CN210822799U - Unmanned aerial vehicle measuring head adjusting device - Google Patents
Unmanned aerial vehicle measuring head adjusting device Download PDFInfo
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- CN210822799U CN210822799U CN201921791192.7U CN201921791192U CN210822799U CN 210822799 U CN210822799 U CN 210822799U CN 201921791192 U CN201921791192 U CN 201921791192U CN 210822799 U CN210822799 U CN 210822799U
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Abstract
The utility model discloses an unmanned aerial vehicle measuring head adjusting device, which belongs to the field of unmanned aerial vehicles, comprising a body, the left and right sides of the lower end of the body are respectively fixedly connected with supporting legs, the lower end of the supporting legs is fixedly connected with a bottom plate, the lower end of the bottom plate is fixedly connected with a cushion pad, the lower end of the body is fixedly connected with a cutting sleeve, the left and right sides of the cutting sleeve are respectively provided with a through groove, the inner upper end surface of the cutting sleeve is fixedly connected with a spring, the lower end of the spring is fixedly connected with a slider, the lower end of the slider is fixedly connected with a square block, the lower end of the cutting sleeve is fixedly connected with a block, the block is connected with a suspender in a sliding manner, through the elastic action of the spring, the square block and the square groove can be automatically clamped, thereby, reduce the vibrations that produce when unmanned aerial vehicle descends.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, more specifically say, relate to an unmanned aerial vehicle measuring head adjusting device.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
At present, the majority of the existing unmanned aerial vehicle measuring head adjusting devices are fixedly mounted at the lower end of an unmanned aerial vehicle, the square shape of the measuring head cannot be adjusted according to the weather condition, so that a lot of troubles are brought to the flight of the unmanned aerial vehicle, meanwhile, the lower ends of the existing unmanned aerial vehicle supporting legs do not have a protection device, when the unmanned aerial vehicle descends and contacts with the ground, the unmanned aerial vehicle can vibrate with the ground, and the unmanned aerial vehicle is easy to damage.
SUMMERY OF THE UTILITY MODEL
To the problem that exists among the prior art, the utility model aims to provide an unmanned aerial vehicle measuring head adjusting device, elastic action through the spring for square piece and square groove can automatic joint, thereby conveniently rotate the caliber, and the trouble of avoiding fixed mounting to bring is connected through bottom plate and blotter to the detection direction of convenient fixed caliber, plays the absorbing effect of buffering to unmanned aerial vehicle, the vibrations that produce when reducing unmanned aerial vehicle and descending.
In order to solve the above problems, the utility model adopts the following technical proposal.
An unmanned aerial vehicle measuring head adjusting device comprises a body, wherein the left side and the right side of the lower end of the body are respectively fixedly connected with supporting legs, the lower ends of the supporting legs are fixedly connected with a bottom plate, the lower end of the bottom plate is fixedly connected with a cushion pad, the lower end of the body is fixedly connected with a clamping sleeve, the left side and the right side of the clamping sleeve are respectively provided with a through groove, the inner upper end surface of the clamping sleeve is fixedly connected with a spring, the lower end of the spring is fixedly connected with a sliding block, the lower end of the sliding block is fixedly connected with a square block, the lower end of the clamping sleeve is fixedly connected with a blocking block, the blocking block is slidably connected with a suspender, the lower end of the suspender is slidably connected with a connecting sleeve, the left side and the right side of the body are respectively fixedly connected, avoid the trouble that fixed mounting brought, through being connected of bottom plate and blotter, play the absorbing effect of buffering to unmanned aerial vehicle, the vibrations that produce when reducing unmanned aerial vehicle and descending.
Further, the left and right sides of slider is fixedly connected with anticreep pole respectively, anticreep pole and logical groove sliding connection through anticreep pole and logical groove sliding connection, make things convenient for the position of fixed slider.
Further, the upper end of jib is equipped with square groove, square piece and square groove joint through square piece and square groove joint, conveniently fix the measuring position of caliber.
Further, the connecting sleeve and the hanging rod are fixedly connected through a bolt, the lower end of the connecting sleeve is fixedly connected with the measurer, and the measurer is conveniently taken down through the connecting sleeve and the hanging rod which are fixedly connected through the bolt.
Furthermore, the one end fixedly connected with wing seat of wing arm, the upper end of wing seat rotates and is connected with the wing, and the wing plays very important effect to unmanned aerial vehicle's flight.
Compared with the prior art, the utility model has the advantages of:
(1) this scheme passes through the elastic action of spring for square piece and square groove can automatic joint, thereby conveniently rotate the caliber, and the trouble of avoiding fixed mounting to bring is convenient to fix the detection direction of caliber, through being connected of bottom plate and blotter, plays the absorbing effect of buffering to unmanned aerial vehicle, the vibrations that produce when reducing unmanned aerial vehicle descending.
(2) The left and right sides of slider is fixedly connected with anticreep pole respectively, anticreep pole and logical groove sliding connection, through anticreep pole and logical groove sliding connection, the position of convenient fixed slider.
(3) The upper end of jib is equipped with square groove, square piece and square groove joint, through square piece and square groove joint, the measuring position of convenient fixed caliber.
(4) The adapter sleeve passes through bolt fixed connection with the jib, and the lower extreme fixedly connected with caliber of adapter sleeve passes through bolt fixed connection through adapter sleeve and jib, conveniently takes off the caliber.
(5) One end fixedly connected with wing seat of wing arm, the upper end of wing seat is rotated and is connected with the wing, and the wing plays very important effect to unmanned aerial vehicle's flight.
Drawings
FIG. 1 is a sectional view of the overall structure of the present invention;
FIG. 2 is a left side view of the junction of the base plate and the cushion pad of the present invention;
fig. 3 is an enlarged view of a portion a of fig. 1 according to the present invention;
fig. 4 is a top view of the hanger bar of the present invention;
fig. 5 is a bottom view of the slider according to the present invention.
The reference numbers in the figures illustrate:
the airplane wing comprises a fuselage 1, supporting legs 2, a bottom plate 3, a cushion 31, a clamping sleeve 4, a through groove 5, a spring 6, a sliding block 7, an anti-dropping rod 8, a square block 9, a block 10, a hanging rod 11, a square groove 12, a connecting sleeve 13, a measurer 14, a wing arm 15, a wing seat 16 and a wing 17.
Detailed Description
The technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiment of the present invention; obviously, the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention based on the embodiments of the present invention.
Referring to fig. 1-5, an unmanned aerial vehicle measuring head adjusting device comprises a body 1, referring to fig. 1-3, wherein the left side and the right side of the lower end of the body 1 are respectively and fixedly connected with supporting legs 2, the lower end of the supporting legs 2 is fixedly connected with a bottom plate 3, the lower end of the bottom plate 3 is fixedly connected with a cushion pad 31, the lower end of the body 1 is fixedly connected with a cutting sleeve 4, the left side and the right side of the cutting sleeve 4 are respectively provided with a through groove 5, the upper surface of the inner part of the cutting sleeve 4 is fixedly connected with a spring 6, the lower end of the spring 6 is fixedly connected with a sliding block 7, the lower end of the sliding block 7 is fixedly connected with a square block 9, the lower end of the cutting sleeve 4 is fixedly connected with a block 10, the block 10 is slidably connected with a suspender 11, the lower end of the suspender 11 is, thereby conveniently rotate caliber 14, the trouble that fixed mounting brought is avoided to the direction of detection of convenient fixed caliber 14, through being connected of bottom plate 3 and blotter 31, plays the absorbing effect of buffering to unmanned aerial vehicle, reduces the vibrations that produce when unmanned aerial vehicle descends.
Referring to fig. 1-3, the left and right sides of the slider 7 are fixedly connected with an anti-falling rod 8, the anti-falling rod 8 is slidably connected with the through groove 5, the position of the slider 7 is conveniently fixed, the upper end of the suspension rod 11 is provided with a square groove 12, the square block 9 is clamped with the square groove 12, and the square block 9 is clamped with the square groove 12, so that the measuring position of the measurer 14 is conveniently fixed.
Referring to fig. 1-3, the connecting sleeve 13 is fixedly connected with the suspension rod 11 through a bolt, the lower end of the connecting sleeve 13 is fixedly connected with the measurer 14, the measurer 14 is conveniently taken down through the connecting sleeve 13 and the suspension rod 11 through the bolt, one end of the wing arm 15 is fixedly connected with the wing seat 16, the upper end of the wing seat 16 is rotatably connected with the wing 17, and the wing 17 plays an important role in flying the unmanned aerial vehicle.
The lower end of a suspender 11 is connected with a connecting sleeve 13 in a sliding manner, and then the suspender is fixed through a bolt, when the detection direction of a measurer 14 needs to be changed, an anti-falling rod 8 is moved upwards firstly, so that the anti-falling rod 8 moves upwards, meanwhile, a spring 6 is extruded and contracted under stress, a square block 9 is driven by a slider 7 to move upwards, so that the square block 9 is separated from a square groove 12, then the measurer 14 can be rotated, so that the measurer 14 drives the suspender 11 to rotate, when the measurer moves to a proper position, the anti-falling rod 8 is released, the spring 6 is stretched and reset, the slider 7 is pushed to reset, the square block 9 is clamped with the square groove 12, the purpose of the rotation direction is achieved, the square block 9 and the square groove 12 can be automatically clamped through the elastic action of the spring 6, so that the measurer 14 can be rotated conveniently, the detection direction of the, through being connected of bottom plate 3 and blotter 31, play the absorbing effect of buffering to unmanned aerial vehicle, the vibrations that produce when reducing unmanned aerial vehicle to descend.
The above description is only the preferred embodiment of the present invention; the scope of the present invention is not limited thereto. Any person skilled in the art should also be able to cover the technical scope of the present invention by replacing or changing the technical solution and the improvement concept of the present invention with equivalents and modifications within the technical scope of the present invention.
Claims (5)
1. The utility model provides an unmanned aerial vehicle measuring head adjusting device, includes fuselage (1), its characterized in that: the left side and the right side of the lower end of the machine body (1) are respectively and fixedly connected with a supporting leg (2), the lower end of the supporting leg (2) is fixedly connected with a bottom plate (3), the lower end of the bottom plate (3) is fixedly connected with a cushion pad (31), a cutting sleeve (4) is fixedly connected at the lower end of the machine body (1), through grooves (5) are respectively arranged at the left side and the right side of the cutting sleeve (4), the surface of the upper end inside the cutting sleeve (4) is fixedly connected with a spring (6), the lower end of the spring (6) is fixedly connected with a sliding block (7), the lower end of the sliding block (7) is fixedly connected with a square block (9), the lower end of the cutting sleeve (4) is fixedly connected with a block (10), the block (10) is connected with a suspender (11) in a sliding way, the lower extreme sliding connection of jib (11) has adapter sleeve (13), the left and right sides of fuselage (1) fixedly connected with wing arm (15) respectively.
2. The adjusting device of claim 1, wherein: the left side and the right side of the sliding block (7) are respectively and fixedly connected with an anti-falling rod (8), and the anti-falling rods (8) are connected with the through grooves (5) in a sliding mode.
3. The adjusting device of claim 1, wherein: the upper end of jib (11) is equipped with square groove (12), square piece (9) and square groove (12) joint.
4. The adjusting device of claim 1, wherein: the connecting sleeve (13) is fixedly connected with the hanging rod (11) through a bolt, and the lower end of the connecting sleeve (13) is fixedly connected with a measurer (14).
5. The adjusting device of claim 1, wherein: one end of the wing arm (15) is fixedly connected with a wing seat (16), and the upper end of the wing seat (16) is rotatably connected with a wing (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921791192.7U CN210822799U (en) | 2019-10-24 | 2019-10-24 | Unmanned aerial vehicle measuring head adjusting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921791192.7U CN210822799U (en) | 2019-10-24 | 2019-10-24 | Unmanned aerial vehicle measuring head adjusting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210822799U true CN210822799U (en) | 2020-06-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921791192.7U Active CN210822799U (en) | 2019-10-24 | 2019-10-24 | Unmanned aerial vehicle measuring head adjusting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210822799U (en) |
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2019
- 2019-10-24 CN CN201921791192.7U patent/CN210822799U/en active Active
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