penetrating by constituting between air inlet (4) and upper casing (5) to detect device (2)
Structure.
4. a kind of unmanned plane for having comprehensive radar and being able to detect air quality according to claim 1, feature exist
In: the bracket (8) is equidistantly uniformly distributed in the top end surface of upper casing (5), and supporting block (10) is set as triangular shape structure,
And supporting block (10) is by integrally changing structure between welding and bracket (8).
5. a kind of unmanned plane for having comprehensive radar and being able to detect air quality according to claim 1, feature exist
In: the traveller (13) is slidably connected with limited block (14), and nave boss frame (15) matching by traveller (13) and limited block (14)
It closes and constitutes slide construction between bottom case (1).
6. a kind of unmanned plane for having comprehensive radar and being able to detect air quality according to claim 1, feature exist
In: it is fitted closely between the top end surface of the spring (16) and the bottom end surface of bottom case (1), and nave boss frame (15) passes through spring
(16) stretching structure is constituted between bottom case (1).
Priority Applications (1)
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CN201821854809.0U CN209258399U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane for having comprehensive radar and being able to detect air quality |
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CN201821854809.0U CN209258399U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane for having comprehensive radar and being able to detect air quality |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113086225A (en) * | 2021-04-14 | 2021-07-09 | 湖南信息学院 | Emergent unmanned aerial vehicle route optimization device in earthquake |
CN113665814A (en) * | 2021-09-24 | 2021-11-19 | 南京拓恒无人系统研究院有限公司 | Unmanned aerial vehicle with air detection system and detection method thereof |
-
2018
- 2018-11-12 CN CN201821854809.0U patent/CN209258399U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113086225A (en) * | 2021-04-14 | 2021-07-09 | 湖南信息学院 | Emergent unmanned aerial vehicle route optimization device in earthquake |
CN113665814A (en) * | 2021-09-24 | 2021-11-19 | 南京拓恒无人系统研究院有限公司 | Unmanned aerial vehicle with air detection system and detection method thereof |
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