CN206782098U - A kind of unmanned plane intelligent positioning sensor - Google Patents
A kind of unmanned plane intelligent positioning sensor Download PDFInfo
- Publication number
- CN206782098U CN206782098U CN201720384801.1U CN201720384801U CN206782098U CN 206782098 U CN206782098 U CN 206782098U CN 201720384801 U CN201720384801 U CN 201720384801U CN 206782098 U CN206782098 U CN 206782098U
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- unmanned plane
- chute
- fixed disk
- groove
- sliding block
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Abstract
The utility model discloses a kind of unmanned plane intelligent positioning sensor, including unmanned plane body and alignment sensor, unmanned plane body lower end is provided with standing groove, clamping is provided with slide bar in chute, slide bar both ends are provided with sliding block, and slide bar both sides extend through two connecting rod upper ends, the lower end of two connecting rods is fixedly mounted on the outside of fixed disk, alignment sensor is placed in the fixing groove of fixed disk, standing groove lower end inner wall is provided with groove, groove the inner is fixed with fixing axle, and movable sleeve is connected to set pivot pin nail in fixing axle.The utility model structure to alignment sensor when installing or removing, draw ring is pulled manually, set pivot pin nail is set to depart from pin-and-hole under a stretching force, so as to which fixed disk be pulled out, slided by sliding block in chute, the stability during fixed disk moves up and down is improved, so as to realize the installation of alignment sensor or pull down, fixed disk is decontroled simultaneously, making it, it is reattached in standing groove under the action of the spring.
Description
Technical field
The utility model unmanned air vehicle technique field, specially a kind of unmanned plane intelligent positioning sensor.
Background technology
Unmanned plane is a kind of unmanned vehicle manipulated by radio robot or itself presetting apparatus.Mesh
Before, in civil area, ground mapping unmanned plane, geological exploration unmanned plane, disaster monitoring unmanned plane, meteorological detection unmanned plane, sky
Middle traffic control unmanned plane, border control unmanned plane, communication relay unmanned plane, pesticide spraying unmanned plane research and apply in state
It is inside and outside all in continuous development.Wherein alignment sensor is sensor important in unmanned plane, due to by airframe structure
Limitation, alignment sensor is typically secured in unmanned plane body, so cause unmanned plane user unmanned plane is reequiped or
It is very inconvenient during more emat sensor, it is this it is proposed that a kind of unmanned plane intelligent positioning sensor is used to solve the above problems.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane intelligent positioning sensor, to solve above-mentioned background technology
The problem of middle proposition.
To achieve the above object, the utility model provides following technical scheme：A kind of unmanned plane intelligent positioning sensor,
Including unmanned plane body and alignment sensor, the unmanned plane body lower end is provided with standing groove, the front and rear inwall of the standing groove
On be fixed with chute, in the chute clamping be provided with slide bar, the slide bar both ends are provided with sliding block, and the sliding block is located at chute
It is interior, and sliding block bottom is fixedly connected with the bottom of chute by spring, and slide bar both sides extend through two connecting rod upper ends, this two
The lower end of individual connecting rod is fixedly mounted on the outside of fixed disk, and the alignment sensor is placed in the fixing groove of fixed disk, and
The left and right sides of fixed disk is provided with pin-and-hole, and the standing groove lower end inner wall of respective pin hole is provided with groove, and the groove is inner solid
Surely fixing axle is provided with, movable sleeve is connected to set pivot pin nail in the fixing axle, and is socketed and sets in the fixing axle in the outside of set pivot pin nail
There is pin spring.
Preferably, the quantity of the chute is two groups, and its inner structure is T font structures, and its A/F is more than slide bar
Diameter, and be more than the length of connecting rod less than the diameter of sliding block, the length of the chute.
Preferably, the spring is located in chute, and its upper and lower ends is fixedly connected with sliding block, chute bottom respectively, should
The reduction length of spring is more than the length of connecting rod, and spring is constantly in compressive state.
Preferably, the diameter of the fixing groove and the diameter of alignment sensor are consistent.
Preferably, the outer end of the set pivot pin nail is dome-type structure, and pin-and-hole is dome-type structure.
Preferably, the fixed disk bottom is movably equipped with draw ring.
Compared with prior art, the beneficial effects of the utility model are：The utility model structure is entered to alignment sensor
During row installation or removal, draw ring is pulled manually, set pivot pin nail is departed from pin-and-hole under a stretching force, so as to which fixed disk be pulled out,
Slided by sliding block in chute, the stability during fixed disk moves up and down is improved, so as to realize the peace of alignment sensor
Fill or pull down, while decontrol fixed disk, making it, it is reattached in standing groove under the action of the spring.
Brief description of the drawings
Fig. 1 is the utility model Structure explosion diagram；
In figure：1 unmanned plane body, 2 standing grooves, 3 slide bars, 31 sliding blocks, 4 chutes, 5 fixed disks, 51 fixing grooves, 6 connecting rods,
7 springs, 8 alignment sensors, 9 grooves, 10 fixing axles, 11 sets of pivot pin nails, 12 pin springs, 13 pin-and-holes, 14 draw rings.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Referring to Fig. 1, the utility model provides a kind of technical scheme：A kind of unmanned plane intelligent positioning sensor, including
Unmanned plane body 1 and alignment sensor 8, the lower end of unmanned plane body 1 are provided with standing groove 2, fix and set on the front and rear inwall of standing groove 2
Have a chute 4, in chute 4 clamping be provided with slide bar 3, the both ends of slide bar 3 are provided with sliding block 31, and sliding block 31 is located in chute 4, and sliding block 31
Bottom is fixedly connected with the bottom of chute 4 by spring 7, and the both sides of slide bar 3 extend through two upper ends of connecting rod 6, the number of chute 4
Measure as two groups, and its inner structure is T font structures, its A/F is more than the diameter of slide bar 3, and is less than the diameter of sliding block 31,
The length of the chute 4 is more than the length of connecting rod 6, and spring 7 is located in chute 4, and its upper and lower ends respectively with sliding block 31, chute
4 bottoms are fixedly connected, and the reduction length of the spring 7 is more than the length of connecting rod 6, and spring 7 is constantly in compressive state, passes through
Sliding block 31 slides in chute 4, improves the stability during fixed disk 5 moves up and down, decontrols fixed disk 5, make it in spring 7
In the presence of its be reattached in standing groove 2.
The lower end of two connecting rods 6 is fixedly mounted on the outside of fixed disk 5, and alignment sensor 8 is placed on fixed disk 5
In fixing groove 51, the diameter of fixing groove 51 and the diameter of alignment sensor 8 are consistent, and the bottom of fixed disk 5 is movably equipped with draw ring
14。
And the left and right sides of fixed disk 5 is provided with pin-and-hole 13, and the lower end inner wall of standing groove 2 of respective pin hole 13 is provided with groove
9, the inner of groove 9 is fixed with fixing axle 10, and movable sleeve is connected to set pivot pin nail 11 in fixing axle 10, and covers the outside of pivot pin nail 11
Fixing axle 10 on set be equipped with pin spring 12, the outer end of set pivot pin nail 11 is dome-type structure, and pin-and-hole 13 is dome-type
Structure, draw ring 14 is pulled manually, set pivot pin nail 11 is departed from pin-and-hole 13 under a stretching force.
Operation principle：The utility model structure pulls draw ring manually when being installed or removed to alignment sensor 8
14, set pivot pin nail 11 is departed from pin-and-hole 13 under a stretching force, so as to which fixed disk 5 be pulled out, slided by sliding block 31 in chute 4
It is dynamic, the stability during fixed disk 5 moves up and down is improved, so as to realize the installation of alignment sensor 8 or pull down, is decontroled simultaneously
Fixed disk 5, make its in the presence of spring 7 its be reattached in standing groove 2.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane intelligent positioning sensor, including unmanned plane body (1) and alignment sensor (8), the unmanned plane
Body (1) lower end is provided with standing groove (2), it is characterised in that：Chute (4) is fixed with the front and rear inwall of the standing groove (2),
The interior clamping of the chute (4) is provided with slide bar (3), and slide bar (3) both ends are provided with sliding block (31), and the sliding block (31) is located at chute
(4) in, and sliding block (31) bottom is fixedly connected with the bottom of chute (4) by spring (7), and slide bar (3) both sides extend through two
Individual connecting rod (6) upper end, the lower end of two connecting rods (6) are fixedly mounted on the outside of fixed disk (5), the alignment sensor
(8) it is placed in the fixing groove (51) of fixed disk (5), and the left and right sides of fixed disk (5) is provided with pin-and-hole (13), and respective pin hole
(13) standing groove (2) lower end inner wall is provided with groove (9), and described groove (9) the inner is fixed with fixing axle (10), described solid
Movable sleeve is connected to set pivot pin nail (11) on dead axle (10), and set is equipped with pin in the fixing axle (10) in the outside of set pivot pin nail (11)
Langrage spring (12).
A kind of 2. unmanned plane intelligent positioning sensor according to claim 1, it is characterised in that：The chute (4)
Quantity is two groups, and its inner structure is T font structures, and its A/F is more than the diameter of slide bar (3), and less than sliding block (31)
Diameter, the length of the chute (4) are more than the length of connecting rod (6).
A kind of 3. unmanned plane intelligent positioning sensor according to claim 1, it is characterised in that：Spring (7) position
In chute (4), and its upper and lower ends is fixedly connected with sliding block (31), chute (4) bottom respectively, the compression length of the spring (7)
Degree is more than the length of connecting rod (6), and spring (7) is constantly in compressive state.
A kind of 4. unmanned plane intelligent positioning sensor according to claim 1, it is characterised in that：The fixing groove (51)
Diameter and the diameter of alignment sensor (8) be consistent.
A kind of 5. unmanned plane intelligent positioning sensor according to claim 1, it is characterised in that：The set pivot pin nail
(11) outer end is dome-type structure, and pin-and-hole (13) is dome-type structure.
A kind of 6. unmanned plane intelligent positioning sensor according to claim 1, it is characterised in that：The fixed disk (5)
Bottom is movably equipped with draw ring (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720384801.1U CN206782098U (en) | 2017-04-05 | 2017-04-05 | A kind of unmanned plane intelligent positioning sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720384801.1U CN206782098U (en) | 2017-04-05 | 2017-04-05 | A kind of unmanned plane intelligent positioning sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206782098U true CN206782098U (en) | 2017-12-22 |
Family
ID=60707577
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720384801.1U Expired - Fee Related CN206782098U (en) | 2017-04-05 | 2017-04-05 | A kind of unmanned plane intelligent positioning sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206782098U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108448061A (en) * | 2018-04-30 | 2018-08-24 | 中航锂电（江苏）有限公司 | Lithium battery cantilever rewinds tooling |
-
2017
- 2017-04-05 CN CN201720384801.1U patent/CN206782098U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108448061A (en) * | 2018-04-30 | 2018-08-24 | 中航锂电（江苏）有限公司 | Lithium battery cantilever rewinds tooling |
| CN108448061B (en) * | 2018-04-30 | 2023-11-28 | 中创新航科技股份有限公司 | Lithium battery cantilever rewinding tool |
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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: 20171222 Termination date: 20200405 |