CN208789923U - A kind of portable fast plug-in unit of unmanned plane - Google Patents
A kind of portable fast plug-in unit of unmanned plane Download PDFInfo
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- CN208789923U CN208789923U CN201821049303.2U CN201821049303U CN208789923U CN 208789923 U CN208789923 U CN 208789923U CN 201821049303 U CN201821049303 U CN 201821049303U CN 208789923 U CN208789923 U CN 208789923U
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- trapezoidal
- plug
- fixedly connected
- aircraft
- fast
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Abstract
The utility model discloses a kind of portable fast plug-in units of unmanned plane, belong to the fast plug-in unit field of unmanned plane.A kind of portable fast plug-in unit of unmanned plane, including fast plate, fast plate is equipped with the trapezoidal plug of the first Loading End and the trapezoidal plug of the second Loading End, and fast plate, which is provided with, mentions a mouthful slot, and bathrocephaly is arranged in the trapezoidal plug of the first Loading End, it is flexibly connected on bathrocephaly with small terraced head, bathrocephaly is connect with the second card slide bar, and bathrocephaly is connect with opening column, and opening column is connect with fixing bolt, the trapezoidal plug of second Loading End is fixedly connected with the first card slide bar, and the trapezoidal plug of the second Loading End is connect with the first connecting column.The trapezoidal plug of first Loading End matches with the second aircraft end trapezoidal socket, and the trapezoidal plug of the second Loading End matches with the first aircraft end trapezoidal socket.It realizes Fast Installation, disassembly and the replacement of load, guarantees the safety and firmness of load, while keeping the tailored appearance of aircraft after installed load good-looking, light-weight, loss when reducing to Aircraft.
Description
Technical field
The utility model relates to the fast plug-in unit fields of unmanned plane, more specifically to a kind of portable fast plug-in unit of unmanned plane.
Background technique
In the fast plug-in unit of current unmanned plane, Fast Installation, disassembly and the replacement of load, process can not achieve in use process
It is cumbersome, while cannot be guaranteed the safety and firmness of load and weight is not light, loss when increasing to Aircraft flies after installed load
The appearance of machine is also wordy good-looking.
Utility model content
1. technical problems to be solved
For the problem that the fast plug-in unit installation and replacement of unmanned plane existing in the prior art are slow, the purpose of this utility model is that
A kind of portable fast plug-in unit of unmanned plane is provided, it is inconvenient that it can solve load installation, and influences the problem of using.
2. technical solution
To solve the above problems, the utility model adopts the following technical scheme.
A kind of portable fast plug-in unit of unmanned plane, including fast plate, the fast plate upper surface right side are equipped with the first load
Trapezoidal plug is held, the trapezoidal plug of the second Loading End is installed on the left of the fast plate upper surface, the fast plate right end is provided with
A mouthful slot is mentioned, bathrocephaly is arranged in the trapezoidal plug of the first Loading End, and the bathrocephaly upper surface is provided with small terraced head slot, described small
It is flexibly connected inside terraced head slot with small terraced head, bathrocephaly left and right sides outer surface middle part and the second fixed company of card slide bar one side
It connects, the bathrocephaly lower surface is fixedly connected with opening column upper end, outer surface lower end and fixed spiral shell at left and right sides of the opening column
Bolt is fixedly connected on one side, and the small terraced head lower end is fixedly connected with first support spring one end, and first support spring is another
End is fixedly connected with connecting plate top upper surface, and connecting plate top lower surface is fixedly connected with second support spring one end,
The second support spring other end is fixedly connected with the trapezoidal plug inside bottom surface of the first Loading End, the connecting plate bottom end and top
Pressing plate one end is fixedly connected, and the top pressing board other end mentions a mouthful slot pivot bush unit, the trapezoidal plug of the second Loading End with described
Left and right sides outer surface is fixedly connected on one side with the first card slide bar, and the trapezoidal plug lower surface of the second Loading End is connect with first
Column upper surface is fixedly connected.
Preferably, the trapezoidal plug of the first Loading End matches with the second aircraft end trapezoidal socket, second aircraft
End trapezoidal socket upper surface rear and front end is provided with the second threaded hole, the setting of second aircraft end trapezoidal socket upper surface middle-end
There is the terraced head slot of card, the terraced head slot of the card matches with the small terraced head, second aircraft end trapezoidal socket inner surface or so two
Middle side part is fixedly connected on one side with the second card sliding slot, and the second card sliding slot matches with the second card slide bar, second aircraft
End is provided with block of postponing on the right side of trapezoidal socket top.
Preferably, it is characterised in that: the trapezoidal plug of the second Loading End matches with the first aircraft end trapezoidal socket, institute
It states the first aircraft end trapezoidal socket upper surface left and right ends and is provided with the first threaded hole, table in the trapezoidal socket of first aircraft end
Middle part is fixedly connected on one side with the first card sliding slot at left and right sides of face, and the first card sliding slot matches with the first card slide bar.
Preferably, described top pressing board one end and connecting plate bottom end junction and rotating shaft device pivot bush unit, the rotation
Shaft device both ends are fixedly connected with opening column two sides inner wall respectively.
Preferably, first connecting column is threadedly coupled by external screw thread with fast plate.
3. beneficial effect
Compared with the prior art, utility model has the advantages that
(1) the utility model is provided with the trapezoidal plug of the first Loading End and the trapezoidal plug of the second Loading End, the first Loading End
Trapezoidal plug is function of tonic chord plug, function plug supplemented by the trapezoidal plug of the second Loading End, the interaction of sound of sighing major-minor function plug
Under, it can be very good to solve safety and firmness when unmanned plane load, reliable fast plug device be provided, diversified load is completed
Problem；
(2) the utility model is connected separately with first on the trapezoidal plug of the first Loading End and the trapezoidal plug of the second Loading End
Card slide bar and the second card slide bar, in the matched trapezoidal plug in the first aircraft end and the second trapezoidal plug in aircraft end respectively
It is connected with the first card sliding slot and the second card sliding slot, passes through the card slip of the first card sliding slot and the first card slide bar, the second card sliding slot
With the card slip of the second card slide bar, the fast firm effect of inserting of the fast plug-in unit is made to get a promotion, while improving load installing and dismounting
It is quick, it is easy；
(3) the utility model is additionally provided with small terraced head, and small terraced head is connected on the trapezoidal plug of the first Loading End, small
Terraced head in fast insert with and its card ladder head slot card column for matching, it is trapezoidal slotting in the trapezoidal plug of the first Loading End and the first aircraft end
When slot is clamped, secondary clamping is formed by small terraced head and the clamping for blocking terraced head slot, further increases the peace of the utility model
Full firm effect, when release, which only need to press top pressing board under force, makes small terraced head stretch inwards, easy to disassemble；
(4) the utility model has the advantages of simple structure, average weight, realizes Fast Installation, disassembly and the replacement of load, process
It is convenient, while loss when guaranteeing the safety and firmness of load and reducing to Aircraft, the aircraft appearance after installed load are also simple
It is clean good-looking.
Detailed description of the invention
Fig. 1 is the plug positive structure diagram of the utility model；
Fig. 2 is the trapezoidal plug schematic perspective view of the first Loading End of the utility model；
Fig. 3 is the second aircraft end trapezoidal socket schematic perspective view of the utility model；
Fig. 4 is the trapezoidal plug inside schematic cross-sectional view of the first Loading End of the utility model；
Fig. 5 is the first aircraft end trapezoidal socket positive structure diagram of the utility model；
Fig. 6 is the first aircraft end trapezoidal socket overlooking structure diagram of the utility model；
Fig. 7 is the trapezoidal plug enlarged structure schematic diagram of the second Loading End of the utility model.
Figure label explanation:
1, fast plate；2, the trapezoidal plug of the first Loading End；3, the trapezoidal plug of the second Loading End；4, catching groove is mentioned；5, first connects
Connect column；6, external screw thread；7, the first card slide bar；8, the first aircraft end trapezoidal socket；9, the first card sliding slot；10, the first threaded hole；
11, fixing bolt；12, bathrocephaly；13, opening column；14, top pressing board；15, small terraced head slot；16, small terraced head；17, the second card is slided
Bar；18, it postpones block；19, the second card sliding slot；20, the second threaded hole；21, block terraced head slot；22, the second aircraft end trapezoidal socket；
23, the first support spring；24, connecting plate；25, the second support spring；26, rotating shaft device.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model；The technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe；Obviously；The described embodiments are only a part of the embodiments of the utility model；Rather than whole
Embodiment.Based on the embodiments of the present invention；Those of ordinary skill in the art are without making creative work
Every other embodiment obtained；It fall within the protection scope of the utility model.
Embodiment 1: Fig. 1-6, a kind of portable fast plug-in unit of unmanned plane, including fast plate 1, fast 1 upper surface of plate are please referred to
Right side is equipped with the trapezoidal plug 2 of the first Loading End, is equipped with the trapezoidal plug of the second Loading End on the left of fast 1 upper surface of plate, fast to insert
1 right end of plate, which is provided with, mentions mouthful slot 4, and bathrocephaly 12 is arranged in the trapezoidal plug 2 of the first Loading End, and 12 upper surface of bathrocephaly is provided with small ladder
Head slot 15, small 15 inside of ladder head slot are flexibly connected with small terraced head 16, slide in the middle part of 12 left and right sides outer surface of bathrocephaly with the second card
Bar 17 is fixedly connected on one side, and 12 lower surface of bathrocephaly is fixedly connected with 13 upper end of opening column, 13 left and right sides outer surface of opening column
Lower end is fixedly connected on one side with fixing bolt 11, and small ladder 16 lower end of head is fixedly connected with 23 one end of the first support spring, and first
Support 23 other end of spring is fixedly connected with 24 top upper surface of connecting plate, 24 top lower surface of connecting plate and the second support spring 25
One end is fixedly connected, and 25 other end of the second support spring is fixedly connected with trapezoidal 2 inner bottom surface of plug of the first Loading End, connecting plate
24 bottom ends are fixedly connected with 14 one end of top pressing board, 14 other end of top pressing board and mention 4 pivot bush unit of mouthful slot, and the second Loading End is trapezoidal to be inserted
First 3 left and right sides outer surface is fixedly connected on one side with the first card slide bar 7, and trapezoidal 3 lower surface of plug of the second Loading End connects with first
5 upper surface of column is connect to be fixedly connected.
The trapezoidal plug 2 of first Loading End matches with the second aircraft end trapezoidal socket 22, the second aircraft end trapezoidal socket 22
Upper surface rear and front end is provided with the second threaded hole 20, and 22 upper surface middle-end of the second aircraft end trapezoidal socket is provided with the terraced head slot of card
21, block terraced head slot 21 and matches with small terraced head 16, middle part and the second card at left and right sides of 22 inner surface of the second aircraft end trapezoidal socket
Sliding slot 19 is fixedly connected on one side, and the second card sliding slot 19 matches with the second card slide bar 17,22 top of the second aircraft end trapezoidal socket
Right side is provided with block 18 of postponing.
The trapezoidal plug 3 of second Loading End matches with the first aircraft end trapezoidal socket 8, on the first aircraft end trapezoidal socket 8
Surface left and right ends are provided with the first threaded hole 10, middle part and the first card at left and right sides of 8 inner surface of the first aircraft end trapezoidal socket
Sliding slot 9 is fixedly connected on one side, and the first card sliding slot 9 matches with the first card slide bar 7.
14 one end of top pressing board and 24 bottom end junction of connecting plate and 26 pivot bush unit of rotating shaft device, 26 liang of rotating shaft device
End is fixedly connected with 13 two sides inner wall of opening column respectively.
First connecting column 5 is threadedly coupled by external screw thread 6 with fast plate 1.
Working principle:
(5) when user uses the utility model device, the utility model device is installed first, utilizes spiral shell
First aircraft end trapezoidal socket 8 is fixed on by silk by the first threaded hole 10 that 8 upper surface of the first aircraft end trapezoidal socket is arranged
On aircraft end, the second aircraft end trapezoidal socket 22 is then passed through into 22 upper surface of the second aircraft end trapezoidal socket using using screw
The second threaded hole 20 being arranged is fixed on aircraft end, and fast plate 1 is fixed on Loading End, then that the second Loading End is trapezoidal
Plug 3 is screwed with fast plate 1 by the external screw thread 6 on the first connecting column 5 for being fixedly connected with its bottom end and is connect, by first
The trapezoidal plug 2 of Loading End with the fixing bolt 11 connecting at left and right sides of its lower end by being connected on fast plate 1；It is being inserted fastly
When operation, the trapezoidal plug 2 of the first Loading End is made to be directed at the second aircraft end trapezoidal socket 22, makes its clamping, while internal second
Card slide bar 17 and the alignment clamping of the second card sliding slot 19, while small terraced head 16 is during the clamping of the trapezoidal plug 2 of the first Loading End
Block 18 is postponed smoothly in slide card to the second aircraft end trapezoidal socket 22 by what is connected on the second aircraft end trapezoidal socket 22
Block in terraced head slot 21, realize safety and firmness effect slotting fastly, when disassembly, user is by press top pressing board 14, in power
Under the action of by rotating shaft device 26 drive 24 top of connecting plate play the role of it is downward then pull first support spring 23,
Make 16 retracted downward of small terraced head under the action of elastic force, while twitching the trapezoidal plug 2 of the first Loading End and dismantling, to top pressing board 14
After shedding power, the extruding force of the second support spring 25 is extended out, and the tensile-elasticity of the first support spring 23 is shunk, and restores small terraced head
Then original state makes the trapezoidal plug 3 of the second Loading End be directed at the first aircraft end trapezoidal socket 8, make its clamping, while internal first
Card slide bar 7 and the alignment clamping of the first card sliding slot 9, Fast Installation, disassembly and the replacement of load, mistake are realized using the utility model
Journey is convenient, while loss when guaranteeing the safety and firmness of load and reducing to Aircraft, the aircraft appearance after installed load
It is succinct good-looking.
It is described above；The only preferable specific embodiment of the utility model；But the protection scope of the utility model is not
It is confined to this；Anyone skilled in the art is within the technical scope disclosed by the utility model；It is practical according to this
Novel technical solution and its improvement design is subject to equivalent substitution or change；It should all cover in the protection scope of the utility model
It is interior.In addition, one word of " comprising " is not excluded for other elements or step, "one" word before the component is not excluded for including " multiple " be somebody's turn to do
Element.The multiple multiple elements stated in claim to a product can also by an element by software or hardware come real
It is existing.The first, the second equal words are used to indicate names, and are not indicated any particular order.
Claims (5)
1. a kind of portable fast plug-in unit of unmanned plane, including fast plate (1), it is characterised in that: on the right side of fast plate (1) upper surface
The trapezoidal plug of first Loading End (2) is installed, the trapezoidal plug of the second Loading End is installed on the left of fast plate (1) upper surface,
Fast plate (1) right end, which is provided with, to be mentioned a mouthful slot (4), and bathrocephaly (12) are arranged in the trapezoidal plug of the first Loading End (2), described
Bathrocephaly (12) upper surface is provided with small terraced head slot (15), and the small terraced head slot (15) is internal to be flexibly connected with small terraced head (16),
It is fixedly connected on one side in the middle part of outer surface with the second card slide bar (17) at left and right sides of the bathrocephaly (12), under the bathrocephaly (12)
Surface is fixedly connected with opening column (13) upper end, outer surface lower end and fixing bolt (11) one at left and right sides of the opening column (13)
Face is fixedly connected, and small terraced head (16) lower end is fixedly connected with the first support spring (23) one end, first support spring
(23) other end is fixedly connected with connecting plate (24) top upper surface, connecting plate (24) the top lower surface and the second support bullet
Spring (25) one end is fixedly connected, the second support spring (25) other end and the trapezoidal plug of the first Loading End (2) inner bottom surface
It is fixedly connected, connecting plate (24) bottom end is fixedly connected with top pressing board (14) one end, top pressing board (14) other end and institute
It states and mentions a mouthful slot (4) pivot bush unit, outer surface and the first card slide bar (7) one at left and right sides of the trapezoidal plug of the second Loading End (3)
Face is fixedly connected, and the trapezoidal plug of the second Loading End (3) lower surface is fixedly connected with the first connecting column (5) upper surface.
2. the portable fast plug-in unit of a kind of unmanned plane according to claim 1, it is characterised in that: first Loading End is trapezoidal
Plug (2) matches with the second aircraft end trapezoidal socket (22), two before and after second aircraft end trapezoidal socket (22) upper surface
End is provided with the second threaded hole (20), and second aircraft end trapezoidal socket (22) upper surface middle-end is provided with the terraced head slot of card
(21), the terraced head slot (21) of the card matches with the small terraced head (16), second aircraft end trapezoidal socket (22) inner surface
It is fixedly connected on one side in the middle part of the left and right sides with the second card sliding slot (19), the second card sliding slot (19) and second card slide bar (17) phase
Matching, second aircraft end trapezoidal socket (22) top right side are provided with block of postponing (18).
3. the portable fast plug-in unit of a kind of unmanned plane according to claim 1, it is characterised in that: second Loading End is trapezoidal
Plug (3) matches with the first aircraft end trapezoidal socket (8), first aircraft end trapezoidal socket (8) upper surface left and right ends
It is provided with the first threaded hole (10), middle part and the first card sliding slot at left and right sides of first aircraft end trapezoidal socket (8) inner surface
(9) it is fixedly connected on one side, the first card sliding slot (9) matches with the first card slide bar (7).
4. the portable fast plug-in unit of a kind of unmanned plane according to claim 1, it is characterised in that: described top pressing board (14) one end
With connecting plate (24) bottom end junction and rotating shaft device (26) pivot bush unit, rotating shaft device (26) both ends respectively with open
Oral pillar (13) two sides inner wall is fixedly connected.
5. the portable fast plug-in unit of a kind of unmanned plane according to claim 1, it is characterised in that: first connecting column (5)
It is threadedly coupled by external screw thread (6) with fast plate (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821049303.2U CN208789923U (en) | 2018-07-04 | 2018-07-04 | A kind of portable fast plug-in unit of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821049303.2U CN208789923U (en) | 2018-07-04 | 2018-07-04 | A kind of portable fast plug-in unit of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208789923U true CN208789923U (en) | 2019-04-26 |
Family
ID=66201843
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821049303.2U Expired - Fee Related CN208789923U (en) | 2018-07-04 | 2018-07-04 | A kind of portable fast plug-in unit of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208789923U (en) |
-
2018
- 2018-07-04 CN CN201821049303.2U patent/CN208789923U/en not_active Expired - Fee Related
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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: 20190426 Termination date: 20190704 |