CN208828093U - A kind of unmanned plane falling defencive function with high-altitude - Google Patents
A kind of unmanned plane falling defencive function with high-altitude Download PDFInfo
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- CN208828093U CN208828093U CN201821605105.XU CN201821605105U CN208828093U CN 208828093 U CN208828093 U CN 208828093U CN 201821605105 U CN201821605105 U CN 201821605105U CN 208828093 U CN208828093 U CN 208828093U
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- unmanned plane
- wall
- mounting plate
- defencive function
- falling
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Abstract
The utility model discloses a kind of unmanned planes that defencive function is fallen with high-altitude, including unmanned plane main body, the unmanned plane main body is internally provided with battery, the top exterior walls of the unmanned plane main body are provided with mounting plate, and the surrounding outer wall of mounting plate is provided with connecting spring, the other side of the connecting spring is provided with sponge block, the top exterior walls quadrangle of the mounting plate is provided with rotating electric machine, the output shaft of its rotating electric machine is provided with propeller, the side of the mounting plate is provided with mounting groove, and the inner wall of mounting groove is provided with miniature GPS locator, the top exterior walls of the mounting plate are provided with admission extinguisher.The electromagnet that the utility model passes through setting, when abnormal electrical power supply occurs for unmanned plane, run out of steam when falling, lose magnetism absorption between the small iron block of Z-type and electromagnet, and then small-sized parachute is popped up admission extinguisher by compressed spring, effectively slows down the speed that unmanned plane is fallen by small-sized parachute.
Description
Technical field
The utility model relates to air vehicle technique field more particularly to it is a kind of fall with high-altitude defencive function nobody
Machine.
Background technique
Unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself, and unmanned plane and tradition fly
Machine is compared to having many good qualities, such as: small in size, light-weight, expense is low, highly-safe etc., unmanned plane has been widely applied at present
In take photo by plane, search and rescue, the fields such as resource exploration.
The most flying height of present unmanned plane is higher, most of to use battery as power, passes through in use
The situation that fault or electric power deficiency can often be encountered, so as to cause abnormal electrical power supply, and then causes unmanned plane to run out of steam, hair
Raw high-altitude is fallen, and traditional unmanned plane, since buffering protection function is poor, frequently results in unmanned plane when generation high-altitude is fallen
Damage.
Summary of the invention
Purpose of the utility model is to solve disadvantages existing in the prior art, and the one kind proposed is fallen with high-altitude
Fall the unmanned plane of defencive function.
To achieve the goals above, the utility model adopts the technical scheme that
A kind of unmanned plane falling defencive function with high-altitude, including unmanned plane main body, the inside of the unmanned plane main body
It is provided with battery, the top exterior walls of the unmanned plane main body are provided with mounting plate, and the surrounding outer wall of mounting plate is provided with
Connecting spring, the other side of the connecting spring are provided with sponge block, and the top exterior walls quadrangle of the mounting plate is provided with
Rotating electric machine, the output shaft of rotating electric machine are provided with propeller, and the side of the mounting plate is provided with mounting groove, and mounting groove
Inner wall be provided with miniature GPS locator, the top exterior walls of the mounting plate are provided with admission extinguisher, and the interior bottom four of admission extinguisher
It is provided with electromagnet week, the top exterior walls of the electromagnet pass through magnetic suck and are connected with the small iron block of Z-type, the admission extinguisher
Interior bottom is provided with compressed spring close to the side of the small iron block of Z-type, and compressed spring is in contact with the small iron block of Z-type, the receipts
It receives the interior bottom the center point of cylinder and the top exterior walls of the small iron block of Z-type is respectively welded the first fixed ring and the second fixed ring.
Preferably, the first fixed ring bolt has small-sized parachute, and the surrounding outer wall of small-sized parachute is stitched with
Rope.
Preferably, the other end of the rope is bolted with the second fixed ring, and the bottom outer wall setting of unmanned plane main body
There is rubber base.
Preferably, the bottom outer wall quadrangle of the rubber base is provided with cylinder body, and the inner wall of cylinder body slidably connects work
Plug.
Preferably, the bottom outer wall of the piston is provided with support rod, and the bottom outer wall of support rod be provided with it is slow
Rush block.
Preferably, the support rod is socketed with buffer spring, and buffer spring close to one end surrounding outer wall of buffer stopper
Specification successively increase from top to bottom.
Preferably, the rotating electric machine and electromagnet pass through conducting wire and are connected with switch, and switch and pass through conducting wire and electric power storage
Pond is connected.
Compared with prior art, the utility model provides a kind of unmanned plane that defencive function is fallen with high-altitude, has
Below the utility model has the advantages that
1. the unmanned plane that there is high-altitude to fall defencive function, by the electromagnet of setting, when unmanned plane generation power supply is different
Often, it runs out of steam when falling, lose magnetism absorption between the small iron block of Z-type and electromagnet, and then compressed spring is by small-sized drop
Umbrella pop-up admission extinguisher is fallen, the speed that unmanned plane is fallen effectively is slowed down by small-sized parachute.
2. the unmanned plane that there is high-altitude to fall defencive function can be in nothing by the connecting spring and sponge block of setting
When man-machine landing, buffer protection function is played to unmanned plane two sides, by the miniature GPS locator of setting, is convenient for operator
It is quickly recycled to unmanned.
3. the unmanned plane that there is high-altitude to fall defencive function, by the rubber base of setting, can when unmanned plane lands,
Good buffer function is played, by cooperating between the cylinder body of setting, piston, support rod, buffer spring and buffer stopper, energy
It is enough that further unmanned plane is buffered, it plays a protective role to unmanned plane.
It is not directed to part in the device to be the same as those in the prior art or can be realized by using the prior art, the utility model
It is easy to operate, can in unmanned plane abnormal electrical power supply the small-sized parachute of automatic spring, nobody is effectively slowed down by small-sized parachute
The speed that machine is fallen.
Detailed description of the invention
Fig. 1 be the utility model proposes a kind of unmanned plane that defencive function is fallen with high-altitude overall structure signal
Figure；
Fig. 2 be the utility model proposes a kind of unmanned plane that defencive function is fallen with high-altitude the small iron block structure of Z-type
Schematic diagram；
Fig. 3 be the utility model proposes a kind of unmanned plane that defencive function is fallen with high-altitude housing structure signal
Figure.
In figure: 1- unmanned plane main body, 2- mounting plate, 3- connecting spring, 4- sponge block, 5- rotating electric machine, 6- propeller, 7-
The small-sized parachute of miniature GPS locator, 8-, the first fixed ring of 9-, 10- battery, 11- cylinder body, 12- support rod, 13- buffering
Block, 14- buffer spring, 15- rubber base, the small iron block of 16-Z type, 17- admission extinguisher, 18- rope, the second fixed ring of 19-, 20- electromagnetism
Iron, 21- compressed spring, 22- piston.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
In the description of the present invention, it should be understood that term " on ", "lower", "front", "rear", "left", "right",
The orientation or positional relationship of the instructions such as "top", "bottom", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
For ease of description the utility model and simplify description, rather than the device or element of indication or suggestion meaning must have it is specific
Orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
Referring to Fig.1-3, a kind of unmanned plane falling defencive function with high-altitude, including unmanned plane main body 1, unmanned plane main body
1 inside is fixed with battery 10 by screw, and the top exterior walls of unmanned plane main body 1 are fixed with mounting plate 2 by screw, and pacify
The surrounding outer wall of loading board 2 passes through screw and is fixed with connecting spring 3, and the other side of connecting spring 3 passes through screw and is fixed with sea
Continuous block 4 can play buffer protection to unmanned plane two sides when colliding by the connecting spring 3 and sponge block 4 of setting
Effect, the top exterior walls quadrangle of mounting plate 2 pass through screw and are fixed with rotating electric machine 5, and the output shaft of rotating electric machine 5 passes through
Screw is fixed with propeller 6, and the side of mounting plate 2 is provided with mounting groove, and the inner wall of mounting groove is fixed with miniature GPS by screw
Locator 7, by the miniature GPS locator 7 of setting, convenient for operator to fall it is unmanned quickly recycled, mounting plate 2
Top exterior walls admission extinguisher 17 is fixed with by screw, and the interior bottom surrounding of admission extinguisher 17 passes through screw and is fixed with electromagnet
20, the top exterior walls of electromagnet 20 pass through magnetic suck and are connected with the small iron block 16 of Z-type, can by the small iron block 16 of the Z-type of setting
Increase the contact area between electromagnet 20, keeps electromagnet 20 and the magnetic suck of the small iron block 16 of Z-type more stable, admission extinguisher 17
Interior bottom pass through screw close to the side of the small iron block 16 of Z-type and be fixed with compressed spring 21, and compressed spring 21 and the small iron of Z-type
Block 16 is in contact, and the top exterior walls of the small iron block 16 of interior bottom the center point and Z-type of admission extinguisher 17 are respectively welded the first fixed ring 9
With the second fixed ring 19, abnormal electrical power supply occurs for unmanned plane, runs out of steam when falling, electromagnet 20 is due to losing power supply, Z-type
Can lose magnetism absorption between small iron block 16 and electromagnet 20, and then small-sized parachute 8 is popped up admission extinguisher by compressed spring 21, by
It hurtles down in unmanned plane, small-sized parachute 8 can be opened quickly, effectively slow down what unmanned plane was fallen by small-sized parachute 8
Speed.
In the utility model, the first fixed ring 9 bolt has small-sized parachute 8, and the surrounding outer wall of small-sized parachute 8 stitches
It is connected to rope 18, the other end of rope 18 is bolted with the second fixed ring 19, and the bottom outer wall of unmanned plane main body 1 passes through screw
It is fixed with rubber base 15.
The bottom outer wall quadrangle of rubber base 15 passes through screw and is fixed with cylinder body 11, and the inner wall of cylinder body 11 slidably connects
The bottom outer wall of 22 piston 22 of piston passes through screw and is fixed with support rod 12, and the bottom outer wall of support rod 12 passes through screw
It is fixed with buffer stopper 13, support rod 12 is socketed with buffer spring 14 close to one end surrounding outer wall of buffer stopper 13, passes through setting
Cylinder body 11, piston 22, support rod 12, cooperate between buffer spring 14 and buffer stopper 13, further unmanned plane is carried out
Buffering, plays a protective role to unmanned plane, and the specification of buffer spring 14 successively increases from top to bottom, by by buffer spring 14
Specification be set as successively increasing from top to bottom, the cushion performance of buffer spring 14 can be effectively increased.
Rotating electric machine 5 and electromagnet 20 are connected with switch by conducting wire, and switch and be connected by conducting wire with battery 10
It connects.
Working principle: it when abnormal electrical power supply occurs for unmanned plane, runs out of steam when falling, electromagnet 20 is due to losing electricity
Source, can lose magnetism absorption between the small iron block 16 of Z-type and electromagnet 20, and then small-sized parachute 8 is popped up and received by compressed spring 21
Receive cylinder, since unmanned plane hurtles down, small-sized parachute 8 can be opened quickly, effectively slow down unmanned plane by small-sized parachute 8
The speed fallen plays buffer protection to unmanned plane two sides by the connecting spring 3 and sponge block 4 of setting when unmanned plane lands
Effect, by cooperating between the cylinder body 11 of setting, piston 22, support rod 12, buffer spring 14 and buffer stopper 13, further
Unmanned plane is buffered, is played a protective role to unmanned plane, the position that operator is emitted by receiving miniature GPS locator 7
Confidence number is quickly recycled to unmanned.
The preferable specific embodiment of the above, only 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, practical according to this
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (7)
1. a kind of unmanned plane for falling defencive function with high-altitude, including unmanned plane main body (1), which is characterized in that it is described nobody
Owner's body (1) is internally provided with battery (10), and the top exterior walls of the unmanned plane main body (1) are provided with mounting plate (2), and
The surrounding outer wall of mounting plate (2) is provided with connecting spring (3), and the other side of the connecting spring (3) is provided with sponge block
(4), the top exterior walls quadrangle of the mounting plate (2) is provided with rotating electric machine (5), and the output shaft of rotating electric machine (5) is all provided with
It is equipped with propeller (6), the side of the mounting plate (2) is provided with mounting groove, and the inner wall of mounting groove is provided with miniature GPS locator
(7), the top exterior walls of the mounting plate (2) are provided with admission extinguisher (17), and the interior bottom surrounding of admission extinguisher (17) is provided with
Electromagnet (20), the top exterior walls of the electromagnet (20) pass through magnetic suck and are connected with the small iron block of Z-type (16), the admission extinguisher
(17) interior bottom is provided with compressed spring (21) close to the side of the small iron block of Z-type (16), and compressed spring (21) and Z-type are small
Iron block (16) is in contact, and the interior bottom the center point of the admission extinguisher (17) and the top exterior walls of the small iron block of Z-type (16) are respectively welded
There are the first fixed ring (9) and the second fixed ring (19).
2. a kind of unmanned plane for falling defencive function with high-altitude according to claim 1, which is characterized in that described first
Fixed ring (9) bolt has small-sized parachute (8), and the surrounding outer wall of small-sized parachute (8) is stitched with rope (18).
3. a kind of unmanned plane for falling defencive function with high-altitude according to claim 2, which is characterized in that the rope
(18) the other end is bolted with the second fixed ring (19), and the bottom outer wall of unmanned plane main body (1) is provided with rubber base (15).
4. a kind of unmanned plane for falling defencive function with high-altitude according to claim 3, which is characterized in that the rubber
The bottom outer wall quadrangle of seat (15) is provided with cylinder body (11), and the inner wall of cylinder body (11) slidably connects piston (22).
5. a kind of unmanned plane for falling defencive function with high-altitude according to claim 4, which is characterized in that the piston
(22) bottom outer wall is provided with support rod (12), and the bottom outer wall of support rod (12) is provided with buffer stopper (13).
6. a kind of unmanned plane for falling defencive function with high-altitude according to claim 5, which is characterized in that the support
Bar (12) is socketed with buffer spring (14) close to one end surrounding outer wall of buffer stopper (13), and the specification of buffer spring (14) from
Top to bottm successively increases.
7. a kind of unmanned plane for falling defencive function with high-altitude according to claim 1, which is characterized in that the rotation
Motor (5) and electromagnet (20) are connected with switch by conducting wire, and switch and be connected by conducting wire with battery (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821605105.XU CN208828093U (en) | 2018-09-29 | 2018-09-29 | A kind of unmanned plane falling defencive function with high-altitude |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821605105.XU CN208828093U (en) | 2018-09-29 | 2018-09-29 | A kind of unmanned plane falling defencive function with high-altitude |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208828093U true CN208828093U (en) | 2019-05-07 |
Family
ID=66318291
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821605105.XU Active CN208828093U (en) | 2018-09-29 | 2018-09-29 | A kind of unmanned plane falling defencive function with high-altitude |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110733654A (en) * | 2019-10-25 | 2020-01-31 | 重庆工程职业技术学院 | unmanned aerial vehicle with safeguard function |
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
| CN112591112A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Unmanned aerial vehicle capable of emergently reducing load |
| CN112678173A (en) * | 2021-01-30 | 2021-04-20 | 江西中建勘察设计有限公司 | Unmanned aerial vehicle is used in survey and drawing |
-
2018
- 2018-09-29 CN CN201821605105.XU patent/CN208828093U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110733654A (en) * | 2019-10-25 | 2020-01-31 | 重庆工程职业技术学院 | unmanned aerial vehicle with safeguard function |
| CN112591127A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Safety landing device for protecting camera during unmanned aerial vehicle fault |
| CN112591112A (en) * | 2021-01-27 | 2021-04-02 | 杭州优旗贸易有限公司 | Unmanned aerial vehicle capable of emergently reducing load |
| CN112678173A (en) * | 2021-01-30 | 2021-04-20 | 江西中建勘察设计有限公司 | Unmanned aerial vehicle is used in survey and drawing |
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