CN203218622U - Power supply cable - Google Patents
Power supply cable Download PDFInfo
- Publication number
- CN203218622U CN203218622U CN 201320060400 CN201320060400U CN203218622U CN 203218622 U CN203218622 U CN 203218622U CN 201320060400 CN201320060400 CN 201320060400 CN 201320060400 U CN201320060400 U CN 201320060400U CN 203218622 U CN203218622 U CN 203218622U
- Authority
- CN
- China
- Prior art keywords
- feed cable
- cable
- power supply
- control
- electric connector
- 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.)
- Expired - Fee Related
Links
- 238000009434 installation Methods 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 238000005266 casting Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
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Abstract
A power supply cable comprises an electric connector (1), a complete cable (2) and binding posts (3); one end of the complete cable (2) is connected with the electric connector (1), and the other end of the complete cable (2) is connected with the binding posts (3); the electric connector (1) is provided with three LED indication lamps (8) and four control buttons (9); the power supply cable specially provided by the utility model is humanized in structural design, low in production cost, wide in application scope, can be used for replacing PJ power supply cable of an original structure, and is for connecting airplane AC ground socket with AC ground power supply vehicle; and the power supply cable provides AC current with rated voltage of 115V and rated power of 20KVA for airplane electrical system.
Description
Technical field
The utility model relates to the design of cable, is specifically related to a kind of feed cable.
Background technology
At present, domestic still do not have a like product, in various electric equipments, the consumption of feed cable is increasing, cable is electrically connected and the signal transmission between device and device, assembly and assembly, system and system, is to constitute the necessary base components of holonomic system, and feed cable mainly comprises electric connector and stranding two parts, but, existing power supply cable complex manufacturing, the production cost height, useful life is short, do not possess signal lamp, coefficient of safety is low.
The utility model content
Technical problem to be solved in the utility model is to overcome existing power supply cable complex manufacturing, the production cost height, and the defective that useful life is short does not possess signal lamp, and coefficient of safety is low.
The technical scheme that its technical problem that solves the utility model adopts is a kind of feed cable, comprise electric connector (1), stranding (2), binding post (3), wherein, stranding (2) one ends are connected with electric connector (1), and the other end is connected with binding post (3); Described electric connector (1) is provided with three LED light (8), four control buttons (9).
Feed cable described in the utility model, wherein, described stranding (2) is provided with mark heat-shrink tube (4), is used for the model of electroactive marker source power cable.
Feed cable described in the utility model, wherein, described mark heat-shrink tube (4) is outside equipped with the transparent heat draw (5), is used for seal protection mark heat-shrink tube (4).
Feed cable described in the utility model, wherein, described stranding (2) comprises 4 70mm
2Power line (6) and 16 1mm
2Control line (7), 4 70mm
2Power line (6) and 16 1mm
2The end of control line (7) all connect binding post (3).
Feed cable described in the utility model, wherein, described three LED light (8) are respectively for the LED1 of expression mated condition, are used for the LED2 of expression charged state and are used for the LED3 that the expression charging is finished.
Feed cable described in the utility model, wherein, described four control buttons (9) are respectively the SB1 buttons that is involved in cable reel installation for the control feed cable, be used for the SB2 button that the control feed cable is emitted from cable reel installation, control 400Hz power supply outputs to the SB3 button of aircraft plug by feed cable, and control 400Hz power supply stops to output to by feed cable the SB4 button of aircraft plug.
Feed cable described in the utility model, the structural design hommization, production cost is low, applied widely, can be used for substituting the PJ class feed cable of original structure, be used for connecting aircraft and exchange floor socket outlet and exchange the ground power supply car, it is that 115V, rated power are the alternating current of 20KVA that feed cable provides rated voltage to Aircraft Electrical System.
Feed cable described in the utility model, inner epoxide-resin glue embedding, the attached cable of adopting of connector, epoxy resin is selected INSULCAST 116FR casting glue for use, have good fluidity, solidify under the normal temperature, with embedding anchor clamps and housing adhesion in solidification process of special use.
Feed cable described in the utility model adopts replaceable plug, behind the jack wear out failure of butt end, the aircraft butt end can be separated and does integral replacing with the cable control end, the cable control end continues to use, and improves the whole service life of power line (6) cable, reduces maintenance cost; Increase LED light (8) on the plug, show current connection status and power supply state, improve reliability and the fail safe of operation; Set up control button (9) according to action need, allow the operator can on plug, directly control the action of 400Hz power switch and cable drum, use safety and convenient more.
Description of drawings
Fig. 1 is the feed cable structural representation;
Fig. 2 is the feed cable wiring schematic diagram.
Embodiment
Below in conjunction with drawings and Examples the utility model is described in further detail:
The described feed cable of present embodiment as shown in Figure 1, comprises electric connector (1), stranding (2), binding post (3), and wherein, stranding (2) one ends are connected with electric connector (1), and the other end is connected with binding post (3); Described electric connector (1) is provided with three LED light (8), four control buttons (9).
The described feed cable of present embodiment, as shown in Figure 1, described stranding (2) is provided with mark heat-shrink tube (4).
The described feed cable of present embodiment, as shown in Figure 1, described mark heat-shrink tube (4) is outside equipped with the transparent heat draw (5).
The described feed cable of present embodiment, as shown in Figure 1, described stranding (2) comprises 4 70mm
2Power line (6) and 16 1mm
2Control line (7), 4 70mm
2Power line (6) and 16 1mm
2The end of control line (7) all connect binding post (3).
The described feed cable of present embodiment, as shown in Figure 2, described three LED light (8) are respectively for the LED1 of expression mated condition, are used for the LED2 of expression charged state and are used for the LED3 that the expression charging is finished.
The described feed cable of present embodiment, as shown in Figure 2, described four control buttons (9) are respectively the SB1 buttons that is involved in cable reel installation for the control feed cable, be used for the SB2 button that the control feed cable is emitted from cable reel installation, control 400Hz power supply outputs to the SB3 button of aircraft plug by feed cable, and control 400Hz power supply stops to output to by feed cable the SB4 button of aircraft plug.
The above only is preferable embodiment of the present utility model, all any modifications of making within spirit of the present utility model and principle, is equal to and replaces and improvement etc., all should be included within the protection range of the present utility model.
Claims (6)
1. feed cable, it is characterized in that: described feed cable comprises electric connector (1), stranding (2), binding post (3), wherein, stranding (2) one ends are connected with electric connector (1), and the other end is connected with binding post (3); Described electric connector (1) is provided with three LED light (8), four control buttons (9).
2. according to the described feed cable of claim 1, it is characterized in that: described stranding (2) is provided with mark heat-shrink tube (4).
3. according to the described feed cable of claim 2, it is characterized in that: described mark heat-shrink tube (4) is outside equipped with the transparent heat draw (5).
4. according to the described feed cable of claim 1, it is characterized in that: described stranding (2) comprises four 70mm
2Power line (6) and 16 1mm
2Control line (7).
5. according to the described feed cable of claim 1, it is characterized in that: described three LED light (8) are respectively for the LED1 of expression mated condition, are used for the LED2 of expression charged state and are used for the LED3 that the expression charging is finished.
6. according to the described feed cable of claim 1, it is characterized in that: described four control buttons (9) are respectively the SB1 buttons that is involved in cable reel installation for the control feed cable, be used for the SB2 button that the control feed cable is emitted from cable reel installation, control 400Hz power supply outputs to the SB3 button of aircraft plug by feed cable, and control 400Hz power supply stops to output to by feed cable the SB4 button of aircraft plug.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320060400 CN203218622U (en) | 2013-06-17 | 2013-06-17 | Power supply cable |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320060400 CN203218622U (en) | 2013-06-17 | 2013-06-17 | Power supply cable |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203218622U true CN203218622U (en) | 2013-09-25 |
Family
ID=49208126
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320060400 Expired - Fee Related CN203218622U (en) | 2013-06-17 | 2013-06-17 | Power supply cable |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203218622U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105896154A (en) * | 2016-05-26 | 2016-08-24 | 四川永贵科技有限公司 | Ground power plug structure of airplane |
| CN112636108A (en) * | 2020-11-24 | 2021-04-09 | 江苏中煤电缆有限公司 | Remote control type cable plug for airport |
-
2013
- 2013-06-17 CN CN 201320060400 patent/CN203218622U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105896154A (en) * | 2016-05-26 | 2016-08-24 | 四川永贵科技有限公司 | Ground power plug structure of airplane |
| CN112636108A (en) * | 2020-11-24 | 2021-04-09 | 江苏中煤电缆有限公司 | Remote control type cable plug for airport |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130925 |
|
| CX01 | Expiry of patent term | ||
| CU01 | Correction of utility model |
Correction item: Termination upon expiration of patent Correct: Revocation of Patent Expiration and Termination False: On July 4, 2023, the expiration and termination of the 39 volume 2701 patent Number: 27-01 Volume: 39 |
|
| CU01 | Correction of utility model | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130925 |