CN209389569U - Unmanned plane ground line carries apparatus - Google Patents
Unmanned plane ground line carries apparatus Download PDFInfo
- Publication number
- CN209389569U CN209389569U CN201920423788.5U CN201920423788U CN209389569U CN 209389569 U CN209389569 U CN 209389569U CN 201920423788 U CN201920423788 U CN 201920423788U CN 209389569 U CN209389569 U CN 209389569U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- lap bars
- annular
- hinged seat
- shaped bracket
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses unmanned plane ground lines to carry apparatus, relates generally to carry apparatus field.Including covering the lap bars of X-shaped bracket, clip, hoop in ground lead pole on unmanned plane undercarriage；The annular that is equipped with of the X-shaped bracket carries platform, and the ring cavity diameter that the annular carries platform is greater than the width of earthing wire clip, and the annular carries platform and is equipped with overlap joint slot；The clip side in the middle part of short axle and lap bars by being rotatablely connected, and the length and overlap joint slot of the lap bars are adapted, and the side of the lap bars is wrapped with one layer of iron sheet.The utility model has the beneficial effects that: the ground lead pole that the worker of high altitude operation can very easily carry out carrying is removed from unmanned plane when using the present apparatus, the risk of high altitude operation is reduced.
Description
Technical field
The utility model relates to carry apparatus field, specifically unmanned plane ground line carries apparatus.
Background technique
The use of unmanned plane is more universal in power industry, rationally effective to utilize the work that mitigate worker significantly
It measures, improves construction efficiency.Ground lead pole was to hang on one's waist to climb up electric pole or pylon by worker in the past, had been had now
Using the mode of UAV flight, the difficulty that UAV flight transports ground lead pole is little, but the worker of high altitude operation is but
The ground lead pole that very easily carrying cannot be carried out is removed from unmanned plane, and high altitude operation is danger close, so design
A kind of device that the ground lead pole that the worker facilitating high altitude operation carrys out carrying is removed from unmanned plane is necessary.
Utility model content
The purpose of this utility model is to provide unmanned plane ground lines to carry apparatus, when using the present apparatus, high altitude operation
Worker can very easily by carrying and come ground lead pole removed from unmanned plane, reduce the risk of high altitude operation.
The utility model to achieve the above object, is achieved through the following technical solutions:
Unmanned plane ground line carries apparatus, is being grounded including covering the X-shaped bracket on unmanned plane undercarriage, clip, hoop
Lap bars in line line bar；The annular that is equipped with of the X-shaped bracket carries platform, and the ring cavity diameter that the annular carries platform is greater than ground connection
The width of line wire clamp, the annular carry platform and are equipped with overlap joint slot；The clip side in the middle part of short axle and lap bars by rotating
Connection, the length and overlap joint slot of the lap bars are adapted, and the side of the lap bars is wrapped with one layer of iron sheet.
One end of the lap bars is equipped with spring groove and telescopic rod, and adjustable spring is equipped in the spring groove, described flexible
One section of limit of bar is arranged in spring groove and contacts at the top of adjustable spring.
The X-shaped bracket includes rubber sleeve, the first hinged seat, hack lever and the second hinged seat, and the rubber sleeve is covered at nobody
Machine undercarriage end, first hinged seat are arranged on rubber sleeve, and the second hinged seat setting carries platform side in annular,
The hack lever both ends are hinged with the first hinged seat, the second hinged seat respectively.
The prior art is compared, the utility model has the beneficial effects that:
When using the present apparatus, lap bars are gone into level, such as the state of Figure of description Fig. 2, are then placed into ring
Shape is carried in the overlap joint slot on platform, is gone up to the air using UAV flight to high altitude operation position.The worker of high altitude operation grasps
The earthing wire clip of bottom is touched to top, can be released lap bars out of overlap joint slot, because the side of lap bars is wrapped with one
Layer iron sheet, the side with iron sheet can be automatically rotated to specification than another quality weight then, lap bars under the effect of gravity
The state of attached drawing Fig. 3 keeps it parallel with ground lead pole.At this moment by ground lead pole from annular carry platform in the middle part of ring cavity in
It pulls out downwards.By using such mode, ground lead pole that the worker of high altitude operation can very easily carry out carrying
It is removed from unmanned plane, reduces the risk of high altitude operation.
Detailed description of the invention
Attached drawing 1 is the utility model X-shaped support casing structural schematic diagram when on unmanned plane undercarriage.
Attached drawing 2 is overlap joint pole band structural schematic diagram in holding level in ground lead pole in the utility model.
Attached drawing 3 is overlap joint pole band structural schematic diagram when keeping vertical in ground lead pole in the utility model.
Attached drawing 4 is unmanned plane undercarriage three dimensional structure diagram in the utility model.
Label shown in attached drawing:
1, unmanned plane undercarriage；2, X-shaped bracket；3, clip；4, ground lead pole；5, lap bars；6, annular carries platform；7,
Overlap slot；8, iron sheet；9, spring groove；10, telescopic rod；11, adjustable spring；12, rubber sleeve；13, the first hinged seat；14, hack lever；
15, the second hinged seat；16, earthing wire clip.
Specific embodiment
The present invention will be further illustrated below in conjunction with specific embodiments.It should be understood that these embodiments are merely to illustrate this
Utility model rather than limitation the scope of the utility model.In addition, it should also be understood that, in the content for having read the utility model instruction
Later, those skilled in the art can make various changes or modifications the utility model, and such equivalent forms equally fall within this Shen
It please limited range.
Embodiment:
Described in the utility model is that unmanned plane ground line carries apparatus, and main structure includes covering in unmanned plane undercarriage 1
On X-shaped bracket 2, clip 3, lap bars 5 of the hoop in ground lead pole 4；The annular that is equipped with of the X-shaped bracket 2 carries platform 6,
The ring cavity diameter that the annular carries platform 6 is greater than the width of earthing wire clip 16, and the annular carries platform 6 and is equipped with overlap joint slot 7；
By being rotatablely connected in the middle part of short axle and lap bars 5, the length and overlap joint slot 7 of the lap bars 5 are adapted for 3 side of clip,
The side of the lap bars 5 is wrapped with one layer of iron sheet 8.One end of lap bars 5 is equipped with spring groove 9 and telescopic rod 10, sets in spring groove 9
There is adjustable spring 11, the limit setting of 10 one end of telescopic rod contacts in spring groove 9 at the top of adjustable spring 11.Lap bars 5 are put
When setting in the overlap joint slot 7 on annular carrying platform 6, telescopic rod 10 can be popped up one under the effect of 11 elastic force of adjustable spring
Point, so that 10 end of telescopic rod is pressed on overlap joint 7 side wall of slot, so that it is more stable to guarantee that lap bars 5 are placed in overlap joint slot 7.
Application method:
When using the present apparatus, lap bars 5 are gone into level, such as the state of Figure of description Fig. 2, are then placed into ring
Shape is carried in the overlap joint slot 7 on platform 6.Telescopic rod 10 can be popped up a part under the effect of 11 elastic force of adjustable spring, make to stretch
10 end of bar is pressed on overlap joint 7 side wall of slot, so that it is more stable to guarantee that lap bars 5 are placed in overlap joint slot 7.
Then it is gone up to the air using UAV flight to high altitude operation position.
Then the earthing wire clip 16 that the worker of high altitude operation grasps bottom is touched to top, can be by lap bars 5
It is released out of overlap joint slot 7, because the side of lap bars 5 is wrapped with one layer of iron sheet 8, the side with iron sheet 8 is than another matter then
Amount weight, lap bars 5 can be automatically rotated to the state of Figure of description Fig. 3 under the effect of gravity, keep it flat with ground lead pole 4
Row.At this moment ground lead pole 4 is being pulled down out out of annular carries 6 middle part of platform ring cavity.By using such mode,
The ground lead pole 4 that the worker of high altitude operation can very easily carry out carrying is removed from unmanned plane, reduces high altitude operation
Risk.
In order to enable device is more convenient to be installed on unmanned plane undercarriage 1, and be suitable for different length and width nobody
Machine undercarriage 1, we set X-shaped bracket 2 to include rubber sleeve 12, the first hinged seat 13, hack lever 14 and the second hinged seat 15,
12 sets of the rubber sleeve is arranged on rubber sleeve 12 in 1 end of unmanned plane undercarriage, first hinged seat 13, second hinge
The setting of joint chair 15 carries 6 side of platform in annular, and 14 both ends of hack lever are cut with scissors with the first hinged seat 13, the second hinged seat 15 respectively
It connects.The angle of X-shaped bracket 2 can be thus adjusted according to actual use situation.
Claims (3)
1. unmanned plane ground line carries apparatus, it is characterised in that: including covering the X-shaped bracket on unmanned plane undercarriage (1)
(2), the lap bars (5) of clip (3), hoop on ground lead pole (4)；
The annular that is equipped with of the X-shaped bracket (2) carries platform (6), and the ring cavity diameter that the annular carries platform (6) is greater than ground lead
The width of (16) is pressed from both sides, the annular carries platform (6) and is equipped with overlap joint slot (7)；
Clip (3) side in the middle part of short axle and lap bars (5) by being rotatablely connected, the length and overlap joint of the lap bars (5)
Slot (7) is adapted, and the side of the lap bars (5) is wrapped with one layer of iron sheet (8).
2. unmanned plane ground line carries apparatus according to claim 1, it is characterised in that: one end of the lap bars (5)
Equipped with spring groove (9) and telescopic rod (10), adjustable spring (11) are equipped in the spring groove (9), described telescopic rod (10) one end
Limit setting contacts in spring groove (9) with adjustable spring (11) top.
3. unmanned plane ground line carries apparatus according to claim 1, it is characterised in that: the X-shaped bracket (2) includes rubber
Gum cover (12), the first hinged seat (13), hack lever (14) and the second hinged seat (15), the rubber sleeve (12) covers to be risen and fallen in unmanned plane
Frame (1) end, first hinged seat (13) are arranged on rubber sleeve (12), and the second hinged seat (15) setting is taken in annular
Microscope carrier (6) side, hack lever (14) both ends are hinged with the first hinged seat (13), the second hinged seat (15) respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920423788.5U CN209389569U (en) | 2019-03-29 | 2019-03-29 | Unmanned plane ground line carries apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920423788.5U CN209389569U (en) | 2019-03-29 | 2019-03-29 | Unmanned plane ground line carries apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209389569U true CN209389569U (en) | 2019-09-13 |
Family
ID=67852516
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920423788.5U Expired - Fee Related CN209389569U (en) | 2019-03-29 | 2019-03-29 | Unmanned plane ground line carries apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209389569U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113708110A (en) * | 2021-09-02 | 2021-11-26 | 广东电网有限责任公司 | Grounding device |
-
2019
- 2019-03-29 CN CN201920423788.5U patent/CN209389569U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113708110A (en) * | 2021-09-02 | 2021-11-26 | 广东电网有限责任公司 | Grounding device |
| CN113708110B (en) * | 2021-09-02 | 2023-10-31 | 广东电网有限责任公司 | Grounding device |
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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: 20190913 Termination date: 20200329 |