CN209051579U - A kind of unmanned machine support of unmanned plane integrated panel rapid cooling - Google Patents
A kind of unmanned machine support of unmanned plane integrated panel rapid cooling Download PDFInfo
- Publication number
- CN209051579U CN209051579U CN201821558488.XU CN201821558488U CN209051579U CN 209051579 U CN209051579 U CN 209051579U CN 201821558488 U CN201821558488 U CN 201821558488U CN 209051579 U CN209051579 U CN 209051579U
- Authority
- CN
- China
- Prior art keywords
- frame
- unmanned plane
- support
- rapid cooling
- integrated panel
- 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
Links
Abstract
The utility model discloses a kind of unmanned machine supports of unmanned plane integrated panel rapid cooling, including frame, the bottom four corners of the frame are connected with first support, the outer upper side of the brace offers groove, the lower inside of the groove is connected with strut, and the top of the strut is rotatably connected to second support by the second pin shaft, and the top of the second support and the bottom of frame are fixedly linked, clearance fit has brandreth above the inner wall of the frame, and the inner wall of the brandreth is connected with iron net.The unmanned machine support of the unmanned plane integrated panel rapid cooling, it stores and uses convenient for user, and carry out certain convenience to conveyer belt, it is easy to carry and transport, and reduce the idle work of fan, so that the wind-force of fan whole all blows to the outer wall of unmanned plane, and then radiating efficiency is improved, so the unmanned machine support of the unmanned plane integrated panel rapid cooling can satisfy nowadays people's needs completely.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of unmanned plane of unmanned plane integrated panel rapid cooling
Bracket.
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 aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer, with someone
It driving an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ", and unmanned plane presses application field,
It can be divided into military with civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone, civilian aspect, and unmanned plane+industrial application is
Unmanned plane has really just needed；It taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observing wild move
The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
The big purposes for having expanded unmanned plane itself, developed country also in actively extension industrial application and develop unmanned air vehicle technique, still
At runtime, internal integrated panel can generate a large amount of heat to unmanned plane, when unmanned plane during flying, surrounding air velocity
Fastly, can play the role of cooling, but after unmanned plane landing, can not to quickly cooling, and then be easy to cause nothing
It is man-machine to be damaged, so the prior art is unable to satisfy nowadays people's needs.
Summary of the invention
The purpose of this utility model is to provide a kind of unmanned machine supports of unmanned plane integrated panel rapid cooling, to solve
The problems mentioned above in the background art.
To achieve the above object, the utility model provides the following technical solutions: a kind of unmanned plane integrated panel rapid cooling
Unmanned machine support, including frame, the bottom four corners of the frame are connected with first support, and the first support is connected with
First pin shaft, the first support are rotatably connected to brace by the first pin shaft, and the bottom of the brace is connected with pedestal, described
The outer upper side of brace offers groove, and the lower inside of the groove is connected with strut, and the top of the strut passes through second
Pin shaft is rotatably connected to second support, and the top of the second support and the bottom of frame are fixedly linked, the inner wall of the frame
Top clearance fit has brandreth, and the inner wall of the brandreth is connected with iron net, and the bottom four corners of the brandreth are connected with iron pin, institute
It states iron pin to be connected together by circular groove and frame, the inner wall of the frame is connected with cross bar, and the outer wall of the cross bar slides card
It is connected to sliding block, fan is connected at the top of the sliding block, the inner wall bottom of the frame is connected with bottom plate.
Preferably, it is connected with curved bar on the inside of the pedestal, the first square groove, the bottom plate are offered at the top of the curved bar
Bottom be connected with multiple bent cylinders, offer curved hole on the left of the outside of the song cylinder, the internal clearance of the curved hole is combined with slotting
Pin, the left end of the bolt are connected with baffle, and the right side of the baffle is connected with spring up and down, passes through on the right side of the spring
Second square groove is fixedly linked with bent cylinder.
Preferably, the bottom of the pedestal is connected with rubber pad.
Preferably, convex block is connected at left and right sides of the top of the frame.
Preferably, multiple through-holes are offered at the top of the bottom plate.
Compared with prior art, the utility model has the beneficial effects that the unmanned plane integrated panel rapid cooling nobody
Machine support, by the cooperation between brace, the first strut and frame, so that the unmanned plane of the unmanned plane integrated panel rapid cooling
Bracket can be folded, so that when not in use, the unmanned machine support of the unmanned plane integrated panel rapid cooling occupies
Minimum space, stores and is used convenient for user, and carrys out certain convenience to conveyer belt, easy to carry and transport, and
And by the cooperation between fan, cross bar and sliding block, so that the position of fan can change, so that the unmanned plane integrates face
The fan thermal potential of the unmanned machine support of plate rapid cooling sets the unmanned plane that can land with its top and matches, not only can be accurate
It radiates for unmanned plane, and reduces the idle work of fan, avoid the waste of electric power, so that the wind-force of fan whole
The outer wall of unmanned plane is all blown to, and then improves radiating efficiency, so the unmanned plane branch of the unmanned plane integrated panel rapid cooling
Frame can satisfy nowadays people's needs completely.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the connection relationship structural schematic diagram of brace, rubber pad and strut in Fig. 1；
Fig. 3 is the connection relationship structural schematic diagram of iron net, cross bar and fan in Fig. 1；
Fig. 4 is the connection relationship structural schematic diagram of bent cylinder, bolt and baffle in Fig. 3.
In figure: 1, frame, 2, first support, the 3, first pin shaft, 4, brace, 5, pedestal, 6, rubber pad, 7, second support,
8, the second pin shaft, 9, strut, 10, groove, 11, brandreth, 12, iron net, 13, iron pin, 14, circular groove, 15, bottom plate, 16, through-hole, 17,
Cross bar, 18, sliding block, 19, fan, 20, bent cylinder, 21, curved hole, 22, bolt, 23, baffle, 24, spring, the 25, second square groove, 26,
Curved bar, the 27, first square groove, 28, baffle.
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. 1-4 is please referred to, the utility model provides a kind of technical solution: a kind of nothing of unmanned plane integrated panel rapid cooling
Man-machine bracket, including frame 1, the bottom four corners of frame 1 are connected with first support 2, and first support 2 is used to install brace 4, the
One bracket 2 is connected with the first pin shaft 3, and first support 2 is rotatably connected to brace 4 by the first pin shaft 3, and the bottom of brace 4 is solid
It is connected to pedestal 5, the outer upper side of brace 4 offers groove 10, and groove 10 facilitates strut 9 to limit brace 4, groove 10
Lower inside be connected with strut 9, the top of strut 9 is rotatably connected to second support 7 by the second pin shaft 8, second support 7
Top and the bottom of frame 1 are fixedly linked, and clearance fit has brandreth 11 above the inner wall of frame 1, and the inner wall of brandreth 11 is connected with
Iron net 12,12 mesh number of iron net are 10, and the bottom four corners of brandreth 11 are connected with iron pin 13, and iron pin 13 is convenient for brandreth 11 and frame
1 is attached, and iron pin 13 is connected together by circular groove 14 with frame 1, and the inner wall of frame 1 is connected with cross bar 17, cross bar 17
Outer wall sliding is connected with sliding block 18, and the top of sliding block 18 is connected with fan 19, the model T610P of fan 19, the inner wall of frame 1
Bottom is connected with bottom plate 15, and the inside of pedestal 5 is connected with curved bar 26, and curved bar 26 and bent cylinder 20 cooperate, under the cooperation of bolt 22,
Realize the limit for brace 4, the top of curved bar 26 offers the first square groove 27, and the bottom of bottom plate 15 is affixed, and there are two bent cylinders
20, the outside left side of bent cylinder 20 offers curved hole 21, and the internal clearance of curved hole 21 is combined with bolt 22, and the left end of bolt 22 is affixed
There is baffle 23, the right side of baffle 23 is connected with spring 24 up and down, and spring 24 gives elastic force of the baffle 23 far from bent cylinder 20, spring
24 right side is fixedly linked by the second square groove 25 and bent cylinder 20, and the bottom of pedestal 5 is connected with rubber pad 6, and rubber pad 6 increases bottom
The friction of 5 bottoms of seat, the top left and right sides of frame 1 are connected with convex block 28, and the top of bottom plate 15 is opened up there are six through-hole 16,
The air velocity of the quickening of through-hole 16 19 bottom of fan.
It is first that the unmanned plane integrated panel is fast when using the unmanned machine support of the unmanned plane integrated panel rapid cooling
The unmanned machine support of speed heat dissipation is placed on void spaces, when subsequent unmanned plane needs to land, falls in the top of iron net 12, subsequent root
According to the position of unmanned plane landing and the integrated panel position of unmanned plane, the position of fan 19 is adjusted, fan 19 is with 18 edge of movable slider
Cross bar 17 slide, until fan 19 position with the external world integrated panel position of unmanned plane it is adjacent, be then switched on fan 19
External power supply, fan 19 rotate, and then the air velocity near the integrated panel of unmanned plane is driven to increase, and realization falls the external world
Unmanned plane integrated panel at 12 top of iron net cools down, and after using completing, powers off the extraneous power supply of fan 19, will be oblique
Bar 4 folds, so that the unmanned machine support of the unmanned plane integrated panel rapid cooling is convenient for storage.
In the description of the present invention, it should be understood that term " coaxial ", " bottom ", " one end ", " top ",
The orientation or position of the instructions such as " middle part ", " other end ", "upper", " side ", " top ", "inner", " front ", " center ", " both ends "
Setting relationship is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of describing the present invention and simplifying the description, and
It is not that the device of indication or suggestion meaning or element must have a particular orientation, be constructed and operated in a specific orientation, therefore
It should not be understood as limiting the present invention.
In the present invention unless specifically defined or limited otherwise, term " installation ", " setting ", " connection ",
The terms such as " fixation ", " being screwed on " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or at one
Body；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, can also indirectly connected through an intermediary, it can
To be the interaction relationship of connection or two elements inside two elements, unless otherwise restricted clearly, for this field
Those of ordinary skill for, can understand the concrete meaning of above-mentioned term in the present invention as the case may be.
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 (5)
1. a kind of unmanned machine support of unmanned plane integrated panel rapid cooling, including frame (1), it is characterised in that: the frame
(1) bottom four corners are connected with first support (2), and the first support (2) is connected with the first pin shaft (3), and described first
Bracket (2) is rotatably connected to brace (4) by the first pin shaft (3), and the bottom of the brace (4) is connected with pedestal (5), described oblique
The outer upper side of bar (4) offers groove (10), and the lower inside of the groove (10) is connected with strut (9), the strut (9)
Top be rotatably connected to second support (7) by the second pin shaft (8), the top of the second support (7) and the bottom of frame (1)
Portion is fixedly linked, and there is brandreth (11) clearance fit above the inner wall of the frame (1), the inner wall of the brandreth (11) is connected with iron
The bottom four corners of net (12), the brandreth (11) are connected with iron pin (13), and the iron pin (13) passes through circular groove (14) and frame
(1) it is connected together, the inner wall of the frame (1) is connected with cross bar (17), and the outer wall sliding of the cross bar (17) is connected with cunning
Block (18) is connected with fan (19) at the top of the sliding block (18), and the inner wall bottom of the frame (1) is connected with bottom plate (15).
2. a kind of unmanned machine support of unmanned plane integrated panel rapid cooling according to claim 1, it is characterised in that: institute
It states and is connected on the inside of pedestal (5) curved bar (26), offer the first square groove (27), the bottom plate at the top of the curved bar (26)
(15) bottom is connected with multiple bent cylinders (20), offers curved hole (21), the curved hole on the left of the outside of the song cylinder (20)
(21) internal clearance is combined with bolt (22), and the left end of the bolt (22) is connected with baffle (23), the baffle (23)
Right side is connected with spring (24) up and down, and the right side of the spring (24) passes through the second square groove (25) and bent cylinder (20) stationary phase
Even.
3. a kind of unmanned machine support of unmanned plane integrated panel rapid cooling according to claim 1, it is characterised in that: institute
The bottom for stating pedestal (5) is connected with rubber pad (6).
4. a kind of unmanned machine support of unmanned plane integrated panel rapid cooling according to claim 1, it is characterised in that: institute
It states and is connected with convex block (28) at left and right sides of the top of frame (1).
5. a kind of unmanned machine support of unmanned plane integrated panel rapid cooling according to claim 1, it is characterised in that: institute
It states and offers multiple through-holes (16) at the top of bottom plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821558488.XU CN209051579U (en) | 2018-09-25 | 2018-09-25 | A kind of unmanned machine support of unmanned plane integrated panel rapid cooling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821558488.XU CN209051579U (en) | 2018-09-25 | 2018-09-25 | A kind of unmanned machine support of unmanned plane integrated panel rapid cooling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209051579U true CN209051579U (en) | 2019-07-02 |
Family
ID=67049320
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821558488.XU Expired - Fee Related CN209051579U (en) | 2018-09-25 | 2018-09-25 | A kind of unmanned machine support of unmanned plane integrated panel rapid cooling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209051579U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113833113A (en) * | 2021-10-27 | 2021-12-24 | 韦燕燕 | Novel support steel construction |
-
2018
- 2018-09-25 CN CN201821558488.XU patent/CN209051579U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113833113A (en) * | 2021-10-27 | 2021-12-24 | 韦燕燕 | Novel support steel construction |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206087353U (en) | For military use unmanned aerial vehicle with monitor function | |
| CN209051579U (en) | A kind of unmanned machine support of unmanned plane integrated panel rapid cooling | |
| CN208439432U (en) | A kind of agricultural powder sprinkling unmanned plane | |
| CN107985624A (en) | A kind of unmanned plane supporting rack | |
| CN208412112U (en) | A kind of unmanned plane undercarriage | |
| CN207106895U (en) | Unmanned plane dispenser and unmanned plane | |
| CN208233352U (en) | One kind using buffer unit based on unmanned plane landing | |
| CN207482211U (en) | A kind of unmanned plane landing stage apparatus | |
| CN216834262U (en) | Big load foldable six-rotor unmanned aerial vehicle | |
| CN207106845U (en) | A kind of stealthy unmanned plane for extending cruising time | |
| CN207106849U (en) | A kind of more rotor unmanned aircrafts of agricultural plant protection | |
| CN209410320U (en) | A kind of hollow vertical touching lever fold mechanism | |
| CN108622423A (en) | A kind of unmanned plane motor fixing seat that damping property is good | |
| CN107826514A (en) | A kind of unmanned plane storage device with fixing device | |
| CN108891584A (en) | A kind of stable unmanned plane that lands | |
| CN209708387U (en) | A kind of unmanned plane simulation training operation show stand easy to remove | |
| CN207773505U (en) | A kind of unmanned plane radiator | |
| CN207670682U (en) | A kind of unmanned plane support construction of stability when can improve ejection | |
| CN208746263U (en) | A kind of demisting formula unmanned plane pick-up lens | |
| CN208134641U (en) | A kind of unmanned plane carry Quick-disassembling mechanism | |
| CN208496916U (en) | It is a kind of can more people assembling the quick assembly or fitting table of unmanned plane | |
| CN107187585A (en) | A kind of unmanned plane | |
| CN208377047U (en) | A kind of controllable unmanned plane takeoff and landing is smoothly verted Power Component | |
| CN218703886U (en) | FPV unmanned aerial vehicle of modularization convenient to detach repacking | |
| CN207851303U (en) | A kind of deliverance apparatus based on unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190702 Termination date: 20210925 |