CN219524259U - Unmanned aerial vehicle operating temperature measuring device - Google Patents
Unmanned aerial vehicle operating temperature measuring device Download PDFInfo
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- CN219524259U CN219524259U CN202223141721.3U CN202223141721U CN219524259U CN 219524259 U CN219524259 U CN 219524259U CN 202223141721 U CN202223141721 U CN 202223141721U CN 219524259 U CN219524259 U CN 219524259U
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- unmanned aerial
- aerial vehicle
- fixedly connected
- vehicle body
- temperature measuring
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model discloses an unmanned aerial vehicle operation temperature measuring device, which belongs to the technical field of unmanned aerial vehicles and comprises an installation strip shell and an unmanned aerial vehicle body, wherein a temperature measuring probe is fixedly connected to the center of the lower side of the installation strip shell, the detection end of the temperature measuring probe extends into the unmanned aerial vehicle body in a penetrating way, a wireless signal module is fixedly connected to the upper side of the installation strip shell, one end of the temperature measuring probe is electrically connected with the wireless signal module, a clamping and fixing mechanism is arranged in the installation strip shell, and two ends of the clamping and fixing mechanism respectively penetrate through two ends of the installation strip shell and are fixedly connected with fixing splints. According to the utility model, the temperature measuring probe and the wireless signal module are arranged to detect the temperature of the unmanned aerial vehicle body during operation, the clamping and fixing mechanism is arranged to drive the two fixing clamping plates to abut against two sides of the unmanned aerial vehicle body to realize fixed installation, the fixing is firm, the operation is simpler, and the stability of the temperature measurement of the unmanned aerial vehicle body is ensured.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle operation temperature measuring device.
Background
Unmanned aerial vehicle is the unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, has advantages such as small, cost low, convenient to use, is applicable to the difficult task of carrying out of unmanned aerial vehicle, in recent years, unmanned aerial vehicle aerial technology becomes the important supplement of aerial survey remote sensing field platform, but unmanned aerial vehicle aerial technology wide application in fields such as basic map survey, digital city construction, city planning, survey, development, in order to know unmanned aerial vehicle's running condition, acquire each item operating parameter, or when overhauling unmanned aerial vehicle, need detect unmanned aerial vehicle's temperature when operating.
In a feedback type unmanned aerial vehicle operation temperature measuring device (patent number: CN 217533262U), the device includes control box and unmanned aerial vehicle shell, terminal surface middle part position is provided with temperature measurement probe under the control box, control box up end one side position is provided with wireless signal module, the terminal surface is provided with image probe before the unmanned aerial vehicle shell, unmanned aerial vehicle shell both sides respectively are provided with a pair of connecting rod, the connecting rod top is provided with the flabellum, control box both ends all are provided with adjustable flexible straight-bar, terminal surface head position is provided with the pole setting under the flexible straight-bar, the inboard terminal surface of pole setting is provided with adjustable splint, through setting up temperature measurement probe in the control box bottom, and be equipped with wireless signal module at the top, can detect the temperature at unmanned aerial vehicle operation in-process, and feed back temperature data through wireless signal, set up flexible straight-bar in the control box both sides simultaneously, pole setting and splint, conveniently install fixedly to the unmanned aerial vehicle shell of different large and small-size, however, the device is fixed on unmanned aerial vehicle with temperature measurement device only through utilizing the elasticity of spring and elasticity cable, the operation is firm, and easy, and the temperature measurement effect is influenced. Accordingly, a person skilled in the art provides an unmanned aerial vehicle operation temperature measuring device to solve the problems set forth in the background art.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle running temperature measuring device so as to solve the problems in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle operation temperature measuring device, includes installation strip shell and unmanned aerial vehicle body, the downside center department fixedly connected with temperature measurement probe of installation strip shell, and temperature measurement probe's detection end runs through and extends to in the unmanned aerial vehicle body, the upside fixedly connected with wireless signal module of installation strip shell, and temperature measurement probe's one end and wireless signal module electric connection, be equipped with clamping fixture in the installation strip shell, and the both ends of clamping fixture run through the equal fixedly connected with fixed splint in both ends of installation strip shell respectively, two fixed splint support tightly with the both sides of unmanned aerial vehicle body respectively and set up, two all be equipped with elasticity adjustment mechanism in the fixed splint, and the L shape cardboard that two elasticity adjustment mechanism's lower extreme fixedly connected with two symmetries set up, the horizontal straight end lateral wall of L shape cardboard and the bottom fixed connection of unmanned aerial vehicle body.
As still further aspects of the utility model: the clamping and fixing mechanism comprises a rotating handle which is inserted into the center of the front side of the installation strip shell and is rotationally connected with the front side of the installation strip shell, one end of the rotating handle extends into the installation strip shell and is fixedly connected with a driving bevel gear, two end inner walls of the installation strip shell are rotationally connected with screw rods through bearing seats, one ends, close to the two screw rods, of the two screw rods are fixedly connected with driven bevel gears which are meshed with the driving bevel gear, two screw rods are connected with threaded blocks which are symmetrically arranged on the screw rods, one side of each threaded block is fixedly connected with two symmetrically arranged connecting rods, and one ends of the two connecting rods penetrate through one end of the installation strip shell and are fixedly connected with a fixed clamping plate.
As still further aspects of the utility model: wherein, two through holes have been seted up to the one end of installation strip shell, and two connecting rods pass two through-holes setting respectively.
As still further aspects of the utility model: the elastic force adjusting mechanism comprises a sliding cavity arranged in the fixed clamping plate, a sliding rod is slidably connected in the sliding cavity through a sliding block, one end of the sliding rod penetrates through the fixed clamping plate and is fixedly connected with the L-shaped clamping plate, a spring is fixedly connected between the sliding block and the sliding cavity, and the spring is sleeved on the sliding rod.
As still further aspects of the utility model: the lower end of the fixed clamping plate is provided with a sliding opening communicated with the sliding cavity, and the sliding rod penetrates through the sliding opening.
As still further aspects of the utility model: wherein, the fixed splint is fixedly connected with anti-skidding cushion with one side lateral wall that the unmanned aerial vehicle body offsets.
As still further aspects of the utility model: four corners of the bottom of the unmanned aerial vehicle body are fixedly connected with four symmetrically-arranged supporting leg frames, and the lower ends of the four supporting leg frames are fixedly connected with two ground supporting rollers which are arranged in parallel.
Compared with the prior art, the utility model has the beneficial effects that:
1. this unmanned aerial vehicle operation temperature measuring device, through setting up temperature measurement probe and wireless signal module, temperature measurement probe stretches into in the shell of unmanned aerial vehicle body, can start the unmanned aerial vehicle body and fly afterwards, temperature measurement probe detects the temperature when unmanned aerial vehicle body operates to feed back temperature data to the inspector through wireless signal module, realize short-term test.
2. This unmanned aerial vehicle operation temperature measuring device, through setting up centre gripping fixture and two fixed splint, when needs install temperature measurement probe on unmanned aerial vehicle body, at first, insert temperature measurement probe's detection end in the unmanned aerial vehicle body, the both sides of unmanned aerial vehicle body are arranged in to fixed splint, then, rotate and change the hand (hold), drive bevel gear rotates, because drive bevel gear respectively with two driven bevel gears meshing, and then drive two lead screws and reverse rotation simultaneously, at this moment, two screw thread pieces force to opposite direction displacement, and then drive two fixed splint and support the both sides of tightly unmanned aerial vehicle body and realize fixed mounting, it is fixed firm, the operation is simpler, the guarantee is to unmanned aerial vehicle body temperature measurement's stability.
3. This unmanned aerial vehicle operating temperature measuring device, through setting up elasticity adjustment mechanism and L shape cardboard, during the installation, pulling L shape cardboard moves down, at this moment, drives the slider that is fixed with the slide bar and shifts in the smooth chamber, and at this moment, the spring receives the extrusion and produces elasticity, when loosening L shape cardboard, utilizes the elasticity effect of spring, makes the bottom of L shape cardboard automatic tight unmanned aerial vehicle body of support, can play auxiliary fixation's effect to the installation.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a schematic perspective view of the mounting bar of the present utility model;
FIG. 3 is a schematic cross-sectional elevation view of the present utility model at the mounting bar housing;
fig. 4 is an enlarged schematic view of the structure of fig. 3 a in the present utility model.
The correspondence between the reference numerals and the component names in the drawings is as follows:
1. mounting a strip shell; 2. an unmanned aerial vehicle body; 3. a temperature measurement probe; 4. a wireless signal module; 5. a fixed clamping plate; 6. an L-shaped clamping plate; 7. turning a handle; 8. a drive bevel gear; 9. a screw rod; 10. a driven bevel gear; 11. a screw block; 12. a connecting rod; 13. a sliding cavity; 14. a slide block; 15. a slide bar; 16. a spring; 17. an anti-slip soft pad; 18. a leg support; 19. and (5) supporting the ground roller.
Detailed Description
Please refer to fig. 1-4, the utility model discloses in the embodiment, an unmanned aerial vehicle operation temperature measuring device, including installation strip shell 1 and unmanned aerial vehicle body 2, the downside center department fixedly connected with temperature measurement probe 3 of installation strip shell 1, and temperature measurement probe 3's detection end runs through and extends to among the unmanned aerial vehicle body 2, the trompil that is used for inserting temperature measurement probe 3 detection end is offered to the shell upside of unmanned aerial vehicle body 2, the upside fixedly connected with wireless signal module 4 of installation strip shell 1, and temperature measurement probe 3's one end and wireless signal module 4 electric connection, temperature measurement probe 3 stretches into among the shell of unmanned aerial vehicle body 2, can start unmanned aerial vehicle body 2 and fly next, temperature measurement probe 3 detects the temperature when unmanned aerial vehicle body 2 operates, and feed back temperature data for the inspector through wireless signal module 4, realize short-term test, be equipped with centre gripping fixed establishment in the installation strip shell 1, and the both ends of centre gripping fixed establishment run through respectively install strip shell 1's both ends and equal fixedly connected with solid fixed splint 5, two solid fixed 5 support the both sides with the both sides of aircraft body 2 tightly set up, and two elastic force adjustment mechanism are equipped with in two solid fixed connection L6, two side wall of the unmanned aerial vehicle is equipped with the side wall of the unmanned aerial vehicle, two elastic force adjustment mechanism is equipped with the side-plate of the unmanned aerial vehicle is fixed, the side-plate is connected with the side-plate of the unmanned aerial vehicle is fixed with the L6.
As shown in fig. 3: the clamping and fixing mechanism comprises a rotating handle 7 which is inserted in the center of the front side of the installation strip shell 1 and is rotationally connected with the installation strip shell, one end of the rotating handle 7 extends into the installation strip shell 1 and is fixedly connected with a driving bevel gear 8, the inner walls of the two ends of the installation strip shell 1 are rotationally connected with screw rods 9 through bearing seats, one ends close to the two screw rods 9 are fixedly connected with driven bevel gears 10 which are meshed with the driving bevel gear 8, two symmetrically arranged thread blocks 11 are connected on the two screw rods 9 in a threaded manner, one side of each thread block 11 is fixedly connected with two symmetrically arranged connecting rods 12, one ends of the two connecting rods 12 penetrate through one end of the installation strip shell 1 and are fixedly connected with a fixed clamping plate 5, when the temperature measurement probe 3 is required to be installed on the unmanned aerial vehicle body 2, firstly, the detection end of the temperature measurement probe 3 is inserted into the unmanned aerial vehicle body 2, the fixed clamping plates 5 are arranged on two sides of the unmanned aerial vehicle body 2, then, the rotating handle 7 is rotated to drive the driving bevel gear 8 to rotate, and the driving bevel gear 8 is meshed with the two driven bevel gears 10 respectively to drive the two screw rods 9 to rotate reversely simultaneously, at the moment, the two screw thread blocks 11 are forced to displace in opposite directions, and then the two fixed clamping plates 5 are driven to abut against two sides of the unmanned aerial vehicle body 2 to realize fixed installation, so that the temperature measurement device is firm in fixation, simpler in operation and capable of guaranteeing the stability of temperature measurement of the unmanned aerial vehicle body 2.
As shown in fig. 3: two through holes are formed in one end of the installation strip shell 1, and two connecting rods 12 penetrate through the two through holes respectively, so that the connecting rods 12 can conveniently displace.
As shown in fig. 3 and 4: the elastic force adjustment mechanism comprises a sliding cavity 13 arranged in the fixed clamping plate 5, a sliding rod 15 is slidably connected in the sliding cavity 13 through a sliding block 14, one end of the sliding rod 15 penetrates through the fixed clamping plate 5 and is fixedly connected with the L-shaped clamping plate 6, a spring 16 is fixedly connected between the sliding block 14 and the sliding cavity 13, the spring 16 is sleeved on the sliding rod 15, the L-shaped clamping plate 6 is pulled to move downwards during installation, at the moment, the sliding block 14 fixed with the sliding rod 15 is driven to displace in the sliding cavity 13, at the moment, the spring 16 is extruded to generate elastic force, and when the L-shaped clamping plate 6 is loosened, the elastic force effect of the spring 16 is utilized to enable the L-shaped clamping plate 6 to automatically abut against the bottom of the unmanned aerial vehicle body 2, so that the auxiliary fixing effect on installation can be achieved.
As shown in fig. 4: the sliding opening communicated with the sliding cavity 13 is formed in the lower end of the fixed clamping plate 5, and the sliding rod 15 penetrates through the sliding opening to facilitate displacement of the sliding rod 15.
As shown in fig. 2: one side wall of the fixed splint 5 propped against the unmanned aerial vehicle body 2 is fixedly connected with an anti-slip cushion 17, and the clamping is firm.
As shown in fig. 1: four corner fixedly connected with four landing leg frames 18 that symmetry set up in the bottom of unmanned aerial vehicle body 2, and the lower extreme fixedly connected with of four landing leg frames 18 prop ground roller 19 of two parallel arrangement, support steadily unmanned aerial vehicle body 2 on the ground.
Working principle: when the temperature of the unmanned aerial vehicle body 2 is measured in the operation process, firstly, the detection end of the temperature measuring probe 3 is inserted into the unmanned aerial vehicle body 2, the fixed clamping plates 5 are arranged on two sides of the unmanned aerial vehicle body 2, then, the rotating handle 7 is rotated to drive the driving bevel gear 8 to rotate, and the driving bevel gear 8 is respectively meshed with the two driven bevel gears 10 to further drive the two screw rods 9 to simultaneously reversely rotate, at the moment, the two screw thread blocks 11 are forced to displace in opposite directions, and then, the two fixed clamping plates 5 are driven to abut against two sides of the unmanned aerial vehicle body 2 to realize fixed installation, so that the unmanned aerial vehicle is firm in fixation, simpler in operation and capable of guaranteeing the stability of temperature measurement of the unmanned aerial vehicle body 2;
secondly, when the L-shaped clamping plate 6 is installed, the L-shaped clamping plate 6 is pulled to move downwards, at the moment, the sliding block 14 fixed with the sliding rod 15 is driven to move in the sliding cavity 13, at the moment, the spring 16 is extruded to generate elastic force, and when the L-shaped clamping plate 6 is loosened, the L-shaped clamping plate 6 automatically abuts against the bottom of the unmanned aerial vehicle body 2 under the action of the elastic force of the spring 16, so that the auxiliary fixing effect on the installation can be achieved;
secondly, start unmanned aerial vehicle body 2 and fly, temperature measurement probe 3 detects the temperature when unmanned aerial vehicle body 2 operates to feed back temperature data to the inspector through wireless signal module 4, realize short-term test.
The foregoing description is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical solution of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (7)
1. The utility model provides an unmanned aerial vehicle operation temperature measuring device, includes installation strip shell (1) and unmanned aerial vehicle body (2), its characterized in that, the downside center department fixedly connected with temperature measurement probe (3) of installation strip shell (1), and in the detection end of temperature measurement probe (3) runs through and extends to unmanned aerial vehicle body (2), the upside fixedly connected with wireless signal module (4) of installation strip shell (1), and the one end and the wireless signal module (4) electric connection of temperature measurement probe (3), be equipped with centre gripping fixed establishment in installation strip shell (1), and the both ends of centre gripping fixed establishment run through the equal fixedly connected with fixed splint (5) in both ends of installation strip shell (1) respectively, two all be equipped with elasticity adjustment mechanism in fixed splint (5) with the both sides of unmanned aerial vehicle body (2) support tight setting, and the lower extreme fixedly connected with two L shape cardboard (6) that the symmetry set up of elasticity adjustment mechanism, the horizontal straight end lateral wall of L shape cardboard (6) and the bottom fixed connection of unmanned aerial vehicle body (2).
2. The unmanned aerial vehicle operation temperature measuring device according to claim 1, wherein the clamping and fixing mechanism comprises a rotating handle (7) which is inserted into the center of the front side of the installation strip shell (1) and is rotationally connected with the same, one end of the rotating handle (7) extends into the installation strip shell (1) and is fixedly connected with a driving bevel gear (8), two end inner walls of the installation strip shell (1) are respectively connected with a screw rod (9) through bearing seat rotation, one ends, close to the two screw rods (9), of each screw rod are respectively fixedly connected with a driven bevel gear (10) which is meshed with the driving bevel gear (8), two screw blocks (11) which are symmetrically arranged are connected with one side of each screw rod (9) in a threaded mode, and one ends of the two connecting rods (12) penetrate through one end of the installation strip shell (1) and are fixedly connected with a fixed clamping plate (5).
3. An unmanned aerial vehicle operating temperature measuring device according to claim 2, wherein two through holes are provided at one end of the mounting bar housing (1), and two connecting rods (12) are provided through the two through holes, respectively.
4. The unmanned aerial vehicle operation temperature measuring device according to claim 1, wherein the elastic force adjusting mechanism comprises a sliding cavity (13) arranged in the fixed clamping plate (5), a sliding rod (15) is slidably connected in the sliding cavity (13) through a sliding block (14), one end of the sliding rod (15) penetrates through the fixed clamping plate (5) and is fixedly connected with the L-shaped clamping plate (6), a spring (16) is fixedly connected between the sliding block (14) and the sliding cavity (13), and the spring (16) is sleeved on the sliding rod (15).
5. The unmanned aerial vehicle operation temperature measuring device according to claim 4, wherein a sliding port communicated with the sliding cavity (13) is formed in the lower end of the fixed clamping plate (5), and the sliding rod (15) penetrates through the sliding port.
6. The unmanned aerial vehicle running temperature measuring device according to claim 1, wherein an anti-slip soft pad (17) is fixedly connected with one side wall of the fixed clamping plate (5) which is propped against the unmanned aerial vehicle body (2).
7. The unmanned aerial vehicle operation temperature measuring device according to claim 1, wherein four symmetrically arranged leg frames (18) are fixedly connected to four corners of the bottom of the unmanned aerial vehicle body (2), and two ground supporting rollers (19) which are arranged in parallel are fixedly connected to the lower ends of the four leg frames (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223141721.3U CN219524259U (en) | 2022-11-25 | 2022-11-25 | Unmanned aerial vehicle operating temperature measuring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223141721.3U CN219524259U (en) | 2022-11-25 | 2022-11-25 | Unmanned aerial vehicle operating temperature measuring device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219524259U true CN219524259U (en) | 2023-08-15 |
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ID=87630348
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223141721.3U Active CN219524259U (en) | 2022-11-25 | 2022-11-25 | Unmanned aerial vehicle operating temperature measuring device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219524259U (en) |
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2022
- 2022-11-25 CN CN202223141721.3U patent/CN219524259U/en active Active
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