CN109878898A - A kind of protection component of unmanned plane transport case - Google Patents
A kind of protection component of unmanned plane transport case Download PDFInfo
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- CN109878898A CN109878898A CN201711278164.0A CN201711278164A CN109878898A CN 109878898 A CN109878898 A CN 109878898A CN 201711278164 A CN201711278164 A CN 201711278164A CN 109878898 A CN109878898 A CN 109878898A
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- plate
- side plate
- unmanned plane
- siding
- bottom plate
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Abstract
The present invention relates to a kind of protection components of unmanned plane transport case, hinged between bottom plate and side plate including the cabinet being made of bottom plate, side plate and top plate, between side plate and side plate, connection fixed by snap between side plate and top plate；Upper plate and lower plate are fixedly installed on side plate, upper plate and lower plate are arranged in parallel with bottom plate；On upper plate bottom surface and lower plate top surface along perpendicular on the direction of side plate plate face, be provided with the corresponding track in position or more, sliding block is slidably connected on track, it is fixed with one and side plate plate face siding disposed in parallel between sliding block, multiple 4th springs are fixedly connected between siding and side plate；Shutdown platform is provided on bottom plate；Unmanned plane of the invention is provided with spring on bottom plate and side plate, so as to form damping device, during transportation, can offset pitch bring active force, guarantee transporting safely for unmanned plane.
Description
Technical field
The invention belongs to air vehicle technique fields, and in particular to a kind of protection component of unmanned plane transport case.
Background technique
UAV, abbreviation unmanned plane are a kind of new concept equipment being in rapid development, with motor-driven spirit
Work, rapid reaction, unmanned flight, operation require low advantage.Currently, unmanned plane has been widely used for military affairs, scientific research, civilian
Three big fields, specifically in fields such as electric power, communication, meteorology, agricultural, ocean, exploration, photography, patrol, anti-terror explosive removings using very
Extensively.
But unmanned plane all parts are part easy to damage, especially rotor part, in transit due to vibration of jolting
It is dynamic, it is easy to unmanned plane is damaged, and in the prior art due to unprofessional unmanned plane means of transport, so, unmanned plane transport
The case where damaging in the process often occurs.
Summary of the invention
In order to solve the technical issues of being easily damaged in unmanned plane transportational process existing in the prior art, the present invention is provided
Following technical scheme:
A kind of protection component of unmanned plane transport case, it is characterised in that: including the cabinet being made of bottom plate, side plate and top plate,
It is hinged between the bottom plate and side plate, between the side plate and side plate, connection fixed by snap between side plate and top plate；
Upper plate and lower plate are fixedly installed on the side plate, the upper plate and lower plate are arranged in parallel with the bottom plate；
On the upper plate bottom surface and lower plate top surface along perpendicular on the direction of the side plate plate face, to be provided with position or more corresponding
Track slidably connects sliding block on the track, one and the side plate plate face wall disposed in parallel is fixed between the sliding block
Plate is fixedly connected with multiple 4th springs between the siding and the side plate；
Shutdown platform is provided on the bottom plate.
As a further explanation of the present invention, spongy layer is provided in the siding plate face.
Compared with prior art, what the present invention obtained has the beneficial effect that
Unmanned plane of the invention, is provided with spring mechanism on side plate, so as to form damping device, during transportation,
Pitch bring active force can be offset, guarantees transporting safely for unmanned plane.
The present invention is described in further details below with reference to accompanying drawings and embodiments.
Detailed description of the invention
Fig. 1 is the unmanned plane main view that embodiment 2 provides.
Fig. 2 is the top view of Fig. 1.
Fig. 3 is unmanned plane linking arm structural schematic diagram.
Fig. 4 is unmanned plane linking arm partial sectional view.
Fig. 5 is top view when transport case is used as shutdown platform.
Fig. 6 is the overall structure diagram of transport case.
Fig. 7 is that unmanned plane is packed into transport case overall structure diagram.
Fig. 8 is unmanned plane spraying mechanism cross-sectional view.
Fig. 9 is unmanned plane spraying mechanism top view.
In figure: 1, rotor platform；2, rotor arm；3, rotor；4, flight motor；5, linking arm；6, Crashworthy plate；7, the first bullet
Spring；8, second spring；9, sleeve；10, piston rod；11, the first fixed part；12, the second fixed part；13, bottom plate；14, side plate；
15, top plate；16, third spring；17, support plate；18, support rod；19, support frame；20, supporting leg；21, arc groove；22, annular
Strut；23, upper plate；24, lower plate；25, sliding block；26, siding；27, the 4th spring；28, supporting block；29, sliding rail；30, water tank；
31, immersible pump；32, water pipe；33, turntable；34, spray head；35, deep groove ball bearing；36, locking nut；37, O-ring seal；38,
Tapped through hole.
Specific embodiment
Reach the technical means and efficacy that predetermined purpose is taken for the present invention is further explained, below in conjunction with attached drawing and reality
Example is applied to a specific embodiment of the invention, structure feature and its effect, detailed description are as follows.
In the description of the invention, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ", "upper", "lower",
The orientation or positional relationship of the instructions such as "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description the invention and simplifies description, rather than indicate
Or imply that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore cannot understand
For the limitation to the invention.
In addition, term " first ", " second ", " third " etc. are used for description purposes only, it is not understood to indicate or imply
Relative importance or the quantity for implicitly indicating indicated technical characteristic.The feature of " first ", " second " etc. is defined as a result,
It can explicitly or implicitly include one or more of the features.In the description of the invention, unless otherwise indicated,
The meaning of " plurality " is two or more.
Term " installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, be also possible to removable
Connection is unloaded, or is integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, it can also be in
Between medium be indirectly connected, can be the connection inside two elements.For the ordinary skill in the art, can pass through
Concrete condition understands concrete meaning of the above-mentioned term in the invention.
Embodiment 1:
To solve the technical issues of being easily damaged in unmanned plane transportational process existing in the prior art, the present embodiment provides one kind
The protection component of unmanned plane transport case, as shown in Figure 6, Figure 7, including the cabinet being made of bottom plate 13, side plate 14 and top plate 15；
It is hinged between bottom plate and side plate, between side plate and side plate, connection fixed by snap between side plate and top plate, when side plate whole exhibition
When opening, which can use as shown in Figure 5 as the unmanned plane platform that rise and fall；The protection component includes vertically solid on side plate 14
Surely the upper plate 23 and lower plate 24 being arranged, upper plate 23 and lower plate 24 are arranged in parallel with bottom plate 13；23 bottom surface of upper plate and lower plate 24 are pushed up
On face along perpendicular on the direction of 14 plate face of side plate, be provided with the corresponding track in position or more, slidably connect sliding block on track
25, one and 14 plate face of side plate siding 26 disposed in parallel are fixed between sliding block 25, are fixedly connected between siding 26 and side plate 14
There are multiple 4th springs 27, is provided with shutdown platform on bottom plate.
It is provided with above-mentioned protection mechanism on each side plate 14, after the completion of unmanned plane is parked, side plate 14 is propped up, and
Top plate 15 is covered, herein, between side plate 14 and side plate 14, fixed by snap between side plate 14 and top plate 15, such as Fig. 6, Fig. 7
It is shown, when unmanned plane touches siding 26, due to the effect of the 4th spring 27, slides siding 26 along track and then reset,
The active force that collision generates is offset, makes unmanned plane during transportation, not will receive strong collision, guarantee the complete of unmanned plane
It is good.
Preferably, one layer of spongy layer is set in siding plate face, further the intracorporal unmanned plane of case can be formed and protected.
Above-mentioned shutdown platform include on bottom plate 13 equally distributed multiple third springs 16,16 top of third spring be fixed with
Support plate 17 is hinged with multiple support rods 18 on 17 side wall of support plate, and 18 free end of support rod is slidably connected with bottom plate 13, support
17 top surface of plate is for parking unmanned plane.
Above-mentioned 17 top surface of support plate is arranged symmetrically, and there are two support frames 19, pass through support between support frame 19 and support plate 17
Leg 20 connects；19 top surface of support frame is provided with the groove to match with unmanned plane undercarriage, and support frame 19 is set in the present embodiment
It is set to arc-shaped, and the center of circle of two support frames 19 is overlapped；19 top surface of support frame has been arranged concentrically arc groove 21.
When unmanned plane is parked, by the effect of third spring 16, damping effect can be played the role of, pass through support rod 18
The stability for further reinforcing support plate 17 keeps parking for unmanned plane more steady.
Above-mentioned 18 free end of support rod is fixedly connected with a supporting block 28, position corresponding with supporting block 28 on 13 top surface of bottom plate
It is respectively arranged with sliding rail 29, supporting block 28 is slidably connected with sliding rail 29.When unmanned plane lands or takes off, third spring 16 is pressed
Contracting plays firm effect to support plate 17 at this point, support rod 18 can be slided along sliding rail 29.
Embodiment 2:
On the basis of the above embodiments, the present embodiment provides a kind of anticollision unmanned planes, as shown in Figure 1 and Figure 2, including rotor
Platform 1,1 edge of rotor platform are evenly distributed with rotor arm 2, and 2 end of rotor arm is provided with rotor 3, and rotor 3 is by flight motor 4
Driving rotation, wherein each 2 end of rotor arm is provided with anticollision mechanism；Anticollision mechanism includes being fixed on 2 end of rotor arm
Linking arm 5,5 end of linking arm are provided with Crashworthy plate 6, and Crashworthy plate 6 is arc-shaped structure, the rotation center in the center of circle and rotor 3
It is overlapped；Linking arm 5 is as shown in Figure 3, Figure 4, including the first spring 7, second spring 8, sleeve 9, piston rod 10, the first fixed part 11
With the second fixed part 12,10 one end of piston rod is protruded into sleeve 9, and 10 other end of piston rod is fixedly connected with the first fixed part 11,
9 bottom end of sleeve is fixedly connected with the second fixed part 12, and the first spring 7 is sheathed on piston rod 10 and sleeve 9 and both ends are supported respectively
On 12 end face of the first fixed part 11 and the second fixed part, second spring 8 is set in sleeve 9 for touching, and one end and 9 bottom surface of sleeve
Contact, the other end are contacted with piston rod 10；Crashworthy plate 6 is fixedly connected with the first fixed part 11, rotor arm 2 and the second fixed part 12
It is fixedly connected.
Above-mentioned unmanned plane protects rotor 3 in flight course, through Crashworthy plate 6, guarantees that rotor 3 will not touch extraneous obstacle
Then Crashworthy plate 6 is fixed on 3 periphery of rotor by the connecting rod of above structure, passes through the first spring 7 and second spring 8 by object
Second level damping can be constituted, when Crashworthy plate 6 touches barrier, the active force that collision generates can be offset by spring force,
To reduce power suffered by rotor arm 2, achieve the purpose that protect rotor 3 and rotor arm 2.
An annular strut 22, when unmanned plane is parked, the annular strut 22 and above-mentioned arc are fixedly connected with below rotor arm 2
Slot matches, and realizes that unmanned plane is steadily parked, and during transportation, can further limit the position of unmanned plane.
It is respectively provided in above-mentioned each anticollision mechanism there are three Crashworthy plate 6 and linking arm 5, three linking arms 5 are in rotor arm 2
Crossing distribution setting；Tapped through hole 38 is provided on second fixed part 12, and three linking arms 5 sequentially pass through spiral shell by screw
Line through-hole 38 is fixedly connected with rotor arm 2.The central angle of Crashworthy plate 6 is.
The central angle of above-mentioned Crashworthy plate 6 is set as 60 ° -90 °, and quantity is three, and each linking arm 5 is and Crashworthy plate
6 circular arc arc centers go out to be fixedly connected, so, the clearance angle between two adjacent Crashworthy plates 6 is up to 30 °, minimum
0, and it is because of in flight, only outside can collide unmanned plane, and inside is revolved that Crashworthy plate 6 is not provided at rotor arm 2
At wing arm 2 will not collision obstacle, so, be not provided with Crashworthy plate 6 at this, and when between two Crashworthy plates 6 angle be 30 °
When, when touching barrier, since two Crashworthy plates 6 are closer, so barrier cannot touch rotor 3, the structure was both
It can be well protected rotor 3, and material can be saved, reduce cost.
Embodiment 3:
The unmanned plane provided in above-described embodiment can carry plurality of devices, be widely used in every field, and the present embodiment only mentions
For a kind of carrying spraying mechanism, which can be applied to haze improvement, plant protection, the fields such as fire-fighting.
Spraying mechanism is as shown in Figure 8, Figure 9, the water tank 30 including the setting of 1 bottom surface of rotor platform, is provided in water tank 30 latent
Water pump 31,31 water outlet of immersible pump are equipped with water pipe 32, and 32 bottom end of water pipe is provided with spray assembly；Spray assembly includes turntable 33
With the multiple spray heads 34 being installed on 33 periphery of turntable, 32 bottom end of water pipe protrude into turntable 33 and with 33 internal cavities of turntable
It is connected to, deep groove ball bearing 35 is fixedly installed in turntable 33, water pipe 32 passes through deep groove ball bearing 35 and 35 inner ring of deep groove ball bearing
It is fixedly connected, to realize being rotatably connected between turntable 33 and water pipe 32；33 inner bottom of turntable is provided with internal screw thread and leads to
It crosses and is threadedly coupled a locking nut 36, to fix deep groove ball bearing 35；It is arranged between 32 top outer wall of water pipe and 33 inner wall of turntable
There is O-ring seal 37, to realize the space sealing between water pipe 32 and turntable 33；Circumferential uniform point along turntable 33 of multiple spray heads 34
Cloth and spray head 34 are tilted to same direction.
Preferably, the inclined direction of spray head 34 is clockwise or counterclockwise.
Liquid pressing in water tank 30 is then sent in turntable 33, the spray by immersible pump 31 in above-mentioned spray assembly
The axial line of spray head 34 and 33 radius of turntable form an obtuse angle in mist component, and multiple spray heads 34 incline to same direction
Tiltedly, the direction can be clockwise is also possible to counterclockwise, when the liquid of pressurization by spray head 34 spray when, can generate one with
Injection direction opposite effect power is not required to increase any driving mechanism, saves cost so will lead to 33 spinning of turntable.?
During 33 spinning of turntable, centrifugal force can be also generated, cover the liquid sprayed can under the influence of centrifugal force bigger
Range is sprayed, spraying efficiency is improved.
The above content is a further detailed description of the present invention in conjunction with specific preferred embodiments, and it cannot be said that
Specific implementation of the invention is only limited to these instructions.For those of ordinary skill in the art to which the present invention belongs, exist
Under the premise of not departing from present inventive concept, a number of simple deductions or replacements can also be made, all shall be regarded as belonging to of the invention
Protection scope.
Claims (2)
1. a kind of protection component of unmanned plane transport case, it is characterised in that: including the case being made of bottom plate, side plate and top plate
Body, it is hinged between the bottom plate and side plate, between the side plate and side plate, connection fixed by snap between side plate and top plate；
Upper plate and lower plate are fixedly installed on the side plate, the upper plate and lower plate are arranged in parallel with the bottom plate；
On the upper plate bottom surface and lower plate top surface along perpendicular on the direction of the side plate plate face, to be provided with position or more corresponding
Track slidably connects sliding block on the track, one and the side plate plate face wall disposed in parallel is fixed between the sliding block
Plate is fixedly connected with multiple 4th springs between the siding and the side plate；
Shutdown platform is provided on the bottom plate.
2. protection component according to claim 1, it is characterised in that: be provided with spongy layer in the siding plate face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711278164.0A CN109878898A (en) | 2017-12-06 | 2017-12-06 | A kind of protection component of unmanned plane transport case |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711278164.0A CN109878898A (en) | 2017-12-06 | 2017-12-06 | A kind of protection component of unmanned plane transport case |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109878898A true CN109878898A (en) | 2019-06-14 |
Family
ID=66924004
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711278164.0A Withdrawn CN109878898A (en) | 2017-12-06 | 2017-12-06 | A kind of protection component of unmanned plane transport case |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109878898A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110803382A (en) * | 2019-11-21 | 2020-02-18 | 武义普巴机械设备有限公司 | Supporting transport case of express delivery transportation unmanned aerial vehicle |
| CN113086384A (en) * | 2021-02-19 | 2021-07-09 | 深圳供电局有限公司 | Unmanned aerial vehicle transportation mount |
-
2017
- 2017-12-06 CN CN201711278164.0A patent/CN109878898A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110803382A (en) * | 2019-11-21 | 2020-02-18 | 武义普巴机械设备有限公司 | Supporting transport case of express delivery transportation unmanned aerial vehicle |
| CN110803382B (en) * | 2019-11-21 | 2020-04-21 | 武义普巴机械设备有限公司 | Supporting transport case of express delivery transportation unmanned aerial vehicle |
| CN113086384A (en) * | 2021-02-19 | 2021-07-09 | 深圳供电局有限公司 | Unmanned aerial vehicle transportation mount |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190614 |