CN205738124U - One is conveniently replaceable load device and unmanned plane - Google Patents

One is conveniently replaceable load device and unmanned plane Download PDF

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Publication number
CN205738124U
CN205738124U CN201620429540.6U CN201620429540U CN205738124U CN 205738124 U CN205738124 U CN 205738124U CN 201620429540 U CN201620429540 U CN 201620429540U CN 205738124 U CN205738124 U CN 205738124U
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China
Prior art keywords
load
base assembly
conveniently replaceable
fixture
unmanned plane
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CN201620429540.6U
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Chinese (zh)
Inventor
黄立
张纯智
黄晟
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Puzhou Technology (Shenzhen) Co.,Ltd.
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Universal Aircraft Technology (shenzhen) Co Ltd
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Abstract

This utility model provides one and is conveniently replaceable load device and unmanned plane, including load fixture, base assembly and latch assembly, load fixture upper surface fits fixing with base assembly lower surface by latch assembly, load fixture upper surface is provided with communication interface male, base assembly lower surface correspondence position is provided with the communication interface female matched with communication interface male, and load is fixed by screws in load fixture lower surface.This utility model is by installed load fixture in load, and set communication interface, different types of load can be installed to on a unmanned plane, and can quickly load be replaced, not only improve conventional load and be fixed to unmanned hands-operation complexity, the situation of inefficiency, also improve the versatility of unmanned plane, meet the demand of carry different loads, greatly increase the range of application of unmanned plane.

Description

One is conveniently replaceable load device and unmanned plane
Technical field
This utility model belongs to vehicle technology field, is specifically related to one and is conveniently replaceable load device and unmanned plane.
Background technology
In unmanned air vehicle technique application, generally load is mounted on unmanned aerial vehicle body, and various hanging equipments of taking photo by plane are loaded in load, the field such as it is widely used in photographing, takes a picture, monitoring.But, it is complicated that existing load is installed to operating process on unmanned plane, inefficiency, and, typically can only load with a load with a unmanned plane, range of application is little.Therefore, along with the difference of people's demand, different load is mounted to on a unmanned plane, it is achieved " one " machine is multiplex, it will become the trend of future development.
In order to realize that the load of unmanned plane is replaced, it is necessary for using the mode of simple and fast, therefore load can be carried out fast assembling-disassembling, there is the most real meaning equally.
Utility model content
The purpose of this utility model is to provide one and is conveniently replaceable load device, for being mounted to by different loads with a unmanned plane, expands the range of application of unmanned plane.
For this, the technical solution of the utility model there is provided one and is conveniently replaceable load device, including load fixture, base assembly and latch assembly, described load fixture upper surface fits fixing with base assembly lower surface by latch assembly, described load fixture upper surface is provided with communication interface male, base assembly lower surface correspondence position is provided with the communication interface female matched with communication interface male, and load is fixed by screws in load fixture lower surface.
Further, above-mentioned load fixture includes that load fixed cover and load fix lower cover, and described load fixed cover and load are fixed and set at regular intervals between lower cover, and load fixed cover and load are fixed the corner of lower cover and connected one to one by shock-absorbing ball.
Further, above-mentioned load fixed cover removably connects with base assembly, and load and load are fixed lower cover and removably connected.
Further, above-mentioned latch assembly includes positioning boss and the clamp being separately positioned on load fixed cover two ends, and it is arranged on the detent at base assembly two ends and by the locking sliding block of locking pull bar control, described positioning boss matches with detent, and clamp matches with the locking sliding block controlled by locking pull bar.
Further, above-mentioned latch assembly also includes the hole, location being arranged in the middle part of load fixed cover, and is arranged on base assembly the locating dowel matched with hole, location.
Further, the load installation place of above-mentioned load fixture is provided with dodges hole, and this is dodged hole and runs through load fixed cover and load fixes lower cover.
Further, above-mentioned base assembly is also equipped with dodging hole, this dodge hole with in load fixed cover to dodge hole site relative.
It addition, this utility model additionally provides a kind of unmanned plane being conveniently replaceable load, including unmanned aerial vehicle body and be conveniently replaceable load device, described base assembly upper surface is connected with unmanned aerial vehicle body.
Further, above-mentioned base assembly is detachably connected on position, middle, unmanned aerial vehicle body lower end.
The beneficial effects of the utility model:
(1) this of this utility model offer is conveniently replaceable load device simple in construction, by load fixture, different loads can carry out Fast Installation, and assembly and disassembly is convenient, and by setting communication interface, it is achieved the transmission of load data.
(2) different types of load can be installed to on a unmanned plane by changing load device by this unmanned plane being conveniently replaceable load that this utility model provides, and can quickly load be replaced, improve conventional load and be fixed to unmanned hands-operation complexity, the situation of inefficiency, improve the versatility of unmanned plane, meet the demand of carry different loads, greatly expand the range of application of unmanned plane.
Below with reference to accompanying drawing, this utility model is described in further details.
Accompanying drawing explanation
Fig. 1 is the structural representation that this utility model is conveniently replaceable load device.
Fig. 2 is the structural representation of load fixture in this utility model.
Fig. 3 is the structural representation of base assembly in this utility model.
Description of reference numerals: 1, shock-absorbing ball;2, load fixed cover;3, load fixes lower cover;4, base assembly;5, locking pull bar;6, communication interface male;7, load fixture;8, load;9, positioning boss;10, hole is dodged;11, clamp;12, hole, location;13, detent;14, locating dowel;15, communication interface female.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, all other embodiments that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
As shown in Figure 1, present embodiments provide one and be conveniently replaceable load device, including load fixture 7, base assembly 4 and latch assembly, described load fixture 7 upper surface fits fixing with base assembly 4 lower surface by latch assembly, described load fixture 7 upper surface is provided with communication interface male 6, base assembly 4 lower surface correspondence position is provided with the communication interface female 15 matched with communication interface male 6, and load 8 is fixed by screws in load fixture 7 lower surface.This replacing load device can carry out Fast Installation replacing by load fixture 7 to different loads, and by the communication interface male 6 set and communication interface female 15, it is achieved the transmission of load data, simple to operate.
Specific embodiment, as shown in Figures 2 and 3, described load fixture 7 includes that load fixed cover 2 and load fix lower cover 3, described load fixed cover 2 and load fix set between lower cover 3 at regular intervals, load fixed cover 2 and load are fixed the corner of lower cover 3 and are connected one to one by shock-absorbing ball 1, the vibrations produced during the effectively reducing unmanned plane during flying impact on load 8;Communication interface male 6 is arranged on load fixed cover 2 and load is fixed between lower cover 3, and its docking port with communication interface female 15 is arranged on the outer surface of load fixed cover 2;Described load fixed cover 2 removably connects with base assembly 4;nullWherein,Described latch assembly includes positioning boss 9 and the clamp 11 being separately positioned on load fixed cover 2 two ends,And it is arranged on the detent 13 at base assembly 4 two ends and by locking the locking sliding block that pull bar 5 controls,Described positioning boss 9 matches with detent 13,Clamp 11 matches with the locking sliding block controlled by locking pull bar 5,When load fixture 7 and base assembly 4 fixedly mount,First by detent 13 corresponding on the positioning boss 9 inserted base assembly 4 of load fixed cover 2 one end,Then by communication interface male 6 with communication interface female 15 to inserting,Realize data transmission,Finally clamp 11 is inserted in locking pull bar 5,Its locking sliding block controlled is made to be pushed down by the clamp 11 in load fixed cover 2,Thus load fixture 7 is locked,Simple to operate,It is easy to fast assembling-disassembling;Load 7 and load are fixed lower cover 3 and are removably connected too.Load fixture 1 volume of this structure is little, lightweight, ease of assembly.
Further preferred, described latch assembly also includes the hole, location 12 being arranged in the middle part of load fixed cover 2, and it is arranged on base assembly 4 locating dowel 14 matched with hole 12, location, fixing by the cooperation location of hole 12, location and locating dowel 14 to lock further between base assembly 4 and load fixture 7.
Additionally, varions type load 8 top is provided with motor, vibrations can be produced during unmanned plane during flying, motor can produce frictional influence its service life with load fixture 7, therefore, the preferably load installation place at described load fixture 7 is provided with and dodges hole 10, this is dodged hole 10 and runs through load fixed cover 2 and load fixes lower cover 3, simultaneously, also can be also equipped with dodging hole 10 on described base assembly 4, this dodge hole 10 with in load fixed cover 2 to dodge position, hole 10 relative, the motor being set in load 8 dodging hole 10 reserves vibrations space, guarantee will not interference between load 8 with load fixture 7 and base assembly 4.
On the basis of the replacing load device of above-mentioned offer, the present embodiment additionally provides a kind of unmanned plane being conveniently replaceable load, and including unmanned aerial vehicle body and be conveniently replaceable load device, described base assembly 4 upper surface is connected with unmanned aerial vehicle body.Preferably, described base assembly 4 is detachably connected on position, middle, unmanned aerial vehicle body lower end, it is ensured that unmanned aerial vehicle body uniform force.Load 8 is arranged on load fixture 7 by this unmanned plane, and set communication interface, base assembly 4 is arranged on unmanned aerial vehicle body, by Fast Installation between load fixture 7 and base assembly 4, can different types of load 8 be installed to on a unmanned plane, and can quickly load 8 be replaced, not only improve conventional load 8 and be fixed to unmanned hands-operation complexity, the situation of inefficiency, also improve the versatility of unmanned plane, meet the demand of carry different loads, greatly increase the range of application of unmanned plane.
Exemplified as above is only to illustration of the present utility model, is not intended that the restriction to protection domain of the present utility model, within the every and same or analogous design of this utility model belongs to protection domain of the present utility model.

Claims (9)

1. one kind is conveniently replaceable load device, it is characterized in that: include load fixture (7), base assembly (4) and latch assembly, described load fixture (7) upper surface fits fixing with base assembly (4) lower surface by latch assembly, described load fixture (7) upper surface is provided with communication interface male (6), base assembly (4) lower surface correspondence position is provided with the communication interface female (15) matched with communication interface male (6), and load (8) is fixed by screws in load fixture (7) lower surface.
It is conveniently replaceable load device the most as claimed in claim 1, it is characterized in that: described load fixture (7) includes that load fixed cover (2) and load fix lower cover (3), described load fixed cover (2) and load are fixed and are set at regular intervals between lower cover (3), and load fixed cover (2) and load are fixed the corner of lower cover (3) and connected one to one by shock-absorbing ball (1).
It is conveniently replaceable load device the most as claimed in claim 2, it is characterized in that: described load fixed cover (2) removably connects with base assembly (4), and load (8) and load are fixed lower cover (3) and removably connected.
It is conveniently replaceable load device the most as claimed in claim 3, it is characterized in that: described latch assembly includes being separately positioned on positioning boss (9) and the clamp (11) at load fixed cover (2) two ends, and it is arranged on the detent (13) at base assembly (4) two ends and by locking the locking sliding block that pull bar (5) controls, described positioning boss (9) matches with detent (13), and clamp (11) matches with the locking sliding block controlled by locking pull bar (5).
It is conveniently replaceable load device the most as claimed in claim 4, it is characterized in that: described latch assembly also includes being arranged on the hole, location (12) at load fixed cover (2) middle part, and is arranged on the upper locating dowel (14) matched with hole, location (12) of base assembly (4).
It is conveniently replaceable load device the most as claimed in claim 2, it is characterized in that: the load installation place of described load fixture (7) is provided with dodges hole (10), this is dodged hole (10) and runs through load fixed cover (2) and load fixes lower cover (3).
It is conveniently replaceable load device the most as claimed in claim 6, it is characterized in that: be also equipped with on described base assembly (4) dodging hole (10), this dodge hole (10) with in load fixed cover (2) to dodge hole (10) position relative.
8. the unmanned plane being conveniently replaceable load as described in any one of claim 1~7, it is characterised in that: including unmanned aerial vehicle body and be conveniently replaceable load device, described base assembly (4) upper surface is connected with unmanned aerial vehicle body.
It is conveniently replaceable the unmanned plane of load the most as claimed in claim 8, it is characterised in that: described base assembly (4) is detachably connected on position, middle, unmanned aerial vehicle body lower end.
CN201620429540.6U 2016-05-12 2016-05-12 One is conveniently replaceable load device and unmanned plane Active CN205738124U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620429540.6U CN205738124U (en) 2016-05-12 2016-05-12 One is conveniently replaceable load device and unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620429540.6U CN205738124U (en) 2016-05-12 2016-05-12 One is conveniently replaceable load device and unmanned plane

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CN205738124U true CN205738124U (en) 2016-11-30

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107422742A (en) * 2017-08-16 2017-12-01 广东容祺智能科技有限公司 A kind of unmanned plane multifunctional service Towed bird system
CN107651202A (en) * 2017-10-13 2018-02-02 北京臻迪科技股份有限公司 A kind of hooking device and its unmanned plane
CN107757934A (en) * 2017-10-13 2018-03-06 北京臻迪科技股份有限公司 A kind of unmanned plane carry device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107422742A (en) * 2017-08-16 2017-12-01 广东容祺智能科技有限公司 A kind of unmanned plane multifunctional service Towed bird system
CN107651202A (en) * 2017-10-13 2018-02-02 北京臻迪科技股份有限公司 A kind of hooking device and its unmanned plane
CN107757934A (en) * 2017-10-13 2018-03-06 北京臻迪科技股份有限公司 A kind of unmanned plane carry device

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Address after: 518000 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.)

Patentee after: Puzhou Technology (Shenzhen) Co.,Ltd.

Address before: 518000 Room 201, building A, 1 front Bay Road, Shenzhen Qianhai cooperation zone, Shenzhen, Guangdong

Patentee before: PRODRONE TECHNOLOGY (SHENZHEN) Co.,Ltd.