CN219285377U - Unmanned aerial vehicle all-in-one cable automatic testing device - Google Patents
Unmanned aerial vehicle all-in-one cable automatic testing device Download PDFInfo
- Publication number
- CN219285377U CN219285377U CN202223484271.8U CN202223484271U CN219285377U CN 219285377 U CN219285377 U CN 219285377U CN 202223484271 U CN202223484271 U CN 202223484271U CN 219285377 U CN219285377 U CN 219285377U
- Authority
- CN
- China
- Prior art keywords
- test
- aerial vehicle
- unmanned aerial
- cable
- module
- 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.)
- Active
Links
Images
Landscapes
- Testing Of Short-Circuits, Discontinuities, Leakage, Or Incorrect Line Connections (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle all-computer cable automatic testing device, which comprises: the device comprises a power module, a display module, a test interface and a test transfer cable; the power supply module is connected to a power supply; the test interface is connected to the test module; the display module and the test module are connected to the power supply module; an inserting port is arranged at one end of the test switching cable and is detachably connected to the test port; the other end of the test switching cable is further provided with a connector, and the connector is detachably connected to the cable to be detected. According to the automatic testing device for the full-automatic cable of the unmanned aerial vehicle, provided by the utility model, through automatic testing, all conducting/non-conducting relation correctness tests of the full-automatic cable of the unmanned aerial vehicle are completed in a short time by utilizing fewer human resources, a qualification conclusion is given, and a plurality of defects of manual testing are overcome.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle all-electric cable automatic testing device.
Background
Currently, the conduction test of the unmanned aerial vehicle all-in-one cable is performed in a form that an operator manually uses a multimeter to check one by one. The main defects are as follows: the testing of the same group of cables is carried out by two or more people, so that the labor resources are occupied, and the problems of error and missing detection caused by human factors are unavoidable because the whole-machine electrical interconnection relationship of the unmanned aerial vehicle is complex and the number of the cables is huge (the point positions to be tested and the groups of the point positions are thousands of groups). Meanwhile, when an operator is used for manual testing of the all-computer cable, only one-to-one conduction relation test can be carried out on the points required by the definition of the cable interface, one-to-many, many-to-many and non-conduction relation test can not be carried out, the measurement items are very single, and the evaluation of the cable quality is greatly limited.
Disclosure of Invention
The utility model provides an unmanned aerial vehicle all-computer cable automatic testing device which solves the technical problems, and specifically adopts the following technical scheme:
an unmanned aerial vehicle all-purpose cable automated test device, includes: the device comprises a power module, a display module, a test interface and a test transfer cable;
the power supply module is connected to a power supply;
the test interface is connected to the test module;
the display module and the test module are connected to the power supply module;
an inserting port is arranged at one end of the test switching cable and is detachably connected to the test port;
the test switching cable other end still is equipped with the connector, the connector can dismantle and be connected to waiting to detect the cable.
Further, the power supply is 220V alternating current.
Further, the power module comprises a rectifying unit and a voltage reducing unit.
Further, the display module is a touch type LED display screen.
Further, the unmanned aerial vehicle all-computer cable automatic testing device comprises a plurality of testing interfaces and a plurality of testing transfer cables;
one end of each of the test transfer cables is provided with the plug interface which is detachably connected to the test interface;
the other ends of the test switching cables are provided with connectors, and the connectors of the test switching cables are detachably connected to the corresponding cables to be detected.
Further, connectors of different test switching cables are detachably connected to cables to be detected of different models.
Further, the power supply is a battery pack.
Further, the unmanned aerial vehicle all-computer cable automatic testing device further comprises a battery pack plug-in port;
the battery pack plug-in port is connected to the power module;
the battery pack is detachably connected to the battery pack plug port.
Further, the battery pack is slidably connected to the battery pack mating port.
The unmanned aerial vehicle all-in-one cable automatic testing device has the advantages that through automatic testing, fewer human resources are utilized, all conduction/non-conduction relation correctness tests of the unmanned aerial vehicle all-in-one cable are completed in a short time, a qualification conclusion is given, and a plurality of defects of manual testing are overcome.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present application, and that other drawings may be obtained according to these drawings without inventive faculty for a person skilled in the art.
Fig. 1 is a schematic view of a part of an all-electric motor automatic test equipment of an unmanned aerial vehicle according to the present utility model.
Detailed Description
Embodiments of the present application are described in detail below, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to like or similar elements or elements having like or similar functions throughout. The embodiments described below by referring to the drawings are exemplary and intended for the purpose of explaining the present application and are not to be construed as limiting the present application.
In the description of the present application, unless explicitly stated and limited otherwise, the terms "connected," "connected," and "fixed" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the terms in this application will be understood by those of ordinary skill in the art in a specific context.
In this application, unless expressly stated or limited otherwise, a first feature "above" or "below" a second feature may include both the first and second features being in direct contact, and may also include the first and second features not being in direct contact but being in contact with each other by way of additional features therebetween. Moreover, a first feature being "above," "over" and "on" a second feature includes the first feature being directly above and obliquely above the second feature, or simply indicating that the first feature is higher in level than the second feature. The first feature being "under", "below" and "beneath" the second feature includes the first feature being directly under and obliquely below the second feature, or simply means that the first feature is less level than the second feature.
Fig. 1 shows an automated testing device for full-plane cables of an unmanned aerial vehicle, which is mainly used for conducting tests of full-plane cables of the unmanned aerial vehicle. The utility model provides an unmanned aerial vehicle all-purpose cable automatic testing device mainly contains: the device comprises a power module, a display module, a test interface and a test transfer cable. The power module is connected to a power supply and used for supplying power to the whole unmanned aerial vehicle all-computer cable automatic testing device. The test interface is connected to the test module. The display module and the test module are connected to the power module. One end of the test switching cable is provided with an inserting port which can be detachably connected to the test port. The other end of the test switching cable is further provided with a connector, and the connector is detachably connected to the cable to be detected. The test module is used for completing data acquisition and processing of a test process, the display module is used for visually displaying the test process and result information, and the test switching cable, the plug interface and the connector are used for connecting the test system and the cable to be tested. The test transfer cable and the plug interface and the connector thereof are manufactured in a matching way according to the connection relation of the unmanned aerial vehicle all-computer cable and the number of the interfaces of the test system.
In the test process, the test module compares the test data with the stored standard sample data of the same type of cable, the test module displays qualified data when the data are consistent, and the test module displays specific inconsistent point position relations when the data are inconsistent. It can be understood that the unmanned aerial vehicle all-computer cable automatic testing device can also perform independent point searching testing.
In the application, the power supply is 220V alternating current, and power is supplied to all components in the system after passing through the power supply module. The power module comprises a rectifying unit and a voltage reducing unit. The 220V alternating current is converted into direct current matched with each component in the system after passing through the rectifying unit and the step-down unit. Preferably, the display module is a touch LED display screen.
As an alternative embodiment, the unmanned aerial vehicle all-in-one cable automation test device comprises a plurality of test interfaces and a plurality of test patch cables. One end of each test switching cable is provided with an inserting port, and the inserting ports are detachably connected to the test interfaces. The other ends of the test switching cables are provided with connectors, and the connectors of the test switching cables are detachably connected to the corresponding cables to be detected. More preferably, the connectors of different test transit cables are detachably connected to different types of cables to be tested. Like this, unmanned aerial vehicle all-electric cable automatic testing device of this application is furnished with the test switching cable of a plurality of different models, and the test switching cable of different models can adapt several kinds of commonly used cables that await measuring. Like this, unmanned aerial vehicle all-purpose cable automatic testing device of this application need not frequent change test switching cable and can directly match multiple cable that awaits measuring.
As another alternative embodiment, the power supply is a battery pack. The unmanned aerial vehicle all-computer cable automatic testing device also comprises a battery pack plug-in port. The battery pack plug-in port is connected to the power module. The battery pack is detachably connected to the battery pack plug port.
Like this, the unmanned aerial vehicle all-purpose cable automatic testing device of this application need not to connect 220V commercial power through the power cord, can work through removable battery pack, and it is more convenient to use.
As a preferred embodiment, the battery pack is slidingly connected to the battery pack mating port. Through sliding connection's design, can quick change the battery package.
The foregoing has shown and described the basic principles, principal features and advantages of the utility model. It will be appreciated by persons skilled in the art that the above embodiments are not intended to limit the utility model in any way, and that all technical solutions obtained by means of equivalent substitutions or equivalent transformations fall within the scope of the utility model.
Claims (9)
1. Unmanned aerial vehicle all-purpose cable automated test device, characterized by contains: the device comprises a power module, a display module, a test interface and a test transfer cable;
the power supply module is connected to a power supply;
the test interface is connected to the test module;
the display module and the test module are connected to the power supply module;
an inserting port is arranged at one end of the test switching cable and is detachably connected to the test port;
the test switching cable other end still is equipped with the connector, the connector can dismantle and be connected to waiting to detect the cable.
2. The automated test equipment for unmanned aerial vehicle all-in-one electronics of claim 1, wherein,
the power supply is 220V alternating current.
3. The automated test equipment of unmanned aerial vehicle all-purpose aircraft according to claim 2, wherein,
the power module comprises a rectifying unit and a voltage reducing unit.
4. The automated test equipment for unmanned aerial vehicle all-in-one electronics of claim 1, wherein,
the display module is a touch type LED display screen.
5. The automated test equipment for unmanned aerial vehicle all-in-one electronics of claim 1, wherein,
the unmanned aerial vehicle all-computer cable automatic testing device comprises a plurality of testing interfaces and a plurality of testing transfer cables;
one end of each of the test transfer cables is provided with the plug interface which is detachably connected to the test interface;
the other ends of the test switching cables are provided with connectors, and the connectors of the test switching cables are detachably connected to the corresponding cables to be detected.
6. The automated test equipment of unmanned aerial vehicle all-purpose aircraft according to claim 5, wherein,
different connectors of the test switching cables are detachably connected to cables to be detected of different models.
7. The automated test equipment for unmanned aerial vehicle all-in-one electronics of claim 1, wherein,
the power supply is a battery pack.
8. The automated test equipment for unmanned aerial vehicle all-in-one electronics of claim 7, wherein,
the unmanned aerial vehicle all-computer cable automatic testing device further comprises a battery pack plug-in port;
the battery pack plug-in port is connected to the power module;
the battery pack is detachably connected to the battery pack plug port.
9. The automated test equipment for unmanned aerial vehicle all-in-one electronics of claim 8, wherein,
the battery pack is slidably connected to the battery pack docking port.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223484271.8U CN219285377U (en) | 2022-12-21 | 2022-12-21 | Unmanned aerial vehicle all-in-one cable automatic testing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223484271.8U CN219285377U (en) | 2022-12-21 | 2022-12-21 | Unmanned aerial vehicle all-in-one cable automatic testing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219285377U true CN219285377U (en) | 2023-06-30 |
Family
ID=86905743
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223484271.8U Active CN219285377U (en) | 2022-12-21 | 2022-12-21 | Unmanned aerial vehicle all-in-one cable automatic testing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219285377U (en) |
-
2022
- 2022-12-21 CN CN202223484271.8U patent/CN219285377U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104569730B (en) | A kind of Cable Testing System applied to moonlet | |
| CN112858952B (en) | Rapid detection device and method for cable connectivity | |
| CN108152650A (en) | The automatic line inspection system of multicore cable | |
| CN207408530U (en) | A kind of portable multi-purpose aerospace cable tester | |
| CN219285377U (en) | Unmanned aerial vehicle all-in-one cable automatic testing device | |
| CN210376649U (en) | General type is used to group and switches on test fixture | |
| CN218585226U (en) | Shelter power station switch board detection device | |
| CN209946352U (en) | HiL wire harness testing device | |
| CN211878149U (en) | Portable aircraft complete machine cable conduction testing device | |
| CN212321803U (en) | Intelligent battery pack offline detection equipment and battery pack production line | |
| CN220419541U (en) | Switching harness testing device | |
| CN208476523U (en) | Handcart-type switch mechanical property intelligent test device | |
| CN115902704A (en) | Unmanned aerial vehicle full-aircraft cable automatic test system | |
| CN108549044B (en) | Insulation line selection tester for direct current system of transformer substation | |
| CN206788291U (en) | A kind of Small General Aircraft electric fuel oil selector valve detector | |
| CN110988483A (en) | Cable insulation tester based on inspection file rapid generation method | |
| CN214335091U (en) | Test cabinet for electric power system control protection device | |
| CN221101005U (en) | Portable multimode composite cable detection device | |
| CN219066030U (en) | Automobile electronic control unit test bench based on hardware-in-loop equipment | |
| CN219658043U (en) | Unmanned aerial vehicle flight control computer testing device | |
| CN103674553A (en) | Novel engine bench wire harness checking instrument | |
| CN116873220B (en) | Multi-agent technology-based aircraft telex bench test system and method | |
| CN218350754U (en) | Automatic test equipment and system for 441 series control panel assembly | |
| CN221406000U (en) | Aviation low frequency cable off-site testing device | |
| CN208506163U (en) | A kind of nuclear power station protection system at regular intervals testing stand detection device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |