Airplane storage battery detection device
By designing an aircraft battery detection device with automatic feeding and rotating mechanisms, the problems of battery fixing inconvenience and manual feeding in the prior art are solved, and the automatic detection and position adjustment of the battery are realized, and the detection efficiency and safety are improved.
Patent Information
- Application Number
- CN202421973850.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-15
- Publication Date
- 2025-07-25
- Estimated Expiration
- 2034-08-15
AI Technical Summary
The existing aircraft battery detection devices cannot adapt to battery fixation of different structures, and manual feeding is cumbersome, making it difficult to achieve efficient inspection.
An aircraft battery detection device including a feeding detection mechanism and a rotating mechanism is designed, and the motor drives the screw and gear system to realize automatic feeding and position adjustment of the battery, and the motor drives the motor to rotate the battery to meet different detection needs.
It realizes automatic fixation and position adjustment of the battery, simplifies the operation process, improves detection efficiency and safety, and avoids the cumbersomeness of manual feeding.
Smart Images

Figure CN223155186U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aircraft battery detection, and particularly relates to an aircraft battery detection device. Background Technique
[0002] The aviation battery, that is, the storage battery on the aircraft, is an important part of the aircraft power supply system and has various uses and characteristics. On the aircraft, the battery is mainly used as an auxiliary power supply or an emergency power supply to supply power to important electrical equipment, and is also the starting power supply of the engine. In special cases, such as in the wild without power, the battery can also be used as the pre-flight inspection power supply for some small-power electrical equipment on the aircraft;
[0003] However, during the existing battery detection, it is not possible to perform fixed detection according to batteries of different structures, and the battery is generally heavy, and manual feeding to the detection table is also required, which is rather cumbersome. Therefore, an aircraft battery detection device is introduced according to the above-mentioned problems. Content of the Utility Model
[0004] The technical problem to be solved by the utility model is to provide an aircraft battery detection device aiming at the deficiencies in the above-mentioned prior art.
[0005] To solve the above technical problems, the technical solution adopted by the utility model is: an aircraft battery detection device, including a detection table, a top plate is installed on the top of the detection table, and a feeding and detection mechanism is arranged on the detection table;
[0006] The feeding and detection mechanism includes a first motor, a first lead screw, a feeding plate, teeth, a double lead screw, a gear, a slider, a limiting rod, a connecting plate, and a detector;
[0007] The first motor is fixedly installed on the detection table, the output end of the first motor is provided with the first lead screw, the outer wall of the first lead screw is threadedly connected with the feeding plate, the feeding plate is slidably connected to the outer wall of the detection table, and teeth are installed on the top of the feeding plate. When the feeding plate reaches a certain position, it drives the connecting plate to contact and press the battery for detection.
[0008] Preferably, a double lead screw is rotatably connected to the inner wall of the detection table, a gear is sleeved on the outer wall of the double lead screw, a slider is threadedly connected to the outer wall of the double lead screw, a limiting rod is installed on the inner wall of the detection table, a connecting plate is installed on the slider, and the other end of the slider is slidably connected to the outer wall of the limiting rod.
[0009] Preferably, a detector is installed on the outer wall of the detection table, the detector is electrically connected to the connecting plate, and the number of the connecting plates is two groups. The two groups of connecting plates are symmetrically arranged at both ends of the outer wall of the double lead screw.
[0010] Preferably, a rotating mechanism is provided on the top plate. The rotating mechanism includes a first cylinder, the first cylinder is installed on the top of the top plate, the extending end of the first cylinder is fixedly installed with a second motor, and the extending end of the second motor is fixedly installed with a pressing block. When the position needs to be changed, the second motor drives the pressing plate, so as to facilitate the rotation and displacement of the battery, and facilitate the overall battery detection and adjustment.
[0011] Preferably, the gear meshes with the teeth on the feeding plate, and support legs are installed at the bottom of the detection table.
[0012] Preferably, the pressing block is flexibly arranged, and the teeth are eccentrically arranged at the edge of the feeding plate. By flexibly arranging the pressing block, it is convenient to protect the battery from damage.
[0013] The utility model adopts the above technical solutions, and can bring the following beneficial effects:
[0014] First, in the aircraft battery detection device, a feeding and detection mechanism is arranged on the detection table. During use, the first motor drives the first lead screw at the output end to rotate. When the first lead screw rotates, it drives the feeding plate to move for feeding. And teeth are arranged on the feeding plate. When the teeth drive the gear to rotate, when the feeding plate is driven to a certain position, the connecting plate is driven to contact and press the battery for detection.
[0015] Second, in the aircraft battery detection device, a rotating mechanism is arranged on the top plate. When the feeding plate drives the battery to a certain position, the cylinder drives the second motor to descend to fix the battery. When the position needs to be changed, the second motor drives the pressing plate, so as to facilitate the rotation and displacement of the battery, and facilitate the overall battery detection and adjustment. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 is the front view structural schematic diagram of the utility model;
[0017] Figure 2 is the rear view structural schematic diagram of the utility model;
[0018] Figure 3 is the side view structural schematic diagram of the utility model;
[0019] Figure 4 is the enlarged structural schematic diagram of A of the utility model.
[0020] In the figure: 1, detection table; 21, feeding and detection mechanism; 211, first motor; 212, first lead screw; 213, feeding plate; 214, teeth; 215, double lead screw; 216, gear; 217, slider; 218, limiting rod; 219, connecting plate; 2111, detector; 22, rotating mechanism; 221, first cylinder; 222, second motor; 223, pressing block; 3, top plate. Detailed implementation manners
[0021] The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all of the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the protection scope of the present utility model.
[0022] In the description of the present utility model, it should be understood that the orientation or positional relationship indicated by the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as a limitation to the present utility model.
[0023] In the description of the present utility model, it should be noted that unless otherwise clearly defined and limited, the terms "installation", "connection", and "setting" should be understood in a broad sense. For example, it can be fixedly connected and set, or detachably connected and set, or integrally connected and set. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.
[0024] Please refer to Figures 1-4, an embodiment of the present utility model is: an aircraft battery detection device, including a detection table 1, a top plate 3 is installed on the top of the detection table 1, a feeding and detecting mechanism 21 is arranged on the detection table 1, and the feeding and detecting mechanism 21 includes a motor one 211, a lead screw one 212, a feeding plate 213, teeth 214, a double lead screw 215, a gear 216, a slider 217, a limiting rod 218, a connecting plate 219, and a detector 2111. The motor one 211 is fixedly installed on the detection table 1, the output end of the motor one 211 is installed with the lead screw one 212, the outer wall of the lead screw one 212 is threadedly connected with the feeding plate 213, the feeding plate 213 is slidably connected to the outer wall of the detection table 1, and the top of the feeding plate 213 is installed with teeth 214. When the feeding plate 213 reaches a certain position, it drives the connecting plate 219 to contact and press the battery for detection. The inner wall of the detection table 1 is rotatably connected with a double lead screw 215, the outer wall of the double lead screw 215 is sleeved with a gear 216, the outer wall of the double lead screw 215 is threadedly connected with a slider 217, the inner wall of the detection table 1 is installed with a limiting rod 218, the slider 217 is installed with a connecting plate 219, and the other end of the slider 217 is slidably connected to the outer wall of the limiting rod 218. A detector 2111 is installed on the outer wall of the detection table 1, the detector 2111 is electrically connected to the connecting plate 219, and the number of the connecting plates 219 is two groups, and the two groups of connecting plates 219 are symmetrically arranged at both ends of the outer wall of the double lead screw 215.
[0025] Working principle: By installing a top plate 3 on the detection table 1 and arranging a feeding and detecting mechanism 21 on the detection table 1, during use, the motor one 211 drives the lead screw one 212 at the output end to rotate. When the lead screw one 212 rotates, it drives the feeding plate 213 to move for feeding. And teeth 214 are arranged on the feeding plate 213. When the teeth 214 drive the gear 216 to rotate, it drives the double lead screw 215 to rotate and a connecting plate 219 is installed on the double lead screw 215, and the other end of the connecting plate 219 is connected to the detector 2111. Therefore, when the feeding plate 213 reaches a certain position, it drives the connecting plate 219 to contact and press the battery for detection.
[0026] Please refer to Figures 1-4 , on the basis of the above embodiment, in another embodiment of the present utility model, a rotating mechanism 22 is arranged on the top plate 3. The rotating mechanism 22 includes a cylinder one 221. The cylinder one 221 is installed on the top of the top plate 3, the extending end of the cylinder one 221 is fixedly installed with a motor two 222, the extending end of the motor two 222 is fixedly installed with a pressing block 223. The gear 216 meshes with the teeth 214 on the feeding plate 213. And support legs are installed at the bottom of the detection table 1. The pressing block 223 is flexibly arranged, and the teeth 214 are eccentrically arranged at the edge of the feeding plate 213. By the flexible arrangement of the pressing block 223, it is convenient to protect the battery from being damaged.
[0027] Working principle: A rotating mechanism 22 is provided on the top plate 3. When the feeding plate 213 drives the battery to a certain position, the cylinder drives the second motor 222 to descend to fix the battery. When the position needs to be changed, the second motor 222 drives the pressing plate, so as to facilitate the rotation and position change of the battery and facilitate the overall battery detection and adjustment.
[0028] The present utility model provides an aircraft battery detection device. There are many methods and ways to specifically implement this technical solution. The above description is only the preferred embodiment of the present utility model. It should be noted that for those of ordinary skill in the art in this technical field, without departing from the principle of the present utility model, several improvements and refinements can be made, and these improvements and refinements should also be regarded as the protection scope of the present utility model. Each component not clearly defined in this embodiment can be implemented by using the prior art.
Claims
1. An aircraft battery detection device, comprising a detection bench (1), characterized in that: A top plate (3) is installed on the top of the detection table (1), and a feeding detection mechanism (21) is arranged on the detection table (1); The feeding detection mechanism (21) includes a first motor (211), a first lead screw (212), a feeding plate (213), teeth (214), a double lead screw (215), a gear (216), a slider (217), a limiting rod (218), a connecting plate (219), and a detector (2111); The first motor (211) is fixedly installed on the detection table (1), the output end of the first motor (211) is installed with a first lead screw (212), the outer wall of the first lead screw (212) is threadedly connected with a feeding plate (213), the feeding plate (213) is slidably connected to the outer wall of the detection table (1), and teeth (214) are installed on the top of the feeding plate (213).
2. The aircraft battery detection device according to claim 1, characterized in that: A double lead screw (215) is rotatably connected to the inner wall of the detection table (1), a gear (216) is sleeved on the outer wall of the double lead screw (215), the outer wall of the double lead screw (215) is threadedly connected with a slider (217), a limiting rod (218) is installed on the inner wall of the detection table (1), a connecting plate (219) is installed on the slider (217), and the other end of the slider (217) is slidably connected to the outer wall of the limiting rod (218).
3. The aircraft battery detection device according to claim 1, characterized in that: A detector (2111) is installed on the outer wall of the detection table (1), the detector (2111) is electrically connected to the connecting plate (219), and the number of the connecting plates (219) is two groups. The two groups of connecting plates (219) are symmetrically arranged at both ends of the outer wall of the double lead screw (215).
4. The aircraft battery detection device according to claim 1, characterized in that: A rotating mechanism (22) is arranged on the top plate (3). The rotating mechanism (22) includes a first cylinder (221). The first cylinder (221) is installed on the top of the top plate (3), and the extending end of the first cylinder (221) is fixedly installed with a second motor (222). The extending end of the second motor (222) is fixedly installed with a pressing block (223).
5. The aircraft battery detection device according to claim 1, characterized in that: The gear (216) meshes with the teeth (214) on the feeding plate (213), and support legs are installed at the bottom of the detection table (1).
6. An aircraft battery detection device according to claim 4, characterized in that: The pressing block (223) is flexibly arranged, and the teeth (214) are eccentrically arranged at the edge of the feeding plate (213).