CN110459995A - A kind of aviation plug harness fixed mechanism and aviation plug fixation kit - Google Patents
A kind of aviation plug harness fixed mechanism and aviation plug fixation kit Download PDFInfo
- Publication number
- CN110459995A CN110459995A CN201910673610.0A CN201910673610A CN110459995A CN 110459995 A CN110459995 A CN 110459995A CN 201910673610 A CN201910673610 A CN 201910673610A CN 110459995 A CN110459995 A CN 110459995A
- Authority
- CN
- China
- Prior art keywords
- aviation plug
- harness
- fixed mechanism
- supporting
- support
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 description 3
- 238000003466 welding Methods 0.000 description 2
- 239000002360 explosive Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/62—Means for facilitating engagement or disengagement of coupling parts or for holding them in engagement
- H01R13/639—Additional means for holding or locking coupling parts together, after engagement, e.g. separate keylock, retainer strap
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
- H02G3/02—Details
- H02G3/04—Protective tubing or conduits, e.g. cable ladders or cable troughs
- H02G3/0456—Ladders or other supports
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Installation Of Indoor Wiring (AREA)
Abstract
The invention discloses a kind of aviation plug harness fixed mechanism and aviation plug fixation kit, aviation plug harness fixed mechanism, including main support, the first supporting support and closed supports；Main support is equipped with multiple harness slits, and multiple harness slits extend each along the width direction of main support, and harness slit has open end and closed end, and the baffle between two neighboring harness slit is equipped with the first supporting support fixed part；First supporting support includes the first supporting section and the first linkage section, has angle between the first supporting section and the first linkage section, and the first supporting section is arranged to be used for support aviation plug harness；Closed supports are arranged to be used for being detachably connected with main support, to enter harness slit rear enclosed open end from open end in aviation plug harness.Aviation plug harness fixed mechanism of the invention can limit aviation plug harness in online narrow slot, and be supported by the first supporting support, to can effectively avoid the loosening of aviation plug.
Description
Technical field
The present invention relates to aviation plug fixed networks, more particularly, to a kind of aviation plug harness fixed mechanism and boat
Blind plug fixation kit.
Background technique
Central Control Room display screen realizes electrical connection using aviation plug.Plugging together and separating come real by aviation plug and socket
Existing circuit is connected and disconnected from.The connection type of aviation plug and socket is usually to be threadedly coupled.
For needing multiple rows of aviation plug to realize the Central Control Room display screen of electrical connection, using the fixed multiple rows of aviation plug of wire clamp
Harness.This fixed form is easy to lead to the loosening of aviation plug because of the clamping of harness and/or the vibration of harness, directly affects
To the normal use of Central Control Room display screen.
Therefore, the mechanism that aviation plug harness is effectively fixed can be stablized as this field urgent need to resolve by how providing one kind
Technical problem.
Summary of the invention
The aviation plug harness that aviation plug harness is effectively fixed can be stablized it is an object of the present invention to provide one kind
The new solution of fixed mechanism.
According to the first aspect of the invention, a kind of aviation plug harness fixed mechanism is provided.
The aviation plug harness fixed mechanism includes main support, the first supporting support and closed supports；Wherein,
The main support is equipped with multiple harness slits, width side of multiple harness slits each along the main support
To extension, and the harness slit has open end and closed end, and the baffle between the two neighboring harness slit is equipped with
First supporting support fixed part；
First supporting support includes the first supporting section and the first linkage section, and first supporting section and described first connect
Connecing has angle between section, first supporting section is arranged to be used for support aviation plug harness, the first linkage section quilt
It is provided for being connected with the first supporting support fixed part；
The closed supports are arranged to be used for being detachably connected with the main support, with aviation plug harness from described in
Open end enters open end described in the harness slit rear enclosed.
Optionally, multiple harness slits are arranged in parallel.
Optionally, the depth of the harness slit is greater than or equal to the 80% of the width of the main support.
Optionally, the main support has plate-like shape, and harness slit overlay area is less than or equal to the main branch
The 40% of the surface area of frame.
Optionally, the first supporting support fixed part is equipped with the first supporting support fixation hole.
Optionally, there are 90 ° of angles between first supporting section and the first linkage section.
Optionally, first supporting section is equipped with multiple binding holes.
Optionally, the closed supports are bolted with the main support.
Optionally, the aviation plug harness fixed mechanism further includes the second supporting support；
Second supporting support includes the second supporting section and the second linkage section, and second supporting section and described second connect
The angle having between section more than or equal to 90 ° is connect, second linkage section and the main support are equipped with the harness slit
The side of the closed end is fixedly connected, and second supporting section is arranged to put with the aviation plug harness fixed mechanism
Horizontalization face is in contact, and aviation plug harness fixed mechanism is supported on holding plane.
According to the second aspect of the invention, a kind of aviation plug fixation kit is provided.
The aviation plug fixation kit includes aviation plug, socket and aviation plug harness fixed mechanism of the invention；Its
In,
The distance between the main support and the socket are greater than or equal to 150mm and are less than or equal to 300mm.
Aviation plug harness fixed mechanism of the invention can limit aviation plug harness in online narrow slot, and pass through the
One supporting support support, to can effectively avoid the loosening of aviation plug.
By referring to the drawings to the detailed description of exemplary embodiment of the present invention, other feature of the invention and its
Advantage will become apparent.
Detailed description of the invention
It is combined in the description and the attached drawing for constituting part of specification shows the embodiment of the present invention, and even
With its explanation together principle for explaining the present invention.
Fig. 1 is the explosive view of the aviation plug harness fixed mechanism embodiment of the disclosure.
It is indicated in figure as follows:
Main support -1, harness slit -11, the first supporting support fixed part -12, the first supporting support fixation hole -120, the
One supporting support -2, the first supporting section -21, binding hole -210, the first linkage section -22, closed supports -3, the second supporting support -
4, second supporting section -41, the second linkage section -42.
Specific embodiment
Carry out the various exemplary embodiments of detailed description of the present invention now with reference to attached drawing.It should also be noted that unless in addition having
Body explanation, the unlimited system of component and the positioned opposite of step, numerical expression and the numerical value otherwise illustrated in these embodiments is originally
The range of invention.
Be to the description only actually of at least one exemplary embodiment below it is illustrative, never as to the present invention
And its application or any restrictions used.
Technology, method and apparatus known to person of ordinary skill in the relevant may be not discussed in detail, but suitable
In the case of, the technology, method and apparatus should be considered as part of specification.
It is shown here and discuss all examples in, any occurrence should be construed as merely illustratively, without
It is as limitation.Therefore, other examples of exemplary embodiment can have different values.
It should also be noted that similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined in a attached drawing, then in subsequent attached drawing does not need that it is further discussed.
As shown in Figure 1, the aviation plug harness fixed mechanism of the disclosure includes main support 1, the first supporting support 2 and closing
Bracket 3.
Main support 1 is equipped with multiple harness slits 11.Multiple harness slits 11 prolong each along the width direction of main support 1
It stretches, and harness slit 11 has open end and closed end.Harness slit 11 can be used for limiting aviation plug harness in main support 1
On.Baffle between two neighboring harness slit 11 is equipped with the first supporting support fixed part 12.
First supporting support 2 includes the first supporting section 21 and the first linkage section 22.First supporting section 21 and the first linkage section
There is angle between 22.First supporting section 21 can be used for supporting aviation plug harness.First linkage section 22 can be used for and first
Support bracket fixture portions 12 are connected.It can be connected by welding or bolt between first linkage section 22 and the first supporting support fixed part 12
It the modes such as connects or snaps connection to link together.
Closed supports 3 can be used for being detachably connected with main support 1, narrow from open end to enter harness in aviation plug harness
11 rear enclosed open end of slot.
First supporting support 2 when in use, is first mounted on main support 1 by the aviation plug harness fixed mechanism of the disclosure
On, then the open end of aviation plug harness from harness slit 11 is moved in harness slit 11.When aviation plug harness is equal
Into after harness slit 11, then the open end of the narrow slot 11 of 2 blockade line of closed supports is used, reliably by aviation plug harness
It is fixed in aviation plug harness fixed mechanism.
The aviation plug harness fixed mechanism of the disclosure can limit aviation plug harness in online narrow slot 11, and pass through
First supporting support 2 support, to can effectively avoid the loosening of aviation plug.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, in order to preferably avoid aviation plug
Harness fixed mechanism shakes, and multiple harness slits 11 are arranged in parallel.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, in order to preferably avoid aviation plug
Harness fixed mechanism shakes, and the depth of harness slit 11 is greater than or equal to the 80% of the width of main support 1.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, in order to preferably avoid aviation plug
Harness fixed mechanism shakes, and main support 1 has plate-like shape, and 11 overlay area of harness slit is less than or equal to the table of main support 1
The 40% of area.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, in order to more convenient reliably by first
In the installation to main support 1 of supporting support 2, the first supporting support fixed part 12 is equipped with the first supporting support fixation hole 120.Pass through
First supporting support fixation hole 120 and the fixation hole that is arranged on the first linkage section 22, and the first supporting support 2 can be with the first support
Bracket fixture portions 12 link together.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, in order to preferably avoid aviation plug
Harness shakes, and has 90 ° of angles between the first supporting section 21 and the first linkage section 22.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, in order to preferably avoid aviation plug
Harness shakes, and the first supporting section 21 is equipped with multiple binding holes 210.By binding hole 210, aviation plug harness can be fixed on
In first supporting support 2.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, closed supports 3 and 1 bolt of main support
Connection, thus the more reliably open end of the narrow slot 11 of blockade line.
In a kind of embodiment of the aviation plug harness fixed mechanism of the disclosure, in order to preferably avoid aviation plug
Harness fixed mechanism shakes, and aviation plug harness fixed mechanism further includes the second supporting support 4.
Second supporting support 4 includes the second supporting section 41 and the second linkage section 42.Second supporting section 41 and the second linkage section
There is the angle more than or equal to 90 ° between 42.Second linkage section 42 is equipped with the one of the closed end of harness slit 11 with main support 1
Side is fixedly connected, and above-mentioned be fixedly connected can be realized by the modes such as welding or being bolted.Second supporting section 41 can be inserted with aviation
The holding plane of head harness fixed mechanism is in contact, and aviation plug harness fixed mechanism is supported on holding plane.
When aviation plug harness fixed mechanism shakes, shaking can be transferred to aviation plug harness by the second supporting support 4
On the holding plane of fixed mechanism, to realize the purpose for avoiding aviation plug harness fixed mechanism from shaking.
The disclosure additionally provides a kind of aviation plug fixation kit, and the aviation including aviation plug, socket and the disclosure is inserted
Head harness fixed mechanism.The distance between main support 1 and socket are greater than or equal to 150mm and are less than or equal to 300mm, with more preferable
Ground avoids aviation plug harness from shaking.
Although some specific embodiments of the invention are described in detail by example, the skill of this field
Art personnel it should be understood that example above merely to being illustrated, the range being not intended to be limiting of the invention.The skill of this field
Art personnel are it should be understood that can without departing from the scope and spirit of the present invention modify to above embodiments.This hair
Bright range is defined by the following claims.
Claims (10)
1. a kind of aviation plug harness fixed mechanism, which is characterized in that including main support, the first supporting support and closed supports；
Wherein,
The main support is equipped with multiple harness slits, and multiple harness slits prolong each along the width direction of the main support
It stretches, and the harness slit has open end and closed end, the baffle between the two neighboring harness slit is equipped with first
Supporting support fixed part；
First supporting support includes the first supporting section and the first linkage section, first supporting section and first linkage section
Between there is angle, first supporting section is arranged to be used for support aviation plug harness, and first linkage section is set
For for being connected with the first supporting support fixed part；
The closed supports are arranged to be used for being detachably connected with the main support, in aviation plug harness from the opening
End enters open end described in the harness slit rear enclosed.
2. aviation plug harness fixed mechanism according to claim 1, which is characterized in that multiple harness slits are parallel
Setting.
3. aviation plug harness fixed mechanism according to claim 1, which is characterized in that the depth of the harness slit is big
In or equal to the main support width 80%.
4. aviation plug harness fixed mechanism according to claim 1, which is characterized in that the main support has plate shape
Shape, harness slit overlay area are less than or equal to the 40% of the surface area of the main support.
5. aviation plug harness fixed mechanism according to claim 1, which is characterized in that first supporting support is fixed
Portion is equipped with the first supporting support fixation hole.
6. aviation plug harness fixed mechanism according to claim 1, which is characterized in that first supporting section and first
There are 90 ° of angles between linkage section.
7. aviation plug harness fixed mechanism according to claim 1, which is characterized in that first supporting section is equipped with
Multiple binding holes.
8. aviation plug harness fixed mechanism according to claim 1, which is characterized in that the closed supports and the master
Support bracket bolt connection.
9. aviation plug harness fixed mechanism according to any one of claim 1 to 8, which is characterized in that the aviation
Plug harness fixed mechanism further includes the second supporting support；
Second supporting support includes the second supporting section and the second linkage section, second supporting section and second linkage section
Between have more than or equal to 90 ° of angle, second linkage section and the main support equipped with the described of the harness slit
The side of closed end is fixedly connected, and second supporting section is arranged to flat with the placement of the aviation plug harness fixed mechanism
Face is in contact, and aviation plug harness fixed mechanism is supported on holding plane.
10. a kind of aviation plug fixation kit, which is characterized in that including any in aviation plug, socket and claim 1 to 9
Aviation plug harness fixed mechanism described in；Wherein,
The distance between the main support and the socket are greater than or equal to 150mm and are less than or equal to 300mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910673610.0A CN110459995A (en) | 2019-07-24 | 2019-07-24 | A kind of aviation plug harness fixed mechanism and aviation plug fixation kit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910673610.0A CN110459995A (en) | 2019-07-24 | 2019-07-24 | A kind of aviation plug harness fixed mechanism and aviation plug fixation kit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110459995A true CN110459995A (en) | 2019-11-15 |
Family
ID=68483350
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910673610.0A Pending CN110459995A (en) | 2019-07-24 | 2019-07-24 | A kind of aviation plug harness fixed mechanism and aviation plug fixation kit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110459995A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3890459A (en) * | 1974-06-17 | 1975-06-17 | Panduit Corp | Wireway system and retaining finger for use therein |
| JP2002046948A (en) * | 2000-07-31 | 2002-02-12 | Yazaki Corp | Mounting structure of wire harness take-up device |
| CN204258190U (en) * | 2014-12-23 | 2015-04-08 | 安徽江淮汽车股份有限公司 | A kind of engine wire bundle fixing bracket |
| CN210167746U (en) * | 2019-07-24 | 2020-03-20 | 河南中烟工业有限责任公司 | Aviation plug wire harness fixing mechanism and aviation plug fixing assembly |
-
2019
- 2019-07-24 CN CN201910673610.0A patent/CN110459995A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3890459A (en) * | 1974-06-17 | 1975-06-17 | Panduit Corp | Wireway system and retaining finger for use therein |
| JP2002046948A (en) * | 2000-07-31 | 2002-02-12 | Yazaki Corp | Mounting structure of wire harness take-up device |
| CN204258190U (en) * | 2014-12-23 | 2015-04-08 | 安徽江淮汽车股份有限公司 | A kind of engine wire bundle fixing bracket |
| CN210167746U (en) * | 2019-07-24 | 2020-03-20 | 河南中烟工业有限责任公司 | Aviation plug wire harness fixing mechanism and aviation plug fixing assembly |
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