CN211336431U - Installation device is transferred to fire control unmanned aerial vehicle electricity - Google Patents
Installation device is transferred to fire control unmanned aerial vehicle electricity Download PDFInfo
- Publication number
- CN211336431U CN211336431U CN201921732767.8U CN201921732767U CN211336431U CN 211336431 U CN211336431 U CN 211336431U CN 201921732767 U CN201921732767 U CN 201921732767U CN 211336431 U CN211336431 U CN 211336431U
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- electricity
- transferred
- drive arrangement
- aerial vehicle
- unmanned aerial
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- Expired - Fee Related
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Abstract
The utility model discloses a fire control unmanned aerial vehicle electricity transfers installation device, including drive arrangement, rotatory fixing device and wing, rotatory fixing device is rotatable to be located on the drive arrangement, the wing is located on the rotatory fixing device, drive arrangement includes drive arrangement storehouse, motor protective layer, motor, the stable piece of cross, coolant liquid storehouse, electricity and electricity are transferred and are transferred the cooling layer, drive arrangement storehouse diapire is located in the coolant liquid storehouse, the coolant liquid storehouse upper wall is located to the motor protective layer, the motor is located in the motor protective layer, electricity is transferred the cooling layer and is located and run through drive arrangement storehouse upper wall and be close to the motor protective layer, electricity is transferred and is located in the electricity and is transferred the cooling layer, the stable piece of cross is located drive arrangement storehouse upper wall. The utility model belongs to unmanned aerial vehicle accessory field specifically indicates a ensure that quick radiating fire control unmanned aerial vehicle electricity is transferred to unmanned aerial vehicle electricity and is installed device through coolant liquid circulative cooling.
Description
Technical Field
The utility model belongs to unmanned aerial vehicle accessory field specifically indicates a fire control unmanned aerial vehicle electricity is transferred installation device.
Background
With the progress of the times, unmanned planes have entered the visual field of people and become more and more popular. Its usage is extensive, can be used for taking photo by plane, fixed point monitoring, activities such as cruise, unmanned aerial vehicle generally drives the screw by a plurality of motors and provides power, in case wherein certain motor or power have taken place the problem, must lead to the fact the machine of exploding, cause the loss of irrecoverable, the installation electricity is transferred in the current unmanned aerial vehicle motor cabinet and is gone on through following mode, at first give the electricity with motor cabinet bottom fretwork and transfer the heat dissipation, then electricity is transferred and is arranged in the motor cabinet inside and tie up with the ribbon and be used for fixing, this mode has a great deal of defect, except that in addition motor and electricity can produce a large amount of heats in the work, the mode of bottom fretwork can.
SUMMERY OF THE UTILITY MODEL
In order to solve the difficult problem, the utility model provides a but ensure that the quick radiating fire control unmanned aerial vehicle electricity of unmanned aerial vehicle electricity is transferred installation device through cooling liquid cooling.
In order to realize the above functions, the utility model discloses the technical scheme who takes as follows: the utility model provides a fire control unmanned aerial vehicle electricity transfers installation device, includes drive arrangement, rotation fixing device and wing, rotation fixing device is rotatable to be located on the drive arrangement, the wing is located on the rotation fixing device, drive arrangement includes drive arrangement storehouse, motor protective layer, motor, cross stabilizing block, coolant liquid storehouse, electricity is transferred and is transferred the cooling layer with electricity, drive arrangement storehouse diapire is located in the coolant liquid storehouse, the coolant liquid storehouse upper wall is located to the motor protective layer, the motor is located in the motor protective layer, electricity is transferred the cooling layer and is located and run through drive arrangement storehouse upper wall and be close to the motor protective layer, electricity is transferred and is located in the electricity and is transferred the cooling layer, drive arrangement storehouse upper wall is located to the cross stabilizing block.
Further, the rotary fixing device comprises a wing supporting block, a rotary shaft and a rotary shaft sleeve head, the wing supporting block is arranged on the upper wall of the driving device bin, a shaft hole is formed in the wing supporting block, the rotary shaft is rotatably arranged in the shaft hole, one end of the rotary shaft penetrates through the wing supporting block and the cross-shaped stabilizing block and is connected with the output shaft end of the motor, the rotary shaft sleeve head is arranged at the other end of the rotary shaft, the motor rotates to drive the rotary shaft to rotate, the rotary shaft drives the rotary shaft sleeve head to rotate, and the wings are sleeved on the rotary shaft sleeve head.
Further, the cavity of the bin of the driving device is arranged.
Furthermore, the cooling liquid bin is a hollow cavity, and cooling liquid is placed in the cooling liquid bin and is introduced into the electric-tuning cooling layer to cool the electric tuning.
Furthermore, the cross-shaped stabilizing blocks are arranged in a cross-shaped structure.
The utility model adopts the above structure to gain beneficial effect as follows: the utility model provides a pair of installation device is transferred to fire control unmanned aerial vehicle electricity, setting up of electricity is transferred can regulate and control the rotational speed of motor, and the cold district liquid is poured into in cooling liquid storehouse and the electricity transfer cooling layer simultaneously, and electricity is transferred and can be produced a large amount of heats in the course of the work, and electricity is transferred and is located the electricity and transfer the cooling of the interior its inside coolant liquid of cooling layer, can effectively transfer the heat to the electricity, reaches the cooling liquid cooling and ensures that unmanned aerial vehicle electricity transfers quick radiating purpose.
Drawings
Fig. 1 is an exploded view of the installation device for the fire fighting unmanned aerial vehicle electric speed regulator of the utility model;
fig. 2 is the utility model relates to a fire control unmanned aerial vehicle electricity transfers overall structure schematic diagram of installation device.
The device comprises a driving device 1, a rotating fixing device 2, a wing 3, a driving device bin 4, a cross-shaped stabilizing block 5, an electric control device 6, an electric control device 7, an electric control cooling layer 8, a motor protective layer 9, a motor 10, a rotating shaft sleeve head 11, a cooling liquid bin 12, a wing supporting block 13, a shaft hole 14 and a rotating shaft.
Detailed Description
The technical solution of the present invention will be described in further detail with reference to the following embodiments, and the technical features or the connection relations of the present invention, which are not described in detail, are the prior art adopted.
The present invention will be described in further detail with reference to the accompanying drawings.
As shown in fig. 1-2, the utility model relates to a fire control unmanned aerial vehicle electricity transfers installation device, including drive arrangement 1, rotary fixing device 2 and wing 3, rotary fixing device 2 is rotatable to be located on drive arrangement 1, wing 3 is located on rotary fixing device 2, drive arrangement 1 includes drive arrangement storehouse 4, motor protective layer 8, motor 9, cross stabilizing block 5, coolant liquid storehouse 11, electricity are transferred 6 and electricity are transferred cooling layer 7, coolant liquid storehouse 11 is located 4 diapalls in the drive arrangement storehouse, 11 upper walls in coolant liquid storehouse are located to motor protective layer 8, motor 9 is located in motor protective layer 8, electricity is transferred cooling layer 7 and is located and run through drive arrangement storehouse 4 upper wall and be close to motor protective layer 8, electricity is transferred 6 and is located in electricity is transferred cooling layer 7, cross stabilizing block 5 is located drive arrangement storehouse 4 upper wall.
The rotary fixing device 2 comprises a wing supporting block 12, a rotating shaft 14 and a rotating shaft sleeve head 10, wherein the wing supporting block 12 is arranged on the upper wall of the driving device bin 4, a shaft hole 13 is formed in the wing supporting block 12, the rotating shaft 14 is rotatably arranged in the shaft hole 13, one end of the rotating shaft 14 penetrates through the wing supporting block 12 and the cross-shaped stabilizing block 5 to be connected with the output shaft end of the motor 9, the rotating shaft sleeve head 10 is arranged at the other end of the rotating shaft 14, and the wings 3 are sleeved on the rotating shaft sleeve head 10.
And the cavity in the 4 th position of the driving device bin is arranged.
The bottom wall of the driving device bin 4 is a hollow cavity.
The cross-shaped stabilizing blocks 5 are arranged in a cross-shaped structure.
During the specific use, motor 9 is rotatory to be driven axis of rotation 14 and is rotatory, axis of rotation 14 drives 3 rotations of wing, electricity is transferred 6 and is regulated and control the motor 9 rotational speed, can give off a large amount of heats in the 6 course of work of electricity, need in time to transfer 6 to electricity and dispel the heat, coolant liquid storehouse 11 and electricity are transferred and are injected cold space liquid in the cooling layer 7, electricity is transferred 6 a large amount of heats that produce in the course of work, the cooling of the inside coolant liquid of cooling layer 7 is transferred to the electricity, can effectively dispel the heat to electricity 6, it ensures that unmanned aerial vehicle electricity is transferred to the coolant liquid cooling and is.
The present invention and the embodiments thereof have been described above, but the description is not limited thereto, and the embodiment shown in the drawings is only one of the embodiments of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should understand that they should not be limited to the embodiments described above, and that they can design the similar structure and embodiments without departing from the spirit of the invention.
Claims (5)
1. The utility model provides a fire control unmanned aerial vehicle electricity transfers installation device which characterized in that: including drive arrangement, rotary fixing device and wing, rotary fixing device is rotatable to be located on the drive arrangement, the wing is located on the rotary fixing device, drive arrangement includes drive arrangement storehouse, motor protective layer, motor, cross stabilizing block, coolant liquid storehouse, electricity is transferred and is transferred the cooling layer with electricity, drive arrangement storehouse diapire is located in the coolant liquid storehouse, the motor protective layer is located the coolant liquid storehouse upper wall, the motor is located in the motor protective layer, electricity is transferred the cooling layer and is located and run through drive arrangement storehouse upper wall and be close to the motor protective layer, electricity is transferred and is located in the electricity and transfers the cooling layer, drive arrangement storehouse upper wall is located to the cross stabilizing block.
2. The electrically-controlled installation device for the fire-fighting unmanned aerial vehicle as claimed in claim 1, wherein: the rotary fixing device comprises a wing supporting block, a rotary shaft and a rotary shaft sleeve head, wherein the wing supporting block is arranged on the upper wall of the driving device bin, a shaft hole is formed in the wing supporting block, the rotary shaft is rotatably arranged in the shaft hole, one end of the rotary shaft penetrates through the wing supporting block and the cross-shaped stabilizing block and is connected with the output shaft end of the motor, the rotary shaft sleeve head is arranged at the other end of the rotary shaft, and the wings are sleeved on the rotary shaft sleeve head.
3. The electrically-controlled installation device for the fire-fighting unmanned aerial vehicle as claimed in claim 1, wherein: the cavity of the bin of the driving device is arranged.
4. The electrically-controlled installation device for the fire-fighting unmanned aerial vehicle as claimed in claim 1, wherein: the bottom wall of the driving device bin is a hollow cavity.
5. The electrically-controlled installation device for the fire-fighting unmanned aerial vehicle as claimed in claim 1, wherein: the cross-shaped stabilizing blocks are arranged in a cross-shaped structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921732767.8U CN211336431U (en) | 2019-10-15 | 2019-10-15 | Installation device is transferred to fire control unmanned aerial vehicle electricity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921732767.8U CN211336431U (en) | 2019-10-15 | 2019-10-15 | Installation device is transferred to fire control unmanned aerial vehicle electricity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211336431U true CN211336431U (en) | 2020-08-25 |
Family
ID=72092587
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921732767.8U Expired - Fee Related CN211336431U (en) | 2019-10-15 | 2019-10-15 | Installation device is transferred to fire control unmanned aerial vehicle electricity |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211336431U (en) |
-
2019
- 2019-10-15 CN CN201921732767.8U patent/CN211336431U/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: 20200825 Termination date: 20211015 |