CN205837169U - Foldable assembly and unmanned plane - Google Patents
Foldable assembly and unmanned plane Download PDFInfo
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- CN205837169U CN205837169U CN201620585588.6U CN201620585588U CN205837169U CN 205837169 U CN205837169 U CN 205837169U CN 201620585588 U CN201620585588 U CN 201620585588U CN 205837169 U CN205837169 U CN 205837169U
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- support seat
- folded piece
- stopper slot
- foldable assembly
- active joint
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Abstract
During for overcoming prior art unmanned plane in the deployed state with lockable mechanism locking, operation is laborious, and the problem that the process of whole assembling locking is cumbersome, this utility model provides a kind of foldable assembly and unmanned plane.A kind of foldable assembly, including supporting seat, folded piece and lockable mechanism；Described support seat is provided with articulated jib；Described folded piece is provided with an active joint；Described folded piece is rotatably connected on described articulated jib by described active joint；In supporting seat, an anti-rotation shell fragment is installed；Anti-rotation shell fragment is provided with an elastic spacing structure；Active joint is provided with the first stopper slot and the second stopper slot, and the elastic spacing structure on anti-rotation shell fragment can coordinate with the first stopper slot or the second stopper slot；Described folded piece locking is fixed on described support seat by described lockable mechanism in the deployed state.The foldable assembly that this utility model provides, its lockable mechanism locking and release the process leicht fallen D/A of locking and smooth and easy.This kind of foldable assembly be easily fabricated and assembling, and cost is lower.
Description
Technical field
This utility model relates to unmanned plane field, especially the horn of unmanned plane or foot rest field.
Background technology
Unmanned plane (or claiming aircraft) is the most increasingly recognized by people, and it can be as simple remote-control toy, it is possible to make
The photographic equipment taken a crane shot for specialty high-altitude.Its structure generally comprises fuselage and (includes skeleton and cover outside skeleton outer device decoration
Shell), horn and undercarriage (or claiming foot rest) etc..
Existing horn or foot rest major part are fixed on fuselage, cause its volume relatively big, not readily portable and transport.As
Improving, existing part horn or foot rest use folding mode to be arranged on fuselage, and as a example by horn, it is installed on horn
Support seat, horn is articulated with rotationally on described support seat；And by lockable mechanism locking.So, nothing is used when needs
Time man-machine, lockable mechanism can make horn be in deployed condition；When not using unmanned plane, by releasing the locking of lockable mechanism,
Make horn fold to pack up, in order to carry and transport.
But, applicant finds in R&D process, after horn or foot rest are hinged to support seat, when it is launching shape
When state is with lockable mechanism locking, it is the most convenient to operate, and needs the docking keeping horn or foot rest on the other hand relative to supporting seat, another
Hands implements the locking action of lockable mechanism；Now find horn or foot rest always can automatically under fall, need staff applying more stable
The power of pop-up, locking just can be made to smoothly complete, this process seems laborious and has some setbacks, and the process of whole assembling locking is number
Tired.
Utility model content
During for overcoming in prior art unmanned plane in the deployed state with lockable mechanism locking, operation is laborious, whole assembling
The problem that the process of locking is cumbersome, this utility model provides a kind of foldable assembly and unmanned plane.
On the one hand this utility model provides a kind of foldable assembly, including supporting seat, folded piece and lockable mechanism；Wherein,
Described support seat is provided with articulated jib；Described folded piece is provided with an active joint；Described folded piece passes through described active joint
It is rotatably connected on described articulated jib；
One anti-rotation shell fragment is installed in described support seat；Described anti-rotation shell fragment is provided with an elastic spacing structure；
Described active joint is provided with the first stopper slot and the second stopper slot, the elastic spacing structure on described anti-rotation shell fragment
Can coordinate with described first stopper slot or the second stopper slot, with by spacing for described folded piece in deployed condition or folded state；
Described lockable mechanism is for being locked at described folded piece on described support seat or by described folded piece from described
Support and release locking on seat.
The foldable assembly that this utility model provides, it passes through anti-rotation shell fragment and the first stopper slot being arranged on active joint
Match with the second stopper slot, when it needs to launch to use, can quickly make folded piece launch, and make its folded piece keep
Stable, will not swing, then by lockable mechanism locking.When it is not in use, locking is released by lockable mechanism, the most quickly
By folded piece fold, to facilitate user to carry and to transport.Owing to having this anti-rotation shell fragment and the first stopper slot and the second stopper slot
Design, its lockable mechanism locking and release the process leicht fallen D/A of locking and smooth and easy.This kind of foldable assembly be easily fabricated and assembling,
Cost is lower.
Further, described support seat is provided with two articulated jibs, and each described articulated jib is correspondingly provided with hinge hole；Described
Folded piece is provided with an active joint, and described active joint is provided with axis hole；
Described active joint is arranged between two described articulated jibs；One rotating shaft through the hinge hole on described articulated jib and
Axis hole on described active joint, is hinged on described folded piece on described support seat.
Further, described lockable mechanism is a pair female connector pipe；The lateral surface of described support seat is provided with external screw thread；Described right
Female connector pipe box is located on the lateral surface of described folded piece, is provided with female thread in described docking sleeve pipe, interior on described docking sleeve pipe
Screw thread can match with the external screw thread on described support seat lateral surface, so that described folded piece locking is fixed on described support seat
On.Use docking sleeve pipe as lockable mechanism, its simple in construction, it is easy to manufacture and assemble.
Further, the end face of described support seat is provided with a ring-type docking boss；Set on described ring-type docking boss
Put said two articulated jib；
The end face of described folded piece is provided with the docking platform matched with described docking boss, and described active joint is arranged
On described docking platform.
Further, described anti-rotation shell fragment includes elastic movable part and a mounting part；
Described mounting part is provided with some screw holes, and described mounting part is pacified through described screw hole by screw
Install in described support seat；
Described elastic spacing structure is arranged on described elastic movable part.
Further, described anti-rotation shell fragment is one-body molded, and mounting part thereon is first quarter moon annular；Described elastic movable
Portion draws from described mounting part, and bends certain angle.
Further, described elastic spacing structure is V-shaped or U-shaped；Described first stopper slot and the second stopper slot is V-shaped or
U-shaped.
Further, described active joint is provided with and the confined planes of described elastic spacing respective outer side edges；
Described first stopper slot and the second stopper slot are located on described confined planes；Described first stopper slot is used for and described bullet
Property position limiting structure coordinate, by spacing for described folded piece in deployed condition；Described second stopper slot is for tying with described elastic spacing
Structure coordinates, by spacing for described folded piece at folded state.
Further, described support seat is provided with a flange, and described flange is provided with rack mounting apertures；Described support seat can
It is arranged on the fuselage of unmanned plane after described rack mounting apertures by screw.
Further, one end of described rotating shaft is provided with cap-like structure, and the other end is provided with jump-ring slot；Install in described jump-ring slot
There is jump ring；Described cap-like structure and jump ring are by the axis hole on spacing for the rotating shaft hinge hole at described articulated jib and described active joint
In.
Further, described support seat end face and described folded piece end face are correspondingly provided with aligning structure.
Further, the docking boss on described support seat is provided with a para-position muscle, the docking platform on described folded piece
Upper concave becomes to have alignment grooves；Described para-position muscle and described alignment grooves match.
This utility model second aspect provides a kind of unmanned plane, wherein, including fuselage and foldable assembly；Described folding group
Support seat on part is fixedly mounted on described fuselage.
The unmanned plane that this utility model provides, owing to it is equipped with the foldable assembly after improving, by anti-rotation shell fragment and setting
The first stopper slot and the second stopper slot on active joint match, and when it needs to launch to use, can quickly make folding
Overlapping piece launches, and makes its folded piece keep stable, will not swing, then by lockable mechanism locking.When it is not in use, pass through
Lockable mechanism releases locking, is very quickly folded by folded piece, to facilitate user to carry and to transport.Owing to there being this anti-rotation shell fragment
And first stopper slot and the design of the second stopper slot, its lockable mechanism locking and release the process leicht fallen D/A of locking and smooth and easy.Should
Kind foldable assembly is easily fabricated and assembles, and cost is lower.
Accompanying drawing explanation
Fig. 1 is the schematic diagram under the unmanned plane horn deployed condition provided in this utility model detailed description of the invention；
Fig. 2 is the schematic diagram under the unmanned plane horn folded state provided in this utility model detailed description of the invention；
Fig. 3 is the foldable assembly exploded perspective view provided in this utility model detailed description of the invention；
Fig. 4 is enlarged diagram at A in Fig. 3；
Fig. 5 is that the anti-rotation shell fragment provided in this utility model detailed description of the invention amplifies schematic perspective view；
Fig. 6 is the foldable assembly provided in this utility model detailed description of the invention schematic perspective view in a folded configuration；
Fig. 7 is the foldable assembly provided in this utility model detailed description of the invention part section signal in the deployed state
Figure；
Fig. 8 is enlarged diagram at B in Fig. 7；
Fig. 9 is the foldable assembly provided in this utility model detailed description of the invention part section signal in a folded configuration
Figure.
Wherein, 1, fuselage；2, foldable assembly；20, rotating shaft；21, seat is supported；22, docking sleeve pipe；23, horn；24, motor；
25, propeller；26, anti-rotation shell fragment；201, jump ring；210, docking boss；211, external screw thread；212, flange；2121, support is installed
Hole；213, articulated jib；214, step surface；221, female thread；222, ring is limited out；230, docking platform；231, active joint；
2130, hinge hole；2310, axis hole；231a, side；231b, confined planes；2311, the first stopper slot；2312, the second stopper slot；
2101, para-position muscle；2301, alignment grooves；26a, screw；261, elastic movable part；262, mounting part；2611, elastic spacing
Structure；2621, screw hole.
Detailed description of the invention
In order to make this utility model be solved the technical problem that, technical scheme and beneficial effect clearer, below
In conjunction with drawings and Examples, this utility model is further elaborated.Should be appreciated that described herein being embodied as
Example, only in order to explain this utility model, is not used to limit this utility model.
Embodiment
Unmanned plane to this utility model offer, and the foldable assembly 2 on unmanned plane below carries out specific explanations explanation.
As shown in Figure 1 and Figure 2, the unmanned plane that this utility model provides includes fuselage 1 and foldable assembly 2；This foldable assembly 2
Including including supporting seat 21 (or claiming support), folded piece and lockable mechanism, described folded piece includes horn 23 and/or foot rest；This
By folded piece for carrying out specific explanations explanation as a example by horn 23 in example, follow-up horn 23 the most replaceable one-tenth foot rest.Described horn 23
On the motor 24 with propeller 25 is installed.Wherein, this support seat 21 is fixedly mounted on described fuselage 1.Meanwhile, this horn
23 are hinged on support seat 21 so that it is horn 23 can be to rotate on relative support seat 21, and in this example, this lockable mechanism is the most right
Female connector pipe 22, is tightened in horn 23 on support seat 21 by docking sleeve pipe 22.So, when unmanned plane uses, this horn 23
Can be as shown in fig. 1 in deployed condition.When unmanned plane does not uses, horn 23 can as shown in Figure 2 in folded state (or
Rounding state).Certainly, the horn 23 in this example can also replace with the foot rest in unmanned plane.Certainly, foot rest is no need for pacifying again
Fill the motor 24 with propeller 25.
Combine Fig. 3-Fig. 9 below and foldable assembly 2 is carried out further specific explanations explanation.
Wherein, as shown in figures 3 to 6, described support seat 21 is provided with articulated jib 213；It is movable that described folded piece is provided with one
Joint 231；Described folded piece is rotatably connected on described articulated jib 213 by described active joint 231.Concrete, described
Support seat 21 is provided with two articulated jibs 213, and each described articulated jib 213 is correspondingly provided with hinge hole 2130；Set on described horn 23
An active joint 231, described active joint 231 is had to be provided with axis hole 2310；
Described active joint 231 is arranged between two described articulated jibs 213；One rotating shaft 20 is through described articulated jib 213
On hinge hole 2130 and axis hole 2310 on described active joint 231, described horn 23 is hinged on described support seat 21；
As shown in figures 3 to 6, an anti-rotation shell fragment 26 is installed in described support seat 21；Described anti-rotation shell fragment 26 is provided with
One elastic spacing structure 2611；
Described active joint 231 is provided with the first stopper slot 2311 and the second stopper slot 2312, on described anti-rotation shell fragment 26
Elastic spacing structure 2611 can coordinate with described first stopper slot 2311 and the second stopper slot 2312, so that described horn 23 is limited
Position is at deployed condition or folded state；
Described lockable mechanism is for being locked at described folded piece on described support seat 21 or by described folded piece from institute
State and release locking on support seat 21.
Under the effect of this anti-rotation shell fragment 26 so that it is horn 23 is spacing under deployed condition or folded state two states,
As long as ensureing that this anti-rotation shell fragment 26 possesses enough elastic force, it is possible to ensure that active joint 231 keeps relative steady with supporting seat 21
Fixed, will not rock.If but apply bigger external force, overcome the elastic force of anti-rotation shell fragment 26, so that it may make anti-rotation shell fragment 26 deform, with
Make its elastic spacing structure 2611 disengage the first stopper slot 2311 and position of the second stopper slot 2312, make the horn 23 can be relative to
Support the smooth and easy rotation of seat 21.So, owing to there being setting of this anti-rotation shell fragment 26 and the first stopper slot 2311 and the second stopper slot 2312
Meter so that it is lockable mechanism locking and release the process of locking and become leicht fallen D/A and smooth and easy.
Wherein, when elastic spacing structure 2611 snaps in described first stopper slot 2311, horn 23 will be made and support seat
21 docking, make the horizontal development state that horn 23 and support seat 21 are in 180 °；When elastic spacing structure snaps in described second limit
Time in the groove 2312 of position, the folded state that horn 23 and support seat 21 will be made to be in 90 °, the horn 23 simultaneously folded can keep
Stable, during user moves or carries unmanned plane, unsettled horn 23 will not rock, and facilitates user to carry and transports.Only
Have when external force is sufficiently large, just can overcome above-mentioned state, make elastic spacing structure 2611 from the first stopper slot 2311 and the second limit
Position groove 2312 is deviate from.
In a word, the above-mentioned foldable assembly that this example provides, it is by anti-rotation shell fragment 26 and the be arranged on active joint 231
One stopper slot 2311 and the second stopper slot 2312 match, and use lockable mechanism mechanism locking, when it needs to launch to use,
Folded piece can be quickly made to launch, and spacing by this anti-rotation shell fragment 26 so that it is and folded piece keeps stable, will not swing, so
Afterwards by lockable mechanism locking.When it is not in use, very quickly can release locking by just locking structure, folded piece is rolled over
Folded, to facilitate user to carry and to transport.Owing to having this anti-rotation shell fragment 26 and the first stopper slot 2311 and the second stopper slot 2312
Design, its lockable mechanism locking and release the process leicht fallen D/A of locking and smooth and easy.
Concrete, as shown in figures 3 to 6, described lockable mechanism is that docking sleeve pipe 22, described horn 23 and support seat 21 cut with scissors
Connect the lateral surface at place all in the face of cylinder；The lateral surface of described support seat 21 is provided with external screw thread 211；Described docking sleeve pipe 22 is set in
On the lateral surface of described horn 23, in described docking sleeve pipe 22, it is provided with female thread 221, the female thread on described docking sleeve pipe 22
221 can match with the external screw thread 211 on described support seat 21 lateral surface, so that described horn 23 locking is fixed on described support
Locking is released on seat 21 or from described support seat 21.Use docking sleeve pipe 22 as lockable mechanism, its simple in construction, it is easy to
Manufacture and assembling.
Wherein, as it is shown on figure 3, one end of described rotating shaft 20 is provided with cap-like structure (unmarked in figure), the other end is provided with card
Spring groove (unmarked in figure)；Jump ring 201 is installed in described jump-ring slot；Described cap-like structure and jump ring 201 are by spacing for rotating shaft 20
In the axis hole 2310 on the hinge hole 2130 and described active joint 231 of described articulated jib 213.
Concrete, this horn 23 docks mutually with the end face supporting seat 21 hinged place, as preferred mode, and this horn 23 He
Support seat 21 is entirety, and in hollow tubular, (so-called entirety is that the position of hollow tubular the most all supports seat 21 is
Hollow tubular, such as subsequent descriptions for install support seat 21 flange 212 be non-hollow tubulose) structure, for making hollow
The horn 23 of tubulose docks mutually with supporting seat 21, as preferred mode, is provided with one ring-type on the end face of described support seat 21
Docking boss 210；On described ring-type docking boss 210, said two articulated jib 213 is set；Set on the end face of described horn 23
The docking platform 230 matched with described docking boss 210, described active joint 231 is had to be arranged on described docking platform 230
On.Such that horn 23 can be hinged on support seat 21 end face by rotating shaft 20 by the active joint 231 on its end face
Between articulated jib 213；Meanwhile, docking boss 210 and docking platform 230 match, to play right to horn 23 and support seat 21
The purpose connect.Wherein, the material of horn 23 and support seat 21 is not particularly limited, and can use known to one of skill in the art
Material make.
The external diameter of above-mentioned docking boss 210 is less than the external diameter of support seat 21 remainder, and its internal diameter is less than remainder
Internal diameter；Therefore, the support seat 21 of hollow tubular is internal can form step surface 214.
Concrete, as it is shown in figure 5, described anti-rotation shell fragment 26 includes elastic movable part 261 and a mounting part 262；Its
In, described anti-rotation shell fragment 26 is one-body molded, and this mounting part 262 is annular in first quarter moon；This elasticity movable part 261 is fixing from installing
Drawing in portion 262, and bend certain angle, its bending angle sets as required, is 90 degree in this example.
Described mounting part 262 is provided with some screw holes 2621, and described mounting part 262 is worn by screw 26a
Cross described screw hole 2621 to be installed in described support seat 21；Concrete, this mounting part 262 is installed on described support seat 21
On internal step surface 214.
Described elastic spacing structure 2611 is arranged on described elastic movable part 261.
Wherein, described elastic spacing structure 2611 is excellent with the shape of described first stopper slot 2311 and the second stopper slot 2312
Choosing is suitable, so can ensure that elastic spacing structure 2611 and this first stopper slot 2311 and the second stopper slot 2312 phase
Adaptation, the most all can V-shaped or U-shaped.
As shown in Figure 4, described active joint 231 is provided with the confined planes coordinated with described elastic spacing structure 2611
231b；Concrete, described active joint 231 also include two sides 231a, confined planes 231b be arranged on described two sides 231a it
Between, in two sides, 231a is mutually perpendicular to；Described axis hole 2310 is arranged between described two sides 231a；
Described first stopper slot 2311 and the second stopper slot 2312 are located on described confined planes 231b；Described first stopper slot
2311 and second stopper slot 2312 be located on described confined planes 231b；Described first stopper slot 2311 is used for and described elastic spacing
Structure 2611 coordinates, by spacing for described folded piece in deployed condition；Described second stopper slot 2312 is used for and described elastic spacing
Structure 2611 coordinates, by spacing for described folded piece at folded state.
In this example, owing to horn 23 and support seat 21 are coupled together by needs by docking sleeve pipe 22, therefore, at least need
Ensure that the lateral surface on the horn 23 installing docking sleeve pipe 22 position and support seat 21 is the face of cylinder, so can will dock
Sleeve pipe 22 is set on horn 23 lateral surface, and meanwhile, its docking sleeve pipe 22 is also by the outstanding mode twisted, in horn 23 and support
Seat 21 complete to dock spacing after, the external screw thread 211 of the female thread 221 on docking sleeve pipe 22 with support seat 21 lateral surface is coordinated stubborn
Tightly, fix with the locking by horn 23 and support seat 21, otherwise, when docking sleeve pipe 22 is turned on from described support seat 21,
Horn 21 and the locking supporting seat can be released.
Wherein, the lateral surface of this horn 23 can arrange external screw thread 211, it is also possible to be not provided with external screw thread 211.Such as
In this example, not arranging external screw thread 211 on the lateral surface of horn 23, its lateral surface is the smooth face of cylinder.Therefore, this docking
Sleeve pipe 22 can slide on the lateral surface of horn 23.For preventing docking sleeve pipe 22 from deviating from from described horn 23, can be in docking
Arrange on sleeve pipe 22 and limit out ring 222；This diameter limiting out ring 222 is less than docking platform 230 diameter on horn 23 end face, therefore
It is possible to prevent this docking sleeve pipe 22 to deviate from from horn 23 end.
Certainly, this support seat 21 and horn 23 can also be solid construction；It is preferable to employ hollow tubular structure, except saving
Outside material, also can be from its internal cabling.
About the concrete mounting means of this support seat 21, it is not particularly limited, as long as it can be fixedly installed on fuselage 1 i.e.
Can.Such as, in this example, described support seat 21 is provided with a flange 212, and described flange 212 is provided with rack mounting apertures 2121；Institute
State support seat 21 to be arranged on the fuselage 1 of unmanned plane after described rack mounting apertures 2121 by screw.
It is correspondingly provided with aligning structure on described support seat 21 end face and described horn 23 end face.By this aligning structure, can
With when support seat 21 and horn 23 being docked, play the effect of location docking.Such as, such as Fig. 3, Fig. 4, Fig. 6, described
Docking boss 210 on support seat 21 is provided with a para-position muscle 2101, and on the docking platform 230 on described horn 23, concave becomes to have
Alignment grooves 2301；Described para-position muscle 2101 and described alignment grooves 2301 match.
Below the deployment lifting process of the horn 23 of the unmanned plane that this utility model provides is described as follows: when needs use
During unmanned plane, horn 23 need to be launched, now, as shown in Figure 7, Figure 8, first apply bigger external force, horn 23 is turned clockwise
And make it become 180 degree (i.e. levels) with supporting seat 21.The elastic spacing structure 2611 on anti-rotation shell fragment 26 is made to be stuck in active joint
In the first stopper slot 2311 on 231, under the effect of anti-rotation shell fragment 26, it is ensured that horn 23 becomes close to water with supporting seat 21
Flat, then the female thread 221 on docking sleeve pipe 22 is coordinated with the external screw thread 211 supported on seat 21 and tightens, by horn 23 with prop up
Support seat 21 is fixing to be connected, and horn 23 is in deployed condition.When not using unmanned plane, by stubborn from supporting seat 21 for docking sleeve pipe 22
Opening, then apply bigger external force, make horn 23 overcome the elastic force of anti-rotation shell fragment 26, from the first stopper slot 2311, abjection is counterclockwise
Rotate, during then the elastic spacing structure 2611 on anti-rotation shell fragment 26 snaps in the second stopper slot 2312, its result as it is shown in figure 9,
Horn 23 is maintained at folded state (or claiming rounding state).Under the effect of anti-rotation shell fragment 26, it is ensured that horn 23 and support
Seat 21, under the effect not having the biggest external force, keeps stable, will not rock.
The foldable assembly 2 of this utility model offer and unmanned plane, it is by anti-rotation shell fragment 26 and is arranged on active joint
The first stopper slot 2311 and the second stopper slot 2312 match, when its need launch use time, can quickly make folded piece
Launch, and make its folded piece keep stable, will not swing, then by lockable mechanism locking.When it is not in use, lockable mechanism
Release locking, can very quickly folded piece be folded, to facilitate user to carry and to transport.Due to have this anti-rotation shell fragment 26 and
First stopper slot 2311 and the design of the second stopper slot 2312, its lockable mechanism locking and release the process leicht fallen D/A of locking and suitable
Freely.This kind of foldable assembly be easily fabricated and assembling, and cost is lower.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all at this
Any amendment, equivalent and the improvement etc. made within the spirit of utility model and principle, should be included in this utility model
Protection domain within.
Claims (13)
1. a foldable assembly, including supporting seat, folded piece and lockable mechanism；It is characterized in that, described support seat is provided with hinge
Connect arm；Described folded piece is provided with an active joint；Described folded piece is rotatably connected on described hinged by described active joint
On arm；
One anti-rotation shell fragment is installed in described support seat；Described anti-rotation shell fragment is provided with an elastic spacing structure；
Described active joint is provided with the first stopper slot and the second stopper slot, and the elastic spacing structure on described anti-rotation shell fragment can be with
Described first stopper slot or the second stopper slot coordinate, with by spacing for described folded piece in deployed condition or folded state；
Described lockable mechanism is for being locked at described folded piece on described support seat or by described folded piece from described support
Locking is released on Zuo.
Foldable assembly the most according to claim 1, it is characterised in that described support seat is provided with two articulated jibs, Mei Gesuo
State and on articulated jib, be correspondingly provided with hinge hole；Described folded piece is provided with an active joint, and described active joint is provided with axis hole；
Described active joint is arranged between two described articulated jibs；One rotating shaft is through the hinge hole on described articulated jib and described
Axis hole on active joint, is hinged on described folded piece on described support seat.
Foldable assembly the most according to claim 1, it is characterised in that described lockable mechanism is a pair female connector pipe；Described
The lateral surface of support seat is provided with external screw thread；Described docking casing pipe sleeve is located on the lateral surface of described folded piece, in described docking sleeve pipe
Being provided with female thread, the female thread on described docking sleeve pipe can match with the external screw thread on described support seat lateral surface, with by institute
State folded piece locking to be fixed on described support seat.
Foldable assembly the most according to claim 3, it is characterised in that it is ring-type right that the end face of described support seat is provided with one
Connect boss；On described ring-type docking boss, said two articulated jib is set；
The end face of described folded piece is provided with the docking platform matched with described docking boss, and described active joint is arranged on
On described docking platform.
Foldable assembly the most according to claim 1, it is characterised in that described anti-rotation shell fragment includes elastic movable part and a peace
Dress fixed part；
Described mounting part is arranged in described support seat；Described elastic spacing structure is arranged on described elastic movable part.
Foldable assembly the most according to claim 5, it is characterised in that described anti-rotation shell fragment is one-body molded, described yielding movable
Dynamic portion draws from described mounting part, and bends certain angle.
Foldable assembly the most according to claim 1, it is characterised in that described active joint is provided with and described elastic spacing
The confined planes of respective outer side edges；
Described first stopper slot and the second stopper slot are located on described confined planes；Described first stopper slot is for limiting with described elasticity
Bit architecture coordinates, by spacing for described folded piece in deployed condition；Described second stopper slot is for joining with described elastic spacing structure
Close, by spacing for described folded piece at folded state.
Foldable assembly the most according to claim 7, it is characterised in that described elastic spacing structure is V-shaped or U-shaped, described
First stopper slot and the second stopper slot is V-shaped or U-shaped.
Foldable assembly the most according to claim 1, it is characterised in that described support seat is provided with a flange, described flange
It is provided with rack mounting apertures；Described support seat can be arranged on the fuselage of unmanned plane after passing described rack mounting apertures by screw
On.
Foldable assembly the most according to claim 2, it is characterised in that one end of described rotating shaft is provided with cap-like structure, another
End is provided with jump-ring slot；In described jump-ring slot, jump ring is installed；Described cap-like structure and jump ring by spacing for rotating shaft at described articulated jib
Hinge hole and described active joint on axis hole in.
11. foldable assemblies according to claim 4, it is characterised in that described support seat end face and described folded piece end face
On be correspondingly provided with aligning structure.
12. foldable assemblies according to claim 11, it is characterised in that the docking boss on described support seat is provided with one
Para-position muscle, on the docking platform on described folded piece, concave becomes to have alignment grooves；Described para-position muscle and described alignment grooves match.
13. 1 kinds of unmanned planes, it is characterised in that include the foldable assembly described in any one in fuselage and claim 1-12；
Support seat on described foldable assembly is fixedly mounted on described fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620585588.6U CN205837169U (en) | 2016-06-15 | 2016-06-15 | Foldable assembly and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620585588.6U CN205837169U (en) | 2016-06-15 | 2016-06-15 | Foldable assembly and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205837169U true CN205837169U (en) | 2016-12-28 |
Family
ID=58153589
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620585588.6U Active CN205837169U (en) | 2016-06-15 | 2016-06-15 | Foldable assembly and unmanned plane |
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| Country | Link |
|---|---|
| CN (1) | CN205837169U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741824A (en) * | 2017-01-24 | 2017-05-31 | 厦门南羽科技有限公司 | Unmanned plane power arm and unmanned plane |
| CN107082124A (en) * | 2017-06-14 | 2017-08-22 | 电子科技大学 | Space suit hip joint |
| CN108128441A (en) * | 2017-12-28 | 2018-06-08 | 成都优艾维智能科技有限责任公司 | A kind of screw-type unmanned plane horn fold mechanism with self-locking |
| CN108177759A (en) * | 2017-12-28 | 2018-06-19 | 王开富 | A kind of unmanned plane horn fold mechanism with locking function |
| CN110127031A (en) * | 2019-05-29 | 2019-08-16 | 北京大工科技有限公司 | A kind of foldable assembly and unmanned plane |
| CN110300704A (en) * | 2018-01-23 | 2019-10-01 | 深圳市大疆创新科技有限公司 | Horn component and unmanned plane |
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2016
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106741824A (en) * | 2017-01-24 | 2017-05-31 | 厦门南羽科技有限公司 | Unmanned plane power arm and unmanned plane |
| CN107082124A (en) * | 2017-06-14 | 2017-08-22 | 电子科技大学 | Space suit hip joint |
| CN107082124B (en) * | 2017-06-14 | 2021-04-06 | 电子科技大学 | Aerospace suit hip joint |
| CN108128441A (en) * | 2017-12-28 | 2018-06-08 | 成都优艾维智能科技有限责任公司 | A kind of screw-type unmanned plane horn fold mechanism with self-locking |
| CN108177759A (en) * | 2017-12-28 | 2018-06-19 | 王开富 | A kind of unmanned plane horn fold mechanism with locking function |
| CN108128441B (en) * | 2017-12-28 | 2023-12-05 | 成都优艾维智能科技有限责任公司 | Threaded unmanned aerial vehicle horn folding mechanism with self-locking function |
| CN110300704A (en) * | 2018-01-23 | 2019-10-01 | 深圳市大疆创新科技有限公司 | Horn component and unmanned plane |
| CN110127031A (en) * | 2019-05-29 | 2019-08-16 | 北京大工科技有限公司 | A kind of foldable assembly and unmanned plane |
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