CN215894897U - Marine aviation plug wiring detector - Google Patents

Marine aviation plug wiring detector Download PDF

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Publication number
CN215894897U
CN215894897U CN202121473029.3U CN202121473029U CN215894897U CN 215894897 U CN215894897 U CN 215894897U CN 202121473029 U CN202121473029 U CN 202121473029U CN 215894897 U CN215894897 U CN 215894897U
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China
Prior art keywords
aviation plug
module
shell
connector
test end
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CN202121473029.3U
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Chinese (zh)
Inventor
李露露
马鸿顺
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Hudong Zhonghua Shipbuilding Group Co Ltd
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Hudong Zhonghua Shipbuilding Group Co Ltd
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Abstract

The utility model discloses a marine aviation plug wiring detector, which comprises: the device comprises two connectors, a power supply, a control module, a test end indicator lamp module and an auxiliary test indicator lamp module; a connector is connected with an aviation plug at one end of the cable to be tested, the connector is connected with a test end indicator lamp module, the test end indicator lamp module is connected with a control module, the control module is connected with a power supply, and the power supply is connected with a shielding layer of the cable to be tested through a wire with a wire clamp; the other connector is connected with the aviation plug at the other end of the cable to be tested, the connector is connected with the auxiliary test indicator lamp module, and the auxiliary test end indicator lamp module is connected with the shielding layer of the cable to be tested through a wire with a wire clamp. The device has the advantages of small volume, simple structure, portability and simple operation, and can quickly measure whether the on-off state of the aviation plug and the core wire is good or not and whether the welding dislocation condition of the cable core wire and the aviation plug contact pin exists or not.

Description

Marine aviation plug wiring detector
Technical Field
The utility model belongs to the field of shipbuilding, and particularly relates to a marine aviation plug wiring detector.
Background
In the work of shipbuilding trade, electrical equipment is numerous, need often use the cable that has the aviation plug, and marine aviation plug wiring detector is an indispensable detection instrument, and in practical application, inserts the aviation plug of cable both ends in the connector of survey line appearance and just can realize the test purpose fast. In many cases, the aviation plug cable with few core wires can be detected by a universal meter; however, for multi-core and ultra-multi-core aviation plug cables, the aviation plug cables are very labor-consuming and have very high error rate in testing.
SUMMERY OF THE UTILITY MODEL
Aiming at the problems in the prior art, the utility model provides a marine aviation plug wiring detector, and partial embodiments can solve the problem that a multi-core or super-multi-core aviation plug cable cannot quickly and accurately test the connection quality of an aviation plug and a core wire.
In order to achieve the purpose, the utility model adopts the following technical scheme:
a marine aviation plug wiring detector, the detector comprising: the device comprises two connectors, a power supply, a control module, a test end indicator lamp module and an auxiliary test indicator lamp module; one connector is connected with an aviation plug at one end of a cable to be tested, the connector is connected with the test end indicator lamp module, the test end indicator lamp module is connected with the control module, the control module is connected with the power supply, and the power supply is connected with the shielding layer of the cable to be tested through a wire with a wire clamp; the other connector is connected with the aviation plug at the other end of the cable to be tested, the connector is connected with the auxiliary test indicator lamp module, and the auxiliary test end indicator lamp module is connected with the shielding layer of the cable to be tested through a wire with a wire clamp.
Preferably, the detector comprises: the shell is assisted to shell owner shell, shell owner shell cover is established power, control module and test end pilot lamp module, shell is assisted shell inner cover and is established supplementary test end pilot lamp module.
Preferably, a switch button hole and a first indicator light hole are formed in the housing main shell, the switch button of the control module is arranged in the switch button hole, and the indicator light of the test end indicator light module is arranged in the first indicator light hole.
Preferably, a second indicator light hole is formed in the shell auxiliary shell, and an indicator light of the auxiliary test indicator light module is arranged in the second indicator light hole.
Preferably, the connector includes a connection module and a conversion module, the connection module is an aviation plug female connector, and the conversion module is an aviation plug male-female adapter.
Compared with the prior art, the utility model has the beneficial effects that: the cable measuring device is small in size, simple in structure, convenient to carry and easy to operate, can quickly measure whether the on-off of the aviation plug and the core wire is good or not, and whether the welding dislocation condition of the cable core wire and the aviation plug contact pin exists or not, so that the operation difficulty caused by the field construction environment is greatly weakened due to the artificial error caused by too much core wire when a field worker measures the cable, the cable measuring time is shortened simultaneously, and the working efficiency is greatly improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic overall structure diagram of an embodiment of the present invention.
FIG. 2 is a type I circuit diagram of the detector.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without inventive effort based on the embodiments of the present invention, are within the scope of the present invention.
In the description of the present invention, it is to be understood that the terms "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention.
The utility model provides a marine aviation plug wiring detector, includes connector 1, power 2, control module 3, test end pilot lamp module 4 and supplementary test end pilot lamp module 5.
The connector 1 comprises a connection module and a conversion module, and the connector can be quickly connected with an aviation plug.
The power supply 2 comprises a wired conductor.
The auxiliary test end indicator light module 5 comprises a wire with a wire clamp.
The I type of this detector is: 24-core connector, 24-core control module, 24-core test end indicator lamp module and 24-core auxiliary test end indicator lamp module; the type II of the detector is as follows: the testing device comprises a 48-core connector, a 48-core control module, a 48-core testing end indicator lamp module and a 48-core auxiliary testing end indicator lamp module; the type III of the detector is as follows: the device comprises a 60-core connector, a 60-core control module, a 60-core test end indicator lamp module and a 60-core auxiliary test end indicator lamp module.
The utility model provides an optional scheme, the anodal 3 that link to each other with control module 2, control module negative pole and 4 anodals of test end pilot lamp module link to each other, and 4 anodes of test end pilot lamp module are linked to each other with connector 1, and connector 1 negative pole links to each other with the aviation plug of being tested cable one end. The aviation plug at the other end is connected with the anode of the connector 1. The negative pole of the connector 1 is connected with the positive pole of the auxiliary test end indicating lamp module 5, the negative pole of the auxiliary test end indicating lamp module 5 is connected with the shielding layer of the aviation plug cable, and the other end of the shielding layer of the aviation plug cable is connected with the negative pole of the power supply module.
Above-mentioned marine aviation plug wiring detector, it still includes: a main shell 6 and an auxiliary shell 7.
Power 2, control module 3, test end pilot lamp module 4, all be located 6 main casings on the shell, supplementary test end pilot lamp module 5 is located 6 supplementary casings on the shell.
There are 24 switch button holes, 24 pilot lamp holes on I type shell owner shell 6 of this detector, and control module, test end pilot lamp module inlay respectively in switch button hole and pilot lamp hole. Shell 7 is assisted to the shell has 24 pilot lamp holes, and the pilot lamp module of supplementary test end is inlayed in the pilot lamp hole.
There are 48 switch button holes, 48 pilot lamp holes on this detector II type shell owner shell 6, and control module, test end pilot lamp module inlay respectively in switch button hole and pilot lamp hole. Shell 7 is assisted to the shell and is gone up there are 48 pilot lamp holes, and the pilot lamp module of supplementary test end is inlayed in the pilot lamp hole.
There are 60 switch button holes, 60 pilot lamp holes on this detector III type shell owner shell 6, and control module, test end pilot lamp module inlay respectively in switch button hole and pilot lamp hole. Shell 7 is assisted to the shell and is gone up to have 60 pilot lamp holes, and the pilot lamp module of supplementary test end is inlayed at pilot lamp downthehole.
The detector can detect cables with 24-core type, 48-core type and 60-core type aviation plugs at two ends, when the detector is connected into the aviation plug cables, the connector, the power supply, the control module and the indicating lamp can form a plurality of series loops, and different loops can be switched through the control module. When the control module detects a certain core wire: if the test end indicator lamp and the auxiliary test end indicator lamp are correspondingly lightened, the aviation plug and the core wire are well welded, and the cable core wires and the plug contact pins are in one-to-one correspondence; if the auxiliary test end indicator light and the test end indicator light are not lightened to correspond to each other, the core wire of the auxiliary test end and the plug contact pin are connected in a wrong sequence; if the test end indicator light is on and a plurality of indicator lights of the auxiliary test end are on, the fact that a plurality of short circuits exist in the test end or the aviation plug of the auxiliary test end is indicated; if the indicator lights are not on, the core wire and the plug contact pin are indicated to be broken; if the test end indicator light is on and the auxiliary test end indicator light is not on, the short circuit between the core wire and the shielding layer is indicated.
As shown in fig. 1, the type iii aviation plug wiring detector for the ship comprises a connector 1, wherein a connection module and a conversion module are arranged in the connector 1, the connection module is a 60-core aviation plug female connector, and the conversion module is a 60-core aviation plug male-female adapter. The indicating lamp holes and the switch holes of the main shell 6 of the shell are numbered 1-60 respectively and have one-to-one correspondence in position, and the indicating lamp holes of the auxiliary shell 7 of the shell are numbered 1-60. 60 switch buttons of the control module 3 are embedded in a switch hole of a main shell of the shell, and 60 light emitting diodes of the test end indicator lamp module 4 are embedded in an indicator lamp hole of a main shell 6 of the shell and are connected in a one-to-one correspondence manner. The light emitting diodes numbered 1-60 are connected with the pins of the connector 1 in a one-to-one correspondence respectively. The connector 1 is directly connected with the tested cable 10 through the aviation plug 8. The other end of the tested cable 10 is directly connected with the connector 1 through the aviation plug 8, 60 light emitting diodes of the auxiliary testing end indicating lamp module 5 are embedded in an indicating lamp hole of the shell auxiliary shell 7, and the connector 1 and the auxiliary testing indicating lamp module 5 are sequentially connected with an indicating lamp of the shell auxiliary shell 7 according to a pin sequence. The other end clip of the auxiliary test end indicator light module 5 is connected with the shielding wire 9 of the end. The positive pole of the power supply is connected with the control module, and the wire clamp at the other end is connected with the shielding wire 9 of the tested cable at the end. At this moment, a plurality of series circuits are formed, the switching circuit is realized through a switch button of the control module 3, and when the control module detects a certain core wire: if the test end indicator lamp and the auxiliary test end indicator lamp are correspondingly lightened, the aviation plug and the core wire are well welded, and the cable core wires and the plug contact pins are in one-to-one correspondence; if the auxiliary test end indicator light and the test end indicator light are not lightened to correspond to each other, the core wire of the auxiliary test end and the plug contact pin are connected in a wrong sequence; if the test end indicator light is on and a plurality of indicator lights of the auxiliary test end are on, the fact that a plurality of short circuits exist in the test end or the aviation plug of the auxiliary test end is indicated; if the indicator lights are not on, the core wire and the plug contact pin are indicated to be broken; if the test end indicator light is on and the auxiliary test end indicator light is not on, the short circuit between the core wire and the shielding layer is indicated.
This embodiment is small, simple structure, and portable, easy operation, but whether the break-make of short-term test aviation plug and heart yearn is good to and whether there is heart yearn and aviation plug contact pin welding dislocation condition, avoided on-the-spot constructor when measuring the line, because the artificial error that the heart yearn arouses too much, weakened the operation degree of difficulty because of the site work environment brings greatly, shortened the volume line time simultaneously in a large number, very big improvement work efficiency.
Although the present invention has been described in detail with respect to the above embodiments, it will be understood by those skilled in the art that modifications or improvements based on the disclosure of the present invention may be made without departing from the spirit and scope of the utility model, and these modifications and improvements are within the spirit and scope of the utility model.

Claims (5)

1. The utility model provides a marine aviation plug wiring detector which characterized in that, the detector includes:
the device comprises two connectors, a power supply, a control module, a test end indicator lamp module and an auxiliary test indicator lamp module;
one connector is connected with an aviation plug at one end of a cable to be tested, the connector is connected with the test end indicator lamp module, the test end indicator lamp module is connected with the control module, the control module is connected with the power supply, and the power supply is connected with the shielding layer of the cable to be tested through a wire with a wire clamp;
the other connector is connected with the aviation plug at the other end of the cable to be tested, the connector is connected with the auxiliary test indicator lamp module, and the auxiliary test end indicator lamp module is connected with the shielding layer of the cable to be tested through a wire with a wire clamp.
2. The marine aviation plug wiring detector of claim 1, wherein the detector comprises: the shell is assisted to shell owner shell, shell owner shell cover is established power, control module and test end pilot lamp module, shell is assisted shell inner cover and is established supplementary test end pilot lamp module.
3. The marine aviation plug wiring detector of claim 2, wherein a switch button hole and a first indicator light hole are formed in the main housing, the switch button of the control module is disposed in the switch button hole, and the indicator light of the test end indicator light module is disposed in the first indicator light hole.
4. The marine aviation plug wiring detector of claim 3, wherein a second indicator light hole is formed in the auxiliary shell of the outer shell, and an indicator light of the auxiliary test indicator light module is arranged in the second indicator light hole.
5. The marine aviation plug wiring detector of claim 4, wherein the connector comprises a connection module and a conversion module, the connection module is an aviation plug female connector, and the conversion module is an aviation plug male-female adapter.
CN202121473029.3U 2021-06-30 2021-06-30 Marine aviation plug wiring detector Active CN215894897U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202121473029.3U CN215894897U (en) 2021-06-30 2021-06-30 Marine aviation plug wiring detector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202121473029.3U CN215894897U (en) 2021-06-30 2021-06-30 Marine aviation plug wiring detector

Publications (1)

Publication Number Publication Date
CN215894897U true CN215894897U (en) 2022-02-22

Family

ID=80561513

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202121473029.3U Active CN215894897U (en) 2021-06-30 2021-06-30 Marine aviation plug wiring detector

Country Status (1)

Country Link
CN (1) CN215894897U (en)

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