CN202282525U - Rectangular connector shield tail clamp for avionics system - Google Patents
Rectangular connector shield tail clamp for avionics system Download PDFInfo
- Publication number
- CN202282525U CN202282525U CN201120329134XU CN201120329134U CN202282525U CN 202282525 U CN202282525 U CN 202282525U CN 201120329134X U CN201120329134X U CN 201120329134XU CN 201120329134 U CN201120329134 U CN 201120329134U CN 202282525 U CN202282525 U CN 202282525U
- Authority
- CN
- China
- Prior art keywords
- tail clamp
- rectangular connector
- connector
- shield tail
- shield
- 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 - Lifetime
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- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The utility model belongs to a connector accessory, relating to a rectangular connector shield tail clamp for an avionics system. The rectangular connector shield tail clamp is used for mounting, shielding and fixing output wire harnesses of a rectangular connector. A hook and a mounting hole are formed at the front end of a shield tail clamp casing; and wire pressing devices are arranged at the rear end of the shield tail clamp casing and are of two U-shaped structures, wherein one U-shaped structure is fixedly arranged on the shield tail clamp casing. The rectangular connector shield tail clamp disclosed by the utility model has the advantages that a connecting mode of the rectangular connector tail clamp and the connector casing and a connecting mode of a cable shield body are designed into a whole so as to bring convenience to realization of the fastening of cable bunches and electromagnetic sealing of the cable bunches. Due to the adoption of the integrated structural design, the requirement on electromagnetic shield can be met and the mounting space of the connector in the length direction is reduced by nearly 40 percent compared with that of a traditional tail clamp.
Description
Technical field
The utility model belongs to connector fitting, relates to a kind of installation that is used for the rectangular connector bundle of outputs and shielding, fixing avionics system with rectangular connector shielding tail folder.
Background technology
At present, the rectangular connector tail folder that in the avionics system product, adopts, its mounting means is split type; Need tail be pressed from both sides housing 6 usefulness screws during installation and be loaded on the rectangular connector compressing tablet 5, bunch of cables line ball folder 7 hangs on the rectangular connector compressing tablet 5 through hook, and the result of this mounting means is; Line ball folder 7 easy and housing 6 disengagings in the use, fastness is poor, simultaneously owing to have structure interval between line ball folder 7 and the housing 6; Cause electromagnetic radiation leakage easily, this effective control to electromagnetic compatibility is disadvantageous, in addition; This structure volume that takes up room is bigger, influences the installation of aeronautical product.
Summary of the invention
The purpose of the utility model is to propose a kind of a kind of avionics system that satisfies electromagnetic compatibility and fastening requirement is installed with rectangular connector shielding tail folder.The technical solution of the utility model is, the front end of shielding tail folder housing is provided with hook and installing hole, and the rear end of shielding tail folder housing is provided with cord grip, and cord grip is two U-shaped structures, and one of them U-shaped structure is fixed on the shielding tail folder housing.Advantage that the utlity model has and beneficial effect; The utility model with rectangular connector tail folder and connector shell be connected and the connected mode of cable shield body is designed to one; Be convenient to the realization of the fastening of bunch of cables and bunch of cables electromagnetic sealing; Owing to adopt incorporate structural design not only to satisfy the needs of electromagnetic shielding, and make connector reduce nearly 40% than existing tail folder at the installing space of length direction.
Description of drawings
Fig. 1 is existing rectangular connector tail clamping structure sketch map;
Fig. 2 is the end view of Fig. 1;
Fig. 3 is the structural representation of the utility model;
Fig. 4 is the end view of Fig. 3.
Embodiment
The utility model is elaborated with Fig. 4 below in conjunction with accompanying drawing 3.The hook 1 and installing hole 2 that carry on the shielding tail folder housing 3 of rectangular connector; Can be directly installed on the rectangular connector housing; U-shaped cord grip 4 on the shielding tail folder housing 3 can directly compress bunch of cables, and forms reliable the electrical connection with screen on the bunch of cables.The front end of connector shielding tail folder housing 3 is provided with the hook 1 and installing hole 2 that is connected with rectangular connector; The U-shaped cord grip 4 that its rear end design is fixed bunch of cables; Cord grip 4 is two U-shaped structures; One of them U-shaped structure is fixed on the shielding tail folder housing 3, and the U-shaped structure helps compressing of bunch of cables and realizes the electromagnetic sealing property of shielded type cable.
The utility model rectangular connector shielding tail folder, during use removes the compressing tablet on the rectangular connector tail end for overall structure, the utility model directly is contained on the housing of rectangular connector.
Claims (1)
1. an avionics system is with rectangular connector shielding tail folder; It is characterized in that; The front end of shielding tail folder housing (3) is provided with hook (1) and installing hole (2); The rear end of shielding tail folder housing (3) is provided with cord grip (4), and cord grip (4) is two U-shaped structures, and one of them U-shaped structure is fixed on the shielding tail folder housing (3).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201120329134XU CN202282525U (en) | 2011-09-01 | 2011-09-01 | Rectangular connector shield tail clamp for avionics system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201120329134XU CN202282525U (en) | 2011-09-01 | 2011-09-01 | Rectangular connector shield tail clamp for avionics system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202282525U true CN202282525U (en) | 2012-06-20 |
Family
ID=46228678
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201120329134XU Expired - Lifetime CN202282525U (en) | 2011-09-01 | 2011-09-01 | Rectangular connector shield tail clamp for avionics system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN202282525U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105071143A (en) * | 2015-08-31 | 2015-11-18 | 南京南车浦镇城轨车辆有限责任公司 | Rectangular connector universal shield card |
CN105490070A (en) * | 2016-01-18 | 2016-04-13 | 创驱(上海)新能源科技有限公司 | Electromagnetic shielding structure for quick pressed cables |
CN111059033A (en) * | 2019-12-18 | 2020-04-24 | 浙江华力新能源科技有限公司 | Electric compressor shielding cover and air conditioner |
-
2011
- 2011-09-01 CN CN201120329134XU patent/CN202282525U/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105071143A (en) * | 2015-08-31 | 2015-11-18 | 南京南车浦镇城轨车辆有限责任公司 | Rectangular connector universal shield card |
CN105490070A (en) * | 2016-01-18 | 2016-04-13 | 创驱(上海)新能源科技有限公司 | Electromagnetic shielding structure for quick pressed cables |
CN111059033A (en) * | 2019-12-18 | 2020-04-24 | 浙江华力新能源科技有限公司 | Electric compressor shielding cover and air conditioner |
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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 | ||
CX01 | Expiry of patent term |
Granted publication date: 20120620 |