CN208828123U - A kind of unmanned plane form into columns in automatic collision protective device - Google Patents
A kind of unmanned plane form into columns in automatic collision protective device Download PDFInfo
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- CN208828123U CN208828123U CN201821407389.1U CN201821407389U CN208828123U CN 208828123 U CN208828123 U CN 208828123U CN 201821407389 U CN201821407389 U CN 201821407389U CN 208828123 U CN208828123 U CN 208828123U
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- unmanned plane
- drone body
- control panel
- intelligence
- ejector
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Abstract
The utility model discloses the automatic collision protective devices in a kind of formation of unmanned plane, belong to unmanned plane field, a kind of unmanned plane form into columns in automatic collision protective device, including drone body, drone body upper end is equipped with control panel and ejection column, ejection column is located at control panel center, bottom end is equipped with ejector in ejection column, ejector upper end is connected with parachute, parachute is located on the inside of ejection column, control panel upper end is equipped with attitude transducer, there are four mounting groove and grooves for the cutting of drone body surrounding, mounting groove inner end is equipped with graphene sensor, drone body is surrounded by intelligence denaturation material, it may be implemented to be denaturalized the variation of material shape by intelligence after hitting to protect unmanned plane effect, simultaneously in any case, it can also realize the effect for making unmanned plane keep balance as far as possible after hitting, and work as nobody Machine be knocked it is out of control after, parachute can protect unmanned plane, make unmanned function safe falling.
Description
Technical field
The utility model relates to unmanned plane fields, protect more specifically to the automatic collision in a kind of formation of unmanned plane
Protection unit.
Background technique
With making rapid progress for technology, unmanned plane is popularized, and is widely used in taking photo by plane, agricultural, plant protection, self-timer, express delivery
Transport, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, system
The fields such as romance are made, unmanned plane rotor is easy for the device that unmanned plane takes off, and main member is motor and rotating vane.
Attitude transducer is the high performance three-dimensional motion attitude measuring system based on MEMS technology.It includes three axis accelerometer
Instrument, three axis accelerometer, the motion sensors such as three axle electronic compass are obtained by embedded low-power consumption arm processor through excess temperature
Spend the data such as 3 d pose and the orientation of compensation.LPMS series and iAHRS-M0 attitude transducer can be embedded into extensively model plane nobody
Machine, robot, mechanical holder, shipping vehicle, ground and underwater equipment, virtual reality, the needs such as human motion analysis are independently surveyed
It measures in 3 d pose and the product facility in orientation.Graphene sensor is that the widely used height that is made by graphene is photosensitive
Spend sensor
The scientific research personnel of Australian National University has issued a kind of intellectual material, meets water material and is curled into suction pipe rapidly
Shape, when the pipe of curling encounters ethyl alcohol, pipe will expand back to original state again.This peculiar material upper layer is polycaprolactone
PCL material, lower layer are made of polyvinylchloride fento, and PCL has hydrophily, and chance water is responsible for material self assembles and is crimped, and lower layer
There is PVC hydrophobicity water droplet can be prevented to be lost.
But unmanned plane often collides in formation flight, so that unmanned plane meeting disequilibrium, collision are serious
When, unmanned plane out of control can even fall.
Summary of the invention
1. technical problems to be solved
Aiming at the problems existing in the prior art, the purpose of this utility model is to provide a kind of unmanned plane form into columns in from
Dynamic anti-collision protection device, it may be implemented to be denaturalized the variation of material shape by intelligence after hitting to protect unmanned plane to imitate
Fruit, while in any case, it can also realize the effect for making unmanned plane keep balance as far as possible after hitting, and work as unmanned plane quilt
Hit it is out of control after, parachute can protect unmanned plane, make unmanned function safe falling.
2. technical solution
To solve the above problems, the utility model adopts the following technical scheme.
A kind of unmanned plane form into columns in automatic collision protective device, including drone body, the drone body upper end
Control panel and ejection column are installed, the ejection column is located at control panel center, and bottom end is equipped with ejector in the ejection column, institute
It states ejector upper end and is connected with parachute, the parachute is located on the inside of ejection column, and the control panel upper end is equipped with posture biography
Sensor, the drone body surrounding are dug there are four mounting groove and groove, and the mounting groove inner end is equipped with graphene sensing
Device, the drone body are surrounded by intelligence denaturation material, fixed between bottom end in the intelligence denaturation material and groove to connect
It is connected to connecting column, the groove is located on the outside of graphene sensor, and the connecting column outer end is fixedly connected with elastic plate, the bullet
Property plate inner end dig and have multiple apopores, be fixedly connected with multiple upper spines, described connecting column or so two below the elastic plate
The groove of side is placed respectively there are two water pocket, and the water pocket is located at below upper spine, is provided with sting device below the water pocket,
It may be implemented to be denaturalized the variation of material shape by intelligence after hitting to protect unmanned plane effect, while in certain situation
Under, it can also realize the effect for making unmanned plane keep balance as far as possible after hitting, and after unmanned plane is knocked out of control, parachute
It can protect unmanned plane, make unmanned function safe falling.
Further, pure water is filled in the water pocket, after water pocket is punctured by upper spine, intelligence is denaturalized material and encounters pure water
After can become curling, and pure water electric conductivity is very weak, can almost ignore, and reduces drone body pure water to the possibility of electric leakage
Property.
Further, the sting device includes lower spine, and bottom end, which is dug, in the groove multiple puncturing holes, described to wear
Acanthopore is located at immediately below water pocket, and the lower spine is located in puncturing hole, and the drone body inner end is dug there are four puncture tank,
The puncture tank is communicated with puncturing hole, and bottom end is fixedly connected there are four electric telescopic rod in the puncture tank, the adjacent institute of every two
The upper end for stating electric telescopic rod is fixedly connected with connecting plate, and the connecting plate is fixedly connected with lower spine, when drone body by
To after shock, one of intelligence denaturation material becomes curling, and making drone body is no longer symmetry status, and control panel can control
Electric telescopic rod elongation, allows lower spine to puncture water pocket, so that other several intelligence denaturation materials become curling, makes nobody
Machine ontology restores symmetry status, facilitates drone body and keeps balance.
Further, the graphene sensor, ejector, attitude transducer and electric telescopic rod pass through with control panel
Wireless signal connection, control panel can control graphene sensor, ejector, attitude transducer and electric telescopic rod.
3. beneficial effect
Compared with the prior art, utility model has the advantages that
(1) this programme may be implemented to be denaturalized the variation of material shape by intelligence after hitting to protect unmanned plane to imitate
Fruit, while in any case, it can also realize the effect for making unmanned plane keep balance as far as possible after hitting, and work as unmanned plane quilt
Hit it is out of control after, parachute can protect unmanned plane, make unmanned function safe falling.
(2) pure water is filled in water pocket, after water pocket is punctured by upper spine, intelligence, which is denaturalized after material encounters pure water, can become volume
Song, and pure water electric conductivity is very weak, can almost ignore, and reduces a possibility that drone body pure water is to leak electricity.
(3) sting device includes lower spine, under bottom end cutting has multiple puncturing holes, puncturing hole to be located at water pocket just in groove
Side, lower spine are located in puncturing hole, and drone body inner end is dug there are four puncture tank, and puncture tank is communicated with puncturing hole, puncture
Bottom end is fixedly connected there are four electric telescopic rod in slot, and the upper end of the adjacent electric telescopic rod of every two is fixedly connected with connecting plate,
Connecting plate is fixedly connected with lower spine, and after drone body is hit, one of intelligence denaturation material becomes curling, makes nothing
Man-machine ontology is no longer symmetry status, and control panel can control electric telescopic rod elongation, allow lower spine to puncture water pocket, make
It obtains other several intelligence denaturation materials and becomes curling, so that drone body is restored symmetry status, facilitate drone body holding
Balance.
(4) graphene sensor, ejector, attitude transducer and electric telescopic rod are connected with control panel by wireless signal
It connects, control panel can control graphene sensor, ejector, attitude transducer and electric telescopic rod.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the top surface of the utility model；
Fig. 2 is the structural schematic diagram in Fig. 1 at A；
Structural schematic diagram when Fig. 3 is the intelligence denaturation material curling of the utility model；
Fig. 4 is the schematic perspective view of the utility model；
Fig. 5 is the positive structural schematic diagram of the utility model；
Fig. 6 is the structural schematic diagram when parachute of the utility model is opened.
Figure label explanation:
1 drone body, 2 ejection columns, 3 intelligence denaturation materials, 4 control panels, 5 graphene sensors, 6 mounting grooves, 7 connections
Column, spine, 9 apopores, 10 water pockets, 11 puncturing holes, 12 lower spines, 13 connecting plates, 14 electric telescopic rods, 15 puncture tanks, 16 on 8
Ejector, 17 grooves, 18 attitude transducers, 19 parachutes.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model；The technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe；Obviously；The described embodiments are only a part of the embodiments of the utility model；Rather than whole
Embodiment, based on the embodiments of the present invention；Those of ordinary skill in the art are without making creative work
Every other embodiment obtained；It fall within the protection scope of the utility model.
In the description of the present invention, it should be noted that term " on ", "lower", "inner", "outside" " top/bottom end " etc.
The orientation or positional relationship of instruction is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of description the utility model
It is described with simplifying, rather than the device or element of indication or suggestion meaning must have a particular orientation, with specific orientation structure
It makes and operates, therefore should not be understood as limiting the present invention.In addition, term " first ", " second " are only used for description mesh
, it is not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " being provided with ", " be arranged/connect ", " connection " etc., shall be understood in a broad sense, such as " connection ", may be a fixed connection, can also be with
It is to be detachably connected, or be integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, it can also be with
Indirectly connected through an intermediary, it can be the connection inside two elements.For the ordinary skill in the art, may be used
The concrete meaning of above-mentioned term in the present invention is understood with concrete condition.
Embodiment 1:
Please refer to Fig. 1-6, a kind of unmanned plane form into columns in automatic collision protective device, including drone body 1, unmanned plane
1 upper end of ontology is equipped with control panel 4 and ejection column 2, and control panel 4 is controlled by single-chip microcontroller, and logical language has been incorporated into single-chip microcontroller, single
Self-balancing program is incorporated into piece machine, after drone body 1 is hit, self-balancing program can keep nobody as far as possible
The balance of machine ontology 1, ejection column 2 are located at 4 center of control panel, launch bottom end in column 2 and are equipped with ejector 16,16 upper end of ejector
It is connected with parachute 19, ejection column 2 is the outwardly projecting hollow cylinder in middle part, so that having inside drone body 1 enough
Parachute 19 is placed in space, and parachute 19 is located at 2 inside of ejection column, and 4 upper end of control panel is equipped with attitude transducer 18, this field
Technical staff can according to need the attitude transducer 18 of selection suitable types, such as iAHRS-M0 attitude transducer, unmanned plane
1 surrounding of ontology is dug there are four mounting groove 6 and groove 17, and 6 inner end of mounting groove is equipped with graphene sensor 5, graphene sensing
Device 5, ejector 16 and attitude transducer 18 are connect with control panel 4 by wireless signal, and control panel 4 can control graphene biography
Sensor 5, ejector 16 and attitude transducer 18, drone body 1 be surrounded by intelligence denaturation material 3, intelligence be denaturalized material 3 with
Connecting column 7 is fixedly connected in groove 17 between bottom end, groove 17 is located at 5 outside of graphene sensor, and 7 outer end of connecting column is fixed
It is connected with elastic plate, elastic plate inner end, which is dug, there are multiple apopores 9, is fixedly connected with multiple upper spines 8 below elastic plate, connects
The groove 17 of 7 left and right sides of column is placed respectively there are two water pocket 10, and water pocket 10 is interior to be filled with pure water, and water pocket 10 is pierced by upper spine 8
After broken, intelligence, which is denaturalized after material 3 encounters pure water, can become curling, and pure water electric conductivity is very weak, can almost ignore, reduce nobody
A possibility that 1 pure water of machine ontology is to leak electricity, water pocket 10 are located at upper 8 lower section of spine, may be implemented to pass through intelligence after hitting
The variation of 3 shape of material is denaturalized to protect unmanned plane effect, while in any case, makes unmanned plane after can also realizing shock
The effect of balance is kept as far as possible, and after unmanned plane is knocked out of control, parachute 19 can protect unmanned plane, make unmanned function
Safe falling.
1-3 is please referred to, sting device is provided with below water pocket 10, sting device includes lower spine 12, bottom end in groove 17
Cutting has multiple puncturing holes 11, and puncturing hole 11 is located at immediately below water pocket 10, and lower spine 12 is located in puncturing hole 11, drone body
1 inner end is dug there are four puncture tank 15, and puncture tank 15 is communicated with puncturing hole 11, and bottom end is fixedly connected with that there are four electric in puncture tank 15
Dynamic telescopic rod 14, the upper end of the adjacent electric telescopic rod 14 of every two are fixedly connected with connecting plate 13, connecting plate 13 and lower spine 12
It is fixedly connected, after drone body 1 is hit, one of intelligence denaturation material 3 becomes curling, makes drone body 1 not
It is symmetry status again, control panel 4 can control the elongation of electric telescopic rod 14, lower spine 12 is allowed to puncture water pocket 10, water pocket
10 material is silicon rubber, and the intensity of silicon rubber is only the half of natural rubber or certain synthetic rubber under room temperature, so that water pocket
10 are easier to be punctured, while silicon rubber has apparent high-temperature stability, so that water pocket 10 is not easy to be affected by temperature and deform,
Water pocket 10 with a thickness of 3MM, make water pocket 10 be easy to be punctured, enable intelligence be denaturalized material 3 meet in time water become curling, improve nobody
The sensibility of machine ontology 1 being knocked makes the recovery pair of drone body 1 so that other several intelligence denaturation materials 3 become curling
Title state facilitates drone body 1 and keeps balance.
When being knocked 1 first time of drone body, the elastic plate close to rum point can be sent out to the direction close to water pocket 10
Raw deformation, makes spine 8 that can puncture water pocket 10, so that the water in water pocket 10 flows out, water flows to intelligence denaturation material by apopore 9
On material 3, intelligence denaturation material 3 becomes curling, and when second of shock occurs, the intelligence denaturation material 3 of curling can produce one
Cushion effect reduces and hits influence to drone body 1, and intelligence is denaturalized after material 3 becomes curling, and drone body 1 is no longer at this time
It is symmetry status, will affect the balance of drone body 1, the graphene sensor 5 of 3 lower section of intelligence denaturation material monitors light
The variation of line, and signal is fed back into control panel 4, control panel 4 controls the starting of self-balancing program, when self-balancing program can not make nothing
When man-machine ontology 1 keeps balance, control panel 4 can control sting device by wireless signal, and the other three is intelligently under denaturation material 3
The sting device of side can puncture water pocket 10, and the water in water pocket 10 is flowed on intelligence denaturation material 3 by apopore 9, so that in addition
Three intelligence denaturation materials 3 also become curling, and at this moment drone body 1 restores symmetry status, protects drone body 1 as far as possible
Maintain an equal level weighing apparatus, and when lasting generations shock is so that drone body 1 cannot keep balance, attitude transducer 18 is by unmanned plane sheet at this time
The state of flight signal that body 1 is unbalance feeds back to control panel 4, and control panel 4 controls ejector 16 and outward pops up parachute 19, lands
Umbrella 19 can protect unmanned plane, make unmanned function safe falling.
It is described above；The only preferable specific embodiment of 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；It is practical according to this
Novel technical solution and its improvement design is subject to equivalent substitution or change；It should all cover in the protection scope of the utility model
It is interior.
Claims (4)
1. the automatic collision protective device in a kind of unmanned plane formation, including drone body (1), it is characterised in that: the nothing
Man-machine ontology (1) upper end is equipped with control panel (4) and ejection column (2), and the ejection column (2) is located at control panel (4) center, described
Ejection column (2) interior bottom end is equipped with ejector (16), and ejector (16) upper end is connected with parachute (19), the parachute
(19) it is located on the inside of ejection column (2), control panel (4) upper end is equipped with attitude transducer (18), the drone body (1)
There are four mounting groove (6) and grooves (17) for surrounding cutting, and mounting groove (6) inner end is equipped with graphene sensor (5), described
Drone body (1) is surrounded by intelligence denaturation material (3), and the intelligence is denaturalized between material (3) and groove (17) interior bottom end
It is fixedly connected with connecting column (7), the groove (17) is located on the outside of graphene sensor (5), and connecting column (7) outer end is fixed
It is connected with elastic plate, the elastic plate inner end, which is dug, to be had multiple apopores (9), is fixedly connected on multiple below the elastic plate
Spine (8), the groove (17) at left and right sides of the connecting column (7) place that there are two water pocket (10), water pocket (10) positions respectively
Below upper spine (8), sting device is provided with below the water pocket (10).
2. the automatic collision protective device in a kind of unmanned plane formation according to claim 1, it is characterised in that: the water
Pure water is filled in capsule (10).
3. the automatic collision protective device in a kind of unmanned plane formation according to claim 1, it is characterised in that: described to wear
Thorn device includes lower spine (12), and the interior bottom end of groove (17), which is dug, to be had multiple puncturing holes (11), puncturing hole (11) position
Immediately below water pocket (10), the lower spine (12) is located in puncturing hole (11), and drone body (1) inner end, which is dug, four
A puncture tank (15), the puncture tank (15) communicate with puncturing hole (11), and the interior bottom end of the puncture tank (15) is fixedly connected with four
The upper end of a electric telescopic rod (14), the adjacent electric telescopic rod (14) of every two is fixedly connected with connecting plate (13), described
Connecting plate (13) is fixedly connected with lower spine (12).
4. the automatic collision protective device in a kind of unmanned plane formation according to claim 1 or 3, it is characterised in that: institute
Graphene sensor (5), ejector (16), attitude transducer (18) and electric telescopic rod (14) is stated to pass through with control panel (4)
Wireless signal connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821407389.1U CN208828123U (en) | 2018-08-30 | 2018-08-30 | A kind of unmanned plane form into columns in automatic collision protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821407389.1U CN208828123U (en) | 2018-08-30 | 2018-08-30 | A kind of unmanned plane form into columns in automatic collision protective device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208828123U true CN208828123U (en) | 2019-05-07 |
Family
ID=66311318
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|---|---|---|---|
| CN201821407389.1U Expired - Fee Related CN208828123U (en) | 2018-08-30 | 2018-08-30 | A kind of unmanned plane form into columns in automatic collision protective device |
Country Status (1)
| Country | Link |
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| CN (1) | CN208828123U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108891616A (en) * | 2018-08-30 | 2018-11-27 | 芜湖翼讯飞行智能装备有限公司 | A kind of unmanned plane form into columns in automatic collision protective device and its application method |
| CN111591465A (en) * | 2020-03-31 | 2020-08-28 | 上海卫星工程研究所 | Autonomous dormancy wakeup survival control method based on external measurement information correction |
-
2018
- 2018-08-30 CN CN201821407389.1U patent/CN208828123U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108891616A (en) * | 2018-08-30 | 2018-11-27 | 芜湖翼讯飞行智能装备有限公司 | A kind of unmanned plane form into columns in automatic collision protective device and its application method |
| CN111591465A (en) * | 2020-03-31 | 2020-08-28 | 上海卫星工程研究所 | Autonomous dormancy wakeup survival control method based on external measurement information correction |
| CN111591465B (en) * | 2020-03-31 | 2021-12-03 | 上海卫星工程研究所 | Autonomous dormancy wakeup survival control method based on external measurement information correction |
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Granted publication date: 20190507 |