CN206528612U - A kind of fixed-wing unmanned plane buckle locking mechanism - Google Patents
A kind of fixed-wing unmanned plane buckle locking mechanism Download PDFInfo
- Publication number
- CN206528612U CN206528612U CN201720071661.2U CN201720071661U CN206528612U CN 206528612 U CN206528612 U CN 206528612U CN 201720071661 U CN201720071661 U CN 201720071661U CN 206528612 U CN206528612 U CN 206528612U
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- China
- Prior art keywords
- grab
- mounting seat
- deck
- unmanned plane
- grab mounting
- Prior art date
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- Expired - Fee Related
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- 230000015572 biosynthetic process Effects 0.000 claims abstract description 5
- 238000010276 construction Methods 0.000 abstract description 3
- 210000003739 neck Anatomy 0.000 description 12
- 238000009434 installation Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model is related to a kind of fixed-wing unmanned plane buckle locking mechanism, it is characterised in that：Including grab mounting seat, grab and deck, the lower surface in described grab mounting seat one end is formed with two chuck, two chuck and grab mounting seat formation deck sliding space；Spring base is fixedly connected with by screw in described grab mounting seat bottom, grab is installed in the grab mounting seat center, the grab is divided into vertical movable post and horizontal dop, the part that the vertical movable post stretches out grab mounting seat is control button, the clamp spring between the spring base and grab；Described deck includes vertical rack and is horizontally arranged at the horizontal stand of vertical rack side, and neck is formed with described horizontal stand, grab and the neck snap fit on deck when deck slides into the deck sliding space of grab mounting seat.The utility model scientific structure design is rationally, simple in construction, can quickly realize that the part of fixed-wing unmanned plane is installed and dismantled, and stable connection is reliable, it is ensured that the safe flight of fixed-wing unmanned plane.
Description
Technical field
The utility model is related to unmanned plane field, more particularly to a kind of buckle locking mechanism of fixed-wing unmanned plane.
Background technology
Fixed-wing unmanned plane is outdoor flight, because its volume is larger, and inconvenient band after splicing is installed is completed indoors
Flight is gone to field.And needed when completing to install in the wild by many instruments, because fixed-wing unmanned plane is complicated, install
After the completion of easily cause installation tool omission lose；If without using instrument, connecting insecure, easily causing the portion of unmanned plane
The danger such as part connection loose or dislocation, cause the unbalance of unmanned plane, ultimately result in out of control etc. dangerous.Therefore, fixed-wing unmanned plane
It is the big problem for needing to solve that outdoor fast and stable, which is installed,.
The content of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art there is provided one kind is simple in construction, can realize nobody
Machine fast and stable is installed and dismantled, and improves the fixed-wing unmanned plane buckle locking mechanism of connection reliability.
The utility model solves its technical problem and is achieved through the following technical solutions：
A kind of fixed-wing unmanned plane buckle locking mechanism, it is characterised in that：Including grab mounting seat, grab and deck,
The lower surface of described grab mounting seat one end is formed with two chuck, and two chuck are slided empty with grab mounting seat formation deck
Between；Spring base is fixedly connected with by screw in described grab mounting seat bottom, card is installed in the grab mounting seat center
Hook, the grab is divided into vertical movable post and horizontal dop, and it is control that the vertical movable post, which stretches out the part of grab mounting seat,
Button, the clamp spring between the spring base and grab；Described deck includes vertical rack and is horizontally arranged at vertical branch
The horizontal stand of frame side, is formed with neck on described horizontal stand, and the deck that deck slides into grab mounting seat slides sky
Between when grab and deck on neck snap fit.
Moreover, being mounted on grab mounting seat fastening screw, the grab in two chuck of described grab mounting seat
The other end of mounting seat is provided with grab mounting seat fastening screw.
Moreover, being provided with deck fastening screw on the vertical rack of the deck.
Advantage of the present utility model and have the beneficial effect that：
1st, this fixed-wing unmanned plane buckle locking mechanism, the lower surface of grab mounting seat one end is formed with two chuck, and this two
Individual chuck and grab mounting seat formation deck sliding space；Grab mounting seat center installs grab, and vertical activity post stretches out card
The part of hook mounting seat is control button, and clamp spring between spring base and grab, deck includes vertical rack and is horizontally mounted
Neck is formed with horizontal stand in vertical rack side, horizontal stand, during work, deck slides into the deck of grab mounting seat
Sliding space, grab and neck snap fit, that realizes part is accurately positioned installation；After aerial mission is completed, pressing is only needed
Control button causes spring-compressed, and now grab departs from out of neck, and deck is pulled out into deck sliding space, completion portion manually
Part is dismantled, and operates rapid and convenient, and stable connection is reliable.
2nd, grab mounting seat is mounted in this fixed-wing unmanned plane buckle locking mechanism, two chuck of grab mounting seat
Fastening screw, the other end of grab mounting seat is provided with grab mounting seat fastening screw, is easy to the company of grab mounting seat and part
Connect, it is ensured that the structural stability of unmanned plane after installation.
3rd, deck fastening screw is installed on this fixed-wing unmanned plane buckle locking mechanism, the vertical rack of deck, is easy to
The connection of deck and part so that stable connection is reliable, is prevented effectively from structure connection and loosens and cause danger.
4th, the utility model scientific structure design is rationally, simple in construction, can quickly realize the part of fixed-wing unmanned plane
Install and dismantle, and stable connection is reliable, it is ensured that the safe flight of fixed-wing unmanned plane.
Brief description of the drawings
Fig. 1 is sectional view of the present utility model；
Fig. 2 is the structural representation of the utility model grab mounting seat；
Fig. 3 is the structural representation of the utility model deck.
Description of reference numerals
The vertical movable post of 1- grab mounting seats trip bolt, 2- grabs mounting seat, 3- control buttons, 4-, the horizontal dops of 5-,
6- necks, 7- vertical racks, 8- spring bases, 9- springs, 10- chuck, 11- horizontal stands, 12- deck trip bolts.
Embodiment
Below by specific embodiment, the utility model is described in further detail, following examples be it is descriptive, no
It is limited, it is impossible to which protection domain of the present utility model is limited with this.
A kind of fixed-wing unmanned plane buckle locking mechanism, its innovation is：Including grab mounting seat 2, grab and card
Seat, the lower surface in grab mounting seat one end is formed with two chuck 10, and two chuck are slided with grab mounting seat formation deck
Space；Spring base 8 is fixedly connected with by screw in grab mounting seat bottom, grab, grab are installed in grab mounting seat center
Be divided into vertical movable post 4 and horizontal card 5, the part that vertical activity post stretches out grab mounting seat is control button 3, in spring base and
Clamp spring 9 between grab, spring one end is fixed with spring base, and the other end is fixed with the vertical movable post of grab；Deck includes perpendicular
Straight bracket 7 and the horizontal stand 11 for being horizontally arranged at vertical rack side, are formed with neck 6, deck slides on horizontal stand
Grab and the neck snap fit on deck during the deck sliding space of grab mounting seat, during work, deck slides into grab peace
The deck sliding space of seat, grab and neck snap fit are filled, that realizes part is accurately positioned installation；When completion aerial mission
Afterwards, need to only control button be pressed so that spring-compressed, now grab departs from out of neck, and deck is pulled out into deck slip manually
Space, completes part dismounting, operates rapid and convenient, and stable connection is reliable.
A grab mounting seat fastening screw 1 is separately installed with two chuck of grab mounting seat, grab mounting seat
The other end is provided with a grab mounting seat fastening screw, is easy to the connection of grab mounting seat and part, it is ensured that after installation nobody
The structural stability of machine.
Two symmetrical deck fastening screws 12 are installed on the vertical rack of deck, are easy to the company of deck and part
Connect so that stable connection is reliable, be prevented effectively from structure connection and loosen and cause danger.
Operation principle of the present utility model is：
During work, deck slides into the deck sliding space of grab mounting seat, grab and neck snap fit, realizes part
Be accurately positioned installation；After aerial mission is completed, control button only need to be pressed so that spring-compressed, now grab is out of neck
Depart from, and deck is pulled out into deck sliding space manually, complete part dismounting, operate rapid and convenient, and stable connection is reliable.
Although disclosing embodiment of the present utility model and accompanying drawing for the purpose of illustration, those skilled in the art can be with
Understand：Do not departing from the utility model and spirit and scope of the appended claims, it is various replace, change and modifications all be can
Can, therefore, scope of the present utility model is not limited to embodiment and accompanying drawing disclosure of that.
Claims (1)
1. a kind of fixed-wing unmanned plane buckle locking mechanism, it is characterised in that：Including grab mounting seat, grab and deck, in institute
The lower surface for stating grab mounting seat one end is formed with two chuck, two chuck and grab mounting seat formation deck sliding space；
Spring base is fixedly connected with by screw in described grab mounting seat bottom, grab is installed in the grab mounting seat center,
The grab is divided into vertical movable post and horizontal dop, and the part that the vertical movable post stretches out grab mounting seat is pressed for control
Button, the clamp spring between the spring base and grab；Described deck includes vertical rack and is horizontally arranged at vertical rack
The horizontal stand of side, is formed with neck on described horizontal stand, and deck slides into the deck sliding space of grab mounting seat
When grab and deck on neck snap fit；
Be mounted on grab mounting seat fastening screw in two chuck of described grab mounting seat, the grab mounting seat it is another
One end is provided with grab mounting seat fastening screw；
Deck fastening screw is installed on the vertical rack of the deck.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720071661.2U CN206528612U (en) | 2017-01-20 | 2017-01-20 | A kind of fixed-wing unmanned plane buckle locking mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720071661.2U CN206528612U (en) | 2017-01-20 | 2017-01-20 | A kind of fixed-wing unmanned plane buckle locking mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206528612U true CN206528612U (en) | 2017-09-29 |
Family
ID=59918773
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720071661.2U Expired - Fee Related CN206528612U (en) | 2017-01-20 | 2017-01-20 | A kind of fixed-wing unmanned plane buckle locking mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206528612U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639308A (en) * | 2018-05-11 | 2018-10-12 | 南京航天猎鹰飞行器技术有限公司 | A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle |
-
2017
- 2017-01-20 CN CN201720071661.2U patent/CN206528612U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639308A (en) * | 2018-05-11 | 2018-10-12 | 南京航天猎鹰飞行器技术有限公司 | A kind of wing mechanism for assembling-disassembling for Fixed Wing AirVehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170929 |