CN108942154A - A kind of fast junction apparatus of rotation locking pin aerospace system sensor - Google Patents
A kind of fast junction apparatus of rotation locking pin aerospace system sensor Download PDFInfo
- Publication number
- CN108942154A CN108942154A CN201811018681.9A CN201811018681A CN108942154A CN 108942154 A CN108942154 A CN 108942154A CN 201811018681 A CN201811018681 A CN 201811018681A CN 108942154 A CN108942154 A CN 108942154A
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- sensor
- locking pin
- rotation
- rotation locking
- butterfly
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
Abstract
The present invention relates to a kind of sensor fast junction apparatus, it in particular is a kind of fast junction apparatus of rotation locking pin aerospace system sensor, including sensor docking mechanism, positioning mechanism and rotation locking pin, sensor docking mechanism includes sensor butt joint body, sensor docking block and mounting hole, it is fixedly connected to sensor docking block on four faces of sensor butt joint body, is fixedly connected to mounting hole on four sensor docking blocks；Rotating locking pin includes butterfly and column spinner, it can make to rotate the mounting hole that locking pin is arranged on sensor docking block by rotation rotation locking pin, rotation locking pin is moved downwards by squeezing compressed spring, will rotation locking pin card into swivelling chute, positioning mechanism and sensor docking mechanism is set to complete rapid abutting joint, there are four guarantee position mechanisms and sensor docking mechanism also can guarantee uniform force when completing rapid abutting joint for positioning mechanism setting.
Description
Technical field
The present invention relates to a kind of sensor fast junction apparatus, are in particular a kind of rotation locking pin aerospace systems
The fast junction apparatus of sensor.
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 rotation locking pin aerospace system sensor, can solve
The problem of certainly 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 rotation locking pin aerospace system sensor, including sensor docking mechanism, positioning
Mechanism and rotation locking pin, the sensor docking mechanism include sensor butt joint body, sensor docking block and mounting hole, sensing
It is fixedly connected to sensor docking block on four faces of device butt joint body, is fixedly connected to installation on four sensor docking blocks
Hole；
The positioning mechanism includes locating support, mounting groove, swivelling chute and rotation blind hole, is provided with installation on locating support
Slot and swivelling chute, mounting groove are connected to swivelling chute, and swivelling chute is located at the downside of mounting groove, and it is blind that rotation is provided on the downside of swivelling chute
Hole；
The rotation locking pin includes butterfly and column spinner, and butterfly is fixedly connected on one end of column spinner, rotation
Rotary column clearance fit rotates in blind hole in rotation blind hole and is provided with compressed spring, the both ends of compressed spring are respectively fixedly connected with
On locating support and column spinner, butterfly passes through mounting hole, and butterfly clearance fit works as butterfly in swivelling chute
Lower end surface and sensor docking block contact, butterfly can be clamped in swivelling chute.
As advanced optimizing for the technical program, the quick of pin aerospace system sensor is locked in a kind of rotation of the present invention
Docking facilities, the sensor docking mechanism also packet location hole, four sensors dock and are provided with location hole on blocks.
As advanced optimizing for the technical program, the quick of pin aerospace system sensor is locked in a kind of rotation of the present invention
Docking facilities, the positioning mechanism further include positioning plate, and positioning plate is fixedly connected on the side of locating support upper end, between positioning plate
Gap cooperates in positioning hole.
As advanced optimizing for the technical program, the quick of pin aerospace system sensor is locked in a kind of rotation of the present invention
Docking facilities, the rotation locking pin further includes rotating handle, and rotating handle is fixedly connected on butterfly.
As advanced optimizing for the technical program, the quick of pin aerospace system sensor is locked in a kind of rotation of the present invention
Docking facilities, the locating support are parts processing.
A kind of fast junction apparatus of rotation locking pin aerospace system sensor of the present invention has the beneficial effect that
A kind of fast junction apparatus of rotation locking pin aerospace system sensor of the present invention, can be by rotating rotation lock
Tight pin, which makes to rotate locking pin, passes through the mounting hole being arranged on sensor docking block, by squeeze compressed spring make to rotate locking pin to
Under moved, will rotation locking pin card into swivelling chute, making positioning mechanism and sensor docking mechanism complete rapid abutting joint, it is fixed
There are four guarantee position mechanisms and sensor docking mechanism also can guarantee uniform force when completing rapid abutting joint for the setting of position mechanism.
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 the fast junction apparatus overall structure diagram of aerospace system sensor of the invention；
Fig. 2 is the fast junction apparatus structural schematic diagram one of aerospace system sensor of the invention；
Fig. 3 is the fast junction apparatus structural schematic diagram two of aerospace system sensor of the invention；
Fig. 4 is the fast junction apparatus structural schematic diagram three of aerospace system sensor of the invention；
Fig. 5 is sensor of the invention docking mechanism structural schematic diagram；
Fig. 6 is sensor of the invention docking block structure schematic diagram；
Fig. 7 is positioning mechanism structural schematic diagram one of the invention；
Fig. 8 is positioning mechanism structural schematic diagram two of the invention；
Fig. 9 is rotation locking latch structure schematic diagram of the invention.
In figure: sensor docking mechanism 1；Sensor butt joint body 1-1；Sensor docks block 1-2；Mounting hole 1-3；Location hole
1-4；Positioning mechanism 2；Locating support 2-1；Mounting groove 2-2；Swivelling chute 2-3；Rotate blind hole 2-4；Positioning plate 2-5；Rotation locking
Pin 3；Butterfly 3-1；Column spinner 3-2；Rotating handle 3-3.
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 of rotation locking pin aerospace system sensor below with reference to Fig. 1-9
Device, including sensor docking mechanism 1, positioning mechanism 2 and rotation locking pin 3 can make to rotate by rotation rotation locking pin 3
Locking pin 3 passes through the mounting hole 1-3 being arranged on sensor docking block 1-2, makes to rotate locking pin 3 downwards by squeezing compressed spring
It is moved, rotation locking pin 3 is sticked into swivelling chute 2-3, complete positioning mechanism 2 and sensor docking mechanism 1 quickly right
Connect, the setting of positioning mechanism 4 there are four guarantee position mechanism 2 and sensor docking mechanism 1 also can guarantee when completing rapid abutting joint by
Power is uniform；
The sensor docking mechanism 1 includes sensor butt joint body 1-1, sensor docking block 1-2 and mounting hole 1-3, is passed
Sensor docking block 1-2 is fixedly connected on four faces of sensor butt joint body 1-1, four sensors dock solid on block 1-2
Surely it is connected with mounting hole 1-3；
The positioning mechanism 2 includes locating support 2-1, mounting groove 2-2, swivelling chute 2-3 and rotation blind hole 2-4, positioning branch
Mounting groove 2-2 and swivelling chute 2-3 are provided on frame 2-1, mounting groove 2-2 is connected to swivelling chute 2-3, and swivelling chute 2-3 is located at installation
The downside of slot 2-2 is provided with rotation blind hole 2-4 on the downside of swivelling chute 2-3；
The rotation locking pin 3 includes butterfly 3-1 and column spinner 3-2, and butterfly 3-1 is fixedly connected on column spinner
One end of 3-2, column spinner 3-2 clearance fit rotate in rotation blind hole 2-4 and are provided with compressed spring in blind hole 2-4, compress bullet
The both ends of spring are respectively fixedly connected on locating support 2-1 and column spinner 3-2, and butterfly 3-1 passes through mounting hole 1-3, rotation
Baffle 3-1 clearance fit is docked block 1-2 with sensor when the lower end surface of butterfly 3-1 and is contacted, rotate in swivelling chute 2-3
Baffle 3-1 can be clamped in swivelling chute 2-3；Positioning mechanism is connected in the fixed position of aerospace system body when use, makes four rotations
Turn baffle 3-1 and be each passed through four mounting hole 1-3 being arranged on four sensor docking block 1-2, pulls down four rotations manually
Turn baffle 3-1, four butterfly 3-1 squeeze four column spinner 3-2 respectively and moved downwards, four column spinner 3-2 difference
It is slided in four rotation blind hole 2-4, four column spinner 3-2 squeeze four compressed springs respectively and moved downwards, rotation
Turn baffle 3-1 to be moved downwards along the axial direction of column spinner 3-2, while rotation butterfly 3-1 manually, keeps off rotation
Plate 3-1 is rotated centered on the axis of column spinner 3-2, and butterfly 3-1 is made to stick into correspondence under the reaction force of spring
Swivelling chute 2-3 in, the lower end of butterfly 3-1 is contacted with sensor docking block 1-2, positioning mechanism 2 and sensor docking machine
The rapid abutting joint of structure 1 is completed, and there are four guarantee that position mechanism 2 and sensor docking mechanism 1 are quickly right in completion for the setting of positioning mechanism 4
Also it can guarantee uniform force when connecing.
Location hole is provided on the sensor docking mechanism 1 also packet location hole 1-4, four sensor docking block 1-2
1-4。
The positioning mechanism 2 further includes positioning plate 2-5, and positioning plate 2-5 is fixedly connected on the one of the upper end locating support 2-1
Side, positioning plate 2-5 clearance fit is in location hole 1-4；Four positioning plate 2-5 are inserted into respectively can be real in four location hole 1-4
It is now pre-positioned, guarantees that the installation of sensor docking mechanism 1 and locating support 2-1 are accurate.
The rotation locking pin 3 further includes rotating handle 3-3, and rotating handle 3-3 is fixedly connected on butterfly 3-1；
Rotating handle 3-3 can help to rotate and pull down butterfly 3-1.
The locating support 2-1 is parts processing；When processing swivelling chute 2-3, since the diameter of swivelling chute 2-3 is greater than peace
The width of tankage 2-2, cutter cannot directly mill out swivelling chute 2-3 from top, can only be by locating support 2-1 parts processing.
A kind of fast junction apparatus of rotation locking pin aerospace system sensor of the invention, its working principle is that:
Positioning mechanism is connected in the fixed position of aerospace system body when use, is each passed through four butterfly 3-1
Four mounting hole 1-3 being arranged on four sensor docking block 1-2 pull down four butterfly 3-1, four rotations manually
Baffle 3-1 squeezes four column spinner 3-2 respectively and is moved downwards, and four column spinner 3-2 are respectively in four rotation blind hole 2-4
It is slided, four column spinner 3-2 squeeze four compressed springs respectively and moved downwards, and butterfly 3-1 is along column spinner
The axial direction of 3-2 is moved downwards, while rotation butterfly 3-1 manually, makes butterfly 3-1 with column spinner 3-2's
It is rotated centered on axis, sticks into butterfly 3-1 in corresponding swivelling chute 2-3, rotated
The lower end of baffle 3-1 is contacted with sensor docking block 1-2, and the rapid abutting joint of positioning mechanism 2 and sensor docking mechanism 1 is completed,
There are four guarantee position mechanisms 2 and sensor docking mechanism 1 also can guarantee that stress is equal when completing rapid abutting joint for the setting of positioning mechanism 4
It is even；Four positioning plate 2-5 are inserted into four location hole 1-4 respectively and may be implemented to be pre-positioned, and guarantee 1 He of sensor docking mechanism
The installation of locating support 2-1 is accurate.
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 (5)
1. a kind of fast junction apparatus of rotation locking pin aerospace system sensor, including sensor docking mechanism (1), positioning
Mechanism (2) and rotation locking pin (3), it is characterised in that: the sensor docking mechanism (1) include sensor butt joint body (1-1),
Sensor docks block (1-2) and mounting hole (1-3), is fixedly connected to sensor on four faces of sensor butt joint body (1-1)
It docks block (1-2), is fixedly connected to mounting hole (1-3) on four sensor docking block (1-2)；
The positioning mechanism (2) includes locating support (2-1), mounting groove (2-2), swivelling chute (2-3) and rotates blind hole (2-4),
Mounting groove (2-2) and swivelling chute (2-3) are provided on locating support (2-1), mounting groove (2-2) is connected to swivelling chute (2-3), rotation
Turn trough (2-3) is located at the downside of mounting groove (2-2), and rotation blind hole (2-4) is provided on the downside of swivelling chute (2-3)；
The rotation locking pin (3) includes butterfly (3-1) and column spinner (3-2), and butterfly (3-1) is fixedly connected on rotation
One end of rotary column (3-2), column spinner (3-2) clearance fit are provided with pressure in rotation blind hole (2-4) in rotation blind hole (2-4)
Contracting spring, the both ends of compressed spring are respectively fixedly connected on locating support (2-1) and column spinner (3-2), butterfly (3-1)
Across mounting hole (1-3), butterfly (3-1) clearance fit is in swivelling chute (2-3), when the lower end surface of butterfly (3-1)
It is contacted with sensor docking block (1-2), butterfly (3-1) can be clamped in swivelling chute (2-3).
2. a kind of fast junction apparatus of rotation locking pin aerospace system sensor according to claim 1, feature
Be: the sensor docking mechanism (1) also packet location hole (1-4), four sensors dock and are provided with positioning on block (1-2)
Hole (1-4).
3. a kind of fast junction apparatus of rotation locking pin aerospace system sensor according to claim 2, feature
Be: the positioning mechanism (2) further includes positioning plate (2-5), and positioning plate (2-5) is fixedly connected on the upper end locating support (2-1)
Side, positioning plate (2-5) clearance fit is in the location hole (1-4).
4. a kind of rapid abutting joint dress of rotation locking pin aerospace system sensor according to any one of claims 1 to 3
It sets, it is characterised in that: the rotation locking pin (3) further includes rotating handle (3-3), and rotating handle (3-3) is fixedly connected on rotation
Turn on baffle (3-1).
5. according to a kind of described in any item fast junction apparatus of rotation locking pin aerospace system sensor of claim 4,
It is characterized by: the locating support (2-1) is parts processing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811018681.9A CN108942154B (en) | 2018-09-03 | 2018-09-03 | A kind of fast junction apparatus of rotation locking pin type aerospace system sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811018681.9A CN108942154B (en) | 2018-09-03 | 2018-09-03 | A kind of fast junction apparatus of rotation locking pin type aerospace system sensor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108942154A true CN108942154A (en) | 2018-12-07 |
| CN108942154B CN108942154B (en) | 2019-07-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811018681.9A Active CN108942154B (en) | 2018-09-03 | 2018-09-03 | A kind of fast junction apparatus of rotation locking pin type aerospace system sensor |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110242652A (en) * | 2019-06-14 | 2019-09-17 | 李忠吉 | A kind of fast junction apparatus of rotation locking |
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| CN102493977A (en) * | 2011-11-25 | 2012-06-13 | 西北工业大学 | Simple abutting device |
| CN103049062A (en) * | 2012-12-28 | 2013-04-17 | 深圳市欣普斯科技有限公司 | Water-cooling heat dissipation system and joint component thereof |
| US20130216214A1 (en) * | 2010-07-29 | 2013-08-22 | Canon Kabushiki Kaisha | Lens apparatus including focus operation device and focus operation device |
| CN103625656A (en) * | 2013-12-24 | 2014-03-12 | 哈尔滨工业大学 | Small-size spacecraft butt-joint mechanism |
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2018
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130216214A1 (en) * | 2010-07-29 | 2013-08-22 | Canon Kabushiki Kaisha | Lens apparatus including focus operation device and focus operation device |
| CN102493977A (en) * | 2011-11-25 | 2012-06-13 | 西北工业大学 | Simple abutting device |
| CN103049062A (en) * | 2012-12-28 | 2013-04-17 | 深圳市欣普斯科技有限公司 | Water-cooling heat dissipation system and joint component thereof |
| CN103625656A (en) * | 2013-12-24 | 2014-03-12 | 哈尔滨工业大学 | Small-size spacecraft butt-joint mechanism |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110242652A (en) * | 2019-06-14 | 2019-09-17 | 李忠吉 | A kind of fast junction apparatus of rotation locking |
| CN110242652B (en) * | 2019-06-14 | 2020-11-03 | 浙江澳川液压器材股份有限公司 | Rotary locking quick butt joint device |
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| Publication number | Publication date |
|---|---|
| CN108942154B (en) | 2019-07-26 |
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