CN213649912U - Special motor for unmanned aerial vehicle with group fixed connection mechanism - Google Patents
Special motor for unmanned aerial vehicle with group fixed connection mechanism Download PDFInfo
- Publication number
- CN213649912U CN213649912U CN202022965181.5U CN202022965181U CN213649912U CN 213649912 U CN213649912 U CN 213649912U CN 202022965181 U CN202022965181 U CN 202022965181U CN 213649912 U CN213649912 U CN 213649912U
- Authority
- CN
- China
- Prior art keywords
- wall
- aerial vehicle
- unmanned aerial
- shell
- damping spring
- 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
- 230000007246 mechanism Effects 0.000 title claims abstract description 36
- 230000003139 buffering effect Effects 0.000 claims abstract description 8
- 239000007787 solid Substances 0.000 claims abstract description 8
- 238000013016 damping Methods 0.000 claims description 49
- 238000001816 cooling Methods 0.000 claims description 20
- 230000017525 heat dissipation Effects 0.000 claims description 14
- 230000000694 effects Effects 0.000 claims description 7
- 230000005855 radiation Effects 0.000 abstract 1
- 239000000428 dust Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a special motor for unmanned aerial vehicle with group fixed connection mechanism, including motor body, casing and wind channel, still including the damper who is used for buffering the vibration, to group erection joint's fixed establishment and increase of service life's heat radiation structure, motor body is installed to the inboard of casing, motor body's output is installed the flight leaf through the drive shaft. The utility model discloses a pass the connecting block to many connecting wires to on placing into the solid fixed splint in the connecting block, make the gear rotate through rotating the knob, the meshing of tooth piece makes the rack downstream, makes the bottom plate drive a plurality of solid fixed splint downstream simultaneously and presss from both sides tightly the connecting wire, is convenient for carry out fixed mounting to the connecting wire.
Description
Technical Field
The utility model relates to a motor technical field for the unmanned aerial vehicle specifically is a special motor for unmanned aerial vehicle with group fixed connection mechanism.
Background
Along with the transformation upgrading of china's economy, the hand labor cost is constantly promoting, and unmanned aerial vehicle realizes that cost reduction increases and promotes the profit, and logistics distribution originates the unmanned aerial vehicle in the military field at the earliest, and unmanned aerial vehicle logistics distribution becomes a popular big trend now, and the special motor that uses on the unmanned aerial vehicle drives the flight, but current motor radiating effect is relatively poor to the life who makes the motor is very short.
With the continuous installation and use of a special motor for an unmanned aerial vehicle with a wire group fixing and connecting mechanism, the following problems are found in the use process:
1. some current special motors for unmanned aerial vehicle do not have the effect of buffering the shock attenuation to the vibration that motor work produced at the in-process of daily use to lead to unmanned aerial vehicle flight unstability.
2. And the special motor for the unmanned aerial vehicle does not have a mechanism for fixedly connecting the wire group in the using process, so that the wire group cannot be arranged and installed.
3. And the special motor for the unmanned aerial vehicle does not have a structure for radiating and dedusting the motor in the use process, thereby shortening the service life of the motor.
Therefore, a special motor for an unmanned aerial vehicle having a wire group fixing and connecting mechanism needs to be designed to solve the above problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a special motor for unmanned aerial vehicle with group fixed connection mechanism to it does not have the shock attenuation, to group fixed connection and the problem that the heat dissipation was removed dust to propose the current special motor for unmanned aerial vehicle with group fixed connection mechanism in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a special motor with a wire group fixing and connecting mechanism for an unmanned aerial vehicle comprises a motor body, a shell, an air duct, a damping mechanism for buffering vibration, a fixing mechanism for installing and connecting a wire group and a heat dissipation structure for prolonging the service life;
the inner side of the shell is provided with a motor body, the output end of the motor body is provided with a flight blade through a driving shaft, the top end of the shell is provided with a cover body, and the damping mechanism is arranged at the bottom end of the motor body;
the outer wall of one end of the shell is uniformly provided with air outlet holes, the outer wall of the shell below the air outlet holes is provided with a controller, the bottom end of the motor body is connected with a connecting wire, and the fixing mechanism is arranged on the outer wall of one side of the shell;
the heat dissipation structure is arranged on the inner wall of one side of the shell.
Preferably, damper includes hinge bar, first damping spring, mounting panel, horizontal pole and second damping spring, the horizontal pole is installed on the inside top of casing, first damping spring is installed to the outer wall of horizontal pole, the top at first damping spring both ends all is connected with the hinge bar, and the top activity hinge of hinge bar has the mounting panel, second damping spring is all installed to the both sides of mounting panel bottom.
Preferably, fixed establishment includes solid fixed splint, movable clamp plate, connecting block, rack, knob, gear, roof and bottom plate, the connecting block is installed in one side outer wall of casing, the roof is installed on the top of connecting block, and the inboard of roof installs the rack, the top of rack is connected with the bottom plate, and the bottom of bottom plate evenly installs movable clamp plate, solid fixed splint are all installed to the inner wall of movable clamp plate below connecting block, the gear is installed to the one end of roof, and one side of gear is connected with the knob.
Preferably, third damping springs are evenly installed on the inner walls of the two sides of the shell, and one ends of the third damping springs are connected with the clamping plate.
Preferably, the heat dissipation structure comprises an air duct, the air duct is mounted on the inner wall of one side of the casing, and the fan is mounted on the outer wall of the casing on one side of the air duct.
Preferably, the inner wall of the air duct is provided with a cooling block, the inner walls of two sides of the cooling block are provided with an electro-hydraulic power micropump, the inner wall of one end of the cooling block is provided with a heat exchanger, and the inner wall of the other end of the cooling block is provided with a refrigerator.
Preferably, one side outer wall of wind channel is connected with the cold air pipe, the inboard of casing below is provided with the cavity, the cold air pipe extends to the inboard of cavity, the outer wall of cold air pipe top evenly is provided with the air outlet.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) the motor body extrudes the clamping plate through the motor body, the clamping plate extrudes the third damping spring to enable the third damping spring to deform, the motor body is buffered and damped, the mounting plate is moved downwards through pressure, the hinge rod extrudes the first damping spring, and the first damping spring and the second damping spring are extruded and deformed, so that the buffering and damping effects are realized, and the flying jitter of the unmanned aerial vehicle is avoided;
(2) the cooling block forms a square block with lower temperature through the work of the electro-hydraulic power micropump, then the air enters the connecting wire to work for air inlet, the air enters the air channel to form cold air, then enters the cold air pipe, is blown out upwards through a plurality of air outlets for heat dissipation, removes dust on the motor body, and is discharged through the air outlet;
(3) through installing connecting wire, knob, movable clamp plate, gear, rack, bottom plate, solid fixed clamp plate and connecting block, through passing many connecting wires the connecting block to on placing the solid fixed clamp plate in the connecting block, make the gear rotate through rotating the knob, the meshing of tooth piece makes the rack downstream, makes the bottom plate drive a plurality of movable clamp plate downstream simultaneously and presss from both sides tightly the connecting wire, is convenient for carry out fixed mounting to the connecting wire.
Drawings
FIG. 1 is a schematic cross-sectional view of the device of the present invention;
FIG. 2 is a schematic view of the front view structure of the device of the present invention;
FIG. 3 is a schematic side sectional view of the fixing mechanism of the present invention;
fig. 4 is a schematic view of the heat dissipation structure of the present invention.
In the figure: 1. a damping mechanism; 101. a hinged lever; 102. a first damping spring; 103. mounting a plate; 104. a cross bar; 105. a second damping spring; 2. a connecting wire; 3. a fixing mechanism; 301. fixing the clamping plate; 302. moving the clamping plate; 303. connecting blocks; 304. a rack; 305. a knob; 306. a gear; 307. a top plate; 308. a base plate; 4. a third damping spring; 5. a clamping plate; 6. a flight blade; 7. a motor body; 8. a cover body; 9. a housing; 10. an air outlet; 11. a controller; 12. a fan; 13. an electro-hydraulic power micropump; 14. cooling the block; 15. a heat exchanger; 16. an air duct; 17. an air outlet; 18. a cavity; 19. a cold air pipe; 20. a refrigerator.
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.
Example 1: referring to fig. 1-4, a special motor for an unmanned aerial vehicle with a wire set fixing and connecting mechanism comprises a motor body 7, a housing 9, an air duct 16, a damping mechanism 1 for buffering vibration, a fixing mechanism 3 for installing and connecting a wire set, and a heat dissipation structure for prolonging service life;
a motor body 7 is arranged on the inner side of the shell 9, a flight blade 6 is arranged at the output end of the motor body 7 through a driving shaft, a cover body 8 is arranged at the top end of the shell 9, and the damping mechanism 1 is arranged at the bottom end of the motor body 7;
air outlet holes 10 are uniformly formed in the outer wall of one end of the shell 9, a controller 11 is mounted on the outer wall of the shell 9 below the air outlet holes 10, the type of the controller 11 can be JY-PH160, the bottom end of the motor body 7 is connected with the connecting wire 2, and the fixing mechanism 3 is mounted on the outer wall of one side of the shell 9;
the heat dissipation structure is arranged on the inner wall of one side of the shell 9;
referring to fig. 1-4, a special motor for an unmanned aerial vehicle with a wire set fixing and connecting mechanism further includes a heat dissipation structure, the heat dissipation structure includes an air duct 16, the air duct 16 is installed on an inner wall of one side of the housing 9, a fan 12 is installed on an outer wall of the housing 9 on one side of the air duct 16, and the model of the fan 12 may be YWF 350-4;
a cooling block 14 is arranged on the inner wall of the air duct 16, an electro-hydraulic power micropump 13 is arranged on the inner walls of two sides of the cooling block 14, the type of the electro-hydraulic power micropump 13 can be SB-3-1, a heat exchanger 15 is arranged on the inner wall of one end of the cooling block 14, the type of the heat exchanger 15 can be BIU1100-4.35, a refrigerator 20 is arranged on the inner wall of the other end of the cooling block 14, and the type of the refrigerator 20 can be DTA-40;
the outer wall of one side of the air duct 16 is connected with a cold air pipe 19, the inner side below the shell 9 is provided with a cavity 18, the cold air pipe 19 extends to the inner side of the cavity 18, and the outer wall above the cold air pipe 19 is uniformly provided with air outlets 17;
specifically, as shown in fig. 1, fig. 2 and fig. 4, when the structure is used, through the work of the electro-hydraulic power micropump 13, the water inlet pipe enters the heat exchanger 15 for heat exchange, then enters the refrigerator 20 for rapid cooling, then the cold water in the cooling block 14 circulates, so that the cooling block 14 forms a square block with a lower temperature, the air enters the work through the connecting wire 2, the air enters the air duct 16 for forming cold air, then enters the cold air pipe 19, the air is blown upwards through the air outlets 17 for heat dissipation, and the dust on the motor body 7 is removed, and the dust is discharged through the air outlet 10.
Example 2: the damping mechanism 1 comprises a hinged rod 101, a first damping spring 102, a mounting plate 103, a cross rod 104 and a second damping spring 105, the cross rod 104 is mounted at the top end inside the shell 9, the first damping spring 102 is mounted on the outer wall of the cross rod 104, the hinged rod 101 is connected above the two ends of the first damping spring 102, the mounting plate 103 is movably hinged to the top end of the hinged rod 101, and the second damping spring 105 is mounted on the two sides of the bottom end of the mounting plate 103;
third damping springs 4 are uniformly arranged on the inner walls of the two sides of the shell 9, and one ends of the third damping springs 4 are connected with clamping plates 5;
specifically, as shown in fig. 1, when using this structure, extrude grip block 5 through motor body 7, grip block 5 extrudes third damping spring 4, make third damping spring 4 warp, cushion the shock attenuation to motor body 7, rethread pressure makes mounting panel 103 remove downwards, make hinge rod 101 extrude first damping spring 102, first damping spring 102 and second damping spring 105 are by extrusion deformation, thereby realize buffering absorbing effect, avoid unmanned aerial vehicle flight shake.
Example 3: the fixing mechanism 3 comprises a fixing clamp plate 301, a movable clamp plate 302, a connecting block 303, a rack 304, a knob 305, a gear 306, a top plate 307 and a bottom plate 308, the connecting block 303 is installed on the outer wall of one side of the shell 9, the top end of the connecting block 303 is provided with the top plate 307, the rack 304 is installed on the inner side of the top plate 307, the top end of the rack 304 is connected with the bottom plate 308, the movable clamp plate 302 is evenly installed at the bottom end of the bottom plate 308, the fixing clamp plate 301 is installed on the inner wall of the connecting block 303 below the movable clamp plate 302, the gear 306 is installed at one end of;
specifically, as shown in fig. 1, 2 and 3, when the structure is used, the plurality of connecting wires 2 pass through the connecting block 303 and are placed on the fixing clamp plate 301 in the connecting block 303, the gear 306 is rotated by rotating the knob 305, the gear blocks are meshed, the rack 304 is moved downwards, and the bottom plate 308 drives the plurality of moving clamp plates 302 to move downwards to clamp the connecting wires 2, so that the connecting wires 2 are fixedly mounted conveniently.
The output end of the controller 11 is electrically connected with the input ends of the fan 12, the electro-hydraulic power micropump 13, the heat exchanger 15 and the refrigerator 20 through leads.
The working principle is as follows: when the device is used, firstly, a plurality of connecting wires 2 penetrate through the connecting block 303 and are placed on the fixed clamping plate 301 in the connecting block 303, the gear 306 is rotated by rotating the knob 305, the gear blocks are meshed, the rack 304 is moved downwards, and meanwhile, the bottom plate 308 drives the plurality of movable clamping plates 302 to move downwards to clamp the connecting wires 2, so that the connecting wires 2 are conveniently and fixedly installed;
afterwards, when the motor body 7 works to generate vibration, the clamping plate 5 is extruded through the motor body 7, the clamping plate 5 extrudes the third damping spring 4, the third damping spring 4 is deformed, the motor body 7 is buffered and damped, the mounting plate 103 moves downwards through pressure, the hinge rod 101 extrudes the first damping spring 102, and the first damping spring 102 and the second damping spring 105 are extruded and deformed, so that the effect of buffering and damping is realized, and the flight jitter of the unmanned aerial vehicle is avoided;
finally, through the work of electric hydraulic power micropump 13, the inlet tube is intake and is heat-exchanged in heat exchanger 15, then enter into quick cooling in refrigerator 20, then the cold water circulation in the cooling block 14, make cooling block 14 form the square that a temperature is lower, rethread connecting wire 2 work air inlet, wind enters into and forms cold wind in the wind channel 16, then enter into cold wind pipe 19, upwards blow off through a plurality of air outlets 17 and dispel the heat, and clear away the dust on motor body 7, the dust is discharged through exhaust vent 10.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a special type motor for unmanned aerial vehicle with group fixed connection mechanism, includes motor body (7), casing (9) and wind channel (16), its characterized in that: the wire group fixing device also comprises a damping mechanism (1) for buffering vibration, a fixing mechanism (3) for installing and connecting the wire group and a heat dissipation structure for prolonging the service life;
a motor body (7) is mounted on the inner side of the shell (9), a flight blade (6) is mounted at the output end of the motor body (7) through a driving shaft, a cover body (8) is mounted at the top end of the shell (9), and the damping mechanism (1) is mounted at the bottom end of the motor body (7);
air outlet holes (10) are uniformly formed in the outer wall of one end of the shell (9), a controller (11) is mounted on the outer wall of the shell (9) below the air outlet holes (10), the bottom end of the motor body (7) is connected with the connecting wire (2), and the fixing mechanism (3) is mounted on the outer wall of one side of the shell (9);
the heat dissipation structure is arranged on the inner wall of one side of the shell (9).
2. The special motor for the unmanned aerial vehicle with the cord set fixing and connecting mechanism as claimed in claim 1, wherein: damper (1) is including hinge bar (101), first damping spring (102), mounting panel (103), horizontal pole (104) and second damping spring (105), install on the inside top of casing (9) horizontal pole (104), first damping spring (102) are installed to the outer wall of horizontal pole (104), the top at first damping spring (102) both ends all is connected with hinge bar (101), and the top activity hinge of hinge bar (101) has mounting panel (103), second damping spring (105) are all installed to the both sides of mounting panel (103) bottom.
3. The special motor for the unmanned aerial vehicle with the cord set fixing and connecting mechanism as claimed in claim 1, wherein: fixed establishment (3) are including solid fixed splint (301), remove splint (302), connecting block (303), rack (304), knob (305), gear (306), roof (307) and bottom plate (308), install in one side outer wall of casing (9) connecting block (303), roof (307) are installed on the top of connecting block (303), and rack (304) are installed to the inboard of roof (307), the top of rack (304) is connected with bottom plate (308), and evenly installs solid fixed splint (302) in the bottom of bottom plate (308), gu fixed splint (301) are all installed to the inner wall of moving splint (302) below connecting block (303), gear (306) are installed to the one end of roof (307), and one side of gear (306) is connected with knob (305).
4. The special motor for the unmanned aerial vehicle with the cord set fixing and connecting mechanism as claimed in claim 1, wherein: third damping spring (4) are all evenly installed to the both sides inner wall of casing (9), and the one end of third damping spring (4) all is connected with grip block (5).
5. The special motor for the unmanned aerial vehicle with the cord set fixing and connecting mechanism as claimed in claim 1, wherein: the heat dissipation structure comprises an air duct (16), the air duct (16) is installed on the inner wall of one side of the shell (9), and a fan (12) is installed on the outer wall of the shell (9) on one side of the air duct (16).
6. The special motor for the unmanned aerial vehicle with the cord set fixing and connecting mechanism as claimed in claim 5, wherein: cooling block (14) are installed to the inner wall in wind channel (16), electric hydraulic power micropump (13) are installed to the both sides inner wall of cooling block (14), heat exchanger (15) are installed to the one end inner wall of cooling block (14), refrigerator (20) are installed to the other end inner wall of cooling block (14).
7. The special motor for the unmanned aerial vehicle with the cord set fixing and connecting mechanism as claimed in claim 5, wherein: the utility model discloses a wind tunnel, including casing (9), air duct (16), one side outer wall connection has cold wind pipe (19), the inboard of casing (9) below is provided with cavity (18), cold wind pipe (19) extend to the inboard of cavity (18), the outer wall of cold wind pipe (19) top evenly is provided with air outlet (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022965181.5U CN213649912U (en) | 2020-12-12 | 2020-12-12 | Special motor for unmanned aerial vehicle with group fixed connection mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022965181.5U CN213649912U (en) | 2020-12-12 | 2020-12-12 | Special motor for unmanned aerial vehicle with group fixed connection mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213649912U true CN213649912U (en) | 2021-07-09 |
Family
ID=76689528
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022965181.5U Expired - Fee Related CN213649912U (en) | 2020-12-12 | 2020-12-12 | Special motor for unmanned aerial vehicle with group fixed connection mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213649912U (en) |
-
2020
- 2020-12-12 CN CN202022965181.5U patent/CN213649912U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN213649912U (en) | Special motor for unmanned aerial vehicle with group fixed connection mechanism | |
| CN205543152U (en) | Temperature regulation apparatus for power battery | |
| CN217882749U (en) | Intensive bus duct with heat dissipation effect | |
| CN111692804A (en) | Device for accelerating air flow in mechanical equipment control cabinet to dissipate heat | |
| CN107131044B (en) | A kind of engine constant-temperature cooling system integrated fan | |
| CN214170735U (en) | Wind power generation tower cylinder structure with good heat dissipation effect | |
| CN212727887U (en) | Do benefit to radiating rack of 5G communication equipment | |
| CN211682217U (en) | Combined detachable mechanical arm control box | |
| CN212457700U (en) | A processing oven for combined material antenna house | |
| CN211791120U (en) | New energy automobile motor heat radiation structure | |
| CN212137573U (en) | High-power variable frequency speed regulation device | |
| CN111864576A (en) | Water-cooling and air-cooling integrated heat dissipation type power distribution cabinet for electric power engineering construction | |
| CN212343141U (en) | Inside cooling system of new forms of energy power station | |
| CN213008518U (en) | Electric energy transmission device of electric vehicle power supply | |
| CN201637026U (en) | Modularized constant-temperature air interchanger based on heat pipe heat exchange | |
| CN221197665U (en) | Novel heat radiation structure of heating ventilation air conditioner | |
| CN217823887U (en) | Box-type substation that radiating effect is good | |
| CN216626431U (en) | High-efficient heat abstractor is used to concatenation screen | |
| CN221328388U (en) | Outdoor ring main unit | |
| CN218941659U (en) | Communication cabinet for communication engineering | |
| CN218498623U (en) | Voltage sag and fall protection device | |
| CN212851622U (en) | Water-cooling heat dissipation structure for high-voltage motor rotor variable-frequency speed control system | |
| CN219304606U (en) | New energy motor with shock-absorbing function | |
| CN220382588U (en) | Power distribution device | |
| CN211090378U (en) | Power communication equipment box of mouse is prevented in heat dissipation |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210709 Termination date: 20211212 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |