CN208393633U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
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- CN208393633U CN208393633U CN201821081920.0U CN201821081920U CN208393633U CN 208393633 U CN208393633 U CN 208393633U CN 201821081920 U CN201821081920 U CN 201821081920U CN 208393633 U CN208393633 U CN 208393633U
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- unmanned plane
- fuselage
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Abstract
This disclosure relates to which a kind of unmanned plane is additionally provided with the fixed part for being adsorbed on the unmanned plane on target object including fuselage (10) and the destructor being arranged on the fuselage (10) on the fuselage (10).Through the above technical solutions, the unmanned plane that the embodiment of the present disclosure provides is accompanied with destructor, remote-controlled detonation is carried out after target position can be dropped to by remote control, avoids the risk of operator's injury.In addition, the fixed part on fuselage can be adsorbed on moveable target object, can be fixed on the target object, so lock and to its explosion.
Description
Technical field
This disclosure relates to unmanned plane during flying device technical field, and in particular, to a kind of unmanned plane.
Background technique
At this stage, when executing some demolition duties, it usually needs operator installs explosive in regional human to be blasted,
Specifically, such as by explosive it is mounted on target object to be blasted, or is mounted near target object to be blasted.This mistake
There are apparent security risks for journey, be easy to cause operator injured.In addition, when target object to be blasted is in moving condition
When, effect is not had in the explosive of region to be blasted installation in advance.
Utility model content
The purpose of the embodiment of the present disclosure is to provide a kind of unmanned plane, the mesh which can be to be blasted by remote control
Mark object is ignited.
To achieve the goals above, the embodiment of the present disclosure provides a kind of unmanned plane, including fuselage and setting in the fuselage
On destructor, the fixed part for being adsorbed on the unmanned plane on target object is additionally provided on the fuselage.
Optionally, the fixed part includes magnetic part.
Optionally, the fixed part includes vacuum chuck.
Optionally, the edge of the fuselage is provided with multiple undercarriages extended vertically, and the undercarriage is formed with peace
Plane is filled, the fixed part is mounted on the undercarriage.
Optionally, the unmanned plane is multi-rotor unmanned aerial vehicle, and the fuselage is formed as plate-like and offers thereon multiple logical
Hole, the rotor of the unmanned plane are mounted on the inside of the through-hole.
Optionally, the center of the fuselage, which is provided with, flies control cabin, to be provided with flight controller in the winged control cabin, institute
It states and flies to be attached to multiple accommodation chambers around control cabin, the destructor is contained in the accommodation chamber and controls with the flight
Device connection, multiple through-holes are arranged around the winged control cabin setting, multiple accommodation chambers around the winged control cabin, and described
Through-hole is circumferentially alternately arranged with the accommodation chamber.
Optionally, the fixed part includes vacuum chuck, and pull of vacuum pump, the vacuum chuck are provided on the fuselage
It is connected by vacuum tube with pull of vacuum pump, the pull of vacuum pump is connect with the flight controller.
Optionally, the vacuum chuck is the sucker being arranged on the fixed part surface.
Optionally, the upper and lower surface of the fuselage is formed from the streamlined structure that the heart is gradually thinned to edge thickness.
Optionally, the fuselage has the inner fovea part that is recessed inwardly of surrounding, and image pickup dress is equipped on the inner fovea part
It sets.
Through the above technical solutions, the unmanned plane that the embodiment of the present disclosure provides is accompanied with destructor, it can be by long-range
Remote control carries out remote-controlled detonation after dropping to target position, avoids the risk of operator's injury.In addition, the fixed part on fuselage
Can be adsorbed on moveable target object, can be fixed on the target object, so lock and to its explosion.
Other feature and advantage of the embodiment of the present disclosure will the following detailed description will be given in the detailed implementation section.
Detailed description of the invention
Attached drawing is to further understand for providing to the embodiment of the present disclosure, and constitute part of specification, under
The specific embodiment in face is used to explain the embodiment of the present disclosure together, but does not constitute the limitation to the embodiment of the present disclosure.Attached
In figure:
Fig. 1 is the structural schematic diagram for the unmanned plane that a kind of illustrative embodiments of the disclosure provide；
Fig. 2 is the top view of Fig. 1；
Fig. 3 is the main view of Fig. 1.
Description of symbols
10 fuselage, 11 fixed part
12 undercarriage, 13 through-hole
14 fly control 15 accommodation chamber of cabin
16 image pick-up device, 111 sucker
131 rotor, 132 support arm
141 flight controller, 151 fuse
Specific embodiment
It is described in detail below in conjunction with specific embodiment of the attached drawing to the embodiment of the present disclosure.It should be understood that this
Locate described specific embodiment and be only used for describing and explaining the embodiment of the present disclosure, is not limited to the embodiment of the present disclosure.
In the embodiments of the present disclosure, in the absence of explanation to the contrary, the noun of locality used such as "upper", "lower" is usually
Refer to that unmanned plane in the upper and lower of real use state, specifically refers to page shown in Fig. 3, and " inside and outside " refers to accordingly
Component outline it is inner and outer.In addition, in the following description when referring to the accompanying drawings, unless otherwise indicated, the same numbers in different attached drawings
Indicate the same or similar element.
Referring to figs. 1 to Fig. 3, the embodiment of the present disclosure provides a kind of unmanned plane, including fuselage 10 and is arranged on fuselage 10
Destructor can drop to mesh by remote control in this way, the unmanned plane that the embodiment of the present disclosure provides is accompanied with destructor
Remote-controlled detonation is carried out after cursor position, avoids the risk of operator's injury.In addition, being that position is unfixed when needing explosion
Movable object object or explosion position are easy exposure and need to be ignited by means of the mobile object at the position
When, the fixed part 11 for being adsorbed on unmanned plane on target object is also provided on fuselage 10, so that explosion dress
Setting can be with movable object object synchronizing moving, and then locks and to its explosion.
Certainly, according to actual needs, the unmanned plane that the embodiment of the present disclosure provides can be revealed simultaneously with destructor, can also
To carry out corresponding destructor dispensing, unmanned plane can return after dispensing.In latter implementation mode, unmanned plane exists
After being adsorbed on target object, destructor can be launched onto target object first, power is then desorbed, at nobody
Machine is far from again igniting target object after blast area.
The absorption of fixed part 11 can be realized in several ways, such as according to one embodiment, fixed part 11 can
It to include magnetic part, such as can be magnet base.Magnetic part has certain magnetic force, can pass through unmanned plane during flying to movement
The lower section of the metal objects such as vehicle, made of metal building or concealed location and then magnetic is on corresponding metal parts.At nobody
In the embodiment that machine needs to reveal with destructor, magnetic part can be permanent magnet.It is needed after unmanned plane launches destructor
It will be far from the electromagnetic adsorption part that in the embodiment of destructor, magnetic part can be changed for magnetic force.Specifically, magnetic part can be with
It include coil and the iron core positioned at coil inside, coil is powered so that iron core generates magnetic field and then unmanned plane electromagnetism can be made to inhale
It is attached on a metal object.It further, can also be by adjusting when unmanned plane needs to release with the suction-operated of metal object
The size of electric current controls electromagnetic force in coil, and the final separation for realizing unmanned plane and metal object makes unmanned plane far from explosion
Device, and then guarantee that unmanned plane makes a return voyage safely.
In another embodiment, fixed part 11 can also include vacuum chuck, so that unmanned plane can pass through
It is adsorbed on smooth surface such as glass and then is fixed on target object.In this case, even if target object does not have
There is metal parts, unmanned plane can be similarly absorbed and fixed on its ontology, and unmanned plane is made to have stronger versatility, it can
Adapt to the target object of various material.Certainly, to further increase absorption fastness of the unmanned plane on target object, magnetic part
Suction-operated can also be carried out simultaneously with vacuum chuck.In addition, in other implementations, Electrostatic Absorption reality can also be passed through
The fixation of existing unmanned plane.
In addition, referring to Figure 1 and Figure 3, the edge of fuselage 10 is provided with multiple undercarriages 12 extended vertically, multiple to rise and fall
Frame 12 is spaced the periphery for being laid in fuselage 10, to guarantee the flat of unmanned aerial vehicle body 10 when unmanned plane carries out VTOL function
Surely.Wherein, undercarriage 12 could be formed with mounting plane, i.e. fixation portions 11 may be mounted on undercarriage 12, such as solid
Determining portion 11 can be set in the top of undercarriage 12, hidden to carry out to facilitate unmanned plane to be adsorbed on the bottom of target object.
Certainly, undercarriage 12 could be formed with multiple planes, and fixed part 11 can be set in multiple planes of undercarriage 12, with energy
Adsorb unmanned plane from multiple positions, and the adsorption plane of fixed part 11 is also planar structure as far as possible, is inhaled to increase
Attached area, and then increase adsorption capacity.It should be noted that no matter which position of fuselage 10 is arranged in fixed part 11, all should
Guarantee that fixed part 11 has the free adsorbing face for extending 10 outer surface of fuselage, to prevent adsorption plane by 10 outer profile of fuselage
Interference effect and can not be fixed on target object.
The embodiment of the present disclosure is not specifically limited the type of unmanned plane, such as can be helicopter, multi-rotor unmanned aerial vehicle
Or fixed-wing unmanned plane etc..According to the specific embodiment that the embodiment of the present disclosure provides, here with a kind of multi-rotor unmanned aerial vehicle
For be further described, referring to figs. 1 to Fig. 3, fuselage 10 can be formed as plate-like and offer multiple through-holes 13, nothing thereon
Man-machine rotor 131 is mounted on the inside of through-hole 13, so as to avoid being wounded by exterior object.In addition, through-hole 13 can be with
Reduce the carrying of fuselage 10 as lightening hole.Specifically, the axis of through-hole 13 runs through fuselage 10 along the vertical direction, inside along diameter
To being provided with support arm 132, the center of support arm 132 is equipped with motor cabinet, motor be mounted on motor cabinet and with 131 phase of rotor
Even.Wherein, support arm 132 can be hollow structure, to form cable tray, so as to improve space utilization rate, while can be with
Play the role of protecting electric wire.Motor wire can extend to the inside of fuselage 10 from the cable tray, to fly with unmanned plane
The electrical connection of the components such as control.In addition, the route for controlling the components such as the electron speed regulator of motor speed can also be from above-mentioned
Extend in cable tray.
Further, as shown in Figure 1 to Figure 3, flying control cabin 14 can be set in the center of fuselage 10, fly in control cabin 14
It is provided with flight controller 141, the components such as including integrated circuit of flight controller 141, to pass through the equipment such as satellite with remote control station
Carry out signal transmission.Fly that multiple accommodation chambers 15 can be attached to around control cabin 14, destructor is contained in accommodation chamber 15 simultaneously
It is connect with flight controller 141, in this way, it is quick-fried to control destructor progress and then remotely controlling flight controller 141
It is broken.Specifically, destructor may include fuse 151 and explosive, the both ends of fuse 151 respectively with flight controller 141 and
Explosive is electrically connected, explosive can be time bomb, with realize target object accurate positionin after by fuse 151 start into
Row time fire.
Further, according to some embodiments, referring to Figures 1 and 2, multiple through-holes 13 can be set around control cabin 14 is flown
It sets, to be supplied to the balanced rising spin of unmanned aerial vehicle body 10, multiple accommodation chambers 15 can also be arranged around control cabin 14 is flown, each
It is placed with destructor in accommodation chamber 15, to carry out explosion to target object from each orientation of unmanned plane, guarantees object
Body can demolish in time.Through-hole 13 is circumferentially alternately arranged with accommodation chamber 15, can save space, and in through-hole 13 and accommodation chamber
15 respectively equally spaced uniformly be looped around fly control 14 surrounding of cabin when, the balance of fuselage 10 can be kept.
In addition, being also provided with pull of vacuum on fuselage 10 in the case where fixation portions 11 includes vacuum chuck
Pump, pull of vacuum pump, which can be set, to fly in control cabin 14, and connect with flight controller 141, and vacuum chuck passes through vacuum tube
It is connected with pull of vacuum pump, carries out aspiratory action to control pull of vacuum pump and then remotely controlling flight controller 141.
Wherein, referring to Fig. 2, vacuum chuck can be the sucker 111 being arranged on 11 surface of fixed part, and vacuum tube is laid in
Inside fuselage 10, and pull of vacuum pump is extended to from sucker 111.Such as Fig. 1 and Fig. 2 shows embodiment in, fuselage 10
Edge be provided with multiple undercarriages 12 extended vertically, the upper surface and lower end surface of undercarriage 12 can be formed as smooth
Mounting surface, sucker 111 can be arranged in the upper surface or lower end surface.That is, in this embodiment, undercarriage 12 is simultaneous simultaneously
Have the effect of fixed part 11, on the one hand unmanned plane landing can be made steady, on the other hand as the formation carrier of vacuum chuck, energy
Enough meets the needs of unmanned plane is fixed on target object.It should be noted that the distribution of above-mentioned sucker 111 can be such as Fig. 2
Shown in arrangement form, be also possible to be formed multiple rows of distribution on 11 surface of fixed part or shapes be set around a variety of distributions such as distribution
Formula.
Further, in this case, when unmanned plane is not ignited simultaneously with destructor, i.e., unmanned plane needs to explode
When device is launched onto target object, fly to be also provided with air pipe line in control cabin 14, air pipe line can be with one end and atmosphere
Connection, the other end is connected to sucker 111, and the on-off of pipeline, solenoid valve and flight can be realized by the control of solenoid valve
Controller 141 is electrically connected.That is, operator is logical when needing to release the suction-operated between unmanned plane and target object
Cross long-range remote control distributor controller 141 and then control solenoid valve and connect vacuum line, atmosphere can enter in sucker 111 into
And complete the separation of unmanned plane and target object.
According to some embodiments, referring to Figure 1 and Figure 3, to reduce resistance when unmanned plane during flying, the upper and lower surface of fuselage 10
It can be formed from the structure that the heart is gradually thinned to edge thickness, for example, the structure can be formed as streamlined.
According to some embodiments, referring to Figures 1 and 2, fuselage 10 has the inner fovea part that is recessed inwardly of surrounding, can on inner fovea part
To be equipped with image pick-up device 16, damaged so as to prevent image pick-up device 16 from being hit by the object of side.It is multiple
Image pick-up device 16 can detect omnidirectional's outdoor scene around fuselage 10 around the setting of the interval of fuselage 10.Image pickup
Device 16 may include any component for the image information that imaging sensor and camera etc. can acquire surrounding articles, Huo Zheduo
The combination of kind component, and can be connect by the way that the corresponding cabling inside fuselage 10 is arranged in flight controller 141, with energy
Enough image informations picked up around unmanned plane in real time simultaneously pass through radio signal transmission to remote control station, are accurately positioned in unmanned plane
On predetermined position or target object, while operator can also be made to grasp the outdoor scene situation in region to be blasted in time, with basis
Actual needs accordingly adjusts explosion, guarantees that blasting work is perfectly safe.
The preferred embodiment of the disclosure is described in detail in conjunction with attached drawing above, still, the embodiment of the present disclosure is not limited to
Detail in above embodiment can be to the embodiment of the present disclosure in the range of the technology design of the embodiment of the present disclosure
Technical solution carries out a variety of simple variants, these simple variants belong to the protection scope of the embodiment of the present disclosure.
It is further to note that specific technical features described in the above specific embodiments, in not lance
In the case where shield, it can be combined in any appropriate way, in order to avoid unnecessary repetition, the embodiment of the present disclosure pair
No further explanation will be given for various combinations of possible ways.
In addition, any combination can also be carried out between a variety of different embodiments of the embodiment of the present disclosure, as long as it is not
The thought of the embodiment of the present disclosure is violated, equally should be considered as embodiment of the present disclosure disclosure of that.
Claims (10)
1. a kind of unmanned plane, which is characterized in that described including fuselage (10) and the destructor being arranged on the fuselage (10)
The fixed part (11) for being adsorbed on the unmanned plane on target object is additionally provided on fuselage (10).
2. unmanned plane according to claim 1, which is characterized in that the fixed part (11) includes magnetic part.
3. unmanned plane according to claim 1 or 2, which is characterized in that the fixed part (11) includes vacuum chuck.
4. unmanned plane according to claim 1, which is characterized in that the edge of the fuselage (10) is provided with multiple vertical
The undercarriage (12) of extension, the undercarriage (12) are formed with mounting plane, and the fixed part (11) is mounted on the undercarriage
(12) on.
5. unmanned plane according to claim 1, which is characterized in that the unmanned plane is multi-rotor unmanned aerial vehicle, the fuselage
(10) be formed as plate-like and offer thereon multiple through-holes (13), the rotor (131) of the unmanned plane is mounted on the through-hole
(13) inside.
6. unmanned plane according to claim 5, which is characterized in that the center of the fuselage (10), which is provided with, flies control cabin
(14), it is provided with flight controller (141) in the winged control cabin (14), is attached to multiple receivings around the winged control cabin (14)
Cabin (15), the destructor are contained in the accommodation chamber (15) and connect with the flight controller (141), multiple described
Through-hole (13) is around winged control cabin (14) setting, and multiple accommodation chambers (15) are arranged around the winged control cabin (14), and institute
It states through-hole (13) and is circumferentially alternately arranged with the accommodation chamber (15).
7. unmanned plane according to claim 6, which is characterized in that the fixed part (11) includes vacuum chuck, the machine
Pull of vacuum pump is provided on body (10), the vacuum chuck is connected by vacuum tube with pull of vacuum pump, the vacuum
Suction pump is connect with the flight controller (141).
8. unmanned plane according to claim 7, which is characterized in that the vacuum chuck is to be arranged in the fixed part (11)
Sucker (111) on surface.
9. unmanned plane according to claim 5, which is characterized in that the upper and lower surface of the fuselage (10) is formed from the heart
The streamlined structure being gradually thinned to edge thickness.
10. unmanned plane according to claim 5, which is characterized in that it is interior that there is the fuselage (10) surrounding to be recessed inwardly
Recess portion is equipped with image pick-up device (16) on the inner fovea part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821081920.0U CN208393633U (en) | 2018-07-09 | 2018-07-09 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821081920.0U CN208393633U (en) | 2018-07-09 | 2018-07-09 | Unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN208393633U true CN208393633U (en) | 2019-01-18 |
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ID=65131235
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821081920.0U Active CN208393633U (en) | 2018-07-09 | 2018-07-09 | Unmanned plane |
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| Country | Link |
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| CN (1) | CN208393633U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110362108A (en) * | 2019-06-17 | 2019-10-22 | 沈阳无距科技有限公司 | Unmanned plane is grounded control method, device, storage medium and electronic equipment |
| CN113232893A (en) * | 2021-04-23 | 2021-08-10 | 北京理工大学 | Distributed homing guidance system |
| GB2618532A (en) * | 2022-05-06 | 2023-11-15 | Purnell Mark | Unmanned aerial vehicle |
-
2018
- 2018-07-09 CN CN201821081920.0U patent/CN208393633U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110362108A (en) * | 2019-06-17 | 2019-10-22 | 沈阳无距科技有限公司 | Unmanned plane is grounded control method, device, storage medium and electronic equipment |
| CN110362108B (en) * | 2019-06-17 | 2022-07-29 | 沈阳无距科技有限公司 | Unmanned aerial vehicle grounding control method and device, storage medium and electronic equipment |
| CN113232893A (en) * | 2021-04-23 | 2021-08-10 | 北京理工大学 | Distributed homing guidance system |
| GB2618532A (en) * | 2022-05-06 | 2023-11-15 | Purnell Mark | Unmanned aerial vehicle |
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