CN108199190B - Four-bar mechanism in airborne weapon system separate connector - Google Patents
Four-bar mechanism in airborne weapon system separate connector Download PDFInfo
- Publication number
- CN108199190B CN108199190B CN201711263644.XA CN201711263644A CN108199190B CN 108199190 B CN108199190 B CN 108199190B CN 201711263644 A CN201711263644 A CN 201711263644A CN 108199190 B CN108199190 B CN 108199190B
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- mounting bracket
- fixed
- connector
- rotation axis
- 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.)
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Classifications
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- 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
- H01R13/629—Additional means for facilitating engagement or disengagement of coupling parts, e.g. aligning or guiding means, levers, gas pressure electrical locking indicators, manufacturing tolerances
- H01R13/62933—Comprising exclusively pivoting lever
-
- 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
- H01R13/46—Bases; Cases
- H01R13/502—Bases; Cases composed of different pieces
Landscapes
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
A kind of four-bar mechanism in airborne weapon system separate connector, including cover board, connecting rod base, rotation axis, connecting rod, washer, screw, mounting bracket, steel ball, spring, the components such as fixed swivel nut, connecting rod base, rotation axis and connecting rod assembly constitute linkage component, four linkage components are mutually indepedent, design has circular groove on connecting rod, one end of connecting rod is fixed in connecting rod base by rotation axis, the other end is fixed on the mounting bracket, design has stopping step in mounting bracket, by steel ball, the pre-pressing structure of spring and fixed swivel nut composition is mounted in stopping step, design has mounting hole in mounting bracket, it can be with the mating installation of different series connector, play tail accessory simultaneously, convenient for connector cable outlet, it is other stop mechanisms that mounting bracket upper end platform can be servo-actuated in separation process simultaneously in connector Machine power is provided.
Description
Technical field
The invention belongs to mechanical designing techniques, and in particular to a kind of novel four-bar mechanism.
Background technique
Airborne weapon system separate connector often will appear following situations in use: connector separate axis with
Body course is vertical, and connector is direct-plug structure, itself does not have locking function.To guarantee connector signal transmission and dividing
From reliable, a kind of novel four-bar mechanism is needed to complete connector with springing separated in synchronization, while initial shape can also be completed
State connector plugs together requirement automatically.
Summary of the invention
The purpose of the present invention is:
It is proposed a kind of novel four-bar mechanism, solution airborne weapon system separate connector plugs together and separation problem, broadening
The separate connector scope of application.
Technical solution of the present invention:
Four-bar mechanism in airborne weapon system separate connector includes cover board 1, connecting rod base 2, rotation axis 3, connecting rod
4, the components such as washer 5, screw 6, mounting bracket 7, steel ball 8, spring 9, fixation swivel nut 10, connecting rod base 2, rotation axis 3 and company
The combination of bar 4 constitutes linkage component, and four linkage components are mutually indepedent, and design has circular groove, one end of connecting rod 4 on connecting rod 4
Be fixed in connecting rod base 2 by rotation axis 3, the other end is fixed in mounting bracket 7, for reduce linkage component shifting amount,
Washer 5 and screw 6 are installed in connecting rod 4 and 7 junction of mounting bracket, guarantee to keep lesser while connecting rod 4 is freely rotated
Shifting amount avoids influencing plugging together for connector.It is simultaneously to guarantee to be in positive status, in mounting bracket 7 when connector plugs together
Design has stopping step, is mounted in stopping step by the pre-pressing structure that steel ball 8, spring 9 and fixed swivel nut 10 form, spring 9
One end is mounted in fixed swivel nut 10, and the other end withstands steel ball 8, by solid with the mating formation connecting rod position of arc groove on connecting rod 4
Fixed, by the way that steel ball 8 to be extruded between connecting rod 4 and mounting bracket 7, spring 9 to form normal pressure between steel ball 8 and connecting rod 4,
And then form locking frictional force, it is ensured that connecting rod 4 is at regulation inserted position.Design has mounting hole, energy in mounting bracket 7
The enough and mating installation of different series connector, while playing tail accessory, it is convenient for connector cable outlet.In mounting bracket 7
End platform can be servo-actuated in separation process simultaneously in connector provides machine power for other stop mechanisms.
Beneficial effects of the present invention:
Four-bar mechanism in airborne weapon system separate connector proposed by the present invention, solve separate connector plug together and
Separation problem has widened the separate connector scope of application.
Detailed description of the invention
Fig. 1 is the four-bar mechanism structural front view in airborne weapon system separate connector；
Fig. 2 is the face the P-P cross-sectional view in the four-bar mechanism structural front view in airborne weapon system separate connector；
Fig. 3 is the four-bar mechanism using renderings in airborne weapon system separate connector；
In figure: 1- cover board, 2- connecting rod base, 3- rotation axis, 4- connecting rod, 5- washer, 6- screw, 7- mounting bracket, 8- steel
The fixed swivel nut of ball, 9- spring, 10-.
Specific embodiment
Shown in Fig. 3 is the four-bar mechanism in a kind of airborne weapon system separate connector designed according to the present invention,
Including cover board 1, connecting rod base 2, rotation axis 3, connecting rod 4, washer 5, screw 6, mounting bracket 7, steel ball 8, spring 9, fixed swivel nut
10 equal components, connecting rod base 2, rotation axis 3 and the combination of connecting rod 4 constitute linkage component, and four linkage components are mutually indepedent, connecting rod
Design has circular groove on 4, and one end of connecting rod 4 is fixed in connecting rod base 2 by rotation axis 3, and the other end is fixed on installation
On bracket 7, for the shifting amount for reducing linkage component, washer 5 and screw 6 are installed in connecting rod 4 and 7 junction of mounting bracket, protected
Card connecting rod 4 keeps lesser shifting amount while being freely rotated, and avoids influencing plugging together for connector.It is inserted simultaneously for guarantee connector
In to positive status when conjunction, design has stopping step in mounting bracket 7, is made of steel ball 8, spring 9 and fixed swivel nut 10
Pre-pressing structure is mounted in stopping step, and 9 one end of spring is mounted in fixed swivel nut 10, and the other end withstands steel ball 8, by with connecting rod
The mating formation connecting rod position of arc groove is fixed on 4, and by the way that steel ball 8 to be extruded between connecting rod 4 and mounting bracket 7, spring 9 makes
It obtains and forms normal pressure between steel ball 8 and connecting rod 4, and then form locking frictional force, it is ensured that connecting rod 4 is at regulation and plugs together position
It sets.Design has mounting hole in mounting bracket 7, while can play tail accessory, just with the mating installation of different series connector
In connector cable outlet.It is other stop machines that 7 upper end platform of mounting bracket can be servo-actuated in separation process simultaneously in connector
Structure provides machine power.
Claims (3)
1. the four-bar mechanism in airborne weapon system separate connector, including cover board (1), connecting rod base (2), rotation axis (3),
Connecting rod (4), washer (5), screw (6), mounting bracket (7), steel ball (8), spring (9), fixed swivel nut (10), feature is loaded on:
Connecting rod base (2), rotation axis (3) and connecting rod (4) combination constitute linkage component, and four linkage components are mutually indepedent, on connecting rod (4)
Design has circular groove, and one end of connecting rod (4) is fixed on connecting rod base (2) by rotation axis (3), and the other end is fixed on peace
It fills on bracket (7), washer (5) and screw (6) is installed in connecting rod (4) and mounting bracket (7) junction, in mounting bracket (7)
Design has stopping step, is mounted in stopping step by the pre-pressing structure that steel ball (8), spring (9) and fixation swivel nut (10) form,
Spring (9) one end is mounted in fixed swivel nut (10), and the other end withstands steel ball (8), by with the mating shape of arc groove on connecting rod (4)
It is fixed at connecting rod position.
2. the four-bar mechanism in airborne weapon system separate connector according to claim 1, feature are loaded on: installation
Design has mounting hole on bracket (7).
3. the four-bar mechanism in airborne weapon system separate connector according to claim 1, feature are loaded on: installation
Bracket (7) upper end is platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711263644.XA CN108199190B (en) | 2017-12-04 | 2017-12-04 | Four-bar mechanism in airborne weapon system separate connector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711263644.XA CN108199190B (en) | 2017-12-04 | 2017-12-04 | Four-bar mechanism in airborne weapon system separate connector |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108199190A CN108199190A (en) | 2018-06-22 |
| CN108199190B true CN108199190B (en) | 2019-10-18 |
Family
ID=62573614
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711263644.XA Active CN108199190B (en) | 2017-12-04 | 2017-12-04 | Four-bar mechanism in airborne weapon system separate connector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108199190B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108281827A (en) * | 2017-12-26 | 2018-07-13 | 中航光电科技股份有限公司 | Four-bar mechanism in separate connector |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102761022A (en) * | 2012-06-27 | 2012-10-31 | 华为技术有限公司 | Connecting rod device for plugging PCB (Printed Circuit Board) plate |
| CN203135093U (en) * | 2012-12-19 | 2013-08-14 | 李福青 | Connecting device for rapid replacing power battery of electric vehicle |
| CN103326183A (en) * | 2013-06-07 | 2013-09-25 | 南京航空航天大学 | Self-calibration electric coupler with buffer device |
| CN104716489A (en) * | 2013-12-11 | 2015-06-17 | 森萨塔科技麻省公司 | Socket |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWM278117U (en) * | 2005-05-12 | 2005-10-11 | Tyco Electronics Amp Kk | Card connector |
-
2017
- 2017-12-04 CN CN201711263644.XA patent/CN108199190B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102761022A (en) * | 2012-06-27 | 2012-10-31 | 华为技术有限公司 | Connecting rod device for plugging PCB (Printed Circuit Board) plate |
| CN203135093U (en) * | 2012-12-19 | 2013-08-14 | 李福青 | Connecting device for rapid replacing power battery of electric vehicle |
| CN103326183A (en) * | 2013-06-07 | 2013-09-25 | 南京航空航天大学 | Self-calibration electric coupler with buffer device |
| CN104716489A (en) * | 2013-12-11 | 2015-06-17 | 森萨塔科技麻省公司 | Socket |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108199190A (en) | 2018-06-22 |
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