General aviation connector cable test equipment
By designing an aviation connector cable testing equipment that includes short-circuit tabs, ship-type switches and LED lamp beads, the problem that traditional methods are difficult to quickly and accurately detect the correctness and resistance synchronization of the aviation connector cable are achieved quickly , accurate cable testing.
Patent Information
- Application Number
- CN202420043430.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-01-08
- Publication Date
- 2025-02-14
- Estimated Expiration
- 2034-01-08
AI Technical Summary
When testing the air connector cable, it is difficult to quickly and accurately detect whether the line is correct and whether the resistance is synchronized, which can easily lead to signal misalignment, disconnection and inexplicable failure.
A general aviation connector cable testing equipment is designed, connected to the cable through the air connector socket and plug, and a detection circuit is formed by using short-circuit tabs and ship-type switches. The line conduction status and wire are judged by the LED lamp beads. Order error.
It realizes rapid testing of aviation connector cables, can intuitively determine whether the line is on and whether the line sequence is correct, simplifies the testing process, and improves detection efficiency and accuracy.
Smart Images

Figure CN222482280U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of aviation connecting line testing, and in particular relates to a general aviation connector cable testing device. Background Art
[0002] Aviation connectors are widely used in the military field and also shine in the civilian industry due to their large number of connections, high reliability, good stability and easy installation. However, aviation connectors have a large number of connections and require the position and order of the pins, which leads to higher industrial requirements for their production than other ordinary connectors.
[0003] Traditionally, after the aviation connector cable is manufactured, each pin and each foot is tested using the resistance range of a multimeter, and the disconnected resistance value is used to determine whether the aviation connector cable is in the wrong sequence and whether the line resistance is synchronized. The more lines inside the cable, the more difficult it is to detect, and the easier it is to confuse the line sequence. This measurement method not only takes a long time to test, but also easily confuses the line sequence, resulting in signal dislocation and disconnection problems, and is prone to inexplicable failures or even signal loss when applied to the device;
[0004] Therefore, the utility model provides a general aviation connector cable testing device which can quickly test the aviation connector cable after the aviation connector is manufactured. Utility Model Content
[0005] The purpose of the utility model is to provide a general aviation connector cable testing device to solve the problems raised in the above background technology.
[0006] In order to achieve the above purpose, the utility model provides the following technical solutions:
[0007] A general aviation connector cable testing device comprises an aviation connector socket, a first terminal block connected to the aviation connector socket, an aviation connector plug, and a second terminal block connected to the aviation connector plug, wherein a power supply compartment is connected between the first terminal block and the second terminal block;
[0008] The first terminal block includes a plurality of first connection terminals respectively connected in series with the aviation connector socket through first wires, and short-circuit pieces respectively connected in series with the plurality of first connection terminals, and a first conductive line connected in parallel with the output end of the short-circuit piece is connected to the negative electrode of the power supply compartment;
[0009] The second terminal block includes a plurality of second connection terminals respectively connected in series with the aviation connector plug through second wires, and a rocker switch respectively connected in series with the plurality of second connection terminals;
[0010] The second conductive wires connected in parallel at the output ends of the boat-shaped switches are connected to the positive pole of the power supply compartment, and each of the boat-shaped switches is correspondingly connected to a short-circuit piece to form a detection loop.
[0011] Furthermore, the power supply compartment is provided with a battery for supplying power to the first terminal block and the second terminal block to generate a detection circuit. Two No. 5 batteries can be placed in the power supply compartment according to test needs. The two No. 5 batteries cooperate with the power supply compartment to supply power to the detection circuit formed by the first terminal block and the second terminal block.
[0012] Furthermore, each of the short-circuit pieces is provided with an LED lamp bead, and an identification area for identifying the position of the short-circuit piece is provided on one side of the short-circuit piece corresponding to the LED lamp bead. By toggling each boat-type switch to control the lighting of the corresponding LED lamp bead in series, it is determined whether the circuit of the aviation connector cable under test can conduct current. If the pins on the aviation connector are well connected to its connecting wires, the LED lamp bead will light up and go out normally under the control of the boat-type switch. If the LED lamp bead does not respond when the boat-type switch is toggled, it means that this pin of the aviation connector cable has poor contact or the cable has a broken wire problem. The identification area is used to identify the order in which the LED lamp beads run, so as to determine whether there is a line sequence error in the tested aviation connector cable during the test.
[0013] Furthermore, the aviation connector socket is fixed by the assembly shell and is arranged on the outer wall of the assembly shell, the aviation connector plug is arranged on the outside of the assembly shell through the second wire, and the aviation connector socket and the aviation connector plug are respectively connected to the connection ends of the aviation connector cable to be tested, and the aviation connector cable to be tested is respectively connected to the aviation connector socket and the aviation connector plug outside the assembly shell, forming a loop for detecting the aviation connector cable to be tested.
[0014] Furthermore, a plurality of second wires connected to the second wiring terminals and the aviation connector plug and arranged outside the assembly housing are wrapped with cable protective covers, and the cable protective covers are used to fix and protect the second wires extending out of the assembly housing.
[0015] The utility model has the following technical effects and advantages:
[0016] The general aviation connector cable testing equipment is connected to the aviation connector socket through a first terminal row, and the second terminal row is connected to the aviation connector plug. The first terminal row and the second terminal row are respectively connected to the negative electrode and the positive electrode of the power supply compartment. The aviation connector socket and the aviation connector plug are respectively connected to the aviation connector cable to be tested, so that a test loop is formed between the aviation cable to be tested and the aviation connector socket and the aviation connector plug. The shorting piece on the first terminal row is correspondingly controlled by the rocker switch on the second terminal row, and the LED lamp bead on the shorting piece is turned on and off to check whether the corresponding pins of the aviation connector cable have poor contact or the problem of internal cable breakage.
[0017] This general aviation connector cable testing equipment uses the series and parallel principles of circuits to test the quality of aviation connector cables, and determines whether the aviation connector cables have broken wires or wrong sequence problems by turning on and off the boat-type switch and the lighting of the LED lamp beads. It has a simple testing principle for aviation connector lines and convenient operation. The test results are intuitive and easy to judge, and the fault can be located. It has broad application prospects in the connector testing equipment market and the industrial maintenance industry. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] Figure 1 It is a schematic diagram of the structure of the utility model;
[0019] Figure 2 This is a state diagram of the aviation connector line detection when the batteries in the power supply compartment of the utility model are two No. 5 batteries.
[0020] In the figure: 1. aviation connector socket; 2. first terminal block; 3. aviation connector plug; 4. second terminal block; 5. power supply compartment; 6. first wire; 7. short-circuit; 8. first conductive wire; 9. second conductive wire; 10. second connection terminal; 11. rocker switch; 12. second conductive wire; 13. battery; 14. LED lamp bead; 15. identification area; 16. assembly shell; 17. cable protective cover; 18. first connection terminal. DETAILED DESCRIPTION
[0021] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0022] The utility model provides Figure 1-2A general aviation connector cable testing device shown includes an aviation connector socket 1, a first terminal block 2 connected to the aviation connector socket 1, an aviation connector plug 3, and a second terminal block 4 connected to the aviation connector plug 3, wherein a power supply compartment 5 is connected between the first terminal block 2 and the second terminal block 4;
[0023] The first terminal block 2 includes a plurality of first connection terminals 18 connected in series with the aviation connector socket 1 through the first wires 6, and shorting pieces 7 connected in series with the plurality of first connection terminals 18, and a first conductive line 8 connected in parallel with the output end of the shorting piece 7 is connected to the negative electrode of the power supply compartment 5;
[0024] The second terminal block 4 includes a plurality of second connection terminals 10 respectively connected in series with the aviation connector plug 3 through the second wires 9, and a rocker switch 11 respectively connected in series with the plurality of second connection terminals 10;
[0025] The second conductive wires 12 connected in parallel to the output ends of the rocker switches 11 are connected to the positive pole of the power supply compartment 5, and each rocker switch 11 is correspondingly connected to the short-circuit piece 7 to form a detection loop.
[0026] A battery 13 is provided in the power supply compartment 5 for supplying power to the first terminal row 2 and the second terminal row 4 to generate a detection circuit. Two No. 5 batteries can be placed in the power supply compartment 5 according to the needs of the test. The two No. 5 batteries cooperate with the power supply compartment 5 to supply power to the detection circuit formed by the first terminal row 2 and the second terminal row 4.
[0027] An LED lamp bead 14 is provided on each short-circuit 7, and an identification area 15 for identifying the position of the short-circuit 7 is provided on one side of the short-circuit 7 corresponding to the LED lamp bead 14. By toggling each rocker switch 11 to control the lighting of the corresponding LED lamp bead 14 in series, it is determined whether the circuit of the aviation connector cable under test can conduct current. If the pins on the aviation connector are well connected to its connecting wires, the LED lamp bead 14 will light up and go out normally under the control of the rocker switch 11. If the LED lamp bead 14 does not respond when the rocker switch 11 is toggled, it means that this pin of the aviation connector cable has poor contact or the cable is broken. The identification area 15 is used to identify the order in which the LED lamp bead 14 runs, so as to determine whether there is a line sequence error in the tested aviation connector cable during the test.
[0028] The aviation connector socket 1 is fixed by the assembly shell 16 and is arranged on the outer wall of the assembly shell 16, the aviation connector plug 3 is arranged outside the assembly shell 16 through the second wire 9, and the aviation connector socket 1 and the aviation connector plug 3 are respectively connected to the connection ends of the aviation connector cable to be tested, and the aviation connector cable to be tested is respectively connected to the aviation connector socket 1 and the aviation connector plug 3 outside the assembly shell 16, forming a loop for detecting the aviation connector cable to be tested.
[0029] A plurality of second wiring terminals are connected to the aviation connector plug 3 and are provided outside the assembly housing 16 , and the second wires 9 are wrapped with cable protective covers 17 . The cable protective covers 17 are used to fix and protect the second wires 9 extending out of the assembly housing 16 .
[0030] The general aviation connector cable testing equipment is connected to the aviation connector socket 1 through the first terminal block 2, and the second terminal block 4 is connected to the aviation connector plug 3, and the first terminal block 2 and the second terminal block 4 are respectively connected to the negative electrode and the positive electrode of the power supply compartment 5, and the aviation connector socket 1 and the aviation connector plug 3 are respectively connected to the aviation connector cable to be tested, so that a test loop is formed between the aviation cable to be tested and the aviation connector socket 1 and the aviation connector plug 3, and the short-circuit 7 on the first terminal block 2 is correspondingly controlled by the rocker switch 11 on the second terminal block 4, and the LED lamp bead 14 on the short-circuit 7 is used to check whether the corresponding pins of the aviation connector cable have poor contact or the problem of internal cable breakage;
[0031] When testing the aviation connector cable after production, the two ends of the aviation connector cable to be tested are respectively plugged into the aviation connector plug 3 and the aviation connector socket 1, and the operator sequentially turns on and off the rocker switch 11 to control the corresponding LED lamp beads 14 in series, thereby judging whether the circuit of the aviation connector cable to be tested can conduct current. If the pins on the aviation connector are well connected to its connecting wires, the LED lamp beads 14 will normally light up and go out under the control of the rocker switch 11. If the LED lamp beads 14 do not respond when the rocker switch 11 is turned on, it means that this pin of the aviation connector cable has poor contact or the cable is broken. When testing the internal line sequence of a multi-pin aviation connector cable, the rocker switch 11 is sequentially turned on and off to observe the corresponding LED lamp beads 14 to judge whether the tested aviation connector cable has a line sequence error or poor contact.
[0032] When the aviation connector cable test equipment uses a wire with a nominal cross-section of 1.5 square and a diameter of 1.38 mm, and the battery compartment 5 is connected in series with two AA batteries, the maximum aviation connector cable measurement length and the internal wire diameter of the aviation connector cable can be measured. Figure 2 As shown;
[0033] The general aviation connector cable testing equipment uses the series and parallel principles of circuits to test the quality of aviation connector cables, and determines whether the aviation connector cables have broken wires or wrong sequence problems by the on and off of the boat-type switch 11 and the on and off of the LED lamp beads 14. It has a simple testing principle for aviation connector lines and convenient operation. It also has intuitive and easy-to-judgment test results and can locate faults. It has broad application prospects in the connector testing equipment market and the industrial maintenance industry.
[0034] Finally, it should be noted that the above is only a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.
Claims
1. A general aviation connector cable testing device, comprising an aviation connector socket (1), a first terminal block (2) connected to the aviation connector socket (1), an aviation connector plug (3), and a second terminal block (4) connected to the aviation connector plug (3), characterized in that: A power supply compartment (5) is connected between the first wiring terminal row (2) and the second wiring terminal row (4); The first terminal block (2) comprises a plurality of first connection terminals (18) respectively connected in series with the aviation connector socket (1) via first wires (6), and shorting pieces (7) respectively connected in series with the plurality of first connection terminals (18); a first conductive line (8) connected in parallel to the output end of the shorting piece (7) is connected to the negative electrode of the power supply compartment (5); The second terminal block (4) comprises a plurality of second connection terminals (10) respectively connected in series with the aviation connector plug (3) via second wires (9), and a rocker switch (11) respectively connected in series with the plurality of second connection terminals (10); The second conductive wires (12) connected in parallel to the output ends of the rocker switches (11) are connected to the positive pole of the power supply compartment (5), and each rocker switch (11) is correspondingly connected to a shorting piece (7) to form a detection circuit.
2. A general aviation connector cable testing device according to claim 1, characterized in that: A battery (13) is provided in the power supply compartment (5) for supplying power to the first wiring terminal row (2) and the second wiring terminal row (4) to generate a detection circuit.
3. A general aviation connector cable testing device according to claim 1, characterized in that: Each of the shorting pieces (7) is provided with an LED lamp bead (14), and a marking area (15) for marking the position of the shorting piece (7) is provided on one side of the shorting piece (7) corresponding to the LED lamp bead (14).
4. A general aviation connector cable testing device according to claim 1, characterized in that: The aviation connector socket (1) is fixed by an assembly shell (16) and is arranged on the outer wall of the assembly shell (16); the aviation connector plug (3) is arranged outside the assembly shell (16) via a second wire (9); and the aviation connector socket (1) and the aviation connector plug (3) are respectively connected to the connection ends of the aviation connector cable to be tested.
5. A general aviation connector cable testing device according to claim 4, characterized in that: A plurality of second wires (9) connected to the second wiring terminal and the aviation connector plug (3) and arranged outside the assembly housing (16) are wrapped with cable protection sleeves (17).