CN204548517U - Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component - Google Patents
Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component Download PDFInfo
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- CN204548517U CN204548517U CN201520174499.8U CN201520174499U CN204548517U CN 204548517 U CN204548517 U CN 204548517U CN 201520174499 U CN201520174499 U CN 201520174499U CN 204548517 U CN204548517 U CN 204548517U
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- quick
- supporting piece
- support division
- supporting
- dismantle component
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- 230000005540 biological transmission Effects 0.000 description 1
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- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
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Abstract
The utility model discloses a kind of Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component.Described Quick-dismantle component is immobilizated in a supporting part by one by fixing part for detouchable.Described Quick-dismantle component comprises the rotating supporting piece be arranged on supporting part, and described supporting piece comprises rotating shaft, and described rotating shaft comprises the first end and the second end that are oppositely arranged; Rotating and the described supporting part pivot joint of the first end of described rotating shaft, the second end of described rotating shaft is provided with the first support division; Described supporting piece can around described axis of rotation, and in the locked state, the first support division is matched by fixing part with described described supporting piece, to be locked described on the load bearing member by fixing part.In the disassembled condition, described first support division and to be describedly separated by fixing part, to allow describedly to be separated by fixing part and supporting part for described supporting piece.
Description
Technical field
The utility model relates to a kind of Quick-dismantle component, uses the unmanned vehicle of the fixing structure of Quick-dismantle component and use fixing structure.
Background technology
Unmanned vehicle, being called for short unmanned plane (UAV, Unmanned Aerial Vehicle), is a kind of flight instruments in developing rapidly that is in.Unmanned plane, by carrying multiclass sensor, can realize image real-time Transmission, high-risk areas detecting function, is that satellite remote sensing and the strong of traditional air remote sensing supplement.At present, unmanned plane in electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the field application such as public security anti-terrorism be very wide.
When unmanned plane using electric platform set up the electronics package such as video camera, photographic camera, the connection mode between usual The Cloud Terrace and unmanned plane has two kinds.
The first adopts between The Cloud Terrace with unmanned plane to be threaded, by arranging threaded connector on The Cloud Terrace, and the mounting hole suitable with described attaching parts is set on unmanned plane, by screwing in described mounting hole by described attaching parts, described The Cloud Terrace is anchored on unmanned plane.Adopt the mode that this kind is threaded, although it is not connection structure is comparatively simple, quick detachable.
The second uses quick-disassembly structure, such as snap close, or the locking piece etc. of similar cam structure realizes the connection between The Cloud Terrace and unmanned plane.General quick-disassembly structure needs reserved certain withdrawal space, and structure is comparatively complicated, the compression dynamics of wayward quick-disassembly structure during dismounting, easily damages relevant parts.
Utility model content
In view of this, the utility model provides a kind of structure simple and can realize the Quick-dismantle component of fast assembling-disassembling, the fixing structure using described Quick-dismantle component and unmanned vehicle in finite space.
A kind of Quick-dismantle component, be immobilizated in a supporting part by one by fixing part for detouchable, described Quick-dismantle component comprises the rotating supporting piece be arranged on supporting part, and described supporting piece comprises rotating shaft, and described rotating shaft comprises the first end and the second end that are oppositely arranged; Rotating and the described supporting part pivot joint of the first end of described rotating shaft, the second end of described rotating shaft is provided with the first support division; Described supporting piece around described axis of rotation, can enter lock-out state and disassembly status to make described supporting piece; Wherein, in the locked state, the first support division is matched by fixing part with described described supporting piece, to be locked on the load bearing member by described by fixing part; In the disassembled condition, described first support division and to be describedly separated by fixing part, to allow describedly to be separated by fixing part and supporting part for described supporting piece.
Further, described first support division is the projection that the second end of the axis of rotation protrudes out, and the setting vertical with described rotating shaft; Matched by the auxiliary section on the housing of fixing part described in described first support division, to be locked described on the load bearing member by fixing part.
Further, described supporting piece also comprises the second support division, and described second support division is used for when supporting piece is in the lock state, and is held on the outside face by fixing part.
Further, the projection that the second end that described first support division and the second support division are the axis of rotation protrudes out, wherein, the length of described first support division is greater than the length of the second support division.
Further, described second support division is the flange of a ring dress of the second end projection of the axis of rotation.
Further, described Quick-dismantle component also comprises operating parts, the rotating and described supporting part pivot joint of described operating parts; Wherein, described supporting piece under the driving of operating parts around described axis of rotation.
Further, described supporting part comprises the first side and the second side that are oppositely arranged, supporting piece is rotating to be arranged on the second side of supporting part, and the first end of described rotating shaft passes from the second side of supporting part the through hole that supporting part is arranged, and stretches out in the first side of supporting part; The first end of described and described rotating shaft is connected; Wherein, described supporting piece under the driving of operating parts around described axis of rotation.
Further, described supporting part is also provided with limiting section, the angle rotatable that described limiting section rotates around the axis on the first side for limiting operating parts.
Further, described limiting section is the stop wall be arranged on the first side of described supporting part.
Further, described limiting section comprises the chute of arc, and described operating parts is also provided with guide part, and described guide part part stretches in described chute, and described chute is for limiting the rotational angle of operating parts, thus restriction supporting piece is around the rotational angle of described rotating shaft; Wherein, when described guide part slides into an end of chute, supporting piece enters lock-out state, when guide part slides into the other end of chute, and supporting piece disassembly status.
Further, described guide part is arranged on operating parts by described elastic component is telescopic; The bottom surface of chute is also provided with the first knock hole and the second knock hole, described first knock hole and the second knock hole are separately positioned on two relative ends of described chute; When described guide part slides in chute, guide part is held in the bottom surface of chute, and described elastic component is in compressive state; When described guide part slides into the position of the second knock hole, guide part is under the return action of elastic component, and when snapping in described second knock hole, supporting piece is in the lock state; When described guide part slides into the position of the first knock hole and snaps in the first knock hole, supporting piece is in disassembly status.
A kind of fixing structure, comprise by fixing part and supporting part, described fixing structure comprises at least one above-mentioned Quick-dismantle component.
Further, describedly the auxiliary section coordinated with described first support division is provided with by fixing part.
Further, described auxiliary section is the groove of strip shape or the latch part that coordinates with described first support division.
A kind of unmanned vehicle, comprise the Quick-dismantle component that at least one is above-mentioned, wherein, described is The Cloud Terrace by fixing part, and described supporting part is vibration damper plate.
Further, describedly the auxiliary section coordinated with described first support division is provided with by fixing part.
Further, described auxiliary section is the groove of strip shape or the latch part that coordinates with described first support division.
Adopt the Quick-dismantle component in the utility model, fastening assembly and unmanned vehicle, just can realize locking and the dismounting of The Cloud Terrace by the rotation of supporting piece, and the reservation operations space that Quick-dismantle component needs is very little, and structure is simple, easy to operate.
Accompanying drawing explanation
Fig. 1 is the part-structure schematic diagram in the utility model one embodiment with the unmanned vehicle of Quick-dismantle component.
Fig. 2 is the lateral plan of structure shown in Fig. 1.
Fig. 3 is the decomposition texture schematic diagram of the Quick-dismantle component in Fig. 1.
Fig. 4 is the birds-eye view of structure shown in Fig. 1.
Main element nomenclature
| Quick-dismantle component | 100 |
| Supporting part | 10 |
| First side | 101 |
| Second side | 102 |
| Through hole | 103 |
| Limiting section | 104 |
| First knock hole | 105 |
| Second knock hole | 106 |
| Chute | 107 |
| Housing | 20 |
| Auxiliary section | 21 |
| Operating parts | 11 |
| First tapped bore | 111 |
| Coupling end | 112 |
| Free end | 113 |
| Bottom surface | 114 |
| Through hole | 115 |
| Supporting piece | 12 |
| Rotating shaft | 121 |
| First end | 1211 |
| Second end | 1212 |
| First support division | 122 |
| Second support division | 123 |
| Second tapped bore | 124 |
| Screw | 50 |
| Plunger | 60 |
| First end face | 601 |
| Second end face | 602 |
| Guide part | 61 |
Following detailed description of the invention will further illustrate the utility model in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
Refer to Fig. 1 and Fig. 2, the part-structure schematic diagram with the unmanned vehicle of Quick-dismantle component 100 in the utility model one embodiment.In the present embodiment, described Quick-dismantle component 100 for The Cloud Terrace (scheming not shown) is fixed on unmanned vehicle (scheming not shown), to realize Fast Installation and the dismounting of The Cloud Terrace.
In fig. 1 and 2, illustrate only the supporting part 10 of unmanned vehicle and the housing 20 of The Cloud Terrace, the miscellaneous part of unmanned vehicle and The Cloud Terrace is not shown.Described The Cloud Terrace is fixed on the supporting part 10 of unmanned vehicle by described Quick-dismantle component 100 detouchable, thus realizes unmanned vehicle and be connected with The Cloud Terrace detouchable.
Described supporting part 10 comprises the first side 101 and the second side 102 be oppositely arranged, and wherein, The Cloud Terrace is fixed on the second side 102 of supporting part 10.
Described Quick-dismantle component 100 comprises operating parts 11 and supporting piece 12.Wherein, described supporting piece 12 is followed described operating parts 11 and is rotated under the driving of operating parts 11.In the present embodiment, operating parts 11 is rotating to be arranged on the first side 101 of supporting part 10, and supporting piece 12 is rotating to be arranged on the second side 102 of supporting part 10, and namely supporting piece 12 is arranged at the side near The Cloud Terrace on supporting part 10.
The housing 20 of The Cloud Terrace is provided with the auxiliary section 21 of matching with the supporting piece 12 of described Quick-dismantle component 100.
In the locked state, described supporting piece 12 matches with the auxiliary section 21 on the housing 20 of The Cloud Terrace Quick-dismantle component 100, and described The Cloud Terrace is locked on the second side 102 of the supporting part 10 of unmanned vehicle closely.By rotating described operating parts 11, make described supporting piece 12 follow described operating parts 11 to rotate, described Quick-dismantle component 100 is switched to disassembly status, under described disassembly status, described supporting piece 12 is separated with the auxiliary section 21 on the housing 20 of The Cloud Terrace, thus removes the locking between The Cloud Terrace and unmanned vehicle.
See also Fig. 3 and Fig. 4, described supporting part 10 is provided with through hole 103.Described supporting piece 12 comprises rotating shaft 121, and described rotating shaft 121 comprises the first end 1211 and the second end 1212 that are oppositely arranged.Described supporting piece 12 also comprises the first support division 122 protruded out from the second end 1212 of rotating shaft 121.Wherein, the setting that described first support division 122 is roughly vertical with described rotating shaft 121.
The first end 1211 of described rotating shaft 121 passes through hole 103 from the second side 102 of supporting part 10 and stretches out in the first side 101 of supporting part 10.Described operating parts 11 is connected with the first end 1211 of rotating shaft 121.Concrete, described operating parts 11 is provided with the first tapped bore 111, the first end 1211 of described rotating shaft 121 is provided with the second tapped bore 124, and screw 50 passes the first tapped bore 111 on described operating parts 11 and screws in the second tapped bore 124, thus is fixed with supporting piece 12 by described operating parts 11.In other embodiments, described operating parts 11 and supporting piece 12 can also by engaging, gluing mode fixes.Wherein, the aperture of described through hole 103 equals or slightly larger than the diameter of rotating shaft 121, described rotating shaft 121 can be rotated in through hole 103.
In the present embodiment, described operating parts 11 is pivot arm, and described operating parts 11 comprises coupling end 112 and free end 113.Described first tapped bore 111 is arranged on the coupling end 112 of operating parts 11, and the first end 1211 of rotating shaft 121 is connected with the coupling end 112 of operating parts 11.Operating parts 11 under the driving of external force, the first side 101 of supporting part 10 121 can be rotated around the shaft.Understandable, described supporting piece 12 is followed described operating parts 11 and 121 is rotated around the shaft on the second side 102 of supporting part 10 under the driving of operating parts 11.
Described supporting part 10 is also provided with limiting section 104, and described limiting section 104 is for limiting the angle rotatables of operating parts 11 121 rotations around the shaft on the first side 101.In one embodiment, described limiting section 104 can be stop wall or position-limited trough, for stopping the free end 113 of described operating parts 11, described operating parts 11 only 121 can be rotated in the angle limited on the first side 101 around the shaft.
In the present embodiment, described limiting section 104 comprises the chute 107 of arc.Described limiting section 104 also comprises the first knock hole 105 and the second knock hole 106, and described first knock hole 105 and the second knock hole 106 are separately positioned on two relative ends of described chute 107.Wherein, described first knock hole 105 and the second knock hole 106 are the shrinkage pool formed that caves inward from the bottom surface of described chute 107.
The free end 113 of described operating parts 11 is also provided with guide part 61, and described guide part 61 part stretches in described chute 107.Concrete, described Quick-dismantle component 100 also comprises plunger 60, and the free end 113 of described operating parts 11 offers through hole 115.Described plunger 60 comprises the first end face 601 and the second end face 602 be oppositely arranged, elastic component (scheming not shown) and guide part 61.Wherein, guide part 61 is arranged on the first end face 601 of plunger 60 by described elastic component is telescopic.Described plunger 60 is fixed in described through hole 115, near the bottom surface 114 of the side of described supporting part 10 on the free end 113 stretching out in operating parts 11 of guide part 61 part.
When installing described Quick-dismantle component 100, first guide part 61 and elastic component being installed on plunger 60, making guide part 61 by telescopic the first end face 601 being raised in plunger 60 of described elastic component; Then plunger 60 is installed in the through hole 115 that the free end 113 of operating parts 11 offers, and makes the bottom surface 114 of the side of close described supporting part 10 on the free end 113 stretching out in operating parts 11 of described guide part 61 part; Again the first end 1211 of the rotating shaft 121 of supporting piece 12 is passed through hole 103 from the second side 102 of supporting part 10, then the coupling end 112 of operating parts 11 is connected with the first end 1211 of rotating shaft 121, and makes in the chute 107 stretching into described limiting section 104 of guide part 61 part on the free end 113 of operating parts 11.When described guide part 61 slides in chute 107, guide part 61 is held in the bottom surface of chute 107, and described elastic component is in compressive state.
Please composition graphs 1 to Fig. 4 in the lump, when guide part 61 slides into the position of the second knock hole 106, guide part 61 is under the effect of the restoring force of elastic component, snap in described second knock hole 106, now Quick-dismantle component 100 is in the lock state, first support division 122 of supporting piece 12 snaps in the auxiliary section 21 that the housing 20 of described The Cloud Terrace is arranged, and described The Cloud Terrace is locked on the second side 102 of the supporting part 10 of unmanned vehicle closely.
In the present embodiment, described auxiliary section 21 is groove.Wherein, described groove is elongated, and the length of groove is greater than the length of described first support division 122, and to make described supporting piece 12 when rotating, the first support division 122 can snap in smoothly and deviate from described groove.In addition, the degree of depth of described groove is less than the length of the first support division 122, and when described first support division 122 snaps in described auxiliary section 21, what described first support division 122 was close to is held on the bottom surface of groove.The thickness of described groove matches with the thickness of described first support division 122.
Under Quick-dismantle component 100 is in the lock state, rotate described operating parts 11, described guide part 61 is departed from from the second knock hole 106, and when sliding into the position of the first knock hole 105, guide part 61 snaps in described second knock hole 106.Now, the auxiliary section 21 that the first support division 122 of supporting piece 12 and the housing 20 of The Cloud Terrace are arranged is separated, and described The Cloud Terrace can be separated with unmanned vehicle, thus realizes the quick lock in of The Cloud Terrace on unmanned vehicle and dismounting.
In the present embodiment, described supporting piece 12 also comprises the second support division 123, described second support division 123, and the outside face for the housing 20 with The Cloud Terrace matches, and when described lock-out state, is held on the outside face of housing 20 of The Cloud Terrace.Concrete, described second support division 123 can be the protruding outward extending lug boss of the second end 1212 of the axis of rotation 121, or the flange etc. of a ring dress of the second end 1212 projection of the axis of rotation 121.
The housing 20 of described The Cloud Terrace can arrange multiple auxiliary section 21, by the Quick-dismantle component 100 arranged with described multiple auxiliary sections 21 one_to_one corresponding, The Cloud Terrace is fixed on the supporting part 10 of unmanned vehicle.
Adopt the Quick-dismantle component 100 in present embodiment, just can be realized locking and the dismounting of The Cloud Terrace by rotary operating member 11, the reservation operations space that Quick-dismantle component 100 needs is very little, and structure is simple, easy to operate.The mode that Quick-dismantle component 100 is matched with the auxiliary section 21 on the housing 20 of The Cloud Terrace by the first support division 122 of supporting piece 12, is locked at closely by The Cloud Terrace on the second side 102 of the supporting part 10 of unmanned vehicle.In addition, by arranging second support division 123 that can offset with the outside face of the housing 20 of The Cloud Terrace on supporting piece 12, further strengthen the stability of The Cloud Terrace locking.
In one embodiment, described supporting part 10 can be vibration damper plate, and The Cloud Terrace is fixed on described vibration damper plate by described Quick-dismantle component 100.
Understandable, described operating parts 11 also can be the operating parts of other shapes such as knob, only needing by driving described operating parts 11 to rotate, supporting piece 12 can be driven to rotate, realize the first support division 122 of supporting piece 12 and coordinating and departing between auxiliary section 21.In other embodiments, described operating parts 11 can be non-essential.
Understandable, in other embodiments, described guide part 61 can be bayonet lock on the bottom surface 114 of the upper side near described supporting part 10 being directly raised in operating parts 11 or projection.Described guide part 61 can be telescopic be raised in described bottom surface 114 arrange, also can be non-telescoping.In one embodiment, described guide part 61 can be directly be raised in described bottom surface 114 to arrange, and wherein, described guide part 61 adopts elastomeric material to prepare.
Understandable, described auxiliary section 21 also can be boss, when Quick-dismantle component 100 is in the lock state, first support division 122 is held on described boss, apply the power towards the direction of supporting part 10 to The Cloud Terrace, be locked at closely on the second side 102 of the supporting part 10 of unmanned vehicle to make The Cloud Terrace.In one embodiment, also can not arrange described auxiliary section 21, first support division 122 to be directly held on the outside face of housing 20 of The Cloud Terrace.In other embodiments, described first support division 122 and auxiliary section 21 also can be a pair buckle or snap close etc. that cooperatively interact.
Understandable, Quick-dismantle component 100 described in the utility model is not only confined to the fixing of The Cloud Terrace on unmanned vehicle and dismounting, can also any by the fixing of fixing part and dismounting on other devices or mechanism.
In addition; those skilled in the art will be appreciated that; above embodiment is only used to the utility model is described; and be not used as restriction of the present utility model; as long as within spirit of the present utility model, the appropriate change do above embodiment and change all drop within the claimed scope of the utility model.
Claims (17)
1. a Quick-dismantle component, for being immobilizated in a supporting part by one by fixing part detouchable, it is characterized in that, described Quick-dismantle component comprises the rotating supporting piece be arranged on supporting part, described supporting piece comprises rotating shaft, and described rotating shaft comprises the first end and the second end that are oppositely arranged; Rotating and the described supporting part pivot joint of the first end of described rotating shaft, the second end of described rotating shaft is provided with the first support division; Described supporting piece around described axis of rotation, can enter lock-out state and disassembly status to make described supporting piece; Wherein, in the locked state, the first support division is matched by fixing part with described described supporting piece, to be locked on the load bearing member by described by fixing part; In the disassembled condition, described first support division and to be describedly separated by fixing part, to allow describedly to be separated by fixing part and supporting part for described supporting piece.
2. Quick-dismantle component as claimed in claim 1, it is characterized in that, described first support division is the projection that the second end of the axis of rotation protrudes out, and the setting vertical with described rotating shaft; Matched by the auxiliary section on the housing of fixing part described in described first support division, in the locked state, the first support division matches with described auxiliary section described supporting piece, to be locked described on supporting part by fixing part.
3. Quick-dismantle component as claimed in claim 1, it is characterized in that, described supporting piece also comprises the second support division, and described second support division is used for when supporting piece is in the lock state, and is held on the outside face by fixing part.
4. Quick-dismantle component as claimed in claim 3, it is characterized in that, the projection that the second end that described first support division and the second support division are the axis of rotation protrudes out, wherein, the length of described first support division is greater than the length of the second support division.
5. Quick-dismantle component as claimed in claim 3, is characterized in that, described second support division is the flange of a ring dress of the second end projection of the axis of rotation.
6. Quick-dismantle component as claimed in claim 1, it is characterized in that, described Quick-dismantle component also comprises operating parts, and described operating parts is connected with the first end of the rotating shaft of described supporting piece; Wherein, described supporting piece under the driving of operating parts around described axis of rotation.
7. Quick-dismantle component as claimed in claim 6, it is characterized in that, described supporting part comprises the first side and the second side that are oppositely arranged, supporting piece is rotating to be arranged on the second side of supporting part, the first end of described rotating shaft passes from the second side of supporting part the through hole that supporting part is arranged, and stretches out in the first side of supporting part; Described operating parts is connected with the first end of rotating shaft; Wherein, described supporting piece under the driving of operating parts around described axis of rotation.
8. Quick-dismantle component as claimed in claim 7, is characterized in that, described supporting part is also provided with limiting section, the angle rotatable that described limiting section rotates around the axis on the first side for limiting operating parts.
9. Quick-dismantle component as claimed in claim 8, it is characterized in that, described limiting section is the stop wall be arranged on the first side of described supporting part.
10. Quick-dismantle component as claimed in claim 8, it is characterized in that, described limiting section comprises the chute of arc, described operating parts is also provided with guide part, described guide part part stretches in described chute, described chute is for limiting the rotational angle of operating parts, thus restriction supporting piece is around the rotational angle of described rotating shaft; Wherein, when described guide part slides into an end of chute, supporting piece enters lock-out state, when guide part slides into the other end of chute, and supporting piece disassembly status.
11. Quick-dismantle components as claimed in claim 10, is characterized in that, described guide part is arranged on operating parts by described elastic component is telescopic; The bottom surface of chute is also provided with the first knock hole and the second knock hole, described first knock hole and the second knock hole are separately positioned on two relative ends of described chute; When described guide part slides in chute, guide part is held in the bottom surface of chute, and described elastic component is in compressive state; When described guide part slides into the position of the second knock hole, guide part is under the return action of elastic component, and when snapping in described second knock hole, supporting piece is in the lock state; When described guide part slides into the position of the first knock hole and snaps in the first knock hole, supporting piece is in disassembly status.
12. 1 kinds of fixing structures, comprise by fixing part and supporting part, it is characterized in that, described fixing structure comprises at least one Quick-dismantle component as described in claim 1-11.
13. fixing structures as claimed in claim 12, is characterized in that, are describedly provided with the auxiliary section coordinated with described first support division by fixing part.
14. fixing structures as claimed in claim 13, is characterized in that, described auxiliary section is the groove of strip shape or the latch part that coordinates with described first support division.
15. 1 kinds of unmanned vehicles, is characterized in that, comprise at least one Quick-dismantle component as described in claim 1-11, wherein, described is The Cloud Terrace by fixing part, and described supporting part is vibration damper plate.
16. unmanned vehicles as claimed in claim 15, is characterized in that, are describedly provided with the auxiliary section coordinated with described first support division by fixing part.
17. unmanned vehicles as claimed in claim 16, is characterized in that, described auxiliary section is the groove of strip shape or the latch part that coordinates with described first support division.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520174499.8U CN204548517U (en) | 2015-03-26 | 2015-03-26 | Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520174499.8U CN204548517U (en) | 2015-03-26 | 2015-03-26 | Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204548517U true CN204548517U (en) | 2015-08-12 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520174499.8U Expired - Fee Related CN204548517U (en) | 2015-03-26 | 2015-03-26 | Quick-dismantle component, has fixing structure and the unmanned vehicle of Quick-dismantle component |
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| CN (1) | CN204548517U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108100281A (en) * | 2018-01-16 | 2018-06-01 | 北京小米移动软件有限公司 | It is rotated with device, holder camera and unmanned plane |
| WO2018188188A1 (en) * | 2017-04-10 | 2018-10-18 | 深圳市大疆创新科技有限公司 | Upper cover of unmanned aerial vehicle and unmanned aerial vehicle |
| CN111731498A (en) * | 2015-09-06 | 2020-10-02 | 深圳市大疆灵眸科技有限公司 | Cloud platform, image device and unmanned vehicles |
-
2015
- 2015-03-26 CN CN201520174499.8U patent/CN204548517U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111731498A (en) * | 2015-09-06 | 2020-10-02 | 深圳市大疆灵眸科技有限公司 | Cloud platform, image device and unmanned vehicles |
| US11104452B2 (en) | 2015-09-06 | 2021-08-31 | SZ DJI Technology Co., Ltd. | Gimbal, imaging device and unmanned aerial vehicle |
| WO2018188188A1 (en) * | 2017-04-10 | 2018-10-18 | 深圳市大疆创新科技有限公司 | Upper cover of unmanned aerial vehicle and unmanned aerial vehicle |
| CN108100281A (en) * | 2018-01-16 | 2018-06-01 | 北京小米移动软件有限公司 | It is rotated with device, holder camera and unmanned plane |
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