A mobile power supply suitable for navigation equipment

Abstract

The utility model belongs to the field of navigation equipment, concretely is a kind of mobile power supply suitable for navigation equipment, it includes: power supply body, the front and rear ends of power supply body are all fixedly connected with connecting plate;Supporting component, the supporting component is set in the bottom of connecting plate;Connecting component, the connecting component is set in the bottom of supporting component;The supporting component includes vertical groove in the middle part of power supply body.This utility model is set in the front and rear sides of power supply body by inner thread pipe, when the inserting rod one of inner thread pipe bottom can be inserted on soft ground, when the stable support of power supply body can be carried out;And if ground is hard, support plate can be installed in the bottom of inserting rod one, the stable support of power supply body is carried out by support plate on hard ground, to avoid the risk that power supply body is in strong wind weather and tilts in charging process, to improve the security of charging process.

Description

Technical Field

[0001] This utility model relates to the field of general aviation equipment, specifically a mobile power supply suitable for general aviation equipment. Background Technology

[0002] General aviation equipment refers to aviation activities including drones. As general aviation equipment technology matures and is widely used, the demand for maintenance and upkeep of general aviation equipment is constantly increasing. The maintenance and upkeep industry for general aviation equipment includes tasks such as fuselage structure repair, electronic component repair, battery replacement and charging. Currently, when charging, it can be done by carrying a portable power bank.

[0003] Currently, when charging drones outdoors using portable power banks, if the outdoor environment is windy and the portable power bank is large but not heavy, its wind resistance is poor, which may cause it to tip over, thus affecting charging safety. Therefore, this paper proposes a portable power bank suitable for general aviation equipment to address the above problems. Utility Model Content

[0004] To overcome the shortcomings of existing technologies and avoid the problem of charging safety being affected by the tipping of portable power banks, this utility model proposes a portable power bank suitable for general aviation equipment.

[0005] The technical solution adopted by this utility model to solve its technical problem is: a mobile power supply suitable for general aviation equipment, comprising:

[0006] The power supply body has connecting plates fixedly connected to both its front and rear ends;

[0007] A support assembly is disposed at the bottom of the connecting plate;

[0008] A connecting component, wherein the connecting component is disposed at the bottom of the supporting component;

[0009] The support assembly includes a vertical slot in the middle of the power supply body. A fixing rod is fixedly connected to the top of the vertical slot. An annular groove is formed on the surface of the middle part of the fixing rod. A rotating ring is rotatably connected to the surface of the fixing rod. A screw is threadedly connected to the inside of the rotating ring. An arc-shaped plate is rotatably connected to the surface of the screw near the inside of the rotating ring. An internally threaded tube is fixedly connected to the bottom of the rotating ring. An externally threaded rod is threadedly connected to the inside of the internally threaded tube. A first insertion rod is rotatably connected to the bottom end of the externally threaded rod. Grooves are formed on both the left and right sides of the surface of the first insertion rod. A handle is fixedly connected to the bottom surface of the externally threaded rod.

[0010] Preferably, the internally threaded tube is located between the vertical grooves, and the end of the arc-shaped plate away from the screw is provided with an anti-slip groove. The arc-shaped plate is adapted to contact the inner wall of the annular groove. The rotatable screw drives the arc-shaped plate to be confined inside the annular groove, thereby confining the rotating ring to the surface of the fixed rod, and thus determining the position of the rotating ring after rotation.

[0011] Preferably, the bottom of the externally threaded rod extends below the internally threaded tube, and the bottom of the first insertion rod is conical, so that the bottom of the first insertion rod can be inserted into the ground to support the power supply body.

[0012] Preferably, the connecting assembly includes two insert rods two disposed on the left and right sides of insert rod one. An outer fixing block is fixedly connected to the end of insert rod two away from insert rod one. A sliding sleeve is slidably connected to the surface of insert rod two. A damping block is fixedly connected to the inner wall of the sliding sleeve. A pressure spring is wound around the surface of insert rod two. A support plate is fixedly connected to the bottom of the sliding sleeve.

[0013] Preferably, the two insert rods are respectively inserted into the two grooves, and the diameter of the outer fixing block is larger than the diameter of the insert rods. The outer fixing block can block the pressure spring and the sliding sleeve.

[0014] Preferably, the damping blocks are fixedly connected to the upper and lower sides of the inner wall of the sliding sleeve, and both damping blocks are slidably connected to the surface of the second insertion rod. Through the damping effect of the damping blocks and the second insertion rod, the sliding sleeve is prevented from shaking on the surface of the second insertion rod.

[0015] Preferably, one end of the pressure spring is fixedly connected to the surface of the outer fixing block, and the other end of the pressure spring is fixedly connected to the surface of the sliding sleeve. The elastic force of the pressure spring will pull the outer fixing block and the insert rod into the inside of the groove.

[0016] Preferably, the support plate and the two sliding sleeves are fixedly connected, and the bottom end of the support plate is provided with an anti-slip groove, so that the support plate can be placed on a hard ground to support the power supply body.

[0017] The advantages of this utility model are:

[0018] This invention features internally threaded tubes on both the front and rear sides of the power supply body. The insertion rod at the bottom of the internally threaded tube can be inserted into a soft surface, providing stable support for the power supply body. If the ground is hard, a support plate can be installed at the bottom of the insertion rod. The support plate, placed on a hard surface, provides stable support for the power supply body, thus avoiding the risk of the power supply body tipping over in strong winds during charging and improving the safety of the charging process. Attached Figure Description

[0019] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0020] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0021] Figure 2 This is a schematic diagram of the rear view structure of this utility model;

[0022] Figure 3 This is a schematic diagram of the support component structure of this utility model;

[0023] Figure 4 This is a schematic cross-sectional view of the internally threaded pipe of this utility model.

[0024] Figure 5 For the present utility model Figure 4 Enlarged structural diagram at point A;

[0025] Figure 6 This is a schematic diagram of the connection component of this utility model.

[0026] In the diagram: 1. Power supply body; 2. Connecting plate; 3. Support assembly; 311. Vertical groove; 312. Fixing rod; 313. Annular groove; 314. Rotating ring; 315. Screw; 316. Arc plate; 321. Internally threaded tube; 322. Externally threaded rod; 323. Insert rod one; 324. Groove; 33. Handle; 4. Connecting assembly; 41. Insert rod two; 42. External fixing block; 43. Sliding sleeve; 44. Damping block; 45. Pressure spring; 46. Support plate. 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 scope of protection of the present utility model.

[0028] The following is in conjunction with the appendix Figure 1-6 This application will be described in further detail.

[0029] This application discloses a portable power supply suitable for general aviation equipment. (Refer to...) Figure 1 A portable power supply suitable for general aviation equipment, comprising:

[0030] The power supply body 1 has connecting plates 2 fixedly connected to both the front and rear ends of the power supply body 1.

[0031] Support component 3 is located at the bottom of connecting plate 2;

[0032] Connecting component 4 is located at the bottom of supporting component 3;

[0033] Reference Figures 2-5 The support assembly 3 includes a vertical groove 311 formed in the middle of the power supply body 1. A fixing rod 312 is fixedly connected to the top of the vertical groove 311. An annular groove 313 is formed on the surface of the middle part of the fixing rod 312. A rotating ring 314 is rotatably connected to the surface of the fixing rod 312. A screw 315 is threadedly connected to the inside of the rotating ring 314. An arc-shaped plate 316 is rotatably connected to the surface of the screw 315 near the inside of the rotating ring 314. An internally threaded tube 321 is fixedly connected to the bottom of the rotating ring 314. The internally threaded tube 321 is located between the vertical grooves 311. An anti-slip groove is formed at the end of the arc-shaped plate 316 away from the screw 315. The arc-shaped plate 316 is adapted to contact the inner wall of the annular groove 313 and can rotate. The moving screw 315 drives the arc plate 316 to be confined inside the annular groove 313, thereby confining the rotating ring 314 to the surface of the fixed rod 312, and thus determining the position of the rotating ring 314 after rotation. The internal thread of the internal threaded tube 321 is connected to the external threaded rod 322. The bottom end of the external threaded rod 322 is rotatably connected to the insertion rod 323. The bottom of the external threaded rod 322 extends to the bottom of the internal threaded tube 321. The bottom of the insertion rod 323 is conical, and the bottom of the insertion rod 323 can be inserted into the ground to support the power supply body 1. Grooves 324 are opened on both the left and right sides of the surface of the insertion rod 323. A handle 33 is fixedly connected to the bottom surface of the external threaded rod 322.

[0034] Reference Figure 6The connecting assembly 4 includes two insert rods 41 disposed on the left and right sides of insert rod 323. An outer fixing block 42 is fixedly connected to the end of insert rod 41 away from insert rod 323. A sliding sleeve 43 is slidably connected to the surface of insert rod 41. A damping block 44 is fixedly connected to the inner wall of the sliding sleeve 43. The damping blocks 44 are respectively fixedly connected to the upper and lower sides of the inner wall of the sliding sleeve 43. Both damping blocks 44 are slidably connected to the surface of insert rod 41. Through the damping effect of the damping blocks 44 and insert rod 41, the sliding sleeve 43 is prevented from shaking on the surface of insert rod 41. A pressure spring 45 is wound around the surface of insert rod 41, and one end of the pressure spring 45 is fixedly connected to the outer fixing block 42. The other end of the pressure spring 45 is fixedly connected to the surface of the sliding sleeve 43. The elastic force of the pressure spring 45 will pull the outer fixing block 42 and the second insertion rod 41 into the groove 324. The two second insertion rods 41 are respectively inserted into the two grooves 324. The diameter of the outer fixing block 42 is larger than the diameter of the second insertion rod 41. The outer fixing block 42 can block the pressure spring 45 and the sliding sleeve 43. The bottom of the sliding sleeve 43 is fixedly connected to the support plate 46. The support plate 46 and the two sliding sleeves 43 are fixedly connected. The bottom end of the support plate 46 is provided with an anti-slip groove, so that the support plate 46 can be placed on a hard ground to support the power supply body 1.

[0035] Working principle: After the operator places the power supply unit 1 on a suitable ground, the power supply unit 1 and the drone are connected through the charging cable to charge the drone.

[0036] If the current environment is relatively stable for the power supply body 1, the internal threaded tube 321 can be rotated. The internal threaded tube 321 will drive the fixedly connected rotating ring 314 to rotate on the surface of the fixed rod 312. When the internal threaded tube 321 rotates to a certain angle with the power supply body 1, the handle 33 can be manually rotated. The handle 33 will drive the fixedly connected external threaded rod 322 to rotate. When the external threaded rod 322 rotates, it will move downward inside the internal threaded tube 321. At this time, the insertion rod 323 moves downward and is inserted into the soft ground. Then, the screw 315 is rotated, so that the screw 315 pushes the rotatingly connected arc plate 316 to abut against the inner wall of the annular groove 313, thereby limiting the angle of the rotating ring 314 after rotation, and thus limiting the tilt angle of the internal threaded tube 321. Therefore, the two fixed rods 312 on the left and right can provide stable support for the power supply body 1.

[0037] If the ground is too hard to insert the first plug 323, the two outer fixing blocks 42 can be pulled to move the second plug 41 and stretch the pressure spring 45 away from each other. Then, the two second plugs 41 can be moved to the left and right sides of the first plug 323. At this time, the two outer fixing blocks 42 can be released. The outer fixing blocks 42 will move the second plug 41 under the action of the pressure spring 45 and lock it into the inside of the groove 324. At this time, the sliding sleeve 43 is stably limited to the surface of the second plug 41 by the damping block 44. The two second plugs 41 are stably inserted into the inside of the groove 324. At this time, the support plate 46 can rotate relative to the first plug 323. Then, the operator can place the support plate 46 stably on the hard ground. At this time, the support plate 46 can stably support the power supply body 1.

[0038] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claimed utility model.

Claims

1. A portable power supply suitable for general aviation equipment, characterized in that: include: The power supply body (1) has connecting plates (2) fixedly connected to both the front and rear ends of the power supply body (1). Support component (3), which is disposed at the bottom of the connecting plate (2); A connecting component (4) is disposed at the bottom of the supporting component (3); The support assembly (3) includes a vertical groove (311) in the middle of the power supply body (1). A fixed rod (312) is fixedly connected to the top of the vertical groove (311). An annular groove (313) is opened on the surface of the middle part of the fixed rod (312). A rotating ring (314) is rotatably connected to the surface of the fixed rod (312). A screw (315) is threadedly connected to the inside of the rotating ring (314). An arc plate (316) is rotatably connected to the surface of the screw (315) near the inside of the rotating ring (314). An internally threaded tube (321) is fixedly connected to the bottom of the rotating ring (314). An externally threaded rod (322) is threadedly connected to the inside of the internally threaded tube (321). A first insertion rod (323) is rotatably connected to the bottom end of the externally threaded rod (322). Grooves (324) are opened on both the left and right sides of the surface of the first insertion rod (323). A handle (33) is fixedly connected to the bottom surface of the externally threaded rod (322).

2. A mobile power supply suitable for general aviation equipment according to claim 1, characterized in that: The internally threaded tube (321) is located between the vertical grooves (311), and the arc plate (316) has an anti-slip groove at one end away from the screw (315). The arc plate (316) is adapted to contact the inner wall of the annular groove (313).

3. A mobile power supply suitable for general aviation equipment according to claim 1, characterized in that: The bottom of the externally threaded rod (322) extends below the internally threaded tube (321), and the bottom of the insert rod (323) is conical.

4. A mobile power supply suitable for general aviation equipment according to claim 1, characterized in that: The connecting assembly (4) includes two insert rods (41) arranged on the left and right sides of insert rod one (323). An outer fixing block (42) is fixedly connected to the end of insert rod two (41) away from insert rod one (323). A sliding sleeve (43) is slidably connected to the surface of insert rod two (41). A damping block (44) is fixedly connected to the inner wall of the sliding sleeve (43). A pressure spring (45) is wound around the surface of insert rod two (41). A support plate (46) is fixedly connected to the bottom of the sliding sleeve (43).

5. A mobile power supply suitable for general aviation equipment according to claim 4, characterized in that: The two insertion rods (41) are respectively inserted into the two grooves (324), and the diameter of the outer fixing block (42) is larger than the diameter of the insertion rods (41).

6. A mobile power supply suitable for general aviation equipment according to claim 4, characterized in that: The damping blocks (44) are fixedly connected to the upper and lower sides of the inner wall of the sliding sleeve (43), and both damping blocks (44) are slidably connected to the surface of the second insert (41).

7. A mobile power supply suitable for general aviation equipment according to claim 4, characterized in that: One end of the pressure spring (45) is fixedly connected to the surface of the outer fixing block (42), and the other end of the pressure spring (45) is fixedly connected to the surface of the sliding sleeve (43).

8. A mobile power supply suitable for general aviation equipment according to claim 4, characterized in that: The support plate (46) and the two sliding sleeves (43) are fixedly connected, and the bottom end of the support plate (46) is provided with an anti-slip groove.

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