CN218055638U - Intelligent flying device for high-altitude measurement - Google Patents
Intelligent flying device for high-altitude measurement Download PDFInfo
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- CN218055638U CN218055638U CN202220970550.6U CN202220970550U CN218055638U CN 218055638 U CN218055638 U CN 218055638U CN 202220970550 U CN202220970550 U CN 202220970550U CN 218055638 U CN218055638 U CN 218055638U
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- high altitude
- flying device
- altitude measurement
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- 238000005259 measurement Methods 0.000 title claims abstract description 20
- 230000000694 effects Effects 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 claims description 7
- 238000005096 rolling process Methods 0.000 claims description 5
- 230000000149 penetrating effect Effects 0.000 claims description 2
- 230000002093 peripheral effect Effects 0.000 claims 1
- 239000000872 buffer Substances 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 229920001821 foam rubber Polymers 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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Abstract
The utility model discloses an intelligent flying device for high altitude measurement relates to high altitude measurement technical field. The utility model discloses mainly include the body, the fixed plate is installed to the bottom of body, the below activity of fixed plate is provided with the baffle, be connected with a plurality of spring one that distributes evenly between baffle and the fixed plate, install a plurality of fender rod on the periphery side of fixed plate, the quantity of fender rod is the same and the one-to-one with the quantity of wing on the body, the length of fender rod is greater than the length of wing to main part on the body, the end connection of fender rod has spring two, the other end of spring two is installed and is had the elasticity piece, be connected with the connecting rod between two adjacent fender rods. The utility model discloses on the way of flight, when hitting the object of high altitude by mistake, the spring cushions two pairs of impact, and the impact that transmits to on the body reduces, has guaranteed the safety of body, guarantees measuring efficiency, and the device is when descending, and the safety of baffle and spring safety guarantee device descends.
Description
Technical Field
The utility model relates to a high altitude measurement technical field, concretely relates to high altitude is intelligent flying device for measurement.
Background
The method and technique for measuring physical and chemical characteristics of atmosphere above the near-ground layer is called high-altitude detection or high-altitude observation. The high-altitude meteorological observation mainly measures the temperature, humidity, air pressure, wind direction and wind speed of the atmosphere at each altitude.
Along with the progress of science and technology and the development of society, at present, when carrying out high altitude measurement, use intelligent flying device to carry out high altitude measurement usually, intelligent flying device volume is less, the operation of being convenient for, be applicable to different terrain environment, operating personnel when operating intelligent flying device and carry out high altitude measurement, misoperation's possibility probably appears, lead to intelligent flying device flight unstability, hit the object of high altitude, take place to damage, influence measuring efficiency, simultaneously, intelligent flying device is when flying, probably self breaks down, lead to falling, thereby damage with ground striking, for this reason, technical staff in the art has designed an intelligent flying device for high altitude measurement.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: when solving the operating personnel who provides among the above-mentioned background art and operating intelligent flying device and carrying out high altitude measurement, misoperation's possibility can appear, leads to intelligent flying device flight unstability, strikes the object of high altitude, takes place to damage, influences the problem of measuring efficiency, the utility model provides an intelligent flying device is used in high altitude measurement.
The utility model discloses a realize above-mentioned purpose and specifically adopt following technical scheme:
the utility model provides an intelligent flying device for high altitude survey, includes the body, the fixed plate is installed to the bottom of body, the below activity of fixed plate is provided with the baffle, the baffle with be connected with a plurality of evenly distributed spring one between the fixed plate, install a plurality of fender rod on the periphery side of fixed plate, the quantity of fender rod with the same and the one-to-one of quantity of wing on the body, the length of fender rod is greater than wing arrives on the body the length of main part on the body, the end connection of fender rod has spring two, the other end of spring two is installed flexible piece, adjacent two be connected with the connecting rod between the fender rod.
Preferably, the fixed plate not with the body is fixed, install on the periphery side of fixed plate and be no less than two and evenly distributed's connecting plate, T type spout has been seted up along length direction on the connecting plate, slidable mounting has the L shaped plate on the T type spout, the L shaped plate with the screw thread runs through on one side that the connecting plate parallels is provided with the screw, the screw is close to one of connecting plate is served and is installed the briquetting.
Preferably, the end fixing of connecting plate has looks vertically installation piece, the installation piece go up the screw thread run through be provided with the threaded rod that the connecting plate parallels, the one end of threaded rod with the L shaped plate rotates to be connected, the cushion is installed to the tip of L shaped plate.
Preferably, the guard bar is L-shaped, the end part of the guard bar is higher than the height of the upper wing of the body, and the second spring is arranged at the end part of the guard bar.
Preferably, a device block is fixed at the end part of the protection rod, a device groove is formed in one side, back to the body, of the device block, the elastic block is movably inserted into the device groove, and the second spring is connected between the elastic block and the inner wall of the device groove.
Preferably, the elastic block comprises a guide block connected with the spring II, and a rolling ball is movably arranged on the guide block.
Preferably, the bottom of the guard bar is provided with a third spring, the end part of the third spring is connected with a cushion block, and the cushion block and the baffle are located on the same horizontal plane.
Has the advantages that:
1. when the device flies and collides with a high-altitude object by mistake, the elastic block at the end part of the protective rod is contacted with the high-altitude object, the two pairs of impact forces of the spring buffer, the impact force transmitted to the body is reduced, the safety of the body is ensured, and the measuring efficiency is ensured;
2. when the device has a fault, the device can suddenly fall from the high altitude, and when the device body falls on the ground, the body can be damped no matter the elastic block contacts the ground firstly or the baffle contacts the ground firstly, so that the damage degree of the body is reduced;
3. when the device descends, the baffle firstly contacts with the ground, force is transmitted to the first spring, the first spring buffers, the safe descending of the device is guaranteed, the using effect is better, and the service life is prolonged.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic perspective view of the present invention;
figure 2 is a front view of the present invention in figure 1;
fig. 3 is a top view of the present invention shown in fig. 1;
fig. 4 isbase:Sub>A cross-sectional view taken along the linebase:Sub>A-base:Sub>A of fig. 3 according to the present invention;
fig. 5 is a cross-sectional view taken along the direction B-B in fig. 3 according to the present invention.
In fig. 1-5:
1. a body; 2. a fixing plate; 3. a baffle plate; 4. a first spring; 5. a guard bar; 6. a second spring; 7. an elastic block; 8. a connecting rod; 21. a connecting plate; 22. a T-shaped chute; 23. an L-shaped plate; 24. a screw; 25. briquetting; 26. mounting blocks; 27. a threaded rod; 28. a soft cushion; 51. a device block; 52. a device slot; 53. a third spring; 54. cushion blocks; 71. a guide block; 72. a ball.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the drawings in the embodiments of the present invention are combined below to clearly and completely describe the technical solutions in the embodiments of the present invention.
Fig. 1 to fig. 5 show an intelligent flying device for high altitude measurement according to the present embodiment; mainly include body 1, body 1 is unmanned aerial vehicle, fixed plate 2 is installed to body 1's bottom, the below activity of fixed plate 2 is provided with baffle 3, be connected with a plurality of spring 4 that distributes evenly between baffle 3 and fixed plate 2, the foam-rubber cushion is installed to baffle 3's bottom, the device is when descending, the foam-rubber cushion of baffle 3 bottom contacts with ground earlier, body 1 is under the effect of gravity, continue to move down, spring 4 compresses, produce elasticity, cushion, can make the device descending more stable, avoid vibrating and damage the electronic component of body 1 inside, install a plurality of fender rod 5 on the periphery side of fixed plate 2, the quantity of fender rod 5 is the same and the wing one-to-one with the quantity on body 1, the length of fender rod 5 is greater than the length of wing main part on body 1, can guarantee the device on the way of flight, when the mistake bumps high altitude object, the one end of fender rod 5 at first takes place the contact with the object, prevent the wing on body 1 and contact with the object, cause the damage, the end connection of fender rod 5 has spring two 6, the other end connection of spring 6 has elasticity, the piece 7, when the elastic impact of spring 5 and the fender rod is used for preventing two adjacent fender rod 5 and the impact and the body, it is used for the improvement, it is adjacent fender rod to bump to prevent that the transmission of the impact strength is used for the transmission, it is used for two fender rod, it is adjacent impact, it is used for the improvement to bump on the body, it is adjacent fender rod, it is adjacent impact, it is connected with the fender rod, it is used for two fender rod, it is adjacent impact, it is in the body, it is used for the impact, it is improved.
Further, please refer to fig. 3 and 4, the fixing plate 2 is not fixed to the body 1, the fixing plate and the body 1 are not directly fixed to each other, at least two connecting plates 21 are installed on the outer periphery of the fixing plate 2 and are evenly distributed, a T-shaped chute 22 is formed in the connecting plate 21 along the length direction, an L-shaped plate 23 is installed on the T-shaped chute 22 in a sliding manner, a screw 24 is arranged on one side of the L-shaped plate 23 parallel to the connecting plate 21 in a penetrating manner, a pressing block 25 is installed on one end of the screw 24 close to the connecting plate 21, when the fixing plate is installed, the body 1 is attached to the fixing plate 2, the L-shaped plate 23 is slid, an opening of the L-shaped plate 23 is sleeved on a frame of the body 1, then the screw 24 is rotated to drive the pressing block 25 to move, the pressing block 25 is tightly abutted to the frame of the body 1, the fixing plate 2 can be connected to the body 1, the fixing plate 2 is conveniently connected to the body 1, a mounting block 26 perpendicular to the end of the connecting plate 21 is fixed with a threaded rod 27 parallel to the connecting plate 21, one end of the threaded rod 27 is rotatably connected to the L-shaped plate 23, if the cushion body 23 is not provided with a smooth face of a cushion, and the cushion, the cushion 23, and the cushion is connected to the cushion body 23.
In this embodiment, please refer to fig. 3 and 5, the guard bar 5 is L-shaped, and the end of the guard bar 5 is higher than the wing of the body 1, the guard bar 5 is L-shaped, when the device accidentally touches an object above the guard bar, the guard bar 5 can prevent the wing from touching the object, and ensure that the wing is not damaged, the second spring 6 is disposed at the end of the guard bar 5, the end of the guard bar 5 is fixed with the device block 51, the device groove 52 is disposed on one side of the device block 51 facing away from the body 1, the elastic block 7 is movably inserted inside the device groove 52, the second spring 6 is connected between the elastic block 7 and the inner wall of the device groove 52, when the elastic block 7 hits the object, the impact force moves the elastic block 7 to drive the second spring 6 to compress, the second spring 6 generates elastic force to buffer, a part of the impact force is counteracted, the elastic block 7 includes the guide block 71 connected with the second spring 6, the guide block 71 is movably mounted with the rolling ball 72, the rolling ball 72 can roll on the guide block 71, the use effect is better, when the ball 72 hits the object, the distance along the surface of the object can be better, the rolling distance, and the service life of the object can be prolonged.
Further, please refer to fig. 2, a third spring 53 is installed at the bottom of the guard bar 5, a cushion block 54 is connected to the end of the third spring 53, and the cushion block 54 and the baffle 3 are located on the same horizontal plane, so that the device can be more stably descended when the device is descended, and the device is prevented from being damaged due to side turning.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (7)
1. The utility model provides an intelligent flying device for high altitude measurement, its characterized in that, includes body (1), fixed plate (2) are installed to the bottom of body (1), the below activity of fixed plate (2) is provided with baffle (3), baffle (3) with be connected with a plurality of evenly distributed spring (4) between fixed plate (2), install a plurality of fender rod (5) on the periphery side of fixed plate (2), the quantity of fender rod (5) with the same and the one-to-one of quantity of wing on body (1), the length of fender rod (5) is greater than wing arrives on body (1) the length of main part on body (1), the end connection of fender rod (5) has spring two (6), elastic block (7) are installed to the other end of spring two (6), adjacent two be connected with connecting rod (8) between fender rod (5).
2. The intelligent flying device for high altitude measurement according to claim 1, wherein the fixed plate (2) is not fixed to the body (1), at least two evenly distributed connecting plates (21) are mounted on the outer peripheral side of the fixed plate (2), a T-shaped chute (22) is formed in the connecting plate (21) along the length direction, an L-shaped plate (23) is mounted on the T-shaped chute (22) in a sliding manner, a screw (24) penetrates through the L-shaped plate (23) and the connecting plate (21) in a threaded manner on one side parallel to each other, and a pressing block (25) is mounted on one end, close to the connecting plate (21), of the screw (24).
3. The intelligent flying device for high altitude measurement according to claim 2, wherein the end of the connecting plate (21) is fixed with a vertical mounting block (26), a threaded rod (27) parallel to the connecting plate (21) is arranged on the mounting block (26) in a threaded penetrating manner, one end of the threaded rod (27) is rotatably connected with the L-shaped plate (23), and a cushion (28) is mounted at the end of the L-shaped plate (23).
4. The intelligent flying device for high altitude measurement according to claim 1, wherein the guard bar (5) is L-shaped and has an end higher than the height of the upper wing of the body (1), and the second spring (6) is arranged at the end of the guard bar (5).
5. The intelligent flying device for high altitude measurement according to claim 1, wherein an installation block (51) is fixed to an end of the protection rod (5), an installation groove (52) is formed in one side, facing away from the body (1), of the installation block (51), the elastic block (7) is movably inserted into the installation groove (52), and the second spring (6) is connected between the elastic block (7) and the inner wall of the installation groove (52).
6. The intelligent flying device for high altitude measurement according to claim 5, wherein the elastic block (7) comprises a guide block (71) connected with the second spring (6), and a rolling ball (72) is movably mounted on the guide block (71).
7. The intelligent flying device for high altitude measurement according to claim 1, wherein a third spring (53) is installed at the bottom of the guard bar (5), a cushion block (54) is connected to the end of the third spring (53), and the cushion block (54) and the baffle (3) are located on the same horizontal plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220970550.6U CN218055638U (en) | 2022-04-22 | 2022-04-22 | Intelligent flying device for high-altitude measurement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220970550.6U CN218055638U (en) | 2022-04-22 | 2022-04-22 | Intelligent flying device for high-altitude measurement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218055638U true CN218055638U (en) | 2022-12-16 |
Family
ID=84427204
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220970550.6U Expired - Fee Related CN218055638U (en) | 2022-04-22 | 2022-04-22 | Intelligent flying device for high-altitude measurement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218055638U (en) |
-
2022
- 2022-04-22 CN CN202220970550.6U patent/CN218055638U/en not_active Expired - Fee Related
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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: 20221216 |