CN206427260U - Collapsible unmanned vehicle and its horn - Google Patents
Collapsible unmanned vehicle and its horn Download PDFInfo
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- CN206427260U CN206427260U CN201621276591.6U CN201621276591U CN206427260U CN 206427260 U CN206427260 U CN 206427260U CN 201621276591 U CN201621276591 U CN 201621276591U CN 206427260 U CN206427260 U CN 206427260U
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Abstract
The utility model provides a kind of collapsible unmanned vehicle and its horn, belongs to unmanned vehicle technical field.Horn includes：Covered on horn；Horn lower cover, the installation portion is rotationally connected with covering the buckling parts of merga pass one that interlocks on horn；A pair of holding sections, are arranged at buckling parts；Revolving part, its upper end is fixedly connected with the groove of installation portion, and its lower end optionally fastens or is separated with any one in a pair of holding sections.Collapsible unmanned vehicle and its horn of the present utility model, by rotating horn, so that one of holding section of revolving part and horn lower cover is separated, and fastened with another holding section, realizing horn can switch relative to fuselage between deployed condition or folded state, it is easy to collapsible unmanned vehicle minimum in the volume shared by off working state, non-state of flight, convenient use person stores and carried.
Description
Technical field
The utility model is related to unmanned vehicle technical field, more particularly to a kind of collapsible unmanned vehicle and its machine
Arm.
Background technology
At present, the unmanned vehicle volume of consumer level is relatively large, is not easy to the carrying and storage of consumer.And small-sized nothing
People's aircraft is relatively low due to manufacturing cost, small volume and is easy to carry, it has also become the trend of aircraft.But, it is existing
The horn of unmanned vehicle can not be folded, and be unfavorable for unmanned vehicle to miniaturization.
Therefore, when how to make unmanned vehicle in idle off working state, non-state of flight, the volume for taking it
It is less, it is easy to store and carries, has yet to be improved and developed.
Utility model content
Main purpose of the present utility model is proposition a kind of collapsible unmanned vehicle and its horn, makes unmanned vehicle
It is minimum in the volume shared by off working state, non-state of flight, it is easy to store and carries.
To achieve the above object, the utility model provides a kind of horn of collapsible unmanned vehicle, is rotationally connected with
The installation portion of collapsible unmanned vehicle, the horn includes：Covered on horn；Lid is interlocked on horn lower cover, with the horn
And the installation portion is rotationally connected with by a buckling parts；A pair of holding sections, are arranged at the buckling parts；Revolving part, thereon
End is fixedly connected with the groove of the installation portion, and its lower end optionally fastens with any one in the pair of holding section
Or be separated；The horn has first position and the second place relative to the installation portion, when the horn is in first
During position, the horn is in folded state, and when the horn is in the second place, the horn is in deployed condition, institute
Revolving part is stated optionally to be separated with one of holding section, and with the rotation of the horn, the revolving part is snapped into
Another holding section, makes the horn switch relative to the installation portion between the first position and the second place.
Alternatively, in addition to bottom, the bottom has the first hole and the second hole being disposed adjacent with first hole, institute
State the lower end covered on horn and be provided with link slot, the horn lower cover is provided with bearing towards the side covered on the horn, passes through spiral shell
Silk sequentially passes through the bearing, first hole and the installation portion and is caught in the link slot, makes to cover and described on the horn
Horn lower cover is snapped together.
Alternatively, the revolving part includes body, from the upper surface of the body towards between direction of body etc.
Every protruding out the multiple auxiliary sections to be formed, the multiple auxiliary section is caught in the groove of the installation portion, under the body
End face fastens through second hole and with any one holding section.
Alternatively, the pair of holding section is located at the both sides of the bearing.
Alternatively, the bearing and the pair of holding section are in the isosceles triangle that drift angle is special angle.
Alternatively, the pair of holding section is respectively equipped with a pair of openings, and the revolving part is optionally opened with one of them
Mouthful be separated or fasten, and fasten or be separated with another opening, make the horn the first position with
Switch between the second place.
Alternatively, the diameter of the opening is less than the diameter of section of the revolving part.
Alternatively, the opening is C-shaped.
Alternatively, the revolving part includes the decorative pearl on top of an official cap, the flexible member for being sheathed on the decorative pearl on top of an official cap and rotating shaft.
Alternatively, in addition to bottom, the bottom has the first hole and the second hole being connected with first hole, described
Lid has connecting hole on horn, and the rotating shaft is corresponding with the connecting hole, and the horn lower cover is towards covering on the horn
Side is provided with bearing, and the bearing, first hole, the installation portion, the connecting hole, Yi Jisuo are sequentially passed through by screw
Rotating shaft is stated, lid and the horn lower cover on the horn is rotationally snapped together.
Alternatively, the decorative pearl on top of an official cap include decorative pearl on top of an official cap body, the top surface from the decorative pearl on top of an official cap body protrude out to be formed multiple auxiliary sections,
And the oblate spheroid portion to be formed is protruded out downwards from the bottom surface of the decorative pearl on top of an official cap body, the flexible member is sheathed on the multiple cooperation
Portion, and the groove of the installation portion is caught in, horn lower cover also includes the projection being connected with the pair of holding section, works as institute
When stating horn rotation, the oblate spheroid portion fastens or is separated with any one described holding section.
Alternatively, the multiple auxiliary section is in cross.
Alternatively, the quantity of the auxiliary section is 4.
Alternatively, the revolving part also includes damper assembly, and the damper assembly includes damped ring and multiple damping gaskets,
The damped ring and damping gasket are stacked in being covered on the horn between the installation portion, are covered on the horn is assembled
During with the horn lower cover, the screw passes through the damper assembly.
In addition, to achieve the above object, the utility model also provides a kind of collapsible unmanned vehicle, including fuselage, sets
It is placed in multiple installation portions of described two sides of fuselage and is rotationally connected with the horn of the installation portion, the horn is upper
State the horn described in any one.
Alternatively, in addition to power set and the rotation oar on the power set, the power set are fixed on
The one end of the horn away from the installation portion, the power set drive the rotation oar rotation.
Alternatively, the installation portion includes main body, extends the connecting portion to be formed from the main body and is formed at the master
Gap between body and the connecting portion, the connecting portion includes rotation section, and the connecting portion is provided with hole, and the rotation section is located at
Rotated in the hole and relative to the connecting portion, the rotation section has centre bore, and the groove is formed at the rotation section
Lower end.
Alternatively, the cable of the power set is contained in lid and horn lower cover on the horn and fastens the cable to be formed receipts
Hold in space, and the cable receiving space is stretched out in part.
Alternatively, there is wire hole and the gap being connected with the wire hole between the rotation section and the hole,
The cable of the power set stretches into the installation portion from the wire hole, then is stretched out from the gap, and is connected to main control
Plate, and then the power set are electrically connected with the master board.
Alternatively, the connecting portion also includes the limiting section for protruding out setting, and the limiting section is used for the horn described
Carried out when switching between first position and the second place secondary spacing.
The utility model proposes collapsible unmanned vehicle and its horn, by rotating horn so that revolving part and machine
One of holding section of arm lower cover is separated, and is fastened with another holding section, realize horn can be relative to fuselage at
In deployed condition or folded state, it is easy to collapsible unmanned vehicle in the body shared by off working state, non-state of flight
Product is minimum, and convenient use person stores and carried.
Brief description of the drawings
The stereogram for the collapsible unmanned vehicle that Fig. 1 provides for the utility model first embodiment, the collapsible nothing
People's aircraft is in deployed condition, and it includes horn, installation portion；
Fig. 2 is the stereogram in folded state of collapsible unmanned vehicle in Fig. 1；
Fig. 3 is the assembling figure of horn and installation portion in Fig. 1；
Fig. 4 is the exploded view of horn and installation portion in Fig. 3；
Fig. 5 is the sectional view of horn and installation portion in Fig. 3；
The stereogram for the collapsible unmanned vehicle that Fig. 6 provides for the utility model second embodiment, collapsible nobody flies
Row device is in deployed condition, and it includes horn, installation portion；
Fig. 7 is the stereogram in folded state of collapsible unmanned vehicle in Fig. 6；
Fig. 8 is the assembling figure of horn and installation portion in Fig. 6；
Fig. 9 is the exploded view of horn and installation portion in Fig. 8, and horn includes revolving part, and the revolving part includes the decorative pearl on top of an official cap；
Figure 10 is the sectional view of horn and installation portion in Fig. 8；
Figure 11 is the partial sectional view in Figure 10；
Figure 12 is the partial enlarged drawing of the decorative pearl on top of an official cap in Fig. 9.
Realization, functional characteristics and the advantage of the utility model purpose will be described further referring to the drawings in conjunction with the embodiments.
Embodiment
Embodiment of the present utility model is described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning
Same or similar element or element with same or like function are represented to same or similar label eventually.Below by ginseng
The embodiment for examining accompanying drawing description is exemplary, it is intended to for explaining the utility model, and it is not intended that to the utility model
Limitation.
Fig. 1 is refer to, the stereogram of the collapsible unmanned vehicle 100 provided for the utility model first embodiment.
In the present embodiment, collapsible unmanned vehicle 100 be used for carry the filming apparatus such as camera, video camera carry out take photo by plane operation,
The work such as figure mapping, Investigating and rescue, aerial monitoring, polling transmission line.Collapsible unmanned vehicle 100 was flying
There is a kind of or the above flight attitude in driftage, roll, pitching in journey.
Referring to Fig. 1-2, collapsible unmanned vehicle 100 include fuselage 10, multiple horns 20, power set 30,
And rotation oar 40.Multiple horns 20 are movably connected with the both sides of fuselage 10.When collapsible unmanned flight 100 is in non-flight
During state, multiple horns 20 can be rotated relative to fuselage 10, and it is in folded state (as shown in Figure 2) to draw in around fuselage 10
And in first position, now, the space shared by collapsible unmanned vehicle 100 is smaller, is easy to store and carries.Work as folding
When formula unmanned vehicle 100 is in state of flight, multiple horns 20 can deploy relative to fuselage and be in the second place.
Fuselage 10 is substantially in cuboid, and it includes chain-drive section 11, the drive end unit 12 being oppositely arranged with chain-drive section 11, the first side
Surface 13, the second side surface 14 being oppositely arranged with the first side surface 13 and multiple installation portions 15.In other the present embodiment
In, the shape of fuselage 10 can also be spheroid, ellipsoid etc..
In the present embodiment, chain-drive section 11 and drive end unit 12 are located at the end face of two relative short sides of fuselage 10 respectively, the
One side surface 13 and the second side surface 14 are located at the end face on two relative long sides of fuselage 10 respectively.Installation portion 15 is by the first side table
Face 13, the surface of the second side surface 14 are directed away from the first side surface 13, the direction of the second side surface 14 and protrude out to be formed.
Referring to 2-3, installation portion 15 includes main body 151, connecting portion 152 and is formed at main body 151 and connecting portion
Gap 153 between 152.Surface of the autonomous agent 151 of connecting portion 152 away from the side of fuselage 10 extends to be formed.In the present embodiment,
The cross-sectional length of connecting portion 152, less than the cross-sectional length of main body 151.
Connecting portion 152 includes rotation section 154, protrudes out the limiting section 155 to be formed from the side of connecting portion 152.Specifically, connect
The center in portion 152 is provided with hole.Rotation section 154 is arranged in the hole, it is possible to rotated relative to connecting portion 152.Rotation section 154
Center there is centre bore 156.In the present embodiment, the hole of centre bore 156 and connecting portion 152 is coaxial.Under rotation section 154
End has groove 157 (as shown in Figure 5).
Further, the shape of rotation section 154 can be torus or have irregular annulus jaggy
Body.When rotation section 154 is has irregular torus jaggy, wire hole 158 is formed between rotation section 154 and hole.
The cable (not shown) that wire hole 158 and gap 153 are used for power set 30 enters walking line, plays a part of hidden wiring.Tool
Body, the cable of power set 30 stretches into installation portion 15 from wire hole 158, then is stretched out from gap 153, and is connected to main control
Plate, realizes the electric connection of power set 30 and master board.
Limiting section 155 convexedly stretches in the surface of installation portion 15, for avoiding horn 20 first position (being in folded state)
It is secondary spacing to being carried out when switching between the second place (being in deployed condition).
Referring to Fig. 4-5, horn 20 matches with installation portion 15.Preferably, multiple horns 20 can symmetrically and rotate
Ground is connected to the installation portion 15 on the first side surface 13 and the second side surface 14 of fuselage, and multiple horns 20 can be relative to fuselage
10 are selectively in deployed condition or folded state.Specifically, one end (i.e. connection end) of horn 20 is rotationally connected with
Installation portion 15, the other end (i.e. free end) is rotated relative to connection end, with away from or close to the first side surface 13 or the
Two side surfaces 14.
When horn 20 is in deployed condition, the free end of horn 20 is away from the first side surface 13 or the second side table
Face 14, when horn 20 is in folded state, the first side surface 13 or the second side surface are close in the free end of horn 20
14。
It will be appreciated by persons skilled in the art that when horn 20 is in deployed condition with folded state, horn 20
Free end is differed relative to the first side surface 13 of fuselage 10 or the distance of the second side surface 14.Specifically, horn 20
In deployed condition relative to the distance of the first side surface 13 or the second side surface 14, more than horn 20 in folded state
When relative to the first side surface 13 or the second side surface 14 distance.
The quantity of horn 20 can be multiple, for example, 2,4,6 etc..In the present embodiment, the quantity of horn 20 is
4, and it is symmetrically disposed on the first side surface 13 and the second side surface 14.
Referring to 3-4, horn 20 includes lid 21, horn lower cover 22, revolving part 23, bottom 24 and spiral shell on horn
Silk 25.Lid 21 and horn lower cover 22 buckling parts of merga pass one that interlocks are rotationally connected with installation portion, and revolving part 23 on horn
It is contained on horn among lid 21 and horn lower cover 22 with bottom 24.
Lid 21 includes upper lid body 211, the first connection end 212 positioned at upper one end of lid body 211 and is located on horn
First free end 213 of the upper other end of lid body 211.Wherein, surface projection of the upper lid body 211 towards the side of horn lower cover 22
Multiple projections 215 (as shown in Figure 5).First connection end 212 is close to installation portion 15, and accordingly, the first free end 213 is away from peace
Dress portion 15.The lower end of first connection end 212 towards the side of horn lower cover 22 is provided with link slot 2121 (as shown in Figure 5).
Horn lower cover 22 includes lower cover body 221, the second connecting portion 222 positioned at the one end of lower cover body 221 and is located at
Second free end 223 of the other end of lower cover body 221.Wherein, the second connection end 222 matches and leaned on the first connection end 212
Nearly installation portion 15, accordingly, the second free end 223 and the first connection end 213 match and away from installation portion 15.
Specifically, lower cover body 221 is provided with multiple locating dowels 224, each positioning towards the surface of the side of lid on horn 21
Post 224 offers positioning hole 2241.When lid 21 is interlocked with horn lower cover 22 on horn, multiple projections of upper lid body 211
215 insert in corresponding positioning hole 2241 respectively.
The surface of second connection end 222 towards the side of the first connection end 212 is provided with bearing 225.A pair of holding sections 226 are set
In buckling parts.The position of bearing 225 is corresponding with the position of the centre bore 156 on installation portion 15, and the center of bearing is opened up
Through hole 2251.A pair of holding sections 226 are located at the both sides of bearing 225.
Further, in the present embodiment, axisymmetricly set relative to bearing 225 with a pair of holding sections 226.
Further, in the present embodiment, if regarding bearing 225 as two bottoms as drift angle, a pair of holding sections 226
Angle, using the line of bearing 225 respectively with a pair of holding sections 226 as waist, the line of a pair of holding sections 226 is then propped up as base
Seat 225 and a pair of holding sections 226 are in the isosceles triangle that drift angle is special angle.
Preferably, the special angle can be 90 degree.
Each holding section 226 is generally cylindrical, and provided with opening 2261, two openings 2261 of a pair of holding sections 226 are relative
Set.
Further, opening 2261 is C-shaped.
When lid 21 is fitted together with horn lower cover 22 on horn, power set 30 are installed on the first freedom of horn 20
End 213.
The upper end of revolving part 23 is fixedly connected with the groove 157 in installation portion 15, and its lower end is mutually blocked with a pair of holding sections 226
Close.
Bottom 24 has the first hole 241 and the second hole 242.Wherein, the first hole 241 is arranged at the center of bottom 24, and
The centre bore 156 of link slot 2121, installation portion 15 with lid on horn 21 and the through hole 2251 of horn lower cover 22 are corresponding.
Second hole 242 is disposed adjacent with the first hole 241, and relative to the first hole 241 closer to installation portion 15.Revolving part 23 passes through second
Hole 242, its upper end is engaged with the groove 157 of installation portion 15, and its lower end is sticked in any one holding section of horn lower cover 22
In 226.
When assembling horn 20 with installation portion 15, installation portion 15 is located on horn between lid 21 and horn lower cover 22, and is located at
The top of bottom 24.The opening 2261 of the lower end of revolving part 23 and one of holding section 226 fastens, and its upper end passes through second
Hole 242 is simultaneously caught in the groove 157 of installation portion 15.Screw 25 inserts horn lower cover from the through hole 2251 of the lower end of horn lower cover 22
22, and sequentially pass through the link slot of lid 21 on the first hole 241, the centre bore 156 of installation portion 15 and the horn of bottom 24
2121, so that lid on horn 21, horn lower cover 22, bottom 24 and installation portion 15 are fixed together.Now, revolving part 23 is in
First position.When rotating horn 20, rotation section 154 is driven to be rotated relative to the main body 151 of installation portion 15, revolving part 23 and card
The opening 2261 in conjunction portion 226 is separated, and with the rotation of horn 20, revolving part 23 snaps into opening for another holding section 226
In mouth 2261, now, revolving part 23 is rotated to the second place by first position.
Further, in the present embodiment, revolving part 23 for rotation fixed column, including columned body 231 and from
The upper surface of body 231 direction protrudes out the multiple auxiliary sections 232 to be formed perpendicular to the direction of body 231 at equal intervals.Body 231 is in post
Body, the opening 2261 of its lower surface and holding section 226 fastens.In the present embodiment, the quantity of auxiliary section 232 is four,
Four auxiliary sections 232 are in substantially " ten " font, for being caught in the groove 157 of installation portion 15.
Further, the diameter of section of body 231 is more than the opening diameter of opening 2261.
Further, opening 2261 is flexible, utilizes the elastic force of itself of opening 2261 so that revolving part 23 can
Opening 2261 is caught in, or, screwed out from opening 2261.
Power set 30 are connected to the free end of horn 20, provide dynamic for the flight for collapsible unmanned vehicle 100
Power.Power set 30 can be motor, for example, alternating current generator or direct current generator.Power set 30 in response to it is collapsible nobody
The command signal of the flight controller of aircraft 100, is rising for collapsible unmanned vehicle 100 to drive rotation oar 40 to rotate
Fly to provide climbing power.
Further, the cable of power set 30 is contained in lid 21 and horn lower cover 22 on horn and fastens the cable receipts formed
Hold in the (not shown) of space, and part stretches out in the cable receiving space.
Further, propeller (not shown) can be set in rotation oar 40, when power set 30 start, driving rotation
Oar 40 drives propeller rotation, is that collapsible unmanned vehicle 100 provides lifting power.
When operating collapsible unmanned vehicle 100, one of holding section 226 of revolving part 23 and horn lower cover 22 is mutually blocked
Close, and positioned at first position, the horn 20 of the collapsible unmanned vehicle 100 of correspondence is in first state (example relative to fuselage 10
Such as：Deployed condition or folded state).When rotation horn 20 so that horn 20 drives rotation section 154 relative to installation portion 15
Main body 151 is rotated, and revolving part 23 and the opening 2261 of one of holding section 226 are separated, and with the rotation of horn 20, rotation
Turn part 23 to snap into the opening 2261 of another holding section 226, revolving part 23 is rotated by first position to the second place, it is right
The horn 20 of collapsible unmanned vehicle 100 is answered to be in the second state (for example relative to fuselage 10：Folded state or expansion shape
State).
The collapsible unmanned vehicle 100 that the utility model is provided, by rotating horn 20 so that revolving part 23 and horn
One of holding section 226 of lower cover 22 is separated, and is fastened with another holding section 226, and realizing horn 20 can be relative
Deployed condition or folded state are in fuselage 10, is easy to collapsible unmanned vehicle 100 in off working state, non-flight shape
Volume shared by state is minimum, and convenient use person stores and carried.
Fig. 6 is refer to, the stereogram of the collapsible unmanned vehicle 200 provided for the utility model second embodiment.
In the present embodiment, the basic phase of structure of collapsible unmanned vehicle 200 and the collapsible unmanned vehicle 100 in first embodiment
Together.Collapsible unmanned vehicle 200 includes fuselage 10 ', multiple horns 20 ', power set 30 ' and rotation oar 40 '.It is multiple
Horn 20 ' is movably connected with the both sides of fuselage 10 ', when collapsible unmanned vehicle 200 is in state of flight, multiple horns
20 ' can deploy relative to fuselage.When collapsible unmanned flight 200 is in non-state of flight, multiple horns 20 ' can be relative
Rotated in fuselage 10 ', and it is in folded state (as shown in Figure 7), now, collapsible unmanned flight to draw in around fuselage 10 '
Space shared by device 200 is smaller, is easy to store and carries.
In the present embodiment, fuselage 10 ', power set 30 ' and the rotation oar 40 ' in collapsible unmanned vehicle 200
Structure and first embodiment in collapsible unmanned vehicle 100 corresponding to fuselage 10, power set 30 and rotation oar
40 structure is identical, and for identical content, the present embodiment will not be repeated here.Collapsible unmanned vehicle in the present embodiment
200 are with the difference of first embodiment：The structure of horn 20 ' is different.
Referring to Fig. 8-11, horn 20 ' includes lid 21 ', horn lower cover 22 ', revolving part 23 ', bottom on horn
24 ', screw 25 ' and damper assembly 26 '.Lid 21 ' is rotationally fastened on one with horn lower cover 22 ' by screw 25 ' on horn
Rise, and revolving part 23 ', bottom 24 ' and damper assembly 26 ' are contained on horn among lid 21 ' and horn lower cover 22 '.
Lid 21 ' includes upper lid body 211 ', the first connection end 212 ' positioned at upper one end of lid body 211 ', is located on horn
First free end 213 ' of the upper other end of lid body 211 ' and the connecting hole 214 ' for being formed at first connection end 212 '.
Wherein, surface projection multiple projections 215 ' (as shown in Figure 10) of the upper lid body 211 ' towards the side of horn lower cover 22 '.First connects
End 212 ' is connect close to installation portion 15 ', accordingly, the first free end 213 ' is away from installation portion 15 '.
Horn lower cover 22 ' include lower cover body 221 ', the second connecting portion 222 ' positioned at the one end of lower cover body 221 and
Positioned at the second free end 223 ' of the other end of lower cover body 221 '.Wherein, the second connection end 222 ' and the phase of the first connection end 212 '
Match and close to installation portion 15 ', accordingly, the second free end 223 ' and the first connection end 213 ' match and away from installation portion
15’。
Specifically, lower cover body 221 ' is provided with multiple locating dowels 224 ', Mei Geding towards the surface of the side of lid 21 ' on horn
Position post 224 ' offers positioning hole 2241 '.When lid 21 ' and horn lower cover 22 ' are interlocked on horn, upper lid body 211 ' it is many
Individual projection 215 ' is inserted in corresponding positioning hole 2241 ' respectively.
The surface of second connection end 222 ' towards the side of the first connection end 212 ' is provided with bearing 225 ', a pair of holding sections
226 ' and connect a pair of holding sections 226 ' projection 227 '.The position of bearing 225 ' and the centre bore 156 ' of installation portion 15 '
Position is corresponding, and the center of bearing opens up through hole 2251 '.A pair of holding sections 226 ' are located at the both sides of bearing 225 ' '.
Further, in the present embodiment, axisymmetricly set relative to bearing 225 ' with a pair of holding sections 226 '.
Further, in the present embodiment, if regarding bearing 225 ' as two bottoms as drift angle, a pair of holding sections 226 '
Angle, using bearing 225 ' respectively with the lines of a pair of holding sections 226 ' as waist, the lines of a pair of holding sections 226 ' is as base, then
Bearing 225 ' and a pair of holding sections 226 ' are in the isosceles triangle that drift angle is in special angle.
Preferably, the number range of the special angle is 80 degree to 120 degree.
Each holding section 226 ' is generally cylindrical, provided with opening 2261 ', two openings 2261 " of a pair of holding sections 226 '
It is oppositely arranged.
The two ends of projection 227 ' are connected with two openings 2261 ' of a pair of holding sections 226 ' respectively.The top surface of projection 227 '
With the top surface flush of holding section 226 '.Preferably, projection 227 ' is excessive band.
Revolving part 23 ' includes the decorative pearl on top of an official cap 27 ', flexible member 28 ' and rotating shaft 29 '.
Figure 12 is refer to, the decorative pearl on top of an official cap 27 ' includes decorative pearl on top of an official cap body 271 ', the top surface from decorative pearl on top of an official cap body 271 ' and protrudes out what is formed upwards
Auxiliary section 272 ' and protrude out the oblate spheroid portion 273 ' to be formed downwards from the bottom surface of decorative pearl on top of an official cap body 272 '.Decorative pearl on top of an official cap body 271 ' is substantially
Be square tabular.The diameter of section of auxiliary section 272 ' is less than the width of decorative pearl on top of an official cap body 271 ', its substantially " ten " font, for being caught in
In the groove 157 ' (as shown in figure 11) of installation portion 15 '.The diameter in oblate spheroid portion 273 ' is used again smaller than the width of decorative pearl on top of an official cap body 271 '
Fastened in any one holding section 226 '.
The auxiliary section 272 ' of the decorative pearl on top of an official cap 27 ' is inserted in one end of flexible member 28 ', and the other end is supported surrounds recessed in installation portion 15 '
The roof of groove 157 '.In the present embodiment, flexible member 28 ' is spiral spring.
Rotating shaft 29 ' and the connecting hole 214 ' of lid 21 ' on horn fasten, and expose to lid on horn through connecting hole 214 '
21 ' (as shown in fig. 6-7).There is axis hole 291 ' below rotating shaft 29 '.
Bottom 24 ' has the first hole 241 ' and the second hole 242 '.Wherein, the first hole 241 ' is arranged at the center of bottom 24 '
Place, and it is corresponding with the connecting hole 214 ' of lid 21 ' on horn.Second hole 242 ' is connected with the first hole 241 '.The decorative pearl on top of an official cap 27 ' and set
The second hole 242 ' is passed through in the flexible member 28 ' on the decorative pearl on top of an official cap 27 ', and is clamped in the groove 157 ' and horn lower cover of installation portion 15 '
In 22 ' any one holding section 226 '.
Damper assembly 26 ' includes damped ring 261 ' and multiple damping gaskets 262 '.Damped ring 261 ' and damping gasket 262 '
It is stacked above the rotation section 154 ' of installation portion 15 ', plays a part of the resistance of increase rotation horn 20 '.
When assembling horn 20 ' with installation portion 15 ', installation portion 15 ' is located on horn between lid 21 ' and horn lower cover 22 ', and
Positioned at the top of bottom 24 ', bottom 24 ' is placed in the second connection end 222 ' of horn lower cover 22 '.Flexible member 28 ' is arranged
In the auxiliary section 272 ' of the decorative pearl on top of an official cap 27 ', and auxiliary section 272 ' and the groove 157 ' that flexible member 28 ' is contained in installation portion 15 ' are interior.Top
The oblate spheroid portion 273 ' of pearl 27 ' is sticked in one of holding section 226 '.Damping gasket 262 ', and screw are arranged on screw 25 '
25 ' from the through hole 2251 ' of the lower end of horn lower cover 22 ' insertion horn lower cover 22 ', and sequentially pass through bottom 24 ' the first hole 241 ',
The centre bore 156 ' of installation portion 15 ', damping gasket 262 ', damped ring 261 ', on horn lid 21 ' connecting hole 214 ', Yi Jizhuan
In the axis hole 291 ' of axle 29 ', so that lid 21 ', horn lower cover 22 ', bottom 24 ' on horn are fixed together with installation portion 15 '.
Now, the decorative pearl on top of an official cap 27 ' is in first position.When rotating horn 20 ', rotation section 154 ' is driven relative to the main body of installation portion 15 '
151 ' rotations, the decorative pearl on top of an official cap 27 ' and the opening 2261 ' of holding section 226 ' are separated, and flexible member 28 ' is compressed, and with horn 20
Rotation, gradually contacted with projection 227 ', and under the resilient force of flexible member 28 ', snapped into by projection 227 ' another
In the opening 2261 ' of individual holding section 226 ', now, the decorative pearl on top of an official cap 27 ' is rotated to the second place by first position.
When operating collapsible unmanned vehicle 200, one of phase of holding section 226 ' of the decorative pearl on top of an official cap 27 ' and horn lower cover 22 '
Engaging, and positioned at first position, the horn 20 ' of the collapsible unmanned vehicle 200 of correspondence is in first state relative to fuselage 10 '
(for example：Deployed condition or folded state).When rotation horn 20 ' so that horn 20 ' drives rotation section 154 ' relative to installation
The main body 151 ' in portion 15 ' is rotated, and the opening 2261 ' in the oblate spheroid portion 273 ' and one of holding section 226 ' of the decorative pearl on top of an official cap 27 ' is separated,
And with the rotation of horn 20 ', gradually contacted with projection 227 ', the oblate spheroid portion 273 ' of the decorative pearl on top of an official cap 27 ' snaps into another holding section
In 226 ' opening 2261 ', the decorative pearl on top of an official cap 27 ' is set to be rotated by first position to the second place, the collapsible unmanned vehicle 200 of correspondence
Horn 20 ' is in the second state (for example relative to fuselage 10 '：Folded state or deployed condition).
The collapsible unmanned vehicle 200 that the utility model is provided, by rotating horn 20 ' so that the decorative pearl on top of an official cap 27 ' and horn
One of holding section 226 ' of lower cover 22 ' is separated, and is fastened with another holding section 226 ', and realizing horn 20 ' can
Deployed condition or folded state are in relative to fuselage 10 ', is easy to collapsible unmanned vehicle 200 in off working state, non-
Volume shared by state of flight is minimum, and convenient use person stores and carried.
Preferred embodiment of the present utility model is these are only, the scope of the claims of the present utility model is not thereby limited, it is every
The equivalent structure or equivalent flow conversion made using the utility model specification and accompanying drawing content, or be directly or indirectly used in
Other related technical fields, are similarly included in scope of patent protection of the present utility model.
Claims (20)
1. a kind of horn of collapsible unmanned vehicle, is rotationally connected with the installation portion of collapsible unmanned vehicle, its feature
It is, the horn includes：
Covered on horn；
The buckling parts of merga pass one that interlocks is covered on horn lower cover, with the horn and is rotationally connected with the installation portion；
A pair of holding sections, are arranged at the buckling parts；
Revolving part, its upper end is fixedly connected with the groove of the installation portion, its lower end optionally with the pair of holding section
Any one fasten or be separated；
The horn has first position and the second place relative to the installation portion, when the horn is in first position,
The horn is in folded state, and when the horn is in the second place, the horn is in deployed condition, the revolving part
Optionally it is separated with one of holding section, and with the rotation of the horn, the revolving part snaps into another card
Conjunction portion, makes the horn switch relative to the installation portion between the first position and the second place.
2. horn according to claim 1, it is characterised in that also including bottom, the bottom have the first hole and with institute
State the lower end covered on the second hole that the first hole is disposed adjacent, the horn and be provided with link slot, the horn lower cover is towards the machine
The side covered on arm is provided with bearing, by screw sequentially pass through the bearing, first hole and the installation portion be caught in it is described
Link slot, snaps together lid and the horn lower cover on the horn.
3. horn according to claim 2, it is characterised in that the revolving part includes body, the upper end from the body
Protrude out the multiple auxiliary sections to be formed at equal intervals facing to the direction perpendicular to body, the multiple auxiliary section is caught in the installation portion
The groove in, the lower surface of the body fastens through second hole and with any one holding section.
4. horn according to claim 2, it is characterised in that the pair of holding section is located at the both sides of the bearing.
5. horn according to claim 4, it is characterised in that the bearing and the pair of holding section are specific in drift angle
The isosceles triangle of angle.
6. horn according to claim 5, it is characterised in that the pair of holding section is respectively equipped with a pair of openings, described
Revolving part is optionally separated or fastened with one of opening, and fastens or be separated with another opening,
The horn is set to switch between the first position and the second place.
7. horn according to claim 6, it is characterised in that the section that the diameter of the opening is less than the revolving part is straight
Footpath.
8. horn according to claim 7, it is characterised in that the opening is C-shaped.
9. horn according to claim 1, it is characterised in that the revolving part includes the decorative pearl on top of an official cap, is sheathed on the decorative pearl on top of an official cap
Flexible member and rotating shaft.
10. horn according to claim 9, it is characterised in that also including bottom, the bottom have the first hole and with institute
Stating lid on the second hole that the first hole is connected, the horn has connecting hole, and the rotating shaft is corresponding with the connecting hole, described
Horn lower cover is provided with bearing towards the side covered on the horn, and the bearing, first hole, institute are sequentially passed through by screw
Installation portion, the connecting hole and the rotating shaft are stated, lid and the horn lower cover on the horn is rotationally fastened on one
Rise.
11. horn according to claim 10, it is characterised in that the decorative pearl on top of an official cap includes decorative pearl on top of an official cap body, from the decorative pearl on top of an official cap sheet
The top surface of body protrudes out the multiple auxiliary sections to be formed and protrudes out the oblate spheroid portion to be formed, institute downwards from the bottom surface of the decorative pearl on top of an official cap body
State flexible member and be sheathed on the multiple auxiliary section, and be caught in the groove of the installation portion, horn lower cover also includes and institute
The projection that a pair of holding sections are connected is stated, when the horn is rotated, the oblate spheroid portion fastens with any one described holding section
Or be separated.
12. horn according to claim 11, it is characterised in that the multiple auxiliary section is in cross.
13. horn according to claim 12, it is characterised in that the quantity of the auxiliary section is 4.
14. horn according to claim 9, it is characterised in that the revolving part also includes damper assembly, the damping group
Part includes damped ring and multiple damping gaskets, and the damped ring and damping gasket are stacked in lid on the horn and the peace
Between dress portion, on the horn is assembled when lid and the horn lower cover, screw passes through the damper assembly.
15. a kind of collapsible unmanned vehicle, it is characterised in that including fuselage, be arranged at the multiple of described two sides of fuselage
Installation portion and the horn for being rotationally connected with the installation portion, the horn are the machine described in claim any one of 1-14
Arm.
16. collapsible unmanned vehicle according to claim 15, it is characterised in that also including power set and positioned at institute
The rotation oar on power set is stated, the power set are fixed on the one end of the horn away from the installation portion, the power
Device drives the rotation oar rotation.
17. collapsible unmanned vehicle according to claim 16, it is characterised in that the installation portion include main body, from
The main body extends the connecting portion to be formed and the gap being formed between the main body and the connecting portion, the connecting portion
Including rotation section, the connecting portion is provided with hole, and the rotation section is rotated in the hole and relative to the connecting portion, described
Rotation section has centre bore, and the groove is formed at the lower end of the rotation section.
18. collapsible unmanned vehicle according to claim 17, it is characterised in that the cable of the power set is housed
Fastened in lid and horn lower cover on the horn in the cable receiving space to be formed, and the cable receiving space is stretched out in part.
19. collapsible unmanned vehicle according to claim 18, it is characterised in that between the rotation section and the hole
The gap being connected with wire hole and with the wire hole, the cable of the power set stretches into described from the wire hole
Installation portion, then stretched out from the gap, and master board is connected to, so the power set and the master board are electrical
Link together.
20. collapsible unmanned vehicle according to claim 17, it is characterised in that the connecting portion also includes protruding out setting
The limiting section put, the limiting section carries out two when switching for the horn between the first position and the second place
It is secondary spacing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621276591.6U CN206427260U (en) | 2016-11-25 | 2016-11-25 | Collapsible unmanned vehicle and its horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621276591.6U CN206427260U (en) | 2016-11-25 | 2016-11-25 | Collapsible unmanned vehicle and its horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206427260U true CN206427260U (en) | 2017-08-22 |
Family
ID=59589486
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621276591.6U Active CN206427260U (en) | 2016-11-25 | 2016-11-25 | Collapsible unmanned vehicle and its horn |
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| Country | Link |
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| CN (1) | CN206427260U (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353487A (en) * | 2018-10-17 | 2019-02-19 | 蔡强 | A kind of unmanned plane of wing rotary folding |
| WO2019041502A1 (en) * | 2017-08-30 | 2019-03-07 | 深圳市大疆创新科技有限公司 | Vehicle arm assembly of unmanned aerial vehicle and unmanned aerial vehicle |
| CN109552602A (en) * | 2018-12-24 | 2019-04-02 | 深圳市道通智能航空技术有限公司 | A kind of unmanned vehicle |
| CN112638765A (en) * | 2019-12-31 | 2021-04-09 | 深圳市大疆创新科技有限公司 | Foldable equipment, unmanned vehicles and handheld cloud platform |
| CN113911355A (en) * | 2021-07-10 | 2022-01-11 | 山东交通学院 | Portable unmanned aerial vehicle and using method thereof |
| CN114347738A (en) * | 2022-01-12 | 2022-04-15 | 广东汇天航空航天科技有限公司 | Arm mechanism and flight device |
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2016
- 2016-11-25 CN CN201621276591.6U patent/CN206427260U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019041502A1 (en) * | 2017-08-30 | 2019-03-07 | 深圳市大疆创新科技有限公司 | Vehicle arm assembly of unmanned aerial vehicle and unmanned aerial vehicle |
| CN109353487A (en) * | 2018-10-17 | 2019-02-19 | 蔡强 | A kind of unmanned plane of wing rotary folding |
| CN109353487B (en) * | 2018-10-17 | 2023-08-29 | 蔡强 | Unmanned aerial vehicle with rotary and folding wings |
| CN109552602A (en) * | 2018-12-24 | 2019-04-02 | 深圳市道通智能航空技术有限公司 | A kind of unmanned vehicle |
| CN112638765A (en) * | 2019-12-31 | 2021-04-09 | 深圳市大疆创新科技有限公司 | Foldable equipment, unmanned vehicles and handheld cloud platform |
| CN113911355A (en) * | 2021-07-10 | 2022-01-11 | 山东交通学院 | Portable unmanned aerial vehicle and using method thereof |
| CN114347738A (en) * | 2022-01-12 | 2022-04-15 | 广东汇天航空航天科技有限公司 | Arm mechanism and flight device |
| CN114347738B (en) * | 2022-01-12 | 2023-06-02 | 广东汇天航空航天科技有限公司 | Arm mechanism and flight device |
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