CN109178353A - A kind of fast junction apparatus of buckle type model aerospace system sensor - Google Patents
A kind of fast junction apparatus of buckle type model aerospace system sensor Download PDFInfo
- Publication number
- CN109178353A CN109178353A CN201811018684.2A CN201811018684A CN109178353A CN 109178353 A CN109178353 A CN 109178353A CN 201811018684 A CN201811018684 A CN 201811018684A CN 109178353 A CN109178353 A CN 109178353A
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- hasp
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- 230000007246 mechanism Effects 0.000 claims abstract description 103
- 238000003032 molecular docking Methods 0.000 claims abstract description 47
- 238000009434 installation Methods 0.000 claims abstract description 25
- 210000001503 joint Anatomy 0.000 claims description 13
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 10
- 238000000034 method Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 239000007787 solid Substances 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000007792 addition Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- 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
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- Engineering & Computer Science (AREA)
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- Aviation & Aerospace Engineering (AREA)
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- Connection Of Plates (AREA)
Abstract
The present invention relates to a kind of docking facilities, it in particular is a kind of fast junction apparatus of buckle type model aerospace system sensor, including drawer type supporting mechanism for location, sensor docking mechanism, hasp retaining mechanism I and hasp retaining mechanism II, the sensor docking mechanism interval cooperation is in drawer type supporting mechanism for location, hasp retaining mechanism I is fixedly connected on drawer type supporting mechanism for location, hasp retaining mechanism II is fixedly connected on sensor docking mechanism, hasp retaining mechanism I is connected on retaining mechanism II；Item can be taken in the displacement mobile to the fixed locking end side of hasp by being rotated up the increase of hasp movable end, allow to take item and be clamped to be in the fixed locking end of its corresponding hasp, making to take item and can generate fastening force with relatively fixed locking end by pushing hasp movable end make drawer type supporting mechanism for location and sensor docking mechanism complete rapid abutting joint, solve the problem of that each sensor Fast Installation erroneous for installation that cannot achieve is docked in aerospace system.
Description
Technical field
The present invention relates to a kind of docking facilities, are in particular a kind of the quick of buckle type model aerospace system sensor
Docking facilities.
Background technique
With the fast development of science and technology, every country is all pushing science and technology to go deep into all trades and professions energetically
Using being similarly obtained great attention in space industry.The rapid development of aerospace industry, each state is all in each portion for pursuing aerospace system
Divide to be mounted on and guarantee to may be implemented rapid automatized installation docking while installation reliability, significantly promotes the peace of sensor
Efficiency is filled, while improving installation accuracy by the positioning mechanism of design.It special is wanted according to aerospace system for what sensor docked
It asks, needs to realize the rapid abutting joint of sensor using mechanical structure as simple as possible, operating must be simple, and can guarantee
Reliability is docked, this proposes problem for the design of docking concept.The considerations of being currently limited to safety, pair of sensor
Most of positioning and locking for relying on bolt and nut is connect, is spent human and material resources, inefficiency, positioning accuracy cannot be completely secured.
Summary of the invention
The object of the present invention is to provide a kind of fast junction apparatus of buckle type model aerospace system sensor, can solve
The problem of each sensor is erroneous for installation in aerospace system, cannot achieve Fast Installation docking.
The purpose of the present invention is achieved through the following technical solutions:
A kind of fast junction apparatus of buckle type model aerospace system sensor, including drawer type supporting mechanism for location, biography
Sensor docking mechanism, hasp retaining mechanism I and hasp retaining mechanism II, the sensor docking mechanism clearance fit is in drawer type
In supporting mechanism for location, it is fixedly connected with hasp retaining mechanism I on drawer type supporting mechanism for location, consolidates on sensor docking mechanism
Surely it is connected with hasp retaining mechanism II, hasp retaining mechanism I is connected on retaining mechanism II.
As advanced optimizing for the technical program, a kind of buckle type model aerospace system sensor of the present invention it is quick right
Connection device, the drawer type supporting mechanism for location include positioning plate, positioning mounting plate and positioning top plate, one end of positioning plate
It is fixedly connected on the lower end of positioning mounting plate, the one end for positioning top plate is fixedly connected on the upper end of positioning mounting plate, positioning plate,
Positioning mounting plate and positioning top plate form docking accommodating chamber.
As advanced optimizing for the technical program, a kind of buckle type model aerospace system sensor of the present invention it is quick right
Connection device, the sensor docking mechanism include sensor butt joint body, be locked plate and installation positioning plate, be locked plate and
Installation positioning plate is respectively fixedly connected with the upper and lower ends in sensor butt joint body, sensor butt joint body clearance fit positioning plate,
In the docking accommodating chamber that positioning mounting plate and positioning top plate are formed.
As advanced optimizing for the technical program, a kind of buckle type model aerospace system sensor of the present invention it is quick right
Connection device, the hasp retaining mechanism I include fixed bottom plate I, connecting block, hasp movable end and take item, and connecting block is fixedly connected
On fixed bottom plate I, one end of hasp movable end is hinged on fixed bottom plate I, and the other end of hasp movable end is rotatably connected to
Item is taken, there are three the settings of hasp retaining mechanism I, and the fixed bottom plate I of two of them is fixedly connected on the upper end of positioning top plate, another
Fixed bottom plate I is fixedly connected on the lower end surface of positioning plate.
As advanced optimizing for the technical program, a kind of buckle type model aerospace system sensor of the present invention it is quick right
Connection device, the hasp retaining mechanism II include fixed bottom plate II and the fixed locking end of hasp, and the fixed locking end of hasp is fixed to be connected
It connects on fixed bottom plate II, there are three the settings of hasp retaining mechanism II, and it is solid that the fixed bottom plate II of two of them is fixedly connected on locking
On fixed board, another fix bottom plate II be fixedly connected on installation positioning plate on, three take item be respectively engaged in its corresponding three
In a fixed locking end.
As advanced optimizing for the technical program, a kind of buckle type model aerospace system sensor of the present invention it is quick right
Connection device, the drawer type supporting mechanism for location further include locating slot I and locating slot II, and locating slot I and locating slot II are set respectively
It sets on positioning plate and positioning top plate.
As advanced optimizing for the technical program, a kind of buckle type model aerospace system sensor of the present invention it is quick right
Connection device, the sensor docking mechanism further include locating piece, and locating piece, which is fixedly connected on, to be locked on plate, locating piece and lock
It fastens fixed board to be integrally formed, locating piece clearance fit installs positioning plate clearance fit in locating slot I in locating slot II.
As advanced optimizing for the technical program, a kind of buckle type model aerospace system sensor of the present invention it is quick right
Connection device, the hasp retaining mechanism II further include anticreep baffle, one end of the fixed locking end of hasp extend dip down it is oblique at
Anticreep baffle.
A kind of fast junction apparatus of buckle type model aerospace system sensor of the invention has the beneficial effect that
A kind of fast junction apparatus of buckle type model aerospace system sensor of the present invention, can be by being rotated up hasp
Movable end increase takes item in the displacement mobile to the fixed locking end side of hasp, allows to take item and be clamped to be that its corresponding hasp is solid
Determine in locking end, making to take item and can generate fastening force with relatively fixed locking end by pushing hasp movable end make drawer type positioning branch
Support mechanism and sensor docking mechanism complete rapid abutting joint, and each sensor is erroneous for installation in solution aerospace system, cannot achieve fast
The problem of speed installation docking.
Detailed description of the invention
The present invention will be further described in detail with specific implementation method with reference to the accompanying drawing.
Fig. 1 is aerospace system sensor fast junction apparatus overall structure diagram of the invention；
Fig. 2 is aerospace system sensor fast junction apparatus connection procedure structural schematic diagram one of the invention；
Fig. 3 is aerospace system sensor fast junction apparatus connection procedure structural schematic diagram two of the invention；
Fig. 4 is aerospace system sensor fast junction apparatus connection procedure structural schematic diagram three of the invention；
Fig. 5 is drawer type supporting mechanism for location structural schematic diagram of the invention；
Fig. 6 is sensor of the invention docking mechanism structural schematic diagram one；
Fig. 7 is sensor of the invention docking mechanism structural schematic diagram two；
Fig. 8 is I structural schematic diagram of hasp retaining mechanism of the invention；
Fig. 9 is II structural schematic diagram one of hasp retaining mechanism of the invention；
Figure 10 is II structural schematic diagram two of hasp retaining mechanism of the invention.
In figure: drawer type supporting mechanism for location 1；Positioning plate 1-1；I 1-2 of locating slot；Positioning mounting plate 1-3；Positioning top
Plate 1-4；II 1-5 of locating slot；Sensor docking mechanism 2；Sensor butt joint body 2-1；Be locked plate 2-2；Locating piece 2-3；Peace
Fill positioning plate 2-4；Hasp retaining mechanism I 3；Fixed I 3-1 of bottom plate；Connecting block 3-2；Hasp movable end 3-3；Take a 3-4；Hasp
Retaining mechanism II 4；Fixed II 4-1 of bottom plate；Hasp fixes locking end 4-2；Anticreep baffle 4-3.
Specific embodiment
The present invention is described in further detail below in conjunction with the accompanying drawings.
Before illustrating specific embodiment, to avoid repeating language, illustrating " being fixedly connected " as described below can be with
It is: is bolted, welds and the modes such as rivet interlacement are fixed, those skilled in the art can be according to different applications
Scene selects the different modes that is fixedly connected, and main purpose is that two pieces part is fixed.
Specific embodiment 1:
Illustrate present embodiment, a kind of rapid abutting joint dress of buckle type model aerospace system sensor below with reference to Fig. 1-10
It sets, including drawer type supporting mechanism for location 1, sensor docking mechanism 2, hasp retaining mechanism I 3 and hasp retaining mechanism II 4, it can
To take a 3-4 in the displacement mobile to the fixed side locking end 4-2 of hasp by being rotated up hasp movable end 3-3 increase, make to take
3-4, which can be clamped, to be on the fixed locking end 4-2 of its corresponding hasp, can by pushing that hasp movable end 3-3 makes to take a 3-4
Generating fastening force with relatively fixed locking end makes drawer type supporting mechanism for location 1 and sensor docking mechanism 2 complete rapid abutting joint,
Solve the problem of that each sensor Fast Installation erroneous for installation that cannot achieve is docked in aerospace system.
2 clearance fit of sensor docking mechanism is in drawer type supporting mechanism for location 1, drawer type supporting mechanism for location
It is fixedly connected with hasp retaining mechanism I 3 on 1, hasp retaining mechanism II 4, hasp lock are fixedly connected on sensor docking mechanism 2
Tight mechanism I 3 is connected on retaining mechanism II 4.
The drawer type supporting mechanism for location 1 includes positioning plate 1-1, positioning mounting plate 1-3 and positioning top plate 1-4, is determined
One end of position bottom plate 1-1 is fixedly connected on the lower end of positioning mounting plate 1-3, and one end of positioning top plate 1-4 is fixedly connected on positioning
The upper end of mounting plate 1-3, positioning plate 1-1, positioning mounting plate 1-3 and positioning top plate 1-4 form docking accommodating chamber.
The sensor docking mechanism 2 includes sensor butt joint body 2-1, be locked plate 2-2 and installation positioning plate 2-4,
The plate 2-2 and installation positioning plate 2-4 that is locked is respectively fixedly connected with the upper and lower ends in sensor butt joint body 2-1, sensor docking
Body 2-1 clearance fit is in the docking accommodating chamber that positioning plate 1-1, positioning mounting plate 1-3 and positioning top plate 1-4 are formed.
The hasp retaining mechanism I 3 includes fixed I 3-1 of bottom plate, connecting block 3-2, hasp movable end 3-3 and takes a 3-4,
Connecting block 3-2 is fixedly connected on fixed I 3-1 of bottom plate, and one end of hasp movable end 3-3 is hinged on fixed I 3-1 of bottom plate, is taken
The other end of button movable end 3-3, which is rotatably connected to, takes a 3-4, and there are three the settings of hasp retaining mechanism I 3, the fixed bottom of two of them
I 3-1 of plate is fixedly connected on the upper end of positioning top plate 1-4, another is fixed I 3-1 of bottom plate and is fixedly connected under positioning plate 1-1
End face.
The hasp retaining mechanism II 4 includes fixed II 4-1 of bottom plate and the fixed locking end 4-2 of hasp, the fixed locking of hasp
End 4-2 is fixedly connected on fixed II 4-1 of bottom plate, and there are three the settings of hasp retaining mechanism II 4, fixed II 4- of bottom plate of two of them
1 is fixedly connected on and is locked on plate 2-2, another is fixed II 4-1 of bottom plate and is fixedly connected on installation positioning plate 2-4, and three
A 3-4 is taken to be respectively engaged on its corresponding three fixed locking end 4-2；Make sensor butt joint body 2-1 to positioning when use
It is slided in the docking accommodating chamber that bottom plate 1-1, positioning mounting plate 1-3 and positioning top plate 1-4 are formed, makes sensor butt joint body 2-
1 clearance fit is rotated up in the docking accommodating chamber that positioning plate 1-1, positioning mounting plate 1-3 and positioning top plate 1-4 are formed
Hasp movable end 3-3 makes hasp movable end 3-3 rotate centered on the hinge joint of connecting block 3-2, makes hasp movable end
3-3 drive takes a 3-4 and rotates centered on the hinge joint of connecting block 3-2, and a 3-4 is taken in rotation, take a 3-4 with hasp
Rotated centered on the center of rotation of movable end 3-3, make to take a 3-4 to the fixed side locking end 4-2 of corresponding hasp into
Row movement, and make to take a 3-4 and be stuck on the fixed locking end 4-2 of corresponding hasp, hasp movable end 3-3 is pulled down,
So that hasp movable end 3-3 is rotated centered on the hinge joint of connecting block 3-2, hasp movable end 3-3 drive is made to take a 3-4
It is rotated centered on the fixed locking end 4-2 card contact of hasp, the motionless other end in one end for taking a 3-4 rotates, and takes
The amount of laterally increasing of 3-4 to rotate is less than the amount of laterally increasing that hasp movable end 3-3 rotates, and it is tight to take a 3-4
Taut locking end 4-2 fixed to hasp generates lateral fastening force, and drawer type supporting mechanism for location 1 and sensor docking mechanism 2 are quick
Docking is completed.
The drawer type supporting mechanism for location 1 further includes II 1-5 of I 1-2 of locating slot and locating slot, I 1-2 of locating slot and positioning
II 1-5 of slot is separately positioned on positioning plate 1-1 and positioning top plate 1-4.
The sensor docking mechanism 2 further includes locating piece 2-3, and locating piece 2-3 is fixedly connected on the plate 2-2 that is locked
On, locating piece 2-3 and the plate 2-2 integrated molding that is locked, locating piece 2-3 clearance fit is in II 1-5 of locating slot, installation positioning
Plate 2-4 clearance fit is in I 1-2 of locating slot；Locating piece 2-3 and installation positioning plate 2-4 can generate centainly preparatory to device
The effect of positioning guarantees that three hasp retaining mechanisms I 3 can be accurately clamped and is its corresponding three hasp retaining mechanism II
Docking speed is further reduced on 4.
The hasp retaining mechanism II 4 further includes anticreep baffle 4-3, and one end of the fixed locking end 4-2 of hasp extends to down
It is formed slopely anticreep baffle 4-3；It is connected on the fixed locking end 4-2 of hasp rotating down hasp movable end 3-3 and making to take a 3-4
When, anticreep baffle 4-3 can generate certain positioning action to a 3-4 is taken, and complete drawer type positioning support machine taking a 3-4
It can be due to that can prevent from taking the fixed locking end 4-2 of 3-4 disengaging hasp after the Fast Installation of structure 1 and sensor docking mechanism 2
To generate certain anti-off effect.
A kind of fast junction apparatus of buckle type model aerospace system sensor of the invention, its working principle is that:
Form sensor butt joint body 2-1 to positioning plate 1-1, positioning mounting plate 1-3 and positioning top plate 1-4
It is slided, make sensor butt joint body 2-1 clearance fit in positioning plate 1-1, positioning mounting plate 1-3 and is determined in docking accommodating chamber
Position top plate 1-4 formed docking accommodating chamber in, be rotated up hasp movable end 3-3, make hasp movable end 3-3 with connecting block 3-
It rotates centered on 2 hinge joint, hasp movable end 3-3 drive is made to take a 3-4 centered on the hinge joint of connecting block 3-2
It rotates, a 3-4 is taken in rotation, takes a 3-4 and is rotated centered on the center of rotation of hasp movable end 3-3, makes to take item
3-4 is moved to the fixed side locking end 4-2 of corresponding hasp, and makes to take a 3-4 to be stuck in corresponding hasp solid
Determine on locking end 4-2, pull down hasp movable end 3-3, make hasp movable end 3-3 with in the hinge joint of connecting block 3-2
The heart rotates, and so that hasp movable end 3-3 drive is taken a 3-4 and is turned centered on the fixed locking end 4-2 card contact of hasp
Dynamic, the motionless other end in one end for taking a 3-4 rotates, and the amount of laterally increasing to rotate for taking a 3-4 is movable less than hasp
The amount of laterally increasing that end 3-3 rotates takes a 3-4 by tight locking end 4-2 fixed to hasp and generates lateral fastening force, drawer
Formula supporting mechanism for location 1 and 2 rapid abutting joint of sensor docking mechanism are completed；Locating piece 2-3 and installation positioning plate 2-4 can be to dresses
Set and generate certain effect being pre-positioned, guarantee three hasp retaining mechanisms I 3 can accurately be clamped be its corresponding three
Docking speed is further reduced on a hasp retaining mechanism II 4；It is connected to rotating down hasp movable end 3-3 and making to take a 3-4
When on the fixed locking end 4-2 of hasp, anticreep baffle 4-3 can generate certain positioning action to a 3-4 is taken, and take a 3-4
Completing after the Fast Installation of drawer type supporting mechanism for location 1 and sensor docking mechanism 2 can be de- due to that can prevent from taking a 3-4
Locking end 4-2 fixed from hasp is to generate certain anti-off effect.
Certainly, above description is not limitation of the present invention, and the present invention is also not limited to the example above, the art
The variations, modifications, additions or substitutions that those of ordinary skill is made within the essential scope of the present invention also belong to guarantor of the invention
Protect range.
Claims (8)
1. a kind of fast junction apparatus of buckle type model aerospace system sensor, including drawer type supporting mechanism for location (1), biography
Sensor docking mechanism (2), hasp retaining mechanism I (3) and hasp retaining mechanism II (4), it is characterised in that: the sensor docking
Mechanism (2) interval cooperation is fixedly connected on drawer type supporting mechanism for location (1) and takes in drawer type supporting mechanism for location (1)
It detains retaining mechanism I (3), is fixedly connected with hasp retaining mechanism II (4), hasp retaining mechanism I on sensor docking mechanism (2)
(3) it is connected on retaining mechanism II (4).
2. a kind of fast junction apparatus of buckle type model aerospace system sensor according to claim 1, feature exist
In: the drawer type supporting mechanism for location (1) includes positioning plate (1-1), positioning mounting plate (1-3) and positions top plate (1-4),
One end of positioning plate (1-1) is fixedly connected on the lower end of positioning mounting plate (1-3), positions top plate (1-4)) one end fixed connect
It connects in the upper end of positioning mounting plate (1-3), positioning plate (1-1), positioning mounting plate (1-3) and positioning top plate (1-4) formation pair
Connect accommodating chamber.
3. a kind of fast junction apparatus of buckle type model aerospace system sensor according to claim 2, feature exist
In: the sensor docking mechanism (2) includes sensor butt joint body (2-1), the plate that is locked (2-2) and installation positioning plate (2-
4) it, is locked and plate (2-2) and positioning plate (2-4) is installed is respectively fixedly connected with upper and lower ends in sensor butt joint body (2-1),
Pair that the cooperation of sensor butt joint body (2-1) interval is formed in positioning plate (1-1), positioning mounting plate (1-3) and positioning top plate (1-4)
It connects in accommodating chamber.
4. a kind of fast junction apparatus of buckle type model aerospace system sensor according to claim 3, feature exist
In: the hasp retaining mechanism I (3) includes fixed bottom plate I (3-1), connecting block (3-2), hasp movable end (3-3) and takes item
(3-4), connecting block (3-2) are fixedly connected on fixed bottom plate I (3-1), and one end of hasp movable end (3-3) is hinged on fixed bottom
On plate I (3-1), the other end of hasp movable end (3-3), which is rotatably connected to, takes item (3-4), and hasp retaining mechanism I (3) is provided with
Three, two of them fixed bottom plate I (3-1) are fixedly connected on the upper end of positioning top plate (1-4), another fixes bottom plate I (3-1)
It is fixedly connected on the lower end surface of positioning plate (1-1).
5. a kind of fast junction apparatus of buckle type model aerospace system sensor according to claim 4, feature exist
In: the hasp retaining mechanism II (4) includes that fixed bottom plate II (4-1) and hasp are fixed locking end (4-2), the fixed locking of hasp
End (4-2) is fixedly connected on fixed bottom plate II (4-1), and there are three hasp retaining mechanism II (4) settings, the fixed bottom of two of them
Plate II (4-1) is fixedly connected on the plate that is locked (2-2), another is fixed bottom plate II (4-1) and is fixedly connected on installation positioning
On plate (2-4), takes item (3-4) for three and be respectively engaged on its corresponding three fixed locking ends (4-2).
6. a kind of fast junction apparatus of buckle type model aerospace system sensor according to any one of claims 1 to 5,
It is characterized by: the drawer type supporting mechanism for location (1) further includes locating slot I (1-2) and locating slot II (1-5), locating slot I
(1-2) and locating slot II (1-5) are separately positioned on positioning plate (1-1) and positioning top plate (1-4).
7. the fast junction apparatus of a kind of buckle type model aerospace system sensor according to claim 6, special
Sign is: the sensor docking mechanism (2) further includes locating piece (2-3), and locating piece (2-3) is fixedly connected on the plate that is locked
On (2-2), locating piece (2-3) and the plate that is locked (2-2) are integrally formed, and locating piece (2-3) clearance fit is in II (1- of locating slot
5) in, installation positioning plate (2-4) clearance fit is in locating slot I (1-2).
8. according to claim 1, a kind of any one of 2,3,4,5,7 buckle type model aerospace system sensors is fast
Fast docking facilities, it is characterised in that: the hasp retaining mechanism II (4) further includes anticreep baffle (4-3), the fixed locking end of hasp
One end extension of (4-2) dips down oblique at anticreep baffle (4-3).
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 true CN109178353A (en) | 2019-01-11 |
| CN109178353B CN109178353B (en) | 2020-05-26 |
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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 |
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| Country | Link |
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| CN (1) | CN109178353B (en) |
Cited By (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 |
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| 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 |
| CN103397823A (en) * | 2013-07-30 | 2013-11-20 | 湖北爱商光电股份有限公司 | Splicing lock catch tightly buckled |
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| CN112141370A (en) * | 2020-09-04 | 2020-12-29 | 中国空间技术研究院 | Connecting interface between module and cabin section |
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| Publication number | Publication date |
|---|---|
| CN109178353B (en) | 2020-05-26 |
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