CN109178353B - Quick butt joint device of hasp type model aerospace system sensor - Google Patents
Quick butt joint device of hasp type model aerospace system sensor Download PDFInfo
- Publication number
- CN109178353B CN109178353B CN201811018684.2A CN201811018684A CN109178353B CN 109178353 B CN109178353 B CN 109178353B CN 201811018684 A CN201811018684 A CN 201811018684A CN 109178353 B CN109178353 B CN 109178353B
- Authority
- CN
- China
- Prior art keywords
- positioning
- hasp
- plate
- locking
- sensor
- 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.)
- Active
Links
- 210000001503 joint Anatomy 0.000 title claims abstract description 45
- 230000007246 mechanism Effects 0.000 claims abstract description 99
- 238000003032 molecular docking Methods 0.000 claims abstract description 37
- 238000009434 installation Methods 0.000 claims description 10
- 238000006073 displacement reaction Methods 0.000 abstract description 3
- 238000005457 optimization Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 238000003825 pressing Methods 0.000 description 2
- 238000007792 addition Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000003252 repetitive effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/646—Docking or rendezvous systems
Abstract
The invention relates to a docking device, in particular to a quick docking device of a hasp type model aerospace system sensor, which comprises a drawer type positioning support mechanism, a sensor docking mechanism, a hasp locking mechanism I and a hasp locking mechanism II, wherein the sensor docking mechanism is intermittently matched in the drawer type positioning support mechanism; the displacement of the lap strip moving towards the fixed locking end side of the hasp can be increased by upwards rotating the movable end of the hasp, so that the lap strip can be clamped on the corresponding fixed locking end of the hasp, the movable end of the hasp is pressed down to enable the lap strip to generate fastening force relative to the fixed locking end so that the drawer type positioning supporting mechanism and the sensor butt-joint mechanism complete quick butt joint, and the problems that all sensors in an aerospace system are complex to install and cannot be quickly installed and butted are solved.
Description
Technical Field
The invention relates to a butt joint device, in particular to a quick butt joint device of a hasp type model aerospace system sensor.
Background
With the rapid development of science and technology, various countries have been greatly promoting the deep application of science and technology in various industries, and the aerospace field has also gained high attention. With the rapid development of the aerospace industry, all countries can realize rapid and automatic installation and butt joint while pursuing that all parts of the aerospace system are installed to ensure the installation reliability, the installation efficiency of the sensor is greatly improved, and meanwhile, the installation precision is improved by depending on the designed positioning mechanism. According to the special requirements of the aerospace system on sensor docking, the rapid docking of the sensors needs to be realized by using a mechanical structure which is as simple as possible, the operation is simple, and the docking reliability can be ensured, which brings a difficult problem to the design of a docking scheme. At present, the method is limited in consideration of safety, most of butt joints of sensors depend on positioning and locking of bolts and nuts, manpower and material resources are consumed, efficiency is low, and positioning accuracy cannot be completely guaranteed.
Disclosure of Invention
The invention aims to provide a quick butt joint device for a hasp type model aerospace system sensor, which can solve the problems that all sensors in an aerospace system are complex to install and cannot be quickly installed and butted.
The purpose of the invention is realized by the following technical scheme:
the utility model provides a quick interfacing apparatus of hasp formula model aerospace system sensor, includes drawer type location support mechanism, sensor docking mechanism, hasp locking mechanism I and hasp locking mechanism II, sensor docking mechanism clearance fit is in drawer type location support mechanism, and last fixedly connected with hasp locking mechanism I of drawer type location support mechanism, the last fixedly connected with hasp locking mechanism II of sensor docking mechanism, I joint of hasp locking mechanism is on locking mechanism II.
As a further optimization of the technical scheme, the quick docking device for the hasp type model aerospace system sensor comprises a drawer type positioning and supporting mechanism, wherein the drawer type positioning and supporting mechanism comprises a positioning bottom plate, a positioning mounting plate and a positioning top plate, one end of the positioning bottom plate is fixedly connected to the lower end of the positioning mounting plate, one end of the positioning top plate is fixedly connected to the upper end of the positioning mounting plate, and the positioning bottom plate, the positioning mounting plate and the positioning top plate form a docking accommodating cavity.
As a further optimization of the technical scheme, the invention relates to a quick docking device for a hasp type model aerospace system sensor, wherein the sensor docking mechanism comprises a sensor docking body, a locking fixing plate and a mounting positioning plate, the locking fixing plate and the mounting positioning plate are respectively and fixedly connected to the upper end and the lower end of the sensor docking body, and the sensor docking body is in clearance fit with a docking accommodating cavity formed by a positioning bottom plate, a positioning mounting plate and a positioning top plate.
According to the technical scheme, the quick butt joint device of the hasp type model aerospace system sensor comprises three hasp locking mechanisms I, wherein each hasp locking mechanism I comprises a fixed base plate I, a connecting block, a hasp movable end and a lapping strip, the connecting block is fixedly connected to the fixed base plate I, one end of the hasp movable end is hinged to the fixed base plate I, the other end of the hasp movable end is rotatably connected with the lapping strip, and the two hasp locking mechanisms I are fixedly connected to the upper end of a positioning top plate, and the other fixing base plate I is fixedly connected to the lower end face of the positioning base plate.
As further optimization of the technical scheme, the invention discloses a quick butt joint device of a hasp type model aerospace system sensor, wherein a hasp locking mechanism II comprises two fixed base plates II and hasp fixed locking ends, the hasp fixed locking ends are fixedly connected to the fixed base plates II, the number of the hasp locking mechanisms II is three, two fixed base plates II are fixedly connected to locking fixed plates, the other fixed base plate II is fixedly connected to an installation positioning plate, and three straps are respectively clamped on the corresponding three fixed locking ends.
As a further optimization of the technical scheme, the drawer type positioning and supporting mechanism further comprises a positioning groove I and a positioning groove II, and the positioning groove I and the positioning groove II are respectively arranged on the positioning bottom plate and the positioning top plate.
As a further optimization of the technical scheme, the sensor docking mechanism of the invention further comprises a positioning block, the positioning block is fixedly connected to the locking fixing plate, the positioning block and the locking fixing plate are integrally formed, the positioning block is in clearance fit in the positioning groove II, and the mounting positioning plate is in clearance fit in the positioning groove I.
As a further optimization of the technical scheme, the quick butt joint device of the hasp type model aerospace system sensor further comprises an anti-falling baffle, wherein one end of the hasp fixing and locking end extends and inclines downwards to form the anti-falling baffle.
The quick butt joint device for the hasp type model aerospace system sensor has the advantages that:
according to the rapid butt joint device for the hasp type model aerospace system sensor, the displacement of the butt joint strip moving to the fixed locking end side of the hasp can be increased by upwards rotating the movable end of the hasp, so that the butt joint strip can be clamped on the corresponding fixed locking end of the hasp, and the butt joint strip can generate fastening force relative to the fixed locking end by downwards pressing the movable end of the hasp, so that the drawer type positioning and supporting mechanism and the sensor butt joint mechanism complete rapid butt joint, and the problems that all sensors in an aerospace system are complex to install and cannot be rapidly installed and butted are solved.
Drawings
The invention is described in further detail below with reference to the accompanying drawings and specific embodiments.
FIG. 1 is a schematic diagram of the overall structure of the rapid docking device for the sensor of the aerospace system;
FIG. 2 is a first structural diagram illustrating a connection process of the rapid sensor docking device of the aerospace system according to the present invention;
FIG. 3 is a schematic structural diagram II of a connection process of the rapid sensor docking device for an aerospace system according to the present invention;
FIG. 4 is a third schematic view of the connection process of the rapid sensor docking device of the aerospace system of the invention;
FIG. 5 is a schematic structural view of a drawer-type positioning and supporting mechanism of the present invention;
FIG. 6 is a first schematic structural diagram of a sensor docking mechanism of the present invention;
FIG. 7 is a second schematic structural view of a sensor docking mechanism of the present invention;
FIG. 8 is a schematic structural view of a buckle locking mechanism I of the present invention;
FIG. 9 is a first schematic structural view of a buckle locking mechanism II of the present invention;
fig. 10 is a second structural schematic diagram of a buckle locking mechanism II of the invention.
In the figure: a drawer type positioning support mechanism 1; positioning a bottom plate 1-1; positioning a groove I1-2; positioning the mounting plate 1-3; positioning a top plate 1-4; positioning grooves II 1-5; a sensor docking mechanism 2; a sensor interface 2-1; locking the fixing plate 2-2; 2-3 of a positioning block; installing a positioning plate 2-4; a hasp locking mechanism I3; a fixed base plate I3-1; 3-2 of a connecting block; a movable end 3-3 of the hasp; 3-4 of lapping strips; a hasp locking mechanism II 4; a fixed bottom plate II 4-1; the locking end 4-2 is fixed by a hasp; and 4-3 of an anti-drop baffle.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
Before describing the embodiments, to avoid repetitive language, it is explained that the "fixed connection" described below may be: the fixing device is fixed through modes such as bolt connection, welding and rivet connection, and technicians in the field can select different fixing and connecting modes according to different application scenes, and the fixing device is mainly used for fixing two parts.
The first embodiment is as follows:
the embodiment is described below with reference to fig. 1 to 10, and the rapid docking device for the hasp type model aerospace system sensor comprises a drawer type positioning support mechanism 1, a sensor docking mechanism 2, a hasp locking mechanism i 3 and a hasp locking mechanism ii 4, wherein the displacement of the strap 3-4 moving to the hasp fixing locking end 4-2 side can be increased by rotating the hasp movable end 3-3 upwards, so that the strap 3-4 can be clamped on the corresponding hasp fixing locking end 4-2, and the strap 3-4 can generate fastening force relative to the fixing locking end by pressing the hasp movable end 3-3 downwards to enable the drawer type positioning support mechanism 1 and the sensor docking mechanism 2 to complete rapid docking, so that the problems that various sensors in an aerospace system are cumbersome to mount and cannot be rapidly mounted and docked are solved.
The sensor docking mechanism 2 is in clearance fit with the drawer type positioning and supporting mechanism 1, the drawer type positioning and supporting mechanism 1 is fixedly connected with a hasp locking mechanism I3, the sensor docking mechanism 2 is fixedly connected with a hasp locking mechanism II 4, and the hasp locking mechanism I3 is clamped on the locking mechanism II 4.
The drawer type positioning and supporting mechanism 1 comprises a positioning bottom plate 1-1, a positioning mounting plate 1-3 and a positioning top plate 1-4, one end of the positioning bottom plate 1-1 is fixedly connected to the lower end of the positioning mounting plate 1-3, one end of the positioning top plate 1-4 is fixedly connected to the upper end of the positioning mounting plate 1-3, and the positioning bottom plate 1-1, the positioning mounting plate 1-3 and the positioning top plate 1-4 form a butt joint accommodating cavity.
The sensor butt joint mechanism 2 comprises a sensor butt joint body 2-1, a locking fixing plate 2-2 and a mounting positioning plate 2-4, the locking fixing plate 2-2 and the mounting positioning plate 2-4 are fixedly connected to the upper end and the lower end of the sensor butt joint body 2-1 respectively, and the sensor butt joint body 2-1 is in clearance fit with a butt joint accommodating cavity formed by a positioning bottom plate 1-1, a positioning mounting plate 1-3 and a positioning top plate 1-4.
The hasp locking mechanism I3 comprises a fixed base plate I3-1, a linking block 3-2, a hasp movable end 3-3 and a lapping strip 3-4, the linking block 3-2 is fixedly connected to the fixed base plate I3-1, one end of the hasp movable end 3-3 is hinged to the fixed base plate I3-1, the other end of the hasp movable end 3-3 is rotatably connected with the lapping strip 3-4, the hasp locking mechanism I3 is three, two fixed base plates I3-1 are fixedly connected to the upper end of a positioning top plate 1-4, and the other fixed base plate I3-1 is fixedly connected to the lower end face of the positioning base plate 1-1.
The hasp locking mechanism II 4 comprises a fixed base plate II 4-1 and hasp fixed locking ends 4-2, the hasp fixed locking ends 4-2 are fixedly connected to the fixed base plate II 4-1, the hasp locking mechanisms II 4 are three, two fixed base plates II 4-1 are fixedly connected to the locking fixed plate 2-2, the other fixed base plate II 4-1 is fixedly connected to the installation positioning plate 2-4, and three lapping strips 3-4 are clamped on the corresponding three fixed locking ends 4-2 respectively; when in use, the sensor butt joint body 2-1 slides towards a butt joint containing cavity formed by the positioning bottom plate 1-1, the positioning mounting plate 1-3 and the positioning top plate 1-4, the sensor butt joint body 2-1 is in clearance fit with the butt joint containing cavity formed by the positioning bottom plate 1-1, the positioning mounting plate 1-3 and the positioning top plate 1-4, the movable end 3-3 of the hasp is rotated upwards, the movable end 3-3 of the hasp is rotated by taking a hinge point of the movable end 3-3 of the hasp as a center, the movable end 3-3 of the hasp drives the lapping strip 3-4 to rotate by taking the hinge point of the movable end 3-2 of the hasp as a center, the lapping strip 3-4 is rotated by taking a rotation center of the movable end 3-3 of the hasp as a center, and the lapping strip 3-4 moves towards the fixed locking end 4-2 side of the hasp corresponding to the lapping strip 3-4, and the lapping strip 3-4 is clamped on the corresponding fixed locking end 4-2 of the hasp, the movable end 3-3 of the hasp is pressed downwards, the movable end 3-3 of the hasp rotates by taking a hinge point of the movable end 3-3 of the hasp and the connecting block 3-2 as a center, the movable end 3-3 of the hasp drives the lapping strip 3-4 to rotate by taking a clamping point of the movable end 3-4-2 of the hasp as a center, one end of the lapping strip 3-4 is fixed, the other end of the lapping strip 3-4 rotates, the transverse increment of the rotation of the lapping strip 3-4 is smaller than the transverse increment of the rotation of the movable end 3-3 of the hasp, the lapping strip 3-4 is tightened to generate transverse fastening force on the fixed locking end 4-2 of the hasp, and the drawer type positioning support mechanism 1 and the sensor butt joint mechanism 2 are quickly butted.
The drawer type positioning support mechanism 1 further comprises a positioning groove I1-2 and a positioning groove II 1-5, and the positioning groove I1-2 and the positioning groove II 1-5 are respectively arranged on the positioning bottom plate 1-1 and the positioning top plate 1-4.
The sensor docking mechanism 2 further comprises a positioning block 2-3, the positioning block 2-3 is fixedly connected to the locking fixing plate 2-2, the positioning block 2-3 and the locking fixing plate 2-2 are integrally formed, the positioning block 2-3 is in clearance fit in the positioning groove II 1-5, and the mounting positioning plate 2-4 is in clearance fit in the positioning groove I1-2; the positioning block 2-3 and the mounting positioning plate 2-4 can play a certain role in pre-positioning the device, so that the three hasp locking mechanisms I3 can be accurately clamped on the corresponding three hasp locking mechanisms II 4 to further reduce the butt joint speed.
The hasp locking mechanism II 4 further comprises an anti-falling baffle 4-3, and one end of the hasp fixing locking end 4-2 extends and inclines downwards to form the anti-falling baffle 4-3; when the movable end 3-3 of the hasp is rotated downwards to enable the lapping strip 3-4 to be clamped on the fixed locking end 4-2 of the hasp, the anti-falling baffle 4-3 can generate a certain positioning effect on the lapping strip 3-4, and after the lapping strip 3-4 completes the quick installation of the drawer type positioning and supporting mechanism 1 and the sensor butt-joint mechanism 2, a certain anti-falling effect can be generated due to the fact that the lapping strip 3-4 can be prevented from being separated from the fixed locking end 4-2 of the hasp.
The invention relates to a quick butt joint device of a hasp type model aerospace system sensor, which has the working principle that:
when in use, the sensor butt joint body 2-1 slides towards a butt joint containing cavity formed by the positioning bottom plate 1-1, the positioning mounting plate 1-3 and the positioning top plate 1-4, the sensor butt joint body 2-1 is in clearance fit with the butt joint containing cavity formed by the positioning bottom plate 1-1, the positioning mounting plate 1-3 and the positioning top plate 1-4, the movable end 3-3 of the hasp is rotated upwards, the movable end 3-3 of the hasp is rotated by taking a hinge point of the movable end 3-3 of the hasp as a center, the movable end 3-3 of the hasp drives the lapping strip 3-4 to rotate by taking the hinge point of the movable end 3-2 of the hasp as a center, the lapping strip 3-4 is rotated by taking a rotation center of the movable end 3-3 of the hasp as a center, and the lapping strip 3-4 moves towards the fixed locking end 4-2 side of the hasp corresponding to the lapping strip 3-4, the lapping strip 3-4 is clamped on the corresponding fixed locking end 4-2 of the hasp, the movable end 3-3 of the hasp is pressed downwards, the movable end 3-3 of the hasp rotates by taking a hinge point of the movable end 3-3 of the hasp and the connecting block 3-2 as a center, the movable end 3-3 of the hasp drives the lapping strip 3-4 to rotate by taking a clamping point of the movable end 3-4-2 of the hasp as a center, one end of the lapping strip 3-4 is fixed, the other end of the lapping strip 3-4 rotates, the transverse increment of the rotation of the lapping strip 3-4 is smaller than the transverse increment of the rotation of the movable end 3-3 of the hasp, the lapping strip 3-4 is tightened to generate transverse fastening force on the fixed locking end 4-2 of the hasp, and the drawer type positioning support mechanism 1 and the sensor butt joint mechanism 2 are quickly butted; the positioning block 2-3 and the mounting positioning plate 2-4 can generate a certain pre-positioning effect on the device, so that the three hasp locking mechanisms I3 can be accurately clamped on the corresponding three hasp locking mechanisms II 4 to further reduce the butt joint speed; when the movable end 3-3 of the hasp is rotated downwards to enable the lapping strip 3-4 to be clamped on the fixed locking end 4-2 of the hasp, the anti-falling baffle 4-3 can generate a certain positioning effect on the lapping strip 3-4, and after the lapping strip 3-4 completes the quick installation of the drawer type positioning and supporting mechanism 1 and the sensor butt-joint mechanism 2, a certain anti-falling effect can be generated due to the fact that the lapping strip 3-4 can be prevented from being separated from the fixed locking end 4-2 of the hasp.
It is to be understood that the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and that various changes, modifications, additions and substitutions which are within the spirit and scope of the present invention and which may be made by those skilled in the art are also within the scope of the present invention.
Claims (3)
1. The utility model provides a quick interfacing apparatus of hasp formula model aerospace system sensor, includes drawer type location supporting mechanism (1), sensor docking mechanism (2), hasp locking mechanism I (3) and hasp locking mechanism II (4), its characterized in that: the sensor butt joint mechanism (2) is intermittently matched in the drawer type positioning and supporting mechanism (1), a hasp locking mechanism I (3) is fixedly connected to the drawer type positioning and supporting mechanism (1), a hasp locking mechanism II (4) is fixedly connected to the sensor butt joint mechanism (2), and the hasp locking mechanism I (3) is clamped on the locking mechanism II (4);
the drawer type positioning and supporting mechanism (1) comprises a positioning bottom plate (1-1), a positioning mounting plate (1-3) and a positioning top plate (1-4), one end of the positioning bottom plate (1-1) is fixedly connected to the lower end of the positioning mounting plate (1-3), one end of the positioning top plate (1-4)) is fixedly connected to the upper end of the positioning mounting plate (1-3), and the positioning bottom plate (1-1), the positioning mounting plate (1-3) and the positioning top plate (1-4) form a butt joint accommodating cavity;
the sensor butt joint mechanism (2) comprises a sensor butt joint body (2-1), a locking fixing plate (2-2) and a mounting positioning plate (2-4), the locking fixing plate (2-2) and the mounting positioning plate (2-4) are fixedly connected to the upper end and the lower end of the sensor butt joint body (2-1) respectively, and the sensor butt joint body (2-1) is intermittently matched in a butt joint accommodating cavity formed by a positioning bottom plate (1-1), a positioning mounting plate (1-3) and a positioning top plate (1-4);
the hasp locking mechanism I (3) comprises a fixed base plate I (3-1), a connecting block (3-2), a hasp movable end (3-3) and a lapping strip (3-4), the connecting block (3-2) is fixedly connected to the fixed base plate I (3-1), one end of the hasp movable end (3-3) is hinged to the fixed base plate I (3-1), the other end of the hasp movable end (3-3) is rotatably connected with the lapping strip (3-4), three hasp locking mechanisms I (3) are arranged, two fixed base plates I (3-1) are fixedly connected to the upper end of the positioning top plate (1-4), and the other fixed base plate I (3-1) is fixedly connected to the lower end face of the positioning base plate (1-1);
the hasp locking mechanism II (4) comprises two fixed base plates II (4-1) and hasp fixed locking ends (4-2), the hasp fixed locking ends (4-2) are fixedly connected to the fixed base plates II (4-1), the hasp locking mechanisms II (4) are three, two fixed base plates II (4-1) are fixedly connected to the locking fixed plates (2-2), the other fixed base plate II (4-1) is fixedly connected to the installation positioning plate (2-4), and the three lapping strips (3-4) are respectively clamped on the corresponding three fixed locking ends (4-2);
the hasp locking mechanism II (4) further comprises an anti-falling baffle (4-3), and one end of the hasp fixing locking end (4-2) extends and inclines downwards to form the anti-falling baffle (4-3).
2. The quick docking device for a snap-on model aerospace system sensor according to claim 1, wherein: the drawer type positioning and supporting mechanism (1) further comprises a positioning groove I (1-2) and a positioning groove II (1-5), and the positioning groove I (1-2) and the positioning groove II (1-5) are respectively arranged on the positioning bottom plate (1-1) and the positioning top plate (1-4).
3. The quick docking device for a snap-on model aerospace system sensor according to claim 2, wherein: the sensor butt-joint mechanism (2) further comprises a positioning block (2-3), the positioning block (2-3) is fixedly connected to the locking fixing plate (2-2), the positioning block (2-3) and the locking fixing plate (2-2) are integrally formed, the positioning block (2-3) is in clearance fit in the positioning groove II (1-5), and the installation positioning plate (2-4) is in clearance fit in the positioning groove I (1-2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811018684.2A CN109178353B (en) | 2018-09-03 | 2018-09-03 | Quick butt joint device of hasp type model aerospace system sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811018684.2A CN109178353B (en) | 2018-09-03 | 2018-09-03 | Quick butt joint device of hasp type model aerospace system sensor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109178353A CN109178353A (en) | 2019-01-11 |
| CN109178353B true CN109178353B (en) | 2020-05-26 |
Family
ID=64917808
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811018684.2A Active CN109178353B (en) | 2018-09-03 | 2018-09-03 | Quick butt joint device of hasp type model aerospace system sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109178353B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112141370A (en) * | 2020-09-04 | 2020-12-29 | 中国空间技术研究院 | Connecting interface between module and cabin section |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101967923A (en) * | 2009-07-27 | 2011-02-09 | 成都盛尔嘉科技有限公司 | Anti-theft lock for automobile window |
| CN103255967A (en) * | 2013-04-26 | 2013-08-21 | 湖北爱商光电股份有限公司 | Splicing lock catch |
| CN203347387U (en) * | 2013-06-04 | 2013-12-18 | 信义汽车玻璃(深圳)有限公司 | Locking device of sliding window |
| CN103397823B (en) * | 2013-07-30 | 2016-01-20 | 湖北爱商光电股份有限公司 | Fasten and splice snap close closely |
| GB2543056A (en) * | 2015-10-06 | 2017-04-12 | Wayne Andrew Carter | Secure slide |
| CN108019122A (en) * | 2017-12-08 | 2018-05-11 | 天长市天鑫粮油贸易有限责任公司 | A kind of grain storage repository door |
-
2018
- 2018-09-03 CN CN201811018684.2A patent/CN109178353B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN109178353A (en) | 2019-01-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207671135U (en) | A kind of coiled handset cord circular conveyor | |
| CN201833294U (en) | Hold-down mechanism | |
| CN107414441B (en) | A kind of FRAME COMPONENTS quick-changing type clamper towards assembly | |
| CN109178353B (en) | Quick butt joint device of hasp type model aerospace system sensor | |
| CN109896283A (en) | A kind of glass bracket installation detecting device | |
| CN107971952A (en) | A kind of more mechanical arm flexible holding devices and its application method | |
| CN210392865U (en) | Filter centre gripping feeding mechanism | |
| CN107803321B (en) | Shell clamping and positioning jig | |
| CN109926862A (en) | A kind of frock clamp based on assembly line | |
| CN215747428U (en) | Welding jig and welding equipment | |
| CN109109327A (en) | A kind of automotive plastic parts hot melting fixture | |
| CN205437624U (en) | Catalyst converter assembly welding jig for automobile exhaust | |
| CN205200885U (en) | Battery installation reinforcing plate fixture device | |
| CN210053583U (en) | Loudspeaker shell positioning and clamping device | |
| CN115070308A (en) | Fixing tool flexible device for welding aluminum alloy battery tray | |
| CN203210047U (en) | Elbow holder | |
| CN207824248U (en) | A kind of attachment device of stitch welding machine module and workbench | |
| CN203956796U (en) | A kind of support arm and inner core pressing type suspension assembling jig | |
| CN208543239U (en) | A kind of Mobile multi-station automobile clamping workpiece tool | |
| CN208117288U (en) | A kind of Quick-positioning clamp and positioning system | |
| CN106378561A (en) | To-be-welded part feeding device | |
| CN206047392U (en) | Welding production line | |
| CN214922451U (en) | Revolving stage processingequipment | |
| CN205660180U (en) | High accuracy rises and tightly installs | |
| CN217254620U (en) | CNC spare universal fixturing |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | 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 |