CN106225570A - A kind of adapter self adaptation plugs together device - Google Patents
A kind of adapter self adaptation plugs together device Download PDFInfo
- Publication number
- CN106225570A CN106225570A CN201610687132.5A CN201610687132A CN106225570A CN 106225570 A CN106225570 A CN 106225570A CN 201610687132 A CN201610687132 A CN 201610687132A CN 106225570 A CN106225570 A CN 106225570A
- Authority
- CN
- China
- Prior art keywords
- plug
- guided missile
- connecting rod
- quadric chain
- self adaptation
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F7/00—Launching-apparatus for projecting missiles or projectiles otherwise than from barrels, e.g. using spigots
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The present invention relates to a kind of adapter self adaptation and plug together device, it is achieved being certainly dynamically connected and separating between guided missile with firing box, comprise: quadric chain, be fixedly installed on firing box by mounting seat；Interlinked mechanism, connects and is arranged between quadric chain and guided missile；Plug, is fixedly installed on described quadric chain；Socket, is fixedly installed on described guided missile, and the position of this socket is corresponding with the position of plug；When missile loading or transmitting, the plug on quadric chain is driven to plug together with being arranged on missile-borne socket self adaptation or be automatically separated by interlinked mechanism.The present invention can not utilize any external force, and only rely on guided missile displacement and provide in the case of power, adaptive completes plugging together or separating of guided missile and firing box, simple in construction, has high reliability.
Description
Technical field
The present invention relates to one and plug together device, specifically refer to a kind of self adaptation for guided missile adapter and plug together device.
Background technology
In prior art, guided missile carries out detecting, powering all by pull-off plug and socket realization in firing box.Socket footpath
To being arranged on guided missile, plug is arranged on the upper connecting rod of the quadric chain of firing box.During MISSILE LAUNCHING, by driving plug
On guide finger, make the connecting rod of quadric chain both sides move forward and downward, thus realize plug and separate with socket.
But, due to assembly crewman need in narrow and small installing space by manual realize on quadric chain plug with
The centering of socket on bullet, plugging together and install fixing, therefore there is working performance low, poor reliability, the work of assembly crewman is strong
The problems such as degree is big.
Based on above-mentioned, need a kind of self adaptation for guided missile adapter of proposition at present badly and plug together device.
Summary of the invention
It is an object of the invention to provide a kind of adapter self adaptation and plug together device, any external force can not utilized, and only depend on
There is provided in the case of power by guided missile displacement, adaptive complete plugging together or separating of guided missile and firing box, simple in construction,
There is high reliability.
For achieving the above object, the present invention provides a kind of adapter self adaptation to plug together device, it is achieved guided missile and firing box it
Between be certainly dynamically connected and separate, comprise: quadric chain, be fixedly installed on firing box by mounting seat；Interlinked mechanism, even
Connect and be arranged between quadric chain and guided missile；Plug, is fixedly installed on described quadric chain；Socket, is fixedly installed
On described guided missile, and the position of this socket is corresponding with the position of plug；When missile loading or transmitting, by interlocking machine
Structure drives the plug on quadric chain to plug together with being arranged on missile-borne socket self adaptation or be automatically separated.
Described interlinked mechanism comprises: guide rail, and it is arranged on described firing box；Slide block, it is arranged on described
In guide rail, can be along slide；Front-slider, its one end is fixedly connected on the front bottom end of described guided missile, and the other end is arranged on
In described guide rail, can be along slide；Rear slider, its one end is fixedly connected on bottom the rear end of described guided missile, the other end
It is arranged in described guide rail, can be along slide, and the position that this rear slider is between slide block and front-slider；Tiltedly connect
Bar, its one end is connected with described slide block, can be around the axis rotation that turns of this slide block, the other end and described quadric chain
Connect.
Described quadric chain comprises: the first side connecting rod, and its bottom is connected with described mounting seat, can be around installing the end
First turn of axis rotation of seat, top is connected with the other end of described diagonal control arm so that diagonal control arm can around it with the first side even
What bar was connected turns axis rotation；Second side connecting rod, its bottom is connected with described mounting seat, can be around the second of mounting seat turn
Axis rotation；Upper connecting rod, its two ends connect top and the top of the second side connecting rod of the first side connecting rod, and described inserting respectively
Head is fixedly installed on this on connecting rod.
The both sides of described plug are also respectively symmetrically and are provided with guide finger, and it is fixedly installed on described upper connecting rod；Institute
The both sides of the socket stated also are respectively symmetrically and are provided with guide pin hole, and it is fixedly installed on described guided missile, and each guide finger
The position in hole is corresponding with the position of each guide finger.
Adapter self adaptation of the present invention plugs together device, also comprises resetting-mechanism, and its connection is arranged on described four
Between linkage and mounting seat, during MISSILE LAUNCHING, after plug and socket are automatically separated, reset and fix double leval jib machine
Structure.
Described resetting-mechanism comprises: hangs spring screw, is respectively fixedly disposed in mounting seat for two, and double leval jib machine
On second side connecting rod of structure；Back-moving spring, two ends are hung on the extension spring screw of correspondence respectively by hook；Buffer stopper, fixing
It is arranged in mounting seat, and is positioned at the lower section of back-moving spring.
When guided missile loads against course, guided missile is slided in guide rail by front-slider and rear slider, and promotes slide block edge
Guide rail slides against course, and the first side connecting rod and the second side connecting rod by diagonal control arm drive quadric chain are rotating around mounting seat
The first rotating shaft heart and the second rotating shaft heart rotate against course, make connecting rod against course translation, and drive plug upwards and inverse course
Motion, makes guide finger correspondence be inserted in guide pin hole, and after guiding a segment distance, makes plug be inserted into socket interior to realize
Self adaptation plugs together.
When guided missile is launched along course, under the promotion of missile flight power, drive quadric chain the first side connecting rod and
Second side connecting rod rotates along course rotating around the first rotating shaft heart and the second rotating shaft heart of mounting seat, makes connecting rod flat along course
Dynamic, and drive plug downwards and to move along course, and after guided missile runs a segment distance, come out of the socket plug to realize
It is automatically separated.
When guided missile is launched along course, after plug separates with socket, quadric chain is at buffer stopper and back-moving spring
Reset under effect and fix.
In sum, adapter self adaptation of the present invention plugs together device, compared with prior art, has following useful
Effect: be spatially to float to arrange due to plug, any external force (such as hydraulic system) can not utilized, and only rely on and lead
Play displacement to provide in the case of power, adaptive complete between socket plugging together or separating；Therefore simple in construction, can
Lean on, non-maintaining, eliminate the uncertain factor of artificial plug, improve and plug together precision and efficiency, significantly reduce assembly crewman
Working strength.
Accompanying drawing explanation
Fig. 1 is the structural representation that the adapter self adaptation of the present invention plugs together when the plug of device separates with socket；
Fig. 2 is the structural representation that the adapter self adaptation of the present invention plugs together when the plug of device is connected with socket.
Detailed description of the invention
Below in conjunction with Fig. 1～Fig. 2, describe a preferred embodiment of the present invention in detail.
As depicted in figs. 1 and 2, the adapter self adaptation provided for the present invention plugs together device, it is achieved guided missile 11 and firing box
Being certainly dynamically connected and separating between 12, comprises: quadric chain 3, is fixedly installed on firing box 12 by mounting seat 15；Even
Motivation structure, connects and is arranged between quadric chain 3 and guided missile 11；Plug 2, is fixedly installed on described quadric chain 3；
Socket 9, is fixedly installed on described guided missile 11, and the position of this socket 9 is corresponding with the position of plug 2；Fill at guided missile 11
When filling out or launch, drive the plug 2 on quadric chain 3 and socket 9 self adaptation being arranged on guided missile 11 by interlinked mechanism
Plug together or be automatically separated.
Described interlinked mechanism comprises: guide rail 8, is arranged on described firing box 12；Slide block 13, it is arranged on described
Guide rail 8 in, can slide along guide rail 8；Front-slider 6, its one end is fixedly connected on the front bottom end of described guided missile 11, the other end
It is arranged in described guide rail 8, can slide along guide rail 8；Rear slider 7, its one end is fixedly connected on the rear end of described guided missile 11
Bottom, the other end is arranged in described guide rail 8, can slide along guide rail 8, and this rear slider 7 is positioned at slide block 13 and front-slider 6
Between position；Diagonal control arm 1, its one end is connected with described slide block 13, can rotate around the rotating shaft heart E of this slide block 13, separately
One end is connected with described quadric chain 3.
Described quadric chain 3 comprises: the first side connecting rod 31, and its bottom is connected with described mounting seat 15, can be around
First rotating shaft heart D of mounting seat 15 rotates, and top is connected with the other end of described diagonal control arm 1 so that diagonal control arm 1 can be around it
The rotating shaft heart C being connected with the first side connecting rod 31 rotates；Second side connecting rod 32, its bottom is connected with described mounting seat 15, can
Rotate around the second rotating shaft heart A of mounting seat 15；Upper connecting rod 33, its two ends connect the top and of the first side connecting rod 31 respectively
The top of two side connecting rods 32, and described plug 2 is fixedly installed on this on connecting rod 33.
The both sides of described plug 2 are also respectively symmetrically and are provided with guide finger 5, and it is fixedly installed on described upper connecting rod 33
On；The both sides of described socket 9 are also respectively symmetrically and are provided with guide pin hole 10, and it is fixedly installed on described guided missile 11, and
The position of each guide pin hole 10 is corresponding with the position of each guide finger 5.
Adapter self adaptation of the present invention plugs together device, also comprises resetting-mechanism, and its connection is arranged on described four
Between linkage 3 and mounting seat 15, when guided missile 11 is launched, after plug 2 and socket 9 are automatically separated, reset and fix four
Linkage 3.
Described resetting-mechanism comprises: hangs spring screw 16, is respectively fixedly disposed in mounting seat 15 for two, and four connect
On second side connecting rod 32 of linkage 3；Back-moving spring 14, two ends are hung on the extension spring screw 16 of correspondence respectively by hook；
Buffer stopper 4, is fixedly installed in mounting seat 15, and is positioned at the lower section of back-moving spring 14.
In the present embodiment, described buffer stopper 4 uses elastomeric material to make.
As depicted in figs. 1 and 2, in figure, top arrow to the left represents the course of guided missile 11.When guided missile 11 loads against course
Time, guided missile 11 is slided in guide rail 8 by front-slider 6 and rear slider 7, is loaded in firing box 12.When rear slider 7 is sliding
During when touching slide block 13, promote slide block to slide along guide rail 8 along inverse course (to the right) simultaneously.Now at slide block 13
Drive under so that diagonal control arm 1 drives the first side connecting rod 31 of quadric chain 3 and the second side connecting rod 32 rotating around mounting seat
The first rotating shaft heart D and the second rotating shaft heart A of 15 rotates along inverse course (to the right), and in drive, connecting rod 33 is put down along inverse course (to the right)
Dynamic, thus drive plug 2 upwards and move along inverse course (to the right), make guide finger 5 correspondence be inserted in guide pin hole 10, and
After guiding a segment distance, plug 2 is made to be inserted in socket 9.As in figure 2 it is shown, when guided missile 11 stop motion, plug 2 is the most slotting
Enter in socket 9, it is achieved self adaptation plugs together, it is ensured that signal conduction.
When guided missile 11 is launched along course, under the promotion of guided missile 11 flight forces so that the first side of quadric chain 3 is even
Bar 31 and the second side connecting rod 32 rotate along course (to the left) rotating around the first rotating shaft heart D and the second rotating shaft heart A of mounting seat 15,
In drive, connecting rod 33 is along course (to the left) translation, thus drives plug 2 downwards and move along course (to the left), and transports at guided missile 11
After row one segment distance, as it is shown in figure 1, plug 2 is extracted from socket 9, it is achieved be automatically separated.Further, quadric chain 3 is slow
Rush and reset under the effect of block 4 and back-moving spring 14 and fix.
The adapter self adaptation that the present invention provides plugs together device, and when socket has 12 extreme positions, plug remains to reality
Existing the most adaptive automatically plug together and separate, and plug not looper can be reached, do not interfere the effect of Missile Motion, it is ensured that even
Connect device self adaptation and plug together the reliability of device.
Although present disclosure has been made to be discussed in detail by above preferred embodiment, but it should be appreciated that above-mentioned
Description is not considered as limitation of the present invention.After those skilled in the art have read foregoing, for the present invention's
Multiple amendment and replacement all will be apparent from.Therefore, protection scope of the present invention should be limited to the appended claims.
Claims (9)
1. an adapter self adaptation plugs together device, it is achieved being certainly dynamically connected and separating between guided missile (11) with firing box (12),
It is characterized by comprising:
Quadric chain (3), is fixedly installed on firing box (12) by mounting seat (15)；
Interlinked mechanism, connects and is arranged between quadric chain (3) and guided missile (11)；
Plug (2), is fixedly installed on described quadric chain (3)；
Socket (9), is fixedly installed on described guided missile (11), and the position of this socket (9) is relative with the position of plug (2)
Should；
When guided missile (11) loads or launches, the plug (2) on quadric chain (3) is driven to lead with being arranged on by interlinked mechanism
Socket (9) self adaptation on bullet (11) plugs together or is automatically separated.
2. adapter self adaptation as claimed in claim 1 plugs together device, it is characterised in that described interlinked mechanism comprises:
Guide rail (8), it is arranged on described firing box (12)；
Slide block (13), it is arranged in described guide rail (8), can slide along guide rail (8)；
Front-slider (6), its one end is fixedly connected on the front bottom end of described guided missile (11), and the other end is arranged on described guide rail
(8), in, can slide along guide rail (8)；
Rear slider (7), its one end is fixedly connected on bottom the rear end of described guided missile (11), and the other end is arranged on described guide rail
(8), in, can slide along guide rail (8), and this rear slider (7) is positioned at the position between slide block (13) and front-slider (6)；
Diagonal control arm (1), its one end is connected with described slide block (13), can turn axis rotation around this slide block (13), another
End is connected with described quadric chain (3).
3. adapter self adaptation as claimed in claim 2 plugs together device, it is characterised in that described quadric chain (3) bag
Contain:
First side connecting rod (31), its bottom is connected with described mounting seat (15), can be around the first rotating shaft of mounting seat (15)
The heart rotates, and top is connected with the other end of described diagonal control arm (1) so that diagonal control arm (1) can be around itself and the first side connecting rod (31)
Be connected turns axis rotation；
Second side connecting rod (32), its bottom is connected with described mounting seat (15), can be around the second rotating shaft of mounting seat (15)
The heart rotates；
Upper connecting rod (33), its two ends connect top and the top of the second side connecting rod (32) of the first side connecting rod (31) respectively, and
Described plug (2) is fixedly installed on connecting rod on this (33).
4. adapter self adaptation as claimed in claim 3 plugs together device, it is characterised in that the both sides of described plug (2) are also
Being respectively symmetrically and be provided with guide finger (5), it is fixedly installed on described upper connecting rod (33)；
The both sides of described socket (9) are also respectively symmetrically and are provided with guide pin hole (10), and it is fixedly installed on described guided missile
(11) on, and the position of each guide pin hole (10) is corresponding with the position of each guide finger (5).
5. adapter self adaptation as claimed in claim 3 plugs together device, it is characterised in that also comprise resetting-mechanism, and it connects
It is arranged between described quadric chain (3) and mounting seat (15), when guided missile (11) is launched, when plug (2) and socket (9)
After being automatically separated, reset and fix quadric chain (3).
6. adapter self adaptation as claimed in claim 5 plugs together device, it is characterised in that described resetting-mechanism comprises:
Hang spring screw (16), be respectively fixedly disposed in mounting seat (15) for two, and the second side of quadric chain (3) is even
On bar (32)；
Back-moving spring (14), two ends are hung on extension spring screw (16) of correspondence respectively by hook；
Buffer stopper (4), is fixedly installed in mounting seat (15), and is positioned at the lower section of back-moving spring (14).
7. adapter self adaptation as claimed in claim 4 plugs together device, it is characterised in that when the inverse course of guided missile (11) is loaded
Time, guided missile (11) is slided in guide rail (8) by front-slider (6) and rear slider (7), and promotes slide block (13) along guide rail (8)
Slide in inverse course, driven the first side connecting rod (31) and the second side connecting rod (32) difference of quadric chain (3) by diagonal control arm (1)
The first rotating shaft heart and the second rotating shaft heart around mounting seat (15) rotate against course, make the inverse course translation of connecting rod (33), and carry
Dynamic plug (2) is upwards and moves in inverse course, makes guide finger (5) correspondence be inserted in guide pin hole (10), and guide one section away from
From rear, make plug (2) be inserted in socket (9) realizing self adaptation and plug together.
8. adapter self adaptation as claimed in claim 6 plugs together device, it is characterised in that when guided missile (11) is launched along course
Time, under the promotion of guided missile (11) flight forces, drive the first side connecting rod (31) and the second side connecting rod (32) of quadric chain (3)
Rotate along course rotating around the first rotating shaft heart of mounting seat (15) and the second rotating shaft heart, make connecting rod (33) along course translation,
And drive plug (2) downwards and to move along course, and after guided missile (11) runs a segment distance, by plug (2) from socket (9)
Extract to realize being automatically separated.
9. adapter self adaptation as claimed in claim 8 plugs together device, it is characterised in that when guided missile (11) is launched along course
Time, after plug (2) separates with socket (9), quadric chain (3) is multiple under the effect of buffer stopper (4) and back-moving spring (14)
Position is also fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610687132.5A CN106225570B (en) | 2016-08-18 | 2016-08-18 | A kind of connector adaptively plugs together device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610687132.5A CN106225570B (en) | 2016-08-18 | 2016-08-18 | A kind of connector adaptively plugs together device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106225570A true CN106225570A (en) | 2016-12-14 |
| CN106225570B CN106225570B (en) | 2017-11-24 |
Family
ID=57553982
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610687132.5A Active CN106225570B (en) | 2016-08-18 | 2016-08-18 | A kind of connector adaptively plugs together device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106225570B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107785718A (en) * | 2017-10-25 | 2018-03-09 | 洛阳瑞极光电科技有限公司 | Umbilical cable plug-in and pull-off device |
| CN110635309A (en) * | 2019-08-20 | 2019-12-31 | 西安航天动力技术研究所 | Guide rail type retractable separating mechanism |
| CN111426242A (en) * | 2020-04-14 | 2020-07-17 | 上海机电工程研究所 | Guided missile fixing mechanism |
| CN111521064A (en) * | 2020-04-02 | 2020-08-11 | 上海机电工程研究所 | Multi-degree-of-freedom constraint auxiliary supporting device for reverse-launched missile |
| CN111664746A (en) * | 2020-05-15 | 2020-09-15 | 上海机电工程研究所 | Temperature self-adaption device for joint mounting interface of launching box |
| CN113237395A (en) * | 2021-04-26 | 2021-08-10 | 上海机电工程研究所 | Bullet fixing device based on lever mechanism |
| CN113983878A (en) * | 2021-11-04 | 2022-01-28 | 上海机电工程研究所 | Dynamic and static combined missile single lifting mechanical separation test device |
| CN114485262A (en) * | 2022-01-29 | 2022-05-13 | 重庆零壹空间航天科技有限公司 | System for guided missile inclined launching reliability verification |
| CN114719675A (en) * | 2022-03-09 | 2022-07-08 | 上海机电工程研究所 | Plug-in mechanism and solid bullet ware synchronous unlocking mechanism |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3610091A (en) * | 1968-02-08 | 1971-10-05 | Transurvey Holding Co Inc | Ballistic device comprising a projectile and its launcher |
| EP0425758A1 (en) * | 1989-09-29 | 1991-05-08 | ERICH JÄGER GmbH & Co. KG | Electrical connecting system of a socket of a multipole connecting device |
| CN201897436U (en) * | 2010-11-10 | 2011-07-13 | 湖北航天技术研究院总体设计所 | Locking mechanism between launch canister and launching beam |
| CN103528439A (en) * | 2013-10-12 | 2014-01-22 | 江西新余国科科技有限公司 | Precipitation Rain enhancement hail prevention rocket launcher |
-
2016
- 2016-08-18 CN CN201610687132.5A patent/CN106225570B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3610091A (en) * | 1968-02-08 | 1971-10-05 | Transurvey Holding Co Inc | Ballistic device comprising a projectile and its launcher |
| EP0425758A1 (en) * | 1989-09-29 | 1991-05-08 | ERICH JÄGER GmbH & Co. KG | Electrical connecting system of a socket of a multipole connecting device |
| CN201897436U (en) * | 2010-11-10 | 2011-07-13 | 湖北航天技术研究院总体设计所 | Locking mechanism between launch canister and launching beam |
| CN103528439A (en) * | 2013-10-12 | 2014-01-22 | 江西新余国科科技有限公司 | Precipitation Rain enhancement hail prevention rocket launcher |
Non-Patent Citations (1)
| Title |
|---|
| 冯斌: ""插头对接机构的动力学仿真分析"", 《机械工程师》 * |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107785718A (en) * | 2017-10-25 | 2018-03-09 | 洛阳瑞极光电科技有限公司 | Umbilical cable plug-in and pull-off device |
| CN107785718B (en) * | 2017-10-25 | 2024-03-12 | 洛阳瑞极光电科技有限公司 | Umbilical cable plugging device |
| CN110635309A (en) * | 2019-08-20 | 2019-12-31 | 西安航天动力技术研究所 | Guide rail type retractable separating mechanism |
| CN111521064A (en) * | 2020-04-02 | 2020-08-11 | 上海机电工程研究所 | Multi-degree-of-freedom constraint auxiliary supporting device for reverse-launched missile |
| CN111521064B (en) * | 2020-04-02 | 2022-04-01 | 上海机电工程研究所 | Multi-degree-of-freedom constraint auxiliary supporting device for reverse-launched missile |
| CN111426242A (en) * | 2020-04-14 | 2020-07-17 | 上海机电工程研究所 | Guided missile fixing mechanism |
| CN111664746B (en) * | 2020-05-15 | 2022-07-12 | 上海机电工程研究所 | Temperature self-adaption device for joint mounting interface of launching box |
| CN111664746A (en) * | 2020-05-15 | 2020-09-15 | 上海机电工程研究所 | Temperature self-adaption device for joint mounting interface of launching box |
| CN113237395A (en) * | 2021-04-26 | 2021-08-10 | 上海机电工程研究所 | Bullet fixing device based on lever mechanism |
| CN113237395B (en) * | 2021-04-26 | 2022-11-08 | 上海机电工程研究所 | Bullet fixing device based on lever mechanism |
| CN113983878A (en) * | 2021-11-04 | 2022-01-28 | 上海机电工程研究所 | Dynamic and static combined missile single lifting mechanical separation test device |
| CN114485262A (en) * | 2022-01-29 | 2022-05-13 | 重庆零壹空间航天科技有限公司 | System for guided missile inclined launching reliability verification |
| CN114485262B (en) * | 2022-01-29 | 2024-03-29 | 重庆零壹空间航天科技有限公司 | System for verifying missile oblique launching reliability |
| CN114719675A (en) * | 2022-03-09 | 2022-07-08 | 上海机电工程研究所 | Plug-in mechanism and solid bullet ware synchronous unlocking mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106225570B (en) | 2017-11-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106225570B (en) | A kind of connector adaptively plugs together device | |
| CN106458315A (en) | Actuator for controlling a horizontal stabiliser of an aircraft | |
| CN105953647B (en) | A kind of floating installation of firing box plug inserting and withdrawing mechanism | |
| EP2604512A3 (en) | Translating cable device sealing | |
| CN102363444B (en) | Transverse folding mechanism for empennage | |
| CN204179360U (en) | To charge under water bindiny mechanism | |
| CN105443050A (en) | Petroleum drilling and exploitation device, automatic pipe discharging device and tubular column supporting mechanism | |
| CN110035156A (en) | A kind of terminal device | |
| CN205906206U (en) | Wing connecting device , wing and aircraft | |
| CN201897436U (en) | Locking mechanism between launch canister and launching beam | |
| CN213392040U (en) | Spacing bolt and applied drilling rod manipulator of this spacing bolt | |
| CN105803653A (en) | Needle selection cam control mechanism in flat knitting machine base plate | |
| CN205503044U (en) | Oil drilling equipment , automatic calandria device and tubular column support mechanism | |
| CN110095314A (en) | A kind of visualization hardground box corer | |
| CN105480425A (en) | Mechanical arm supplement connecting device between aircrafts | |
| CN204015643U (en) | Slide rail stop configurations | |
| CN110641706B (en) | Combined unmanned aerial vehicle unit based on folding combination form and combination method thereof | |
| CN107565304A (en) | The kinetic energy separating mechanism of emitter hot-line insertion and extraction mechanism | |
| CN208531948U (en) | A kind of cable reel hand arrangement of clutch | |
| CN209409671U (en) | A kind of mechanical arm plotting unit | |
| CN112253018B (en) | Drill rod manipulator of spacing bolt and applied this spacing bolt | |
| CN106542111A (en) | It is applied to the unmanned plane fixing device of unmanned plane transmitting | |
| CN207142279U (en) | Shot terminal feed mechanism | |
| CN209198585U (en) | A kind of wiring harness test jig | |
| CN210220831U (en) | Direct-ejection type ejection device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |