CN215025976U - Stably-descending unmanned aerial vehicle toy - Google Patents
Stably-descending unmanned aerial vehicle toy Download PDFInfo
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- CN215025976U CN215025976U CN202121171978.6U CN202121171978U CN215025976U CN 215025976 U CN215025976 U CN 215025976U CN 202121171978 U CN202121171978 U CN 202121171978U CN 215025976 U CN215025976 U CN 215025976U
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Abstract
The utility model discloses an unmanned plane toy with stable descending, which comprises an unmanned plane body and a buffer component; an unmanned body: side wings are symmetrically arranged on two sides of the unmanned aerial vehicle body, a motor is arranged on each side wing, blades are arranged on an output shaft of the motor, and landing gears are symmetrically arranged on two sides of the bottom surface of the unmanned aerial vehicle body; a buffer assembly: including side slot, guide arm, clamp plate, first spring, square groove and block rubber, the both sides of undercarriage are located to the side slot symmetry, the side inslot is located to the guide arm, the both ends activity respectively of clamp plate is cup jointed on the guide arm of both sides, first spring cup joints on the guide arm, and first spring is located the upside of clamp plate, the bottom surface of undercarriage is located to the square groove, and this stable unmanned aerial vehicle toy that descends is equipped with energy storage structure, can prolong duration to be equipped with buffer structure, alleviate the collision with ground, make unmanned aerial vehicle stabilize descending, effectively reduced unmanned aerial vehicle because of the impaired probability of falling of electric quantity exhaustion, the practicality is stronger.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a stable unmanned aerial vehicle toy descends.
Background
Unmanned aerial vehicle is the unmanned aerial vehicle who utilizes radio remote control equipment and self-contained program control device to control, along with the rapid development of science and technology, unmanned aerial vehicle is used more and more extensively, makes unmanned aerial vehicle become for a new and emerging toy, current partial unmanned aerial vehicle's time of endurance is shorter, leads to unmanned aerial vehicle outage out of control easily and falls to probably produce violent collision with ground and make unmanned aerial vehicle damage, for this, we propose a stable unmanned aerial vehicle toy that descends.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is to overcome current defect, provide a descend stable unmanned aerial vehicle toy, be equipped with energy storage structure, can prolong duration to be equipped with buffer structure, alleviate with the collision on ground, make unmanned aerial vehicle stabilize the descending, effectively reduced unmanned aerial vehicle because of the impaired probability of falling of electric quantity exhaustion, the practicality is stronger, can effectively solve the problem in the background art.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned plane toy with stable descending comprises an unmanned plane body and a buffer component;
an unmanned body: side wings are symmetrically arranged on two sides of the unmanned aerial vehicle body, a motor is arranged on each side wing, blades are arranged on an output shaft of the motor, and landing gears are symmetrically arranged on two sides of the bottom surface of the unmanned aerial vehicle body;
a buffer assembly: the undercarriage comprises side grooves, guide rods, a pressing plate, a first spring, a square groove and a rubber block, wherein the side grooves are symmetrically arranged on two sides of the undercarriage, the guide rods are arranged in the side grooves, two ends of the pressing plate are respectively movably sleeved on the guide rods on the two sides, the first spring is sleeved on the guide rods and is positioned on the upper side of the pressing plate, the square groove is arranged on the bottom surface of the undercarriage, the rubber block is arranged at the bottom of the pressing plate, and the rubber block is correspondingly matched with the square groove;
wherein: the unmanned aerial vehicle further comprises a single chip microcomputer, and the single chip microcomputer is arranged on the end face of the unmanned aerial vehicle body.
Further, the buffering subassembly still includes telescopic link and second spring, the bottom surface both sides of clamp plate are located to the telescopic link symmetry, and the bottom of telescopic link and the fixed surface of block rubber are connected, the second spring cup joints on the telescopic link, and the buffering subassembly can be about to fall to the ground the back at the unmanned aerial vehicle body, and the automatic metal block that releases of electro-magnet utilizes reseing of first spring, and the clamp plate slides down, makes the block rubber stretch out the square groove, in the twinkling of an eye that the block rubber falls to the ground, the telescopic link is compressed, and the clamp plate upwards slides, can utilize first spring and second spring to realize the buffering to the block rubber, makes the unmanned aerial vehicle body stably descend.
Further, still include mounting groove and group battery, the bottom surface of unmanned aerial vehicle body is located to the mounting groove, the group battery is located in the mounting groove, and the output of group battery is connected with the input electricity of singlechip, utilizes the group battery to realize electric power storage and discharge.
Further, still include electro-magnet and metal block, the bottom surface of unmanned aerial vehicle body is located to the electro-magnet, the surface of clamp plate is located to the metal block, and the metal block corresponds with the electro-magnet, and the input of electro-magnet is connected with the output electricity of singlechip, and the electro-magnet passes through the actuation metal block, can make first spring be in compression state to, when the group battery electric quantity exhausts, the electro-magnet outage, automatic release metal block can automatic start buffering subassembly, alleviates the collision with ground.
Further, still include mount pad and range sensor, the bottom surface middle part of unmanned aerial vehicle body is located to the mount pad, range sensor locates on the mount pad, range sensor's output is connected with the input electricity of singlechip, and range sensor detectable unmanned aerial vehicle body and the distance on ground can be about to the automatic start buffering subassembly after reacing ground at unmanned aerial vehicle.
Further, still include support, solar cell panel, kerve and solar control ware, the surface of unmanned aerial vehicle body is located to the support, the both sides of support are located to the solar cell panel symmetry, the bottom surface of unmanned aerial vehicle body is located to the kerve, in the kerve was located to the solar control ware, solar cell panel's output and solar control ware's input electricity are connected, and solar control ware's output is connected with the input electricity of group battery, and when the electric quantity in the group battery was about to run out, but automatic utilization solar cell panel, convert solar energy into the electric energy and supply power for the group battery, extension duration.
Compared with the prior art, the beneficial effects of the utility model are that: this descend stable unmanned aerial vehicle toy has following benefit:
1. this stable unmanned aerial vehicle toy's of decline buffering subassembly can be about to fall to the ground the back at the unmanned aerial vehicle body, and the automatic metal block that releases of electro-magnet utilizes reseing of first spring, and the clamp plate slides down, makes the block rubber stretch out the square groove, in the twinkling of an eye that the block rubber falls to the ground, and the telescopic link is compressed, and the clamp plate upwards slides, can utilize first spring and second spring to realize the buffering to the block rubber, makes the unmanned aerial vehicle body stable descending.
2. This descend stable unmanned aerial vehicle toy's electro-magnet through the actuation metal block, can make first spring be in compression state to, when the group battery electric quantity exhausts, the electro-magnet outage, automatic release metal block can the automatic start buffering subassembly, alleviates the collision with ground.
3. This decline stable usable solar cell panel of unmanned aerial vehicle toy can be stored solar energy conversion for the electric energy in the group battery, then can be when the electric quantity in the group battery is about to exhaust, for the group battery is automatic to charge, and extension duration avoids the unmanned aerial vehicle body to cut off the power supply suddenly and falls.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged schematic view of the structure at A of the present invention;
fig. 3 is a schematic bottom structure diagram of the present invention.
In the figure: the device comprises an unmanned aerial vehicle body 1, a single chip microcomputer 11, a side wing 12, a blade 13, an undercarriage 14, a buffer component 2, a side groove 21, a guide rod 22, a pressing plate 23, a first spring 24, a square groove 25, a rubber block 26, a telescopic rod 27, a second spring 28, an electromagnet 3, a metal block 31, a mounting seat 4, a distance measuring sensor 41, a support 5, a solar cell panel 51, a bottom groove 52, a solar controller 53, a mounting groove 6 and a battery pack 61.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present embodiment provides a technical solution: an unmanned plane toy with stable descending comprises an unmanned plane body 1 and a buffer component 2;
the unmanned aerial vehicle body 1: the two sides of the unmanned aerial vehicle body 1 are symmetrically provided with side wings 12, the side wings 12 are provided with motors, the output shafts of the motors are provided with blades 13, and the two sides of the bottom surface of the unmanned aerial vehicle body 1 are symmetrically provided with landing gears 14;
the buffer assembly 2: the buffering component 2 further comprises telescopic rods 27 and second springs 28, the telescopic rods 27 are symmetrically arranged on two sides of the bottom surface of the pressing plate 23, the bottom ends of the telescopic rods 27 are fixedly connected with the surfaces of the rubber blocks 26, and the second springs 28 are sleeved on the telescopic rods 27;
wherein: still include singlechip 11, singlechip 11 locates the terminal surface of unmanned aerial vehicle body 1.
Wherein: the unmanned aerial vehicle further comprises a mounting groove 6 and a battery pack 61, wherein the mounting groove 6 is arranged on the bottom surface of the unmanned aerial vehicle body 1, the battery pack 61 is arranged in the mounting groove 6, and the output end of the battery pack 61 is electrically connected with the input end of the singlechip 11; the unmanned aerial vehicle is characterized by further comprising an electromagnet 3 and a metal block 31, wherein the electromagnet 3 is arranged on the bottom surface of the unmanned aerial vehicle body 1, the metal block 31 is arranged on the surface of the pressing plate 23, the metal block 31 corresponds to the electromagnet 3, and the input end of the electromagnet 3 is electrically connected with the output end of the single chip microcomputer 11; the unmanned aerial vehicle further comprises a mounting seat 4 and a ranging sensor 41, wherein the mounting seat 4 is arranged in the middle of the bottom surface of the unmanned aerial vehicle body 1, the ranging sensor 41 is arranged on the mounting seat 4, and the output end of the ranging sensor 41 is electrically connected with the input end of the singlechip 11; still include support 5, solar cell panel 51, kerve 52 and solar controller 53, support 5 locates the surface of unmanned aerial vehicle body 1, and the both sides of support 5 are located to solar cell panel 51 symmetry, and the bottom surface of unmanned aerial vehicle body 1 is located to kerve 52, and solar controller 53 locates in kerve 52, and the output of solar cell panel 51 is connected with solar controller 53's input electricity, and solar controller 53's output is connected with the input electricity of group battery 61.
After the unmanned aerial vehicle body 1 is about to fall to the ground, ranging sensor 41 sends a signal to singlechip 11, and 3 automatic release metal blocks 31 of electro-magnet reset, and first spring 24 resets, and clamp plate 23 slides down, makes block rubber 26 stretch out square groove 25, and in the twinkling of an eye that block rubber 26 falls to the ground, telescopic link 27 is compressed, and clamp plate 23 upwards slides, can utilize the compression realization of first spring 24 and second spring 28 to block rubber 26's buffering.
The utility model provides a pair of stable unmanned aerial vehicle toy's of decline theory of operation as follows: firstly, after the unmanned aerial vehicle body 1 is about to fall to the ground, distance measuring sensor 41 sends a signal to singlechip 11, 3 automatic release metal blocks 31 of electro-magnet, first spring 24 resets, clamp plate 23 slides down, make rubber block 26 stretch out square groove 25, in the twinkling of an eye that rubber block 26 falls to the ground, telescopic link 27 is compressed, clamp plate 23 slides up, can utilize the compression of first spring 24 and second spring 28 to realize the buffering to rubber block 26, make unmanned aerial vehicle body 1 stably descend, and, when group battery 61 electric quantity exhausts, 3 outage of electro-magnet, automatic release metal blocks 31, can automatic start buffer assembly 2, alleviate the collision with ground, when electric quantity in group battery 61 is about to exhaust, usable solar cell panel 51, convert solar energy into the electric energy and charge for group battery 61, the extension duration.
It should be noted that the specific model of the single chip microcomputer 11 disclosed in the above embodiments is an STM32 single chip microcomputer, the electromagnet 3 and the distance measuring sensor 41 can be freely configured according to the actual application scenario, the electromagnet 3 can be a direct current electromagnet, and the distance measuring sensor 41 can be a laser distance measuring sensor. The single chip microcomputer 11 controls the electromagnet 3 and the distance measuring sensor 41 to work by adopting a common method in the prior art.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.
Claims (6)
1. The utility model provides a decline stable unmanned aerial vehicle toy which characterized in that: comprises an unmanned body (1) and a buffer component (2);
unmanned body (1): the unmanned aerial vehicle is characterized in that side wings (12) are symmetrically arranged on two sides, a motor is arranged on each side wing (12), blades (13) are arranged on an output shaft of the motor, and landing gears (14) are symmetrically arranged on two sides of the bottom surface of the unmanned aerial vehicle body (1);
cushioning assembly (2): the undercarriage structure comprises side grooves (21), guide rods (22), a pressing plate (23), first springs (24), square grooves (25) and rubber blocks (26), wherein the side grooves (21) are symmetrically arranged on two sides of the undercarriage (14), the guide rods (22) are arranged in the side grooves (21), two ends of the pressing plate (23) are respectively movably sleeved on the guide rods (22) on the two sides, the first springs (24) are sleeved on the guide rods (22), the first springs (24) are located on the upper sides of the pressing plate (23), the square grooves (25) are arranged on the bottom surface of the undercarriage (14), the rubber blocks (26) are arranged at the bottom of the pressing plate (23), and the rubber blocks (26) are correspondingly matched with the square grooves (25);
wherein: the unmanned aerial vehicle is characterized by further comprising a single chip microcomputer (11), wherein the single chip microcomputer (11) is arranged on the end face of the unmanned aerial vehicle body (1).
2. A descent stabilizing drone toy according to claim 1, characterised in that: buffer unit (2) still include telescopic link (27) and second spring (28), the bottom surface both sides of clamp plate (23) are located to telescopic link (27) symmetry, and the fixed surface of the bottom of telescopic link (27) and rubber block (26) is connected, second spring (28) cup joint on telescopic link (27).
3. A descent stabilizing drone toy according to claim 1, characterised in that: still include mounting groove (6) and group battery (61), the bottom surface of unmanned aerial vehicle body (1) is located in mounting groove (6), group battery (61) are located in mounting groove (6), and the output of group battery (61) is connected with the input electricity of singlechip (11).
4. A descent stabilizing drone toy according to claim 1, characterised in that: still include electro-magnet (3) and metal block (31), the bottom surface of unmanned aerial vehicle body (1) is located in electro-magnet (3), the surface of clamp plate (23) is located in metal block (31), and metal block (31) correspond with electro-magnet (3), and the input of electro-magnet (3) is connected with the output electricity of singlechip (11).
5. A descent stabilizing drone toy according to claim 1, characterised in that: still include mount pad (4) and range sensor (41), the bottom surface middle part of unmanned aerial vehicle body (1) is located in mount pad (4), range sensor (41) are located on mount pad (4), the output of range sensor (41) is connected with the input electricity of singlechip (11).
6. A descent stabilizing drone toy according to claim 3, characterised in that: still include support (5), solar cell panel (51), kerve (52) and solar control ware (53), the surface of unmanned organism (1) is located in support (5), the both sides of support (5) are located to solar cell panel (51) symmetry, the bottom surface of unmanned organism (1) is located in kerve (52) is located in solar control ware (53), and the output of solar cell panel (51) is connected with the input electricity of solar control ware (53), and the output of solar control ware (53) is connected with the input electricity of group battery (61).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121171978.6U CN215025976U (en) | 2021-05-28 | 2021-05-28 | Stably-descending unmanned aerial vehicle toy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121171978.6U CN215025976U (en) | 2021-05-28 | 2021-05-28 | Stably-descending unmanned aerial vehicle toy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215025976U true CN215025976U (en) | 2021-12-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121171978.6U Active CN215025976U (en) | 2021-05-28 | 2021-05-28 | Stably-descending unmanned aerial vehicle toy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215025976U (en) |
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2021
- 2021-05-28 CN CN202121171978.6U patent/CN215025976U/en active Active
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