CN108258519A - The plane relocation mechanism of separate connector in airborne weapon system - Google Patents
The plane relocation mechanism of separate connector in airborne weapon system Download PDFInfo
- Publication number
- CN108258519A CN108258519A CN201711264102.4A CN201711264102A CN108258519A CN 108258519 A CN108258519 A CN 108258519A CN 201711264102 A CN201711264102 A CN 201711264102A CN 108258519 A CN108258519 A CN 108258519A
- Authority
- CN
- China
- Prior art keywords
- locking
- sleeve
- float plate
- guide rod
- axle sleeve
- 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.)
- Granted
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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
- H01R13/629—Additional means for facilitating engagement or disengagement of coupling parts, e.g. aligning or guiding means, levers, gas pressure electrical locking indicators, manufacturing tolerances
- H01R13/62905—Additional means for facilitating engagement or disengagement of coupling parts, e.g. aligning or guiding means, levers, gas pressure electrical locking indicators, manufacturing tolerances comprising a camming member
- H01R13/62916—Single camming plate
-
- 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
Landscapes
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The plane relocation mechanism of separate connector in airborne weapon system, belong to mechanical designing technique, more particularly to a kind of novel Purely mechanical, plane relocation mechanism can be touched, mainly it is made of parts such as pedestal, shell, guide rod, guide sleeve, rotation cam, locking sleeve, locking end cap, locking spring, locking axle sleeve, locking steel ball, retaining ring, float plate, power springs, designed by the present invention is a kind of novel Purely mechanical, can touch plane relocation mechanism, it solves the problems, such as that separate connector is plugged together and locked, has widened the separate connector scope of application.
Description
Technical field
The invention belongs to mechanical designing techniques, and in particular to a kind of novel Purely mechanical can touch plane relocation mechanism.
Background technology
Separate connector in airborne weapon system often will appear following situations in use：Connector separation shaft
Line is vertical with body course, and connector is direct-plug structure, itself does not have locking function.To ensure connector signal transmission
It is reliable with separation, a kind of novel planar relocation mechanism is needed to complete the variation and fixation of connector position, while using process
In the demand of additional power supply is not brought to emission system and body.
Invention content
The purpose of the present invention is：
It proposes a kind of novel Purely mechanical, plane relocation mechanism can be touched, solve the problems, such as that separate connector is plugged together and locked,
The separate connector scope of application is widened.
Technical scheme of the present invention：
The plane relocation mechanism of separate connector is mainly by pedestal 1, shell 2, guide rod 3, guiding in airborne weapon system
Set 4, locking sleeve 6, locking end cap 7, locking spring 8, locking axle sleeve 9, locking steel ball 10, retaining ring 11, floats at rotation cam 5
The parts such as movable plate 12, power spring 13 form.
Locking axle sleeve 9 is mounted in 6 lower end of locking sleeve, and locking end cap 7 is mounted in 6 upper end of locking sleeve, and locking spring 8 is loaded on lock
In the cavity that mandrel set 9 and locking sleeve 6 are formed, steel ball is locked in one end against locking axle sleeve 9, the other end against locking end cap 7
10 are stuck in by retaining ring 11 between locking axle sleeve 9 and locking sleeve 6, and composition can touch locking member.
Pedestal 1 fills integral with shell 2, can touch locking member on the shell 2, guide rod 3 is mounted on pedestal 1
On, guide sleeve 4, retaining ring 11 are fixed in float plate 12, make whole, form float plate assembly, float plate assembly dress
It on guide rod 3, can move up and down along guide rod 3, the guiding parts that pedestal 1 and guide rod 3 are formed can ensure float plate
It is moved according to desired trajectory；Such as Fig. 1.
Rotation cam 5 by the way that spanner class tool is assisted to apply torsional forces to rotation cam 5 during use, turns loaded on shell 2
Moving cam 5 forms power transmission member, realizes float plate shift in position.
Locking steel ball 10 is in retaining ring 11 and locking sleeve 6, and the presence of locking axle sleeve 9 and locking spring 8 to lock
Tight 10 position of steel ball remains unchanged, and float plate assembly is remained unchanged relative to pedestal 1,2 position of shell at this time, indirectly realizes peace
Structural member position in float plate 12 remains unchanged.When detachment is desired, along arrow direction shown in Fig. 1 to locking axle sleeve 9
Apply mechanical force, locking axle sleeve 9 moves in the direction of the arrow under mechanical force, compresses locking spring 8 at this time.Work as locking axle sleeve
9 when moving to position shown in Fig. 2, and locking steel ball 10, which will obtain enough spaces, makes it be no longer on retaining ring 11 and locking
Between casing 6, at this time under the effect of power spring 13, float plate assembly will be moved quickly in the direction of the arrow, direct mechanical position limitation.
When needing to reuse, torsional forces is applied to rotation cam 5 using auxiliary spanner class tool, passes through rotation cam
5 realize the conversion of torsional forces and straight thrust, and when float plate assembly moves to position shown in Fig. 1, locking steel ball 10 is in locking bullet
Spring 13 is again under acting between retaining ring 11 and locking sleeve 6, and float plate assembly position is fixed again.
Beneficial effects of the present invention：
Designed by the present invention is a kind of novel Purely mechanical, can touch plane relocation mechanism, solves separate connector and inserts
Problem is closed and locked, has widened the separate connector scope of application.
Description of the drawings
Fig. 1 is when the plane relocation mechanism of separate connector in airborne weapon system of the present invention is in locking state
Structure diagram；
Fig. 2 is when the plane relocation mechanism of separate connector in airborne weapon system of the present invention is in discrete state
Structure diagram；
In figure, 1- pedestals, 2- shells, 3- guide rods, 4- guide sleeves, 5- rotation cams, 6- locking sleeves, 7- locking ends
Lid, 8- locking springs, 9- locking axle sleeves, 10- locking steel ball, 11- retaining rings, 12- float plates, 13- power springs.
Specific embodiment
In a kind of airborne weapon system the plane relocation mechanism of separate connector mainly by pedestal 1, shell 2, guide rod 3,
Guide sleeve 4, rotation cam 5, locking sleeve 6, locking end cap 7, locking spring 8, locking axle sleeve 9, locking steel ball 10, retaining ring
11st, the parts such as float plate 12, power spring 13 form.Locking sleeve 6, locking end cap 7, locking spring 8,9 and of locking axle sleeve
The locking composition of steel ball 10 can touch locking member, control float plate location status；Pedestal 1 and guide rod 3 form guiding parts, protect
Card float plate is moved according to desired trajectory；Rotation cam 5 forms power transmission member, realizes float plate shift in position；Guide sleeve
4th, retaining ring 11 and float plate 12 form float plate assembly.
Locking member is mounted on shell 2, and guide rod 3 is mounted on pedestal 1, and it is whole that pedestal 1 with shell 2 may be mounted to one
Body.Guide sleeve 4, retaining ring 11 are fixed in float plate 12, make whole, form float plate assembly, therefore floating plate portion
Part can move up and down along guide rod 3.Such as Fig. 1, locking steel ball 10 is in retaining ring 11 and locking sleeve 6,9 He of locking axle sleeve
The presence of locking spring 8 so that locking 10 position of steel ball remains unchanged, and float plate assembly is relative to pedestal 1,2 position of shell at this time
It remains unchanged, indirectly realizes that the structural member position being mounted in float plate 12 remains unchanged.When detachment is desired, along Fig. 1 institutes
Show that arrow direction applies mechanical force to locking axle sleeve 9, locking axle sleeve 9 moves in the direction of the arrow under mechanical force, presses at this time
Contracting locking spring 8.When locking axle sleeve 9 moves to position shown in Fig. 2, locking steel ball 10 makes it by enough spaces are obtained
It is no longer between retaining ring 11 and locking sleeve 6, at this time under the effect of power spring 13, float plate assembly will be quickly along arrow
Direction moves, direct mechanical position limitation.When needing to reuse, torque is applied to rotation cam 5 using auxiliary spanner class tool
Power realizes the conversion of torsional forces and straight thrust by rotation cam 5, when float plate assembly moves to position shown in Fig. 1, locking
Steel ball 10 is again under the effect of locking spring 13 between retaining ring 11 and locking sleeve 6, and float plate assembly position is solid again
It is fixed.
Claims (1)
1. the plane relocation mechanism of separate connector in airborne weapon system including pedestal (1), shell (2), guide rod (3), is led
To set (4), rotation cam (5), locking sleeve (6), locking end cap (7), locking spring (8), locking axle sleeve (9), locking steel ball
(10), retaining ring (11), float plate (12), power spring (13), it is characterised in that：Locking axle sleeve (9) is mounted in locking sleeve (6)
Lower end, locking end cap (7) is mounted in locking sleeve (6) upper end, and locking spring (8) is loaded on locking axle sleeve (9) and locking sleeve (6) structure
Into cavity in, against locking axle sleeve (9), the other end passes through retaining ring against locking end cap (7), locking steel ball (10) for one end
(11) it is stuck between locking axle sleeve (9) and locking sleeve (6), composition can touch locking member；Pedestal (1) is dressed up with shell (2)
One is whole, can touch locking member on shell (2), and guide rod (3) is on pedestal (1), guide sleeve (4), locking
Ring (11) is fixed in float plate (12), makes whole, forms float plate assembly, and float plate assembly is loaded on guide rod (3)
On, can move up and down along guide rod (3), the guiding parts that pedestal (1) and guide rod (3) are formed can ensure float plate according to
Desired trajectory moves；Rotation cam (5) is loaded on shell (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711264102.4A CN108258519B (en) | 2017-12-04 | 2017-12-04 | The plane relocation mechanism of separate connector in airborne weapon system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711264102.4A CN108258519B (en) | 2017-12-04 | 2017-12-04 | The plane relocation mechanism of separate connector in airborne weapon system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108258519A true CN108258519A (en) | 2018-07-06 |
| CN108258519B CN108258519B (en) | 2019-11-15 |
Family
ID=62722110
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711264102.4A Active CN108258519B (en) | 2017-12-04 | 2017-12-04 | The plane relocation mechanism of separate connector in airborne weapon system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108258519B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108598800A (en) * | 2017-12-26 | 2018-09-28 | 中航光电科技股份有限公司 | The plane relocation mechanism of separate connector |
| CN111653901A (en) * | 2020-06-18 | 2020-09-11 | 贵州航天电器股份有限公司 | Automatic separating mechanism |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201008048Y (en) * | 2006-11-02 | 2008-01-16 | 贵州航天电器股份有限公司 | Minisize fast locking and separation electric connector |
| CN201833026U (en) * | 2010-09-30 | 2011-05-18 | 芜湖日升重型机床有限公司 | Positioning device for boring lathe headstock |
| CN102957044A (en) * | 2012-10-29 | 2013-03-06 | 中航光电科技股份有限公司 | Ejection mechanism and electric connector utilizing same |
| CN103618169A (en) * | 2013-11-14 | 2014-03-05 | 贵州航天电器股份有限公司 | Separable electric connector capable of electrically connecting shells |
-
2017
- 2017-12-04 CN CN201711264102.4A patent/CN108258519B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201008048Y (en) * | 2006-11-02 | 2008-01-16 | 贵州航天电器股份有限公司 | Minisize fast locking and separation electric connector |
| CN201833026U (en) * | 2010-09-30 | 2011-05-18 | 芜湖日升重型机床有限公司 | Positioning device for boring lathe headstock |
| CN102957044A (en) * | 2012-10-29 | 2013-03-06 | 中航光电科技股份有限公司 | Ejection mechanism and electric connector utilizing same |
| CN103618169A (en) * | 2013-11-14 | 2014-03-05 | 贵州航天电器股份有限公司 | Separable electric connector capable of electrically connecting shells |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108598800A (en) * | 2017-12-26 | 2018-09-28 | 中航光电科技股份有限公司 | The plane relocation mechanism of separate connector |
| CN111653901A (en) * | 2020-06-18 | 2020-09-11 | 贵州航天电器股份有限公司 | Automatic separating mechanism |
| CN111653901B (en) * | 2020-06-18 | 2021-10-01 | 贵州航天电器股份有限公司 | Automatic separating mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108258519B (en) | 2019-11-15 |
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