Aviation electric connector suitable for power distribution automation terminal
A technology for power distribution automation and electrical connectors, which is applied in the direction of connection, parts and circuits of connecting devices, and achieves the effects of not easy aging, diverse functions, and high safety.
Active Publication Date: 2021-08-20
深圳市本航本技术有限公司
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- Application Information
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Problems solved by technology
[0004] The technical problem to be solved by the present invention is an aeronautical electrical connector suitable for power distribution automation terminals that can solve the above problems, which is not easy to damage and has a longer service life
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[0022] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.
[0023] Any feature disclosed in this specification, including any appended claims, abstract and drawings, may, unless expressly stated otherwise, be replaced by alternative features which are equivalent or serve a similar purpose. That is, unless expressly stated otherwise, each feature is one example only of a series of equivalent or similar features.
[0024] In describing the present invention, it is to be understood that the terms "one end", "the other end", "outer side", "upper", "inner side", "horizontal", "coaxial", "central", "end ", "length", "outer end" and other indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, which are only for the convenience of describing the present invention and simplifying the d...
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The invention discloses an aviation electric connector suitable for a power distribution automation terminal. The electric connector comprises an aviation electric connector main body, the aviation electric connector main body comprises a connector shell, the connector shell comprises an outer shell, a middle shell and an inner shell from outside to inside, the middle shell and the inner shell are tightly attached, and the middle shell and the outer shell are in floating connection. A plurality of mounting grooves are formed in the inner side of the middle shell, elastic blocks are fixed in the mounting grooves, the elastic blocks and the inner shell are fixed, the outer shell and the middle shell are rotatably connected, a waterproof layer is arranged on the surface of the outer shell, a plurality of protruding parts are formed on the waterproof layer, a buffering cavity is formed between the protruding parts and the outer shell, and a suspended heat conduction piece is arranged in the buffering cavity; and a connecting hole is formed in the outer shell, one end of the connecting hole is connected with the buffering cavity, the other end of the connecting hole is connected with the middle shell, and a waterproof breathable film is fixed in the connecting hole. The electric connector is long in service life, diversified in function and not prone to damage.
Description
technical field [0001] The invention relates to the field of connectors, in particular to an aviation electrical connector suitable for power distribution automation terminals. Background technique [0002] Aviation plug is a kind of connector. The aviation plug is an electromechanical component that connects electrical lines, so its own electrical parameters are the first considerations when choosing an aviation plug. The correct selection and use of aviation plugs is an important aspect to ensure circuit reliability. [0003] At present, the aviation electrical connector includes a shell, but the structure of the shell is simple, there are problems such as poor waterproofness, low structural strength, and a short service life. Contents of the invention [0004] The technical problem to be solved by the present invention is an aeronautical electrical connector suitable for power distribution automation terminals that can solve the above problems, is not easy to be damag...
Claims
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IPC IPC(8): H01R13/52H01R13/717H01R13/502
CPCH01R13/502H01R13/52H01R13/717
Inventor 胡杰
Owner 深圳市本航本技术有限公司