CN205266112U - Electrodynamic type aircraft tractor heat abstractor for power - Google Patents
Electrodynamic type aircraft tractor heat abstractor for power Download PDFInfo
- Publication number
- CN205266112U CN205266112U CN201521091284.6U CN201521091284U CN205266112U CN 205266112 U CN205266112 U CN 205266112U CN 201521091284 U CN201521091284 U CN 201521091284U CN 205266112 U CN205266112 U CN 205266112U
- Authority
- CN
- China
- Prior art keywords
- flexible pipe
- supplying air
- air bin
- fixed head
- shaped fixed
- 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.)
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Abstract
The utility model relates to a heat abstractor especially relates to an electrodynamic type aircraft tractor heat abstractor for power. The to -be -solved technical problem of the utility model is to provide an electrodynamic type aircraft tractor heat abstractor for power. In order to solve the technical problem, the utility model provides such electrodynamic type aircraft tractor heat abstractor for power which comprises there is automobile body, fan, spiral pipe, water tank, water pump, cooler, hose I, hose II, hose III, left L shape fixed plate, the right L fixed plate that appears and advance air chamber, the inside of automobile body is equipped with the water tank, and the water tank is connected with the hose I that sets up in its below, hose I is connected with the cooler of setting in its below. The utility model overcomes current battery operated aircraft tractor power often carries out the charge -discharge operation, produces a large amount of heats, if the shortcoming of huge injury can be caused to the power to untimely the processing.
Description
Technical field
The utility model relates to a kind of heat abstractor, relates in particular to a kind of electrodynamic type aircraft tractor power supply heat abstractor.
Background technology
In numerous aircraft tractors, the advantage that electric airplane tractor has according to himself, is more and more attracted attention, and the especially electronic focus of paying close attention to especially without bar tractor has electronicly been successfully used to draw middle-size and small-size aircraft abroad without bar tractor. According to the relation of tractor operating personnel and tractor, electronicly can be divided into two kinds of forms, i.e. riding type and legged without bar tractor. Generally speaking, riding type car body is large, speed is higher, for drawing the relatively large aircraft of quality; And legged majority is used for drawing the aircraft that quality is relatively little, its job area is also less. Can be divided into again contact and contactless two kinds according to legged non-rod aircraft tractor operating personnel's mode of operation, the implication of contact is that operator directly contacts with tractor, manipulates tractor by devices such as the handles on operation tractor; The latter is by wired or wireless remote operation tractor.
Existing electrodynamic type aircraft tractor power supply is core component, often discharge and recharge operation, produce a large amount of heats, if processed not in time, can cause huge injury to power supply, therefore needing research and development one badly can dispel the heat by accessory power supply, prevents that power supply is overheated and is damaged, and extends the power supply electrodynamic type aircraft tractor power supply heat abstractor in service life.
Utility model content
(1) technical problem that will solve
The utility model often discharges and recharges operation in order to overcome existing electrodynamic type aircraft tractor power supply, produce a large amount of heats, if processed not in time, the shortcoming that can cause to power supply huge injury, the technical problems to be solved in the utility model is to provide a kind of electrodynamic type aircraft tractor power supply heat abstractor.
(2) technical scheme
In order to solve the problems of the technologies described above, the utility model provides so a kind of electrodynamic type aircraft tractor power supply heat abstractor, includes car body, blower fan, helix tube, water tank, water pump, cooler, flexible pipe I, flexible pipe II, flexible pipe III, left L shaped fixed head, right L shaped fixed head and supplying air bin; The inside of car body is provided with water tank, and water tank is connected with the flexible pipe I arranging thereunder; Flexible pipe I is connected with the cooler arranging thereunder, and cooler is arranged on car body; Cooler is connected with the flexible pipe II that is arranged on its left side, and flexible pipe II is provided with water pump, and the left side of water pump is provided with supplying air bin; On the right wall of supplying air bin, arrange porosely, the hole arranging on the right wall of flexible pipe II by supplying air bin extend into the inside of supplying air bin; The right wall top of supplying air bin is provided with right L shaped fixed head, is provided with helix tube in supplying air bin, and the below of helix tube is provided with blower fan, and blower fan is connected with You Bi with the Zuo Bi of supplying air bin; The left wall of supplying air bin is provided with hole, the left side of supplying air bin is provided with flexible pipe III, the hole arranging on the left wall of flexible pipe III by supplying air bin extend into the inside of supplying air bin, the left wall top of supplying air bin is provided with left L shaped fixed head, the two ends, left and right of helix tube are connected with flexible pipe II with flexible pipe III respectively, and flexible pipe III is connected with water tank.
Preferably, also include controller and temperature sensor, controller is arranged on the right side wall of right L shaped fixed head, and temperature sensor is located at the top of right L shaped fixed head, and temperature sensor is connected with right L shaped fixed head; Blower fan, water pump, cooler and temperature sensor are all connected with controller respectively.
Operation principle: first battery is placed on left L shaped fixed head and right L shaped fixed head, left L shaped fixed head and right L shaped fixed head are symmetrical expression setting, are provided with certain gap, for the circulation of upper downstream between the L shaped fixed head in a left side and right L shaped fixed head. In the time of a large amount of heat of battery operated generation, start water pump, water is extracted out from water tank, water flow to cooler from flexible pipe I, cooler is by water cooling, flow through successively flexible pipe II, helix tube and flexible pipe III of cooled water, finally gets back in water tank subsequently, so circulation, battery is carried out to water cooling processing, start blower fan, blower fan carries out wind-cooling heat dissipating processing to battery simultaneously, reduces the temperature of battery with this.
Because also include controller and temperature sensor, so temperature sensor can detect the temperature of battery continuously, and the temperature information of detection is fed back to controller, in the time that the temperature value of temperature sensor detection reaches preset temperature value, controller control blower fan, water pump, cooler start, and start the battery processing of lowering the temperature.
(3) beneficial effect
The utility model has overcome existing electrodynamic type aircraft tractor power supply and has has often discharged and recharged operation, produces a large amount of heats, if processed not in time, can cause to power supply the shortcoming of huge injury, the utility model has reached and can dispel the heat by accessory power supply, prevents that power supply is overheated and is damaged, and extends the power supply effect in service life, adopt the air-cooled mode combining with water-cooled, improve greatly radiating efficiency, good heat dissipation effect, simple in structure, easy to use, be easy to maintenance and repair.
Brief description of the drawings
Fig. 1 is front view structural representation of the present utility model.
Fig. 2 is front view structural representation of the present utility model.
Being labeled as in accompanying drawing: 1-car body, 2-battery, 3-blower fan, 4-helix tube, 5-water tank, 6-water pump, 7-cooler, 8-flexible pipe I, 9-flexible pipe II, 10-flexible pipe III, the left L shaped fixed head of 11-, the right L shaped fixed head of 12-, 13-supplying air bin, 14-controller, 15-temperature sensor.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further described.
Embodiment 1
A kind of electrodynamic type aircraft tractor power supply heat abstractor, as shown in Figure 1-2, include car body 1, blower fan 3, helix tube 4, water tank 5, water pump 6, cooler 7, flexible pipe I 8, flexible pipe II 9, flexible pipe III 10, left L shaped fixed head 11, right L shaped fixed head 12 and supplying air bin 13; The inside of car body 1 is provided with water tank 5, and water tank 5 is connected with the flexible pipe I 8 arranging thereunder; Flexible pipe I 8 is connected with the cooler 7 arranging thereunder, and cooler 7 is arranged on car body 1; Cooler 7 is connected with the flexible pipe II 9 that is arranged on its left side, and flexible pipe II 9 is provided with water pump 6, and the left side of water pump 6 is provided with supplying air bin 13; On the right wall of supplying air bin 13, arrange porosely, the hole arranging on the right wall of flexible pipe II 9 by supplying air bin 13 extend into the inside of supplying air bin 13; The right wall top of supplying air bin 13 is provided with right L shaped fixed head 12, is provided with helix tube 4 in supplying air bin 13, and the below of helix tube 4 is provided with blower fan 3, and blower fan 3 is connected with You Bi with the Zuo Bi of supplying air bin 13; The left wall of supplying air bin 13 is provided with hole, the left side of supplying air bin 13 is provided with flexible pipe III 10, the hole arranging on the left wall of flexible pipe III 10 by supplying air bin 13 extend into the inside of supplying air bin 13, the left wall top of supplying air bin 13 is provided with left L shaped fixed head 11, the two ends, left and right of helix tube 4 are connected with flexible pipe II 9 with flexible pipe III 10 respectively, and flexible pipe III 10 is connected with water tank 5.
Also include controller 14 and temperature sensor 15, controller 14 is arranged on the right side wall of right L shaped fixed head 12, and temperature sensor 15 is located at the top of right L shaped fixed head 12, and temperature sensor 15 is connected with right L shaped fixed head 12; Blower fan 3, water pump 6, cooler 7 and temperature sensor 15 are all connected with controller 14 respectively.
Operation principle: first battery 2 is placed on left L shaped fixed head 11 and right L shaped fixed head 12, left L shaped fixed head 11 is symmetrical expression setting with right L shaped fixed head 12, between the L shaped fixed head 11 in a left side and right L shaped fixed head 12, be provided with certain gap, for the circulation of upper downstream. In the time that battery 2 work produce a large amount of heats, start water pump 6, water is extracted out from water tank 5, water flow to cooler 7 from flexible pipe I 8, cooler 7 is by water cooling, flow through successively flexible pipe II 9, helix tube 4 and flexible pipe III 10 of cooled water, finally gets back in water tank 5 subsequently, so circulation, battery 2 is carried out to water cooling processing, start blower fan 3, blower fan 3 carries out wind-cooling heat dissipating processing to battery 2 simultaneously, reduces the temperature of battery 2 with this.
Because also include controller 14 and temperature sensor 15, so temperature sensor 15 can detect the temperature of battery 2 continuously, and the temperature information of detection is fed back to controller 14, when the temperature value detecting when temperature sensor 15 reaches preset temperature value, controller 14 is controlled blower fan 3, water pump 6, cooler 7 and is started, and starts battery 2 processing of lowering the temperature.
The above embodiment has only expressed preferred embodiment of the present utility model, and it describes comparatively concrete and detailed, but can not therefore be interpreted as the restriction to the utility model the scope of the claims. It should be pointed out that for the person of ordinary skill of the art, without departing from the inventive concept of the premise, can also make some distortion, improvement and substitute, these all belong to protection domain of the present utility model. Therefore, the protection domain of the utility model patent should be as the criterion with claims.
Claims (2)
1. an electrodynamic type aircraft tractor power supply heat abstractor, it is characterized in that, include car body (1), blower fan (3), helix tube (4), water tank (5), water pump (6), cooler (7), flexible pipe I (8), flexible pipe II (9), flexible pipe III (10), left L shaped fixed head (11), right L shaped fixed head (12) and supplying air bin (13); The inside of car body (1) is provided with water tank (5), and water tank (5) is connected with the flexible pipe I (8) arranging thereunder; Flexible pipe I (8) is connected with the cooler (7) arranging thereunder, and cooler (7) is arranged on car body (1); Cooler (7) is connected with the flexible pipe II (9) that is arranged on its left side, and flexible pipe II (9) is provided with water pump (6), and the left side of water pump (6) is provided with supplying air bin (13); On the right wall of supplying air bin (13), arrange porosely, the hole arranging on the right wall of flexible pipe II (9) by supplying air bin (13) extend into the inside of supplying air bin (13); The right wall top of supplying air bin (13) is provided with right L shaped fixed head (12), is provided with helix tube (4) in supplying air bin (13), and the below of helix tube (4) is provided with blower fan (3), and blower fan (3) is connected with You Bi with the Zuo Bi of supplying air bin (13); The left wall of supplying air bin (13) is provided with hole, the left side of supplying air bin (13) is provided with flexible pipe III (10), the hole arranging on the left wall of flexible pipe III (10) by supplying air bin (13) extend into the inside of supplying air bin (13), the left wall top of supplying air bin (13) is provided with left L shaped fixed head (11), the two ends, left and right of helix tube (4) are connected with flexible pipe II (9) with flexible pipe III (10) respectively, and flexible pipe III (10) is connected with water tank (5).
2. a kind of electrodynamic type aircraft tractor power supply heat abstractor according to claim 1, it is characterized in that, also include controller (14) and temperature sensor (15), controller (14) is arranged on the right side wall of right L shaped fixed head (12), temperature sensor (15) is located at the top of right L shaped fixed head (12), and temperature sensor (15) is connected with right L shaped fixed head (12); Blower fan (3), water pump (6), cooler (7) and temperature sensor (15) are all connected with controller (14) respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521091284.6U CN205266112U (en) | 2015-12-25 | 2015-12-25 | Electrodynamic type aircraft tractor heat abstractor for power |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521091284.6U CN205266112U (en) | 2015-12-25 | 2015-12-25 | Electrodynamic type aircraft tractor heat abstractor for power |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205266112U true CN205266112U (en) | 2016-05-25 |
Family
ID=56007608
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521091284.6U Expired - Fee Related CN205266112U (en) | 2015-12-25 | 2015-12-25 | Electrodynamic type aircraft tractor heat abstractor for power |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205266112U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106095020A (en) * | 2016-05-27 | 2016-11-09 | 国网山东省电力公司定陶县供电公司 | Power system calculation machine cooling system |
-
2015
- 2015-12-25 CN CN201521091284.6U patent/CN205266112U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106095020A (en) * | 2016-05-27 | 2016-11-09 | 国网山东省电力公司定陶县供电公司 | Power system calculation machine cooling system |
| CN106095020B (en) * | 2016-05-27 | 2019-07-26 | 国网山东省电力公司定陶县供电公司 | Power system calculation machine cooling system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20160525 Termination date: 20161225 |