CN207876015U - A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin - Google Patents
A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin Download PDFInfo
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- CN207876015U CN207876015U CN201820200401.5U CN201820200401U CN207876015U CN 207876015 U CN207876015 U CN 207876015U CN 201820200401 U CN201820200401 U CN 201820200401U CN 207876015 U CN207876015 U CN 207876015U
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- screw
- fixed seat
- aerial vehicle
- unmanned aerial
- locking pin
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Abstract
The utility model discloses a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pins, including ejector pin, fixed seat, screw and resetting spring, fixed seat is fixedly connected in fixed plate, ejector pin is Step Shaft, it is socketed with resetting spring, fixed seat endoporus rear screw is inserted into and is connected to screw, resetting spring one end is resisted against on ejector pin step, the other end is resisted against in fixed seat endoporus, and screw is connected to rotating handles across endoporus.The utility model is mounted on positioning and locking of the locking pin to shifting sledge of fixed guide rail both sides fixed plate, it is loosened after effectivelying prevent fixed guide rail and shifting sledge docking, to improve holder or gondola installation reliability, solve the problems, such as that the existing installation of current existing fast assembling disassembling structure is unreliable and there is loosening, the locking of the sliding panel after installation can be fast implemented, it is also convenient for when dismounting quick, the locking pin formed using ejector pin, fixed seat, resetting spring and screw, lock convenient and efficient, reliable lock.
Description
Technical field
The utility model is related to a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pins, belong to multi-rotor unmanned aerial vehicle
Inspection technology multi-load configuration technology field.
Background technology
With the development of science and technology, multi-rotor unmanned aerial vehicle technology reaches its maturity, it is widely applied to electric inspection process, security protection is patrolled
The various fields such as inspection, forestry inspection, and the various carry equipment in the successful application and unmanned plane of unmanned air vehicle technique have closely
Relationship.Under normal conditions, it is that the load such as video camera are mounted on holder or in gondola, then by holder or gondola and unmanned plane
It is connected, unmanned plane obtains the certain types of environmental informations such as image when executing patrol task by carry camera loading device.
Existing holder or pod equipment are largely that the mode being connected by screw is fixed in multi-rotor unmanned aerial vehicle,
Holder or gondola are to separate with unmanned plane in transit, are reached after specifying region of patrolling and examining, then holder or gondola are mounted on
On unmanned plane, patrol task could be executed after the completion of assembly, at present frequently with screw installation form need expend more time,
It is unfavorable for the convenient installation and dismounting of carry equipment, influences the rapidity that aircraft executes patrol task, have been unable to meet more rotors
The demand for development of one machine multi-load of unmanned plane configuration, and there are the following problems：
1）The mounting means majority of existing multi-rotor unmanned aerial vehicle carry equipment is directly fixed by holder or gondola using screw
On unmanned plane, unmanned plane will consume a longer time that installation holder or gondola, scene also need to be equipped with before executing patrol task
The kit of mounting screw after unmanned plane has executed aerial mission, also needs to utilize corresponding machine tool by fixing screws
It disassembles, inconvenient victory, time used time is long；
2）Also there are a small number of holders or gondola to use rapid dismounting apparatus at present, but the structure that changes the outfit is complex, and is easy
There are reliability or the phenomenons of stability deficiency.
Invention content
The technical problems to be solved in the utility model is：A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking is provided
Pin mainly solves the problems such as inconvenient prompt, short time consumption is long when holder or gondola are mounted on unmanned plane, and mission payload changes the outfit
Simple operation and connection is reliable.
The technical solution that the utility model is taken is：A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin, packet
Ejector pin, fixed seat, screw and resetting spring are included, fixed seat is fixedly connected in fixed plate, and ejector pin is Step Shaft, is socketed with reset
Spring is inserted into fixed seat endoporus rear screw and is connected to screw, and resetting spring one end is resisted against on ejector pin step, and the other end is resisted against
In fixed seat endoporus, screw is connected to rotating handles across endoporus.
Preferably, above-mentioned locking pin outside setting two in every piece of fixed plate.
Preferably, above-mentioned rotating handles are a strip bar, and fixed seat outer end is provided with limiting slot, and rotating handles are movably
It is embedded into limiting slot, limit groove depth is more than ejector pin and stretches out fixed plate inside length.
Preferably, above-mentioned ejector pin front end is provided with tapered portion, and cylinder brachycephaly is arranged in tapered portion outer end.
Preferably, above-mentioned fixed seat is connected to by two engaging lugs in fixed plate.
Advantageous effect：Compared with prior art, the utility model is mounted on the locking pin pair of fixed guide rail both sides fixed plate
The positioning and locking of shifting sledge loosens after effectivelying prevent fixed guide rail and shifting sledge docking, to improve holder or
Gondola installation reliability solves the problems, such as that the existing installation of current existing fast assembling disassembling structure is unreliable and there is loosening,
Can fast implement the locking of the sliding panel after installation, when dismounting be also convenient for it is quick, use ejector pin, fixed seat, resetting spring with
And the locking pin of screw composition, lock convenient and efficient, reliable lock.
Description of the drawings
Fig. 1 is the front end perspective structural schematic diagram that the utility model is used for Rapid replacing device；
Fig. 2 is the back end perspective structural schematic diagram that the utility model is used for Rapid replacing device；
Fig. 3 is the structural schematic diagram of the utility model；
Fig. 4 is the cross-sectional view of Fig. 3.
Specific implementation mode
Below in conjunction with the accompanying drawings and the utility model is described further in specific embodiment.
Embodiment 1：As Figure 1-Figure 4, a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin, the locking pin
8 include ejector pin 9, fixed seat 10, screw 11 and resetting spring 12, and fixed seat 10 is fixedly connected by two engaging lugs 6 using screw
In fixed plate, ejector pin 9 is Step Shaft, is socketed with resetting spring 12, is inserted into 10 endoporus rear screw of fixed seat and is connected to screw 11,
12 one end of resetting spring is resisted against on 9 step of ejector pin, and the other end is resisted against in 10 endoporus of fixed seat, and endoporus is stepped hole, screw
11 are connected to rotating handles 13 across endoporus, and rotating handles 13 are located at outside fixed seat 10.
Preferably, two locking pins 8 are arranged in the above-mentioned outside in every piece of fixed plate.
Preferably, above-mentioned rotating handles 13 are a strip bar, and inner end is arcwall face, and 10 outer end of fixed seat is provided with limiting slot
14, rotating handles are movably embedded into limiting slot 14, and 14 depth of limiting slot is more than ejector pin 9 and stretches out fixed plate inside length.
Preferably, 9 front end of above-mentioned ejector pin is provided with tapered portion, and cylinder brachycephaly is arranged in tapered portion outer end.
Preferably, above-mentioned fixed seat 10 is connected to by two engaging lugs 6 in fixed plate.
Locking pin operating principle：Rotating handle is exited into limiting slot, ejector pin 9 is retracted into fixed plate, and sliding panel installs
Afterwards, rotating handle is pushed into limiting slot, under the action of resetting spring, ejector pin ejection is resisted against on sliding panel, to realize
Locking positioning can adjust the length of locking pin using screw, adjust spring force, and application range is wider.
Embodiment 2：As Figure 1-Figure 4, above-mentioned locking pin is used for a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal
Device, including fixed guide rail 1 and shifting sledge 4, fixed guide rail 1 is using the fixed plate of two relatively symmetrically placed L-types, shifting sledge
4 using two back to symmetrical handstand L-type sliding panel, lower end is fixedly connected on the carry plate 5 of holder or gondola, two sliding panels
Upper end corresponds to and is articulated on two fixed plate lower ends and can be moved along fixed plate length direction, and the fixed plate of fixed guide rail both sides is logical
Bolt hole carry corresponding to immediately below unmanned plane the position connection of eight, top is crossed, corresponding shifting sledge passes through solid in its bottom
Determine bolt to connect with holder or gondola carry plate.
Preferably, it is provided with connecting plate 7 on rear side of two fixed plates of above-mentioned fixed guide rail 1, electrical public affairs is installed on connecting plate 7
Connector connector 2 and electrical female pin end connector 3, the two sliding panels rear side of shifting sledge 4 are provided with buttcover plate 16, buttcover plate
The electrical female connector connector 17 and electricity of the electrical pin end connector 2 of face and electrical female pin end connector 3 are installed on 16
Gas pin and box sub connector 18.
Preferably, it is provided with locking pin 8 on the outside of above-mentioned fixed plate, 8 inner end of locking pin is resisted against sliding after stretching into fixed plate
Plate upper end locking.
Preferably, it is both provided with symmetrical lightening hole 15 on above-mentioned two fixed plate and two sliding panels.
Operating process：1）Two fixed plates are mounted on unmanned plane lower part using screw is opposite, and electrical connector is installed
On connecting plate, connecting plate is fixedly connected on by screw in two fixed plates；2）By two sliding panels back to being fixedly connected on carry
On plate, and buttcover plate is fixedly connected on sliding panel, gondola or holder are fixedly connected on carry plate；3）Shifting sledge pushes away
Enter in fixed guide rail, using locking pin locked after cable butting is good, completes Quick universal, when dismounting unclamps locking pin first, pushes away
Go out sliding panel.
Above-mentioned Rapid replacing device has the following advantages that：
（1）By the two opposite L-type fixed plates being fixedly connected on unmanned plane and it is fixedly connected on gondola or holder
Back to handstand L-type sliding panel, sliding panel can mount sliding in fixed plate, and guidance quality is good, realize gondola or holder
Quickly installation, convenient disassembly greatly improve the efficiency of loading and unloading, improve the efficiency that aircraft executes patrol task, also have structure letter
Single, easy to operate feature；
（2）It is arranged on rear side of fixed plate on rear side of electrical pin end connector and electrical female pin end connector and positive sliding panel
Electrical female connector connector and electrical pin and box sub connector are set, by sliding the sliding panel of lower end, can quickly carry out electricity
The grafting of cable jointing realizes multiple processes, further improves installation effectiveness, reduce independent connecting cable to dress, once mounting
Caused installation effectiveness is low, solves the inconvenience that also plug electric connector after Quick universal structure removes again, and installation is electrical
The connecting plate and the electrical female connector connector of installation of pin end connector and electrical female pin end connector and electrical pin and box sub
On the one hand the buttcover plate of connector plays the role of installation, on the other hand, play reinforce the fixed plate firm effect of fixed guide rail with
And position-limiting action, support relatively reliable, stability higher；
（3）By the locking pin mounted on fixed guide rail both sides fixed plate to the positioning and locking of shifting sledge, it effectively prevent
It loosens after fixed guide rail and shifting sledge docking, to improve holder or gondola installation reliability, solves at present
The existing installation of some fast assembling disassembling structures is unreliable and there are problems that loosening, and can fast implement the sliding panel after installation
Locking, when dismounting, are also convenient for quick, to be formed using ejector pin, fixed seat, resetting spring and screw locking pin, and locking facilitates fast
Victory, reliable lock；
（4）Lightening hole is set and combines easy guide rail structure, it is light-weight, while ensureing Quick universal function, reach
Light-weighted requirement has been arrived, the carry load weight of multi-rotor unmanned aerial vehicle is reduced, has been conducive to unmanned plane and easily enters inspection
In flight operation；
（5）The fast assembling-disassembling mission payload being related to meets the exchange of multiple-task load, is not necessarily to any installation tool, operation
Simply, solve unmanned plane multi-load configuration in be alternately accomplished patrol task when Quick universal task and demand.
In conclusion the Rapid replacing device being related to, can shorten multi-rotor unmanned aerial vehicle carry load in cruising inspection system
Time that changes the outfit for replacing does not need auxiliary tools dismounting can be completed, while can realize electric interfaces pin end and female connector
To inserting connection, it is easy to operate, simple in structure, reliability is high, meet the hair of one machine multi-load of modern multi-rotor unmanned aerial vehicle configuration
Exhibition demand.
Above description is only a specific implementation of the present invention, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art within the technical scope disclosed by the utility model, can readily occur in variation
Or replace, it should be covered within the scope of the utility model, therefore, the scope of protection of the utility model should be with the power
Subject to the protection domain that profit requires.
Claims (5)
1. a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin, it is characterised in that：Including ejector pin（9）, fixed seat
（10）, screw（11）And resetting spring（12）, fixed seat（10）It is fixedly connected in fixed plate, ejector pin（9）For Step Shaft, socket
There is resetting spring（12）, it is inserted into fixed seat（10）Endoporus rear screw is connected to screw（11）, resetting spring（12）One end is resisted against
Ejector pin（9）On step, the other end is resisted against fixed seat（10）In endoporus, screw（11）It is connected to rotating handles across endoporus
（13）.
2. a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin according to claim 1, it is characterised in that：Lock
Rationed marketing（8）The outside setting two in every piece of fixed plate.
3. a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin according to claim 1, it is characterised in that：Rotation
Handle hand（13）For a strip bar, fixed seat（10）Outer end is provided with limiting slot（14）, rotating handles are movably embedded into limit
Position slot（14）It is interior, limiting slot（14）Depth is more than ejector pin（9）Stretch out fixed plate inside length.
4. a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin according to claim 1, it is characterised in that：Top
Pin（9）Front end is provided with tapered portion, and cylinder brachycephaly is arranged in tapered portion outer end.
5. a kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin according to claim 1, it is characterised in that：Gu
Reservation（10）Pass through two engaging lugs（6）It is connected in fixed plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820200401.5U CN207876015U (en) | 2018-02-06 | 2018-02-06 | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820200401.5U CN207876015U (en) | 2018-02-06 | 2018-02-06 | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207876015U true CN207876015U (en) | 2018-09-18 |
Family
ID=63509909
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820200401.5U Active CN207876015U (en) | 2018-02-06 | 2018-02-06 | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin |
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| CN (1) | CN207876015U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110654556A (en) * | 2019-10-08 | 2020-01-07 | 深圳供电局有限公司 | Unmanned aerial vehicle load dismouting structure |
| CN113232877A (en) * | 2021-06-11 | 2021-08-10 | 江西洪都航空工业集团有限责任公司 | Nacelle quick-release suspension joint |
-
2018
- 2018-02-06 CN CN201820200401.5U patent/CN207876015U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110654556A (en) * | 2019-10-08 | 2020-01-07 | 深圳供电局有限公司 | Unmanned aerial vehicle load dismouting structure |
| CN113232877A (en) * | 2021-06-11 | 2021-08-10 | 江西洪都航空工业集团有限责任公司 | Nacelle quick-release suspension joint |
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