CN110077609A - One kind falls off prior-warning device for suspension equipment on unmanned plane - Google Patents
One kind falls off prior-warning device for suspension equipment on unmanned plane Download PDFInfo
- Publication number
- CN110077609A CN110077609A CN201910367698.3A CN201910367698A CN110077609A CN 110077609 A CN110077609 A CN 110077609A CN 201910367698 A CN201910367698 A CN 201910367698A CN 110077609 A CN110077609 A CN 110077609A
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- CN
- China
- Prior art keywords
- block
- fixed
- hole
- fixed block
- unmanned plane
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The present invention relates to air vehicle technique fields, it is especially a kind of to fall off prior-warning device for suspension equipment on unmanned plane, including connecting column, connection top end is fixedly connected with the first limited block, connecting column bottom end is placed with the second limited block, second limited block bottom end is fixedly connected with the first fixed block and the second fixed block, first fixed block side is provided with first through hole, connecting rod is placed in first through hole, second fixed block is with respect to being provided with the second through-hole at connecting rod, return mechanism is installed on the outside of connecting rod, return mechanism is between the first fixed block and the second fixed block, second fixed block is provided with putting hole far from the second through-hole side, putting hole is connected to the second through-hole, Attraction block is placed in putting hole, coil is wound on the outside of Attraction block, coil circumscripted power line, second fixed block installs limited position mechanism far from the first fixed block side, second Fixed block is equipped with button, the external early warning mechanism of button close to the first fixed block side.The configuration of the present invention is simple is worthy to be popularized.
Description
Technical field
The present invention relates to air vehicle technique field, more particularly to a kind of fall off early warning dress for suspension equipment on unmanned plane
It sets.
Background technique
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or have car-mounted computer completely or intermittently automatically operate, compared with manned aircraft, unmanned plane is past
Toward being more suitable for those dirty or dangerous tasks, unmanned plane is mainly used in taking photo by plane at civilian aspect, agricultural, plant protection, miniature
Self-timer and express transportation etc., can not when distance manipulates unmanned plane staff farther out during using unmanned plane
Clearly distinguish whether the filming apparatus hung on unmanned plane loosens or fall.
Summary of the invention
The purpose of the present invention is to solve the bats existing in the prior art that can not clearly distinguish and hang on unmanned plane
The one kind taking the photograph the shortcomings that whether device loosens or fall, and proposing falls off prior-warning device for suspension equipment on unmanned plane.
To achieve the goals above, present invention employs following technical solutions:
Design it is a kind of fall off prior-warning device, including connecting column for suspension equipment on unmanned plane, the connection top end is consolidated
Surely it is connected with the first limited block, the connecting column bottom end is placed with the second limited block, and second limited block bottom end is equipped with tightly
Gu mechanism is connected between second limited block and connecting column by retention mechanism, it is socketed with fixed ring on the outside of the connecting column,
The fixed ring is equipped with fixed mechanism, the connection between the first limited block and the second limited block in the fixed ring
Column is connect by fixed mechanism with unmanned plane body, and second limited block bottom end is fixedly connected with the first fixed block and second and consolidates
Determine block, first fixed block side is provided with first through hole, and connecting rod, second fixed block are placed in the first through hole
It is provided with the second through-hole at opposite connecting rod, described connecting rod one end is located in first through hole, and the other end of the connecting rod protrudes into
In second through-hole, return mechanism is installed on the outside of the connecting rod, the return mechanism, which is located at the first fixed block and second, to be fixed
Between block, second fixed block is provided with putting hole far from the second through-hole side, and the putting hole is connected to the second through-hole, described
It is placed with Attraction block in putting hole, coil is wound on the outside of the Attraction block, the coil circumscripted power line, described second is fixed
Block far from the first fixed block side install limited position mechanism, second fixed block close to the first fixed block side be equipped with by
Button, the external early warning mechanism of button.
Preferably, the retention mechanism includes counter sink threaded hole, and the countersunk head threaded hole is located at the second limited block bottom end,
The countersunk head threaded hole is through the second limited block and extends in connecting column, and the countersunk head threaded hole internal screw thread is connected with screw.
Preferably, the fixed mechanism includes several concave slots, and several concave slots are located at fixed ring top, and several
Concave slot is circumferentially distributed along fixed ring, and convex block is placed in the concave slot, and the convex block is solid far from fixed ring one end
Surely be connected with fixed link, the fixed link is equipped with bindiny mechanism far from convex block one end, the bindiny mechanism by fixed link with
The connection of unmanned plane body.
Preferably, the bindiny mechanism includes two through holes, and two through holes are located at fixed link far from fixed ring
The side of one end is placed with buckle at respect to two through holes of the fixed link respectively, is placed with fixation on the outside of the fixed link
Band, the both ends of the fixing belt are each passed through after two through holes and snap connection, and described fixing belt one end passes through winding
In the middle part of buckle with snap connection.
Preferably, the return mechanism includes spring, and the spring one end is fixedly connected with the second fixed block, the spring
The other end be fixedly connected with round briquetting, the circle briquetting is socketed on the outside of connecting rod, and the circle briquetting is close to second
There are gaps for fixed block side and button.
Preferably, the position-limit mechanism includes third limited block, and third limited block side is provided with fixation hole, and described
Two fixed blocks are fixedly connected with elastic clip at relatively fixed hole, contain in the elastic clip far from second fixed block one end convex
Part out, the protrusion in the elastic clip partially pass through fixation hole and fix third limited block.
Preferably, the early warning mechanism includes LED light strip, and the LED light strip is wrapped on the outside of fixed link, the LED light
Band is electrically connected with button, the button external power supply.
It is proposed by the present invention it is a kind of fall off prior-warning device for suspension equipment on unmanned plane, beneficial effect is:
1, the present invention can be observed how the loosening situation of junction by the way that early warning mechanism is arranged, when the work of early warning mechanism,
LED light strip is powered, and LED light strip work is flashed to remind operator；
2, the present invention is firmly connect convenient for early warning mechanism with unmanned plane body by setting fixed mechanism, while connecting machine
Structure is convenient for that fixed link and unmanned plane body are bound and dismantled；
3, the present invention can be connected by setting return mechanism when needing to transport object using unmanned plane with active control
The movement of bar, the spring in return mechanism have the effect of auxiliary connecting rod return；
4, the present invention is easily installed the second limited block and connecting column, while countersunk head by setting countersunk head threaded hole and screw
Threaded hole can expose the second limited block to avoid screw, influence beauty.
Detailed description of the invention
Fig. 1 is that a kind of suspension equipment on unmanned plane proposed by the present invention falls off the structural schematic diagram of prior-warning device；
Fig. 2 is proposed by the present invention a kind of falls off prior-warning device front view for suspension equipment on unmanned plane；
Fig. 3 is partial enlarged view of the Fig. 2 at A；
Fig. 4 is that a kind of suspension equipment on unmanned plane proposed by the present invention falls off section view of the prior-warning device at connecting column
Figure；
Fig. 5 is that a kind of suspension equipment on unmanned plane proposed by the present invention falls off prior-warning device cuing open at return mechanism
View；
Fig. 6 is cross-sectional view of the Fig. 5 at B；
Fig. 7 is that a kind of suspension equipment on unmanned plane proposed by the present invention falls off prior-warning device cuing open at retention mechanism
View；
Fig. 8 is proposed by the present invention a kind of falls off buckle structure signal in prior-warning device for suspension equipment on unmanned plane
Figure.
In figure: fixed link 1, connecting column 2, the first limited block 3, fixing belt 4, fixed ring 5, concave slot 6, the second limited block 7,
Through hole 8, buckle 9, convex block 10, screw 11, button 12, the first fixed block 13, the second fixed block 14, third limited block 15,
Elastic clip 16, round briquetting 17, connecting rod 18, spring 19, first through hole 20, the second through-hole 21, Attraction block 22, coil 23,
Countersunk head threaded hole 24, fixation hole 25, putting hole 26, LED light strip 27.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Referring to Fig.1-8, a kind of to fall off prior-warning device, including connecting column 2 for suspension equipment on unmanned plane, connecting column 2 pushes up
End is fixedly connected with the first limited block 3, and 2 bottom end of connecting column is placed with the second limited block 7, and 7 bottom end of the second limited block is equipped with tightly
Gu mechanism, retention mechanism includes countersunk head threaded hole 24, and countersunk head threaded hole 24 is located at 7 bottom end of the second limited block, countersunk head threaded hole 24
It through the second limited block 7 and extends in connecting column 2,24 internal screw thread of countersunk head threaded hole is connected with screw 11, and retention mechanism can
Second limited block 7 is connect with connecting column 2.
Fixed ring 5 is socketed on the outside of connecting column 2, fixed ring 5 is fixed between the first limited block 3 and the second limited block 7
Fixed mechanism is installed, fixed mechanism includes several concave slots 6, and several concave slots 6 are located at 5 top of fixed ring, and several in ring 5
Concave slot 6 is circumferentially distributed along fixed ring 5, and convex block 10 is placed in concave slot 6, and convex block 10 is solid far from 5 one end of fixed ring
Surely it is connected with fixed link 1, fixed link 1 is equipped with bindiny mechanism far from 10 one end of convex block, and bindiny mechanism is by fixed link 1 and nobody
The connection of machine body can choose the fixed link 1 of installation different number, pass through fixed link 1 and nothing for different types of unmanned plane
Man-machine body connection.
Bindiny mechanism includes two through holes 8, and two through holes 8 are located at side of the fixed link 1 far from 5 one end of fixed ring,
Fixed link 1 is placed with fixing belt 4 with respect to buckle 9 is placed with respectively at two through holes 8 on the outside of fixed link 1, and the two of fixing belt 4
End is connect after being each passed through two through holes 8 with buckle 9, and 4 one end of fixing belt is connect by being wrapped in 9 middle part of buckle with buckle 9,
Buckle page 9 can take out from out of through hole 8.
Second limited block, 7 bottom end is fixedly connected with the first fixed block 13 and the second fixed block 14,13 side of the first fixed block
It is provided with first through hole 20, connecting rod 18 is placed in first through hole 20, is provided with second at the opposite connecting rod 18 of the second fixed block 14
Through-hole 21,18 one end of connecting rod are located in first through hole 20, and the other end of connecting rod 18 protrudes into the second through-hole 21, connecting rod 18
Outside is equipped with return mechanism, and return mechanism is between the first fixed block 13 and the second fixed block 14, and connecting rod 18 is first
It can be moved in through-hole 20 and the second through-hole 21, return mechanism can assist connecting rod 18 mobile, and connecting rod 18 is ferrous material
It is made.
Return mechanism includes spring 19, and 19 one end of spring is fixedly connected with the second fixed block 14, and the other end of spring 19 is solid
Surely it is connected with round briquetting 17, round briquetting 17 is socketed in 18 outside of connecting rod, and round briquetting 17 is close to the second fixed block 14 1
There are gaps to power on when round briquetting 17 presses button 12 for side and button 12, LED light strip work.
Second fixed block 14 is provided with putting hole 26 far from 21 side of the second through-hole, and putting hole 26 is connected to the second through-hole 21,
It is placed with Attraction block 22 in putting hole 26, coil 23,23 circumscripted power line of coil, the second fixed block are wound on the outside of Attraction block 22
14 install limited position mechanism far from 13 side of the first fixed block, and Attraction block 22 is fixed in putting hole 26 by position-limit mechanism, adsorb
Block 22 is iron block, and after being powered in coil 23, iron block can generate magnetism, can adsorb the movement of connecting rod 18, and the second fixed block 14 leans on
Nearly first fixed block, 13 side is equipped with button 12, and the external early warning mechanism of button 12, early warning mechanism includes LED light strip 27, LED light
Band 27 is wrapped in 1 outside of fixed link, and LED light strip 27 and button 12 are electrically connected, 12 external power supply of button.
Position-limit mechanism includes third limited block 15, and 15 side of third limited block is provided with fixation hole 25,14 phase of the second fixed block
To elastic clip 16 is fixedly connected at fixation hole 25, protrusion is contained in separate second fixed block, 14 one end in elastic clip 16
Point, the protrusion in elastic clip 16 partially passes through fixation hole 25, and third limited block 15 is fixed.
Working principle, mobile in connecting rod 18, round briquetting 17 presses button 12, and button 12 can power on, LED light strip
27 work, flash, and remind manipulation unmanned plane personnel, and suspension equipment loosens, if transport object using unmanned plane,
It can power on, so that Attraction block 22 adsorbs the movement of connecting rod 18, hanging articles take out from connecting rod 18.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (7)
1. one kind falls off prior-warning device, including connecting column (2) for suspension equipment on unmanned plane, which is characterized in that the connection
Column (2) top is fixedly connected with the first limited block (3), and connecting column (2) bottom end is placed with the second limited block (7), and described
Two limited blocks (7) bottom end is equipped with retention mechanism, is connected between second limited block (7) and connecting column (2) by retention mechanism
It connects, is socketed with fixed ring (5) on the outside of the connecting column (2), the fixed ring (5) is located at the first limited block (3) and the second limit
Between block (7), fixed mechanism is installed in the fixed ring (5), the connecting column (2) passes through fixed mechanism and unmanned plane body
Connection, the second limited block (7) bottom end are fixedly connected with the first fixed block (13) and the second fixed block (14), and described first is solid
Determine block (13) side to be provided with first through hole (20), be placed with connecting rod (18) in the first through hole (20), described second is fixed
With respect to being provided with the second through-hole (21) at connecting rod (18), described connecting rod (18) one end is located in first through hole (20) block (14),
The other end of the connecting rod (18) protrudes into the second through-hole (21), is equipped with return mechanism on the outside of the connecting rod (18), institute
Return mechanism is stated between the first fixed block (13) and the second fixed block (14), second fixed block (14) is logical far from second
Hole (21) side is provided with putting hole (26), and the putting hole (26) is connected to the second through-hole (21), is put in the putting hole (26)
It is equipped with Attraction block (22), is wound with coil (23) on the outside of the Attraction block (22), coil (23) circumscripted power line, described the
Two fixed blocks (14) install limited position mechanism far from the first fixed block (13) side, and second fixed block (14) is solid close to first
Determine block (13) side to be equipped with button (12), the external early warning mechanism of button (12).
It a kind of falls off prior-warning device for suspension equipment on unmanned plane 2. according to claim 1, which is characterized in that described
Retention mechanism includes countersunk head threaded hole (24), and the countersunk head threaded hole (24) is located at the second limited block (7) bottom end, the countersunk head spiral shell
Pit (24) is through the second limited block (7) and extends in connecting column (2), and countersunk head threaded hole (24) internal screw thread is connected with spiral shell
It follows closely (11).
It a kind of falls off prior-warning device for suspension equipment on unmanned plane 3. according to claim 1, which is characterized in that described
Fixed mechanism includes several concave slots (6), and several concave slots (6) are located at fixed ring (5) top, and several concave slots (6)
It is circumferentially distributed along fixed ring (5), it is placed with convex block (10) in the concave slot (6), the convex block (10) is far from fixed
Ring (5) one end is fixedly connected with fixed link (1), and the fixed link (1) is equipped with bindiny mechanism far from convex block (10) one end, institute
It states bindiny mechanism and connect fixed link (1) with unmanned plane body.
It a kind of falls off prior-warning device for suspension equipment on unmanned plane 4. according to claim 3, which is characterized in that described
Bindiny mechanism includes two through holes (8), and two through holes (8) are located at the side of fixed link (1) far from fixed ring (5) one end
Face, the fixed link (1) are placed on the outside of the fixed link (1) with respect to being placed with respectively buckle (9) at two through holes (8)
Fixing belt (4), the both ends of the fixing belt (4) are each passed through two through holes (8) and connect afterwards with buckle (9), described solid
Fixed band (4) one end is connect by being wrapped in the middle part of buckle (9) with buckle (9).
It a kind of falls off prior-warning device for suspension equipment on unmanned plane 5. according to claim 1, which is characterized in that described
Return mechanism includes spring (19), and described spring (19) one end is fixedly connected with the second fixed block (14), the spring (19)
The other end is fixedly connected with round briquetting (17), and the circle briquetting (17) is socketed on the outside of connecting rod (18), the round pressure
There are gaps with button (12) close to the second fixed block (14) side for block (17).
It a kind of falls off prior-warning device for suspension equipment on unmanned plane 6. according to claim 1, which is characterized in that described
Position-limit mechanism includes third limited block (15), and third limited block (15) side is provided with fixation hole (25), and described second is fixed
Block (14) is fixedly connected with elastic clip (16) at relatively fixed hole (25), far from the second fixed block in the elastic clip (16)
(14) protrusion part is contained in one end, and the protrusion in the elastic clip (16) partially passes through fixation hole (25) for third limited block
(15) fixed.
It a kind of falls off prior-warning device for suspension equipment on unmanned plane 7. according to claim 1 or 3, which is characterized in that
The early warning mechanism includes LED light strip (27), and the LED light strip (27) is wrapped on the outside of fixed link (1), the LED light strip
(27) it is electrically connected with button (12), button (12) external power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910367698.3A CN110077609A (en) | 2019-05-05 | 2019-05-05 | One kind falls off prior-warning device for suspension equipment on unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910367698.3A CN110077609A (en) | 2019-05-05 | 2019-05-05 | One kind falls off prior-warning device for suspension equipment on unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110077609A true CN110077609A (en) | 2019-08-02 |
Family
ID=67418482
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910367698.3A Pending CN110077609A (en) | 2019-05-05 | 2019-05-05 | One kind falls off prior-warning device for suspension equipment on unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110077609A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203601574U (en) * | 2013-12-04 | 2014-05-21 | 广州地理研究所 | Single-rotation-wing power-driven unmanned plane balance adjusting device |
| CN105857603A (en) * | 2016-04-08 | 2016-08-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor wing unmanned aerial vehicle of which booms can be folded |
| KR20170086194A (en) * | 2016-01-18 | 2017-07-26 | 김성호 | Fall warning device and uav having the same |
| KR20180076015A (en) * | 2016-12-27 | 2018-07-05 | 한국항공우주산업 주식회사 | Drop sensing apparatus for unmanned vehicle |
| CN207816574U (en) * | 2017-12-13 | 2018-09-04 | 浙江中烟工业有限责任公司 | A kind of device of detection nut loosening |
| CN108527415A (en) * | 2018-05-16 | 2018-09-14 | 六安德茂彩钢板有限公司 | A kind of rotatable pipe clamping mechanical arm |
| CN208315107U (en) * | 2018-04-27 | 2019-01-01 | 天津光电星球显示设备有限公司 | A kind of outdoor LED display screen rotating device |
| CN109693803A (en) * | 2019-01-23 | 2019-04-30 | 广东玖洲机场建设有限公司 | A kind of helideck safety net anti-dropout prior-warning device |
-
2019
- 2019-05-05 CN CN201910367698.3A patent/CN110077609A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203601574U (en) * | 2013-12-04 | 2014-05-21 | 广州地理研究所 | Single-rotation-wing power-driven unmanned plane balance adjusting device |
| KR20170086194A (en) * | 2016-01-18 | 2017-07-26 | 김성호 | Fall warning device and uav having the same |
| CN105857603A (en) * | 2016-04-08 | 2016-08-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor wing unmanned aerial vehicle of which booms can be folded |
| KR20180076015A (en) * | 2016-12-27 | 2018-07-05 | 한국항공우주산업 주식회사 | Drop sensing apparatus for unmanned vehicle |
| CN207816574U (en) * | 2017-12-13 | 2018-09-04 | 浙江中烟工业有限责任公司 | A kind of device of detection nut loosening |
| CN208315107U (en) * | 2018-04-27 | 2019-01-01 | 天津光电星球显示设备有限公司 | A kind of outdoor LED display screen rotating device |
| CN108527415A (en) * | 2018-05-16 | 2018-09-14 | 六安德茂彩钢板有限公司 | A kind of rotatable pipe clamping mechanical arm |
| CN109693803A (en) * | 2019-01-23 | 2019-04-30 | 广东玖洲机场建设有限公司 | A kind of helideck safety net anti-dropout prior-warning device |
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Application publication date: 20190802 |
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| RJ01 | Rejection of invention patent application after publication |