Energy storage type airplane ground power supply vehicle

Abstract

The utility model discloses a kind of energy storage type airplane ground power supply vehicles, and it is related to energy storage type airplane ground power supply vehicle technical field, including bottom plate, the upper end surface of bottom plate is fixedly connected with battery box, the side surface of battery box is fixedly connected with trailer hook, the lower end surface of battery box is fixedly connected with mounting bracket one, the end surface of mounting bracket one is provided with the slot of penetration, the groove wall of slot is rotatably connected with rotating rod one, the end surface of rotating rod one is fixedly connected with gyro wheel, the upper side of gyro wheel is also provided with mudguard, the end surface of mudguard is fixedly connected with the side surface of bottom plate, the upper end surface of battery box is fixedly connected with fixed rod one, the upper end surface of fixed rod one is fixedly connected with fixed block one, the surface of fixed block one is hinged with curved rod one, the surface of curved rod one is rotatably connected with rotating sleeve one, it can be quickly radiated while shading under the sun, and when not using, fold up triangle board one and triangle board two, simultaneously, the effect that dustproof is prevented by plugging up heat dissipation opening.

Description

Technical Field

[0001] This utility model relates to the technical field of energy storage aircraft ground power vehicles, specifically an energy storage aircraft ground power vehicle. Background Technology

[0002] The energy storage aircraft ground power vehicle is a mobile ground power supply device that integrates energy storage batteries, energy conversion systems and intelligent control systems. It is designed to provide stable power to aircraft while they are on the ground and is known as the aircraft's "mobile power station" or "power bank".

[0003] For example, the mobile power supply vehicle disclosed in announcement number "CN218400793U" includes a power supply vehicle chassis; the power supply vehicle chassis has a rotating shaft rotatably connected to it via bearings, with wheels fixedly connected to both ends of the shaft; a tow bar is provided on the lower right side of the power supply vehicle chassis, with a tow ring at the right end of the tow bar; a power supply vehicle compartment is provided on the upper end of the power supply vehicle chassis, and a battery pack is installed inside the power supply vehicle compartment; wherein: a mounting plate is provided at the front end of the power supply vehicle compartment, and a control switch and a socket are respectively provided at the front end of the mounting plate, with the input ends of the control switch and the socket electrically connected to the output end of the battery pack; connecting columns are evenly arranged on the upper end of the power supply vehicle compartment. This mobile power supply vehicle, while ventilating and cooling the battery pack, can prevent external rainwater from entering the power supply vehicle compartment, allowing the mobile power supply vehicle to maintain good working condition even in rainy weather, making it convenient to use and with a wide range of applications.

[0004] However, the above-mentioned devices still have the following problems in implementation: When used at the airport, the power supply vehicle is rarely used on rainy days. Most of the time, the power supply vehicle is used under the scorching sun. When used under the scorching sun for a long time, the battery will not only generate a lot of heat and become hot, but also absorb a lot of heat under the sun for a long time. The existing power supply vehicles lack sunshade equipment, which can easily cause the equipment to overheat when working under the scorching sun for a long time. Utility Model Content

[0005] The purpose of this invention is to provide an energy storage aircraft ground power vehicle, which solves the technical problems mentioned in the background art.

[0006] To achieve the above objectives, this utility model provides the following technical solution: an energy storage aircraft ground power vehicle, comprising a base plate, a battery box fixedly connected to the upper end face of the base plate, a trailer hook fixedly connected to the side of the battery box, a mounting bracket fixedly connected to the lower end face of the battery box, a through slot opened on the end face of the mounting bracket, a rotating rod rotatably connected to the slot wall, a roller fixedly connected to the end face of the rotating rod, and a mudguard provided above the roller, the end face of the mudguard being fixedly connected to the side face of the base plate.

[0007] Optionally, a fixing rod is fixedly connected to the upper end face of the battery box, a fixing block is fixedly connected to the upper end surface of the fixing rod, a curved rod is hinged to the surface of the fixing block, a rotating sleeve is rotatably connected to the surface of the curved rod, and a triangular plate is fixedly connected to the outer surface of the rotating sleeve.

[0008] Optionally, a rotating sleeve 2 is rotatably connected to the surface of the crank rod 1, and a triangular plate 2 is fixedly connected to the outer surface of the rotating sleeve 2. The end face of the rotating sleeve 2 is rotatably connected to the end face of the rotating sleeve 1.

[0009] Optionally, a rotating sleeve three is fixedly connected to the end face of the triangular plate two away from the rotating sleeve one, and a rotating sleeve four is rotatably connected to the end face of the rotating sleeve three. The surface of the rotating sleeve four is fixedly connected to the end face of the triangular plate one away from the rotating sleeve one, and the rotating sleeve one is located directly above the battery box.

[0010] Optionally, a rotating sleeve five is rotatably connected to the end face of the rotating sleeve three, a rotating rod two is rotatably connected to the inner wall of the rotating sleeve five, the surface of the rotating rod two is also rotatably connected to the inner wall of the rotating sleeve three, and the surface of the rotating rod two is also rotatably connected to the surface of the rotating sleeve four.

[0011] Optionally, a fixing block two is fixedly connected to the surface of the rotating sleeve five, a curved rod two is hinged to the surface of the fixing block two, a fixing block three is hinged to the end of the curved rod two away from the fixing block two, a sliding ring one is fixedly connected to the surface of the fixing block three, and the inner wall of the sliding ring one is slidably connected to the surface of the fixing rod one.

[0012] Optionally, a placement block is fixedly connected to the lower end surface of the sliding ring, and an electric push rod is fixedly connected to the lower end surface of the placement block. The lower end surface of the electric push rod is fixedly connected to the upper end surface of the battery box.

[0013] Optionally, a fixing block four is fixedly connected to the lower end surface of the sliding ring one. A crank three is hinged to the surface of the fixing block four. A baffle one is hinged to the end of the crank three away from the fixing block four. A sliding column one is fixedly connected to the end of the baffle one away from the crank three. A sliding frame one is slidably connected to the surface of the sliding column one. The outer surface of the sliding frame one is fixedly connected to the upper end surface of the battery box. A through slot is opened on the upper end surface of the battery box. A fan is fixedly connected to the wall of the through slot.

[0014] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0015] I. This utility model reduces the heat accumulated by the battery in the battery box during operation and under prolonged exposure to the sun by placing four triangular plates (first and second) horizontally to form a sunshade, thereby reducing the probability of the battery in the battery box burning out due to high temperature.

[0016] Second, this utility model uses the rotating sleeve five connected by the fixed block two to drive the rotating rod two to move, which further causes the four sets of triangular plates one and two to close together, reducing the space occupied by the power vehicle when it is not in use, and making it more convenient to store the power vehicle when it is not in use.

[0017] Third, by sliding the sliding column, the fan inside the baffle can be exposed to better dissipate heat from the inside of the battery box. Furthermore, when the power supply vehicle is not in use, the baffle can block the fan, further preventing dust from entering the inner wall of the battery box from the fan and keeping the inside of the battery box clean and tidy. Attached Figure Description

[0018] Figure 1 This is a front view of the structure of this utility model;

[0019] Figure 2 This is a top view of the structure of this utility model;

[0020] Figure 3 In the structure of this utility model Figure 2 Enlarged view of the structure at point A inside;

[0021] Figure 4 In the structure of this utility model Figure 2 Enlarged view of the structure at point B;

[0022] Figure 5 In the structure of this utility model Figure 2 Enlarged view of the structure at point C;

[0023] Figure 6 This is an enlarged view of the mounting bracket's position structure in this utility model;

[0024] Figure 7 In this utility model Figure 6 Enlarged view of the structure at point D;

[0025] Figure 8 This is an enlarged view of one structure of the baffle in this utility model.

[0026] In the diagram: 1. Battery box; 2. Tow hook; 3. Base plate; 4. Rotating rod one; 5. Mudguard; 6. Roller; 7. Triangle plate two; 8. Triangle plate one; 9. Fixing block one; 10. Curved rod one; 11. Fixing rod one; 12. Rotating sleeve one; 13. Rotating sleeve two; 14. Rotating sleeve four; 15. Rotating sleeve three; 16. Rotating sleeve five; 17. Rotating rod two; 18. Electric push rod; 19. Mounting bracket one; 20. Placement block one; 21. Sliding ring one; 22. Curved rod two; 23. Fixing block two; 24. Fixing block three; 25. Fixing block four; 26. Curved rod three; 27. Baffle one; 28. Sliding frame one; 29. ​​Sliding column one; 30. Fan. Detailed Implementation

[0027] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0028] Example 1:

[0029] Please see Figures 1 to 8 This utility model provides a technical solution: an energy storage aircraft ground power vehicle, including a base plate 3, a battery box 1 fixedly connected to the upper end face of the base plate 3, a trailer hook 2 fixedly connected to the side of the battery box 1, a mounting bracket 19 fixedly connected to the lower end face of the battery box 1, a through slot opened on the end face of the mounting bracket 19, a rotating rod 4 rotatably connected to the slot wall, a roller 6 fixedly connected to the end face of the rotating rod 4, and a mudguard 5 provided above the roller 6, the end face of the mudguard 5 being fixedly connected to the side of the base plate 3.

[0030] More specifically, in this embodiment: during use, the battery in the battery box 1 is charged, and then the battery box 1 is transported to the vicinity of the aircraft by connecting the towing vehicle with the trailer hook 2. Then, the connecting cable on the aircraft is connected to the connector of the battery box 1 to charge the battery. The setting of the rollers 6 and the trailer hook 2 at the bottom of the battery box 1 not only greatly facilitates the movement of this energy vehicle, but also reduces the size of this energy vehicle, making it more compact and space-saving when charging.

[0031] Example 2:

[0032] Based on the above embodiments, in this embodiment: a fixing rod 11 is fixedly connected to the upper end face of the battery box 1, a fixing block 9 is fixedly connected to the upper end surface of the fixing rod 11, a curved rod 10 is hinged to the surface of the fixing block 9, a rotating sleeve 12 is rotatably connected to the surface of the curved rod 10, a triangular plate 8 is fixedly connected to the outer surface of the rotating sleeve 12, a rotating sleeve 2 13 is also rotatably connected to the surface of the curved rod 10, a triangular plate 2 7 is fixedly connected to the outer surface of the rotating sleeve 2 13, the end face of the rotating sleeve 2 13 is rotatably connected to the end face of the rotating sleeve 12, a rotating sleeve 3 15 is also fixedly connected to the end face of the triangular plate 2 7 away from the rotating sleeve 12, a rotating sleeve 4 14 is rotatably connected to the end face of the rotating sleeve 3 15, and the surface of the rotating sleeve 4 14 is fixedly connected to the end face of the triangular plate 8 away from the rotating sleeve 12. The rotating sleeve 12 is located directly above the battery box 1.

[0033] More specifically, in this embodiment: by rotating the crank 10, the four triangular plates 8 and 7 are placed horizontally, thereby forming a sunshade. This reduces the heat accumulated in the battery box 1 when the battery is working and under prolonged exposure to the sun, thus reducing the probability of the battery in the battery box 1 burning out due to high temperature.

[0034] Example 3:

[0035] Based on the above embodiments, in this embodiment: the end face of the rotating sleeve three 15 is rotatably connected to the rotating sleeve five 16, the inner wall of the rotating sleeve five 16 is rotatably connected to the rotating rod two 17, the surface of the rotating rod two 17 is also rotatably connected to the inner wall of the rotating sleeve three 15, the surface of the rotating rod two 17 is also rotatably connected to the surface of the rotating sleeve four 14, the surface of the rotating sleeve five 16 is fixedly connected to the fixing block two 23, the surface of the fixing block two 23 is hinged to the curved rod two 22, the end of the curved rod two 22 away from the fixing block two 23 is hinged to the fixing block three 24, the surface of the fixing block three 24 is fixedly connected to the sliding ring one 21, the inner wall of the sliding ring one 21 is slidably connected to the surface of the fixing rod one 11, the lower end surface of the sliding ring one 21 is fixedly connected to the placement block one 20, the lower end surface of the placement block one 20 is fixedly connected to the electric push rod 18, and the lower end surface of the electric push rod 18 is fixedly connected to the upper end surface of the battery box 1.

[0036] More specifically, in this embodiment: the electric push rod 18 drives the placement block 20 to move, and the movement of the placement block 20 simultaneously drives the sliding ring 21 to slide on the fixed rod 11, thereby driving the crank rod 22 to move. The rotating sleeve 5 16 connected to the fixed block 23 drives the rotating rod 2 17 to move, further causing the four sets of triangular plates 8 and 7 to close together, reducing the space occupied by the power vehicle when not in use, making it more convenient to store the power vehicle when not in use.

[0037] Example 4:

[0038] Based on the above embodiments, in this embodiment: a fixing block 25 is fixedly connected to the lower end surface of the sliding ring 21, a crank rod 26 is hinged to the surface of the fixing block 25, a baffle 27 is hinged to the end of the crank rod 26 away from the fixing block 25, a sliding column 29 is fixedly connected to the end of the baffle 27 away from the crank rod 26, a sliding frame 28 is slidably connected to the surface of the sliding column 29, the outer surface of the sliding frame 28 is fixedly connected to the upper end surface of the battery box 1, a through groove is opened on the upper end surface of the battery box 1, and a fan 30 is fixedly connected to the groove wall.

[0039] More specifically, in this embodiment: the movement of sliding ring 21 simultaneously drives the movement of fixed block 25, and the movement of fixed block 25 simultaneously drives crank rod 26, thereby causing baffle 27 to drive sliding column 29 to slide within sliding frame 28. Through the sliding of sliding column 29, fan 30 inside baffle 27 can be exposed to better dissipate heat from the inside of battery box 1. Furthermore, when the power supply vehicle is not in use, baffle 27 blocks fan 30, which can further prevent dust from entering the inner wall of battery box 1 from fan 30, keeping the inside of battery box 1 clean and tidy.

[0040] Working principle: When using this type of energy storage aircraft ground power vehicle, the following steps are performed:

[0041] In use, the battery in battery box 1 is charged, and then the battery box 1 is transported to the vicinity of the aircraft by connecting the tow hook 2 to the tractor. The connecting cable from the aircraft is then connected to the connector of battery box 1 to charge the battery. The rollers 6 and tow hook 2 located at the bottom of battery box 1 greatly facilitate the movement of this energy vehicle and reduce its size. The electric push rod 18 moves the placement block 20, and the movement of placement block 20 simultaneously... Sliding ring 21 slides on fixed rod 11, thereby driving crank rod 22 to move. Rotating sleeve 5 16 connected by fixed block 23 drives rotating rod 2 17 to move, further causing the four sets of triangular plates 1 8 and 2 triangular plates 7 to close, reducing the space occupied by the power cart when not in use. The movement of sliding ring 21 also drives fixed block 4 25 to move, and the movement of fixed block 4 25 simultaneously drives crank rod 3 26 to move, thereby causing baffle 27 to drive sliding column 29 to slide within sliding frame 28. The sliding of sliding column 29 allows fan 30 inside baffle 27 to be exposed, so as to better dissipate heat from the inside of battery box 1. When the power cart is not in use, baffle 27 blocks fan 30, which can further prevent dust from entering the inner wall of battery box 1 from fan 30, keeping the inside of battery box 1 clean and tidy.

[0042] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. An energy storage type aircraft ground power vehicle, comprising a base plate (3), characterized in that: A battery box (1) is fixedly connected to the upper end face of the base plate (3). A trailer hook (2) is fixedly connected to the side of the battery box (1). A mounting bracket (19) is fixedly connected to the lower end face of the battery box (1). A through slot is opened on the end face of the mounting bracket (19). A rotating rod (4) is rotatably connected to the wall of the slot. A roller (6) is fixedly connected to the end face of the rotating rod (4). A mudguard (5) is also provided above the roller (6). The end face of the mudguard (5) is fixedly connected to the side face of the base plate (3).

2. The energy storage aircraft ground power vehicle according to claim 1, characterized in that: The upper end face of the battery box (1) is fixedly connected to a fixing rod (11), the upper end surface of the fixing rod (11) is fixedly connected to a fixing block (9), the surface of the fixing block (9) is hinged to a crank rod (10), the surface of the crank rod (10) is rotatably connected to a rotating sleeve (12), and the outer surface of the rotating sleeve (12) is fixedly connected to a triangular plate (8).

3. The energy storage aircraft ground power vehicle according to claim 2, characterized in that: The surface of the crank rod (10) is also rotatably connected to the rotating sleeve (13), and the outer surface of the rotating sleeve (13) is fixedly connected to the triangular plate (7). The end face of the rotating sleeve (13) is rotatably connected to the end face of the rotating sleeve (12).

4. The energy storage type aircraft ground power vehicle according to claim 3, characterized in that: The end face of the second triangular plate (7) away from the first rotating sleeve (12) is also fixedly connected to the third rotating sleeve (15). The end face of the third rotating sleeve (15) is rotatably connected to the fourth rotating sleeve (14). The surface of the fourth rotating sleeve (14) is fixedly connected to the end face of the first triangular plate (8) away from the first rotating sleeve (12). The first rotating sleeve (12) is located directly above the battery box (1).

5. The energy storage type aircraft ground power vehicle according to claim 4, characterized in that: Rotating sleeve three (15) is rotatably connected to rotating sleeve five (16) at its end face. Rotating rod two (17) is rotatably connected to the inner wall of rotating sleeve five (16). The surface of rotating rod two (17) is also rotatably connected to the inner wall of rotating sleeve three (15). The surface of rotating rod two (17) is also rotatably connected to the surface of rotating sleeve four (14).

6. The energy storage type aircraft ground power vehicle according to claim 5, characterized in that: The rotating sleeve five (16) is fixedly connected to a fixing block two (23), the surface of the fixing block two (23) is hinged to a crank rod two (22), the end of the crank rod two (22) away from the fixing block two (23) is hinged to a fixing block three (24), the surface of the fixing block three (24) is fixedly connected to a sliding ring one (21), and the inner wall of the sliding ring one (21) is slidably connected to the surface of the fixing rod one (11).

7. The energy storage aircraft ground power vehicle according to claim 6, characterized in that: The lower end surface of the sliding ring (21) is fixedly connected to the placement block (20), and the lower end surface of the placement block (20) is fixedly connected to the electric push rod (18). The lower end surface of the electric push rod (18) is fixedly connected to the upper end surface of the battery box (1).

8. The energy storage aircraft ground power vehicle according to claim 7, characterized in that: The lower end surface of the sliding ring (21) is also fixedly connected to a fixing block (25). The surface of the fixing block (25) is hinged to a crank rod (26). The end of the crank rod (26) away from the fixing block (25) is hinged to a baffle (27). The end of the baffle (27) away from the crank rod (26) is fixedly connected to a sliding column (29). The surface of the sliding column (29) is slidably connected to a sliding frame (28). The outer surface of the sliding frame (28) is fixedly connected to the upper end surface of the battery box (1). The upper end surface of the battery box (1) is provided with a through slot. The wall of the through slot is fixedly connected to a fan (30).

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