CN110329525A - A kind of unmanned plane and its assemble method - Google Patents
A kind of unmanned plane and its assemble method Download PDFInfo
- Publication number
- CN110329525A CN110329525A CN201910576816.1A CN201910576816A CN110329525A CN 110329525 A CN110329525 A CN 110329525A CN 201910576816 A CN201910576816 A CN 201910576816A CN 110329525 A CN110329525 A CN 110329525A
- Authority
- CN
- China
- Prior art keywords
- mounting portion
- holding section
- unmanned plane
- mounting
- fixed part
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 17
- 239000006096 absorbing agent Substances 0.000 claims description 21
- 230000035939 shock Effects 0.000 claims description 21
- 238000009434 installation Methods 0.000 claims description 10
- 230000006978 adaptation Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 7
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
- B64C1/069—Joining arrangements therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of unmanned plane, including fuselage and connection structure, fuselage is equipped with the mounting groove for mounting connection structure, is equipped with the first holding section and the first fixed part in mounting groove；Connection structure includes the first mounting portion and the second mounting portion from the inclination extension of one end of the first mounting portion, and the first mounting portion is equipped with the second holding section, and the second mounting portion is equipped with the second fixed part far from one end of the first mounting portion；First holding section is matched with the second holding section with fixed connection structure in a first direction, and the second fixed part is fixed to fixed connection structure in a second direction on the first fixed part, and first direction is vertical with second direction.The invention also discloses a kind of assemble method of unmanned plane, unmanned plane and its assemble method provided by the invention, by the cooperation of the first holding section and the second holding section and the cooperation of the first fixed part and the second fixed part, realization is rapidly assembled and disassembled.
Description
Technical field
The present invention relates to unmanned plane field more particularly to unmanned planes and its assemble method.
Background technique
Holder Quick Release interface on unmanned plane is the important feature that realization unmanned plane replaces different holders, but existing nothing
During man-machine replacement holder, it is not easy to mount and dismount.
Summary of the invention
In order to be not easy to installation and removal, the purpose of the present invention when overcoming the problems, such as unmanned plane replacement holder in the prior art
It is to provide a kind of unmanned plane and its assemble method.
To achieve the above object, the embodiment of the present invention provides a kind of unmanned plane, including fuselage and connection structure, the fuselage
It is equipped with the mounting groove for installing the connection structure, is equipped with the first holding section and the first fixed part in the mounting groove；Institute
State connection structure include the first mounting portion and from one end of first mounting portion inclination extend the second mounting portion, described first
Mounting portion is equipped with the second holding section, and second mounting portion is equipped with the second fixed part far from one end of first mounting portion；Institute
It states the first holding section to be matched with second holding section to fix the connection structure in a first direction, described second is fixed
Portion is fixed on first fixed part to fix the connection structure, the first direction and described second in a second direction
Direction is vertical.
Preferably, first holding section be extend internally from the side wall of the mounting groove first protrusion, described second
Holding section is from outwardly extending second protrusion in the side of first mounting portion.
Preferably, the angle being formed between first mounting portion and second mounting portion is obtuse angle.
Preferably, the unmanned plane further includes fastener, first fixed part be equipped with the first mounting hole, described second
Fixed part is equipped with the second mounting hole, and the fastener is arranged in the first mounting hole and the second mounting hole with fixed by described second
Portion is fixed on first fixed part.
Preferably, second fixed part is the elastic card fastener being flexibly connected with second mounting portion, described first
Fixed part is the card slot matched with the elastic card fastener.
Preferably, the unmanned plane further includes the holder for being used to install photographic device being installed in the connection structure.
Preferably, the connection structure further includes the third mounting portion for installing the holder, the third mounting portion
The inside of angle, one end installation of the third mounting portion are formed by set on first mounting portion and second mounting portion
In the one end of first mounting portion far from second mounting portion, the other end of the third mounting portion is installed on described second
The one end of mounting portion far from first mounting portion.
Preferably, the connector further includes the first damping being connected between third mounting portion and first mounting portion
Part and the second shock absorber part being connected between the third mounting portion and second mounting portion.
Preferably, the quantity of first shock absorber part is two, and the quantity of second shock absorber part is two；The third
Mounting portion includes mounting portion ontology and four connectors, and four connectors are from the both ends of the mounting portion ontology to the peace
It is extended to form on the outside of dress portion ontology, two of them connector passes through two first shock absorber parts respectively and is installed on described first
The two sides of mounting portion, other two connector pass through two second shock absorber parts respectively and are installed on the two of second mounting portion
Side.
Preferably, the connector further includes the away from the side of the third mounting portion set on first mounting portion
Three shock absorber parts.
Preferably, guide groove compatible with first mounting portion is equipped in the mounting groove.
The embodiment of the present invention further provides for a kind of assemble method of unmanned plane, comprising:
First mounting portion of the connection structure is installed in the mounting groove so that first holding section with
Second holding section is not overlapped in this second direction；
Make first mounting portion close to second mounting portion one end to the slot bottom of the mounting groove move until
Second holding section and first holding section be not be overlapped in said first direction；
Second mounting portion is pushed along the second direction so that second holding section and first holding section exist
It is least partially overlapped in the second direction；
Second fixed part is fixed on first fixed part.
Preferably, first mounting portion of the connection structure is installed in the mounting groove and includes:
First mounting portion of the connection structure is slided along the second direction to the head of the unmanned plane.
Compared with prior art, the beneficial effects of the present invention are: by the way that the first holding section and first are arranged in mounting groove
Fixed part；Second holding section is set on the first mounting portion, the second fixed part is set on the second mounting portion, the first holding section with
Second holding section is matched with fixed connection structure in a first direction, and the second fixed part is fixed on the first fixed part
Fixed connection structure on two directions, thus easy to disassemble and install.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of unmanned plane provided in an embodiment of the present invention；
Fig. 2 is the structural schematic diagram of the unmanned plane at another visual angle provided in an embodiment of the present invention；
Fig. 3 is the assembling figure of connection structure provided in an embodiment of the present invention and unmanned plane；
Fig. 4 is the fixed form schematic diagram that one embodiment of the invention provides；
Fig. 5 be another embodiment of the present invention provides fixed form schematic diagram；
Fig. 6 is attachment structure schematic diagram provided in an embodiment of the present invention；
Fig. 7 is the assemble method flow chart of unmanned plane provided in an embodiment of the present invention；
Fig. 8 is the first state schematic diagram of the assembling process of unmanned plane provided in an embodiment of the present invention；
Fig. 9 is the second status diagram of the assembling process of unmanned plane provided in an embodiment of the present invention.
In figure: 1, fuselage；11, mounting groove；111, guide groove；12, the first holding section；121, the first protrusion；13, first is fixed
Portion；131, card slot；132, the first mounting hole；2, connection structure；21, the first mounting portion；22, the second mounting portion；221, connecting column；
23, the second holding section；231, the second protrusion；24, the second fixed part；241, elastic card fastener；242, the second mounting hole；25,
Three mounting portions；251, installation position；252, mounting portion ontology；253, connector；26, the first shock absorber part；27, the second shock absorber part；28,
Third shock absorber part；3, holder；31, photographic device.
Specific embodiment
To facilitate the understanding of the present invention, in the following with reference to the drawings and specific embodiments, the present invention will be described in more detail.
It should be noted that be expressed " being fixed on " another element when element, it can directly on the other element or therebetween
There may be one or more elements placed in the middle.When an element is expressed " connection " another element, it, which can be, directly connects
It is connected to another element or there may be one or more elements placed in the middle therebetween.Term used in this specification is " vertical
", " horizontal ", "left", "right" and similar statement for illustrative purposes only.
Unless otherwise defined, technical and scientific term all used in this specification is led with technology of the invention is belonged to
The normally understood meaning of the technical staff in domain is identical.Used term is only in the description of the invention in this specification
The purpose of description specific embodiment is not intended to the limitation present invention.Term "and/or" used in this specification includes one
Any and all combinations of a or multiple relevant listed items.
In the following, being described further in conjunction with attached drawing and specific embodiment to the present invention, it should be noted that not
Under the premise of conflicting, new implementation can be formed between various embodiments described below or between each technical characteristic in any combination
Example.
As shown in Figure 1, unmanned plane provided in an embodiment of the present invention, including fuselage 1, connection structure 2 and holder 3, connection knot
Structure 2 is used to for holder 3 being installed on fuselage 1, power supply of the holder 3 for installing photographic device 31, on photographic device 31 and fuselage 1
Component or control chip electrical connection, the data of photographic device 31 are powered and acquired to photographic device 31.It is appreciated that connection
Sensor or other monitor components can also be connected on fuselage 1 by structure 2.
As Figure 2-3, fuselage 1 includes head, tail and several wings, and head, which is equipped with, is used for mounting connection structure 2
Mounting groove 11,11 two sides of mounting groove are respectively equipped with the first holding section 12, and it is solid that mounting groove 11 far from one end of head is equipped with first
Determine portion 13.
Connection structure 2 includes the first mounting portion 21 and the second mounting portion from the inclination extension of one end of the first mounting portion 21
22,21 two sides of the first mounting portion are respectively equipped with the second holding section 23, and the second mounting portion 22 is set far from one end of the first mounting portion 21
There is the second fixed part 24.First holding section 12 is matched with the second holding section 23 with fixed connection structure 2 in a first direction, tool
Body, the second holding section 23 is affiliated in 12 inside/top of the first holding section to be supported by it.Second fixed part 24 is fixed on
With fixed connection structure 2 in a second direction on one fixed part 13, wherein first direction is vertical with second direction.The present embodiment
In, first direction is the short transverse of unmanned plane, and second direction is the length direction of unmanned plane.In installation process, by the first peace
Dress portion 21 is directed at mounting groove 11 far from one end of the second mounting portion 22, makes the first holding section 12 and the second holding section 23 in second party
It is not overlapped upwards；Pressing the second mounting portion 22 moves the first mounting portion 21 until the second holding section towards the slot bottom of mounting groove 11
23 is not be overlapped in a first direction namely the second holding section 23 is fully located at the interior of the first holding section 12 with the first holding section 12
Side/top；The second mounting portion 22 is pushed to move the first mounting portion 21 in a second direction in a second direction, to make the second engaging
Portion 23 and the first holding section 12 are least partially overlapped in a second direction, and the second holding section 23 is affiliated in the first holding section 12
Side/top, so that the first holding section 12 be made to play support and position-limiting action to the second holding section 23 in a first direction.Again by
Two fixed parts 24 are fixed on the first fixed part 13, thus fixed connection structure 2 in a second direction.In disassembly process, by
Two fixed parts 24 are removed from the first fixed part 13, reversed to push the second mounting portion 22, make the first mounting portion 21 to heading
Movement, so that the first holding section 12 and the second holding section 23 are not overlapped in a second direction, so as to remove connection structure 2.
During replacing holder 3, connection structure 2 can be quickly removed from fuselage 1, after the completion of holder 3 is replaced, then will connect knot
Structure 2 is installed on fuselage 1, realizes Fast Installation, and easy to operate.
As shown in figure 3, in one embodiment, the first holding section 12 be extend internally from the side wall of mounting groove 11 it is first convex
121 are played, the second holding section 23 is from outwardly extending second protrusion 231 in 21 side of the first mounting portion, the first protrusion 121 and second
When protrusion 231 is overlapped, first raised 121 pair of second protrusion 231 is played a supporting role.In other embodiments, the first holding section
12 can be pillar, and the second holding section 23 is equipped with the through-hole cooperated with pillar, 23 weight of the first holding section 12 and the second holding section
Through-hole is stacked as to be sheathed on pillar.
As shown in figure 4, in one embodiment, the second fixed part 24 is the Elastic buckle being flexibly connected with the second mounting portion 22
Part 241, wherein the second mounting portion 22 is equipped with connecting column 221, the connection that elastic card fastener 241 is connect with the second mounting portion 22
End sets connecting hole, and connecting hole is sheathed on connecting column 221, and elastic card fastener 241 sets V-type far from the free end of the second mounting portion 22
Buckle structure, the first fixed part 13 are the card slot 131 matched with elastic card fastener 241, the V-type buckle of elastic card fastener 241
Structure is sticked in card slot 131 with fixed connection structure 2 in a second direction.
As shown in figure 5, in another embodiment, unmanned plane further includes fastener 4, the first fixed part 13 is equipped with the first peace
Hole 132 is filled, the second fixed part 24 is equipped with the second mounting hole 242, and fastener 4 is arranged in the first mounting hole 132 and the second installation
Hole 242 is the second fixed part 24 to be fixed on the first fixed part 13.
As shown in Figure 6, it is preferable that the angle between the first mounting portion 21 and the second mounting portion 22 is obtuse angle, easy to disassemble
And installation.Connection structure 2 further includes the third mounting portion 25 for installing holder 3, and third mounting portion 25 is set to the first mounting portion
21 and second mounting portion 22 be formed by the inside of angle, one end of third mounting portion 25 is installed on the first mounting portion 21 far from
One end of two mounting portions 22, the other end of third mounting portion 25 are installed on one of the second mounting portion 22 far from the first mounting portion 21
End.Third mounting portion 25 is equipped with the installation position 251 for installing holder 3, and holder 3 is installed on third mounting portion 25, avoids
Damage of the connection structure 2 during installation and removal to holder 3.
As shown in fig. 6, connection structure 2 further includes that first be connected between third mounting portion 25 and the first mounting portion 21 subtracts
Shake part 26 and the second shock absorber part 27 being connected between third mounting portion 25 and the second mounting portion 22.Preferably, the first shock absorber part
26 quantity is two, and the quantity of the second shock absorber part 27 is two；Third mounting portion 25 includes mounting portion ontology 252 and four companies
Fitting 253, four connectors 253 are extended to form from the both ends of mounting portion ontology 252 to the outside of mounting portion ontology 252, wherein
Two connectors 253 are installed on the two sides of the first mounting portion 21, other two connector by two the first shock absorber parts 26 respectively
253 are installed on the two sides of the second mounting portion 22 by two the second shock absorber parts 27 respectively, install in third mounting portion 25 and first
Cushioning effect is played between portion 21 and the second mounting portion 22, to prevent the vibration of horizontal direction in flight course to the damage of holder 3
It is bad.Connection structure 2 further includes the third shock absorber part 28 set on the first mounting portion 21 away from the side of third mounting portion 25, to prevent
Damage of the vibration of vertical direction to holder 3 in flight course.
As shown in figure 4, mounting groove 11 is equipped with guide groove 111 compatible with the first mounting portion 21, the first mounting portion 21 is right
It can be slided to unmanned plane heading after quasi- guide groove 111, realize Fast Installation.
As Figure 7-9, the embodiment of the present invention also provides a kind of assemble method of unmanned plane, comprising:
Step S101: first mounting portion 21 of the connection structure 2 is installed in the mounting groove 11, so that institute
It is not be overlapped in this second direction to state the first holding section 12 and second holding section 23；
Step S102: make one end close to second mounting portion 22 of first mounting portion 21 to the mounting groove 11
Slot bottom movement until second holding section 23 and first holding section 12 it is not be overlapped in said first direction；
Step S103: along the second direction push second mounting portion 22 so that second holding section 23 with it is described
First holding section 12 is least partially overlapped in this second direction；
Step S104: second fixed part 24 is fixed on first fixed part 13.
Wherein, first mounting portion 21 of the connection structure 2 is installed on include: in the mounting groove 11 will be described
First mounting portion 21 of connection structure 2 is slided along the second direction to the head of the unmanned plane.
Connection structure 2 and the assembly and disassembly method of unmanned plane are same with the above-mentioned embodiment, and details are not described herein.
Unmanned plane and its assemble method provided by the invention make the first mounting portion 21 exist by pressing the second mounting portion 22
Sliding in mounting groove 11 forms the mode that the first holding section 12 and the second holding section 23 overlap, and the first holding section 12 is played
To the position-limiting action of the second holding section 23, fixed connection structure 2 in a first direction, then the second fixed part 24 is fixed on first
On fixed part 13, so that fixed connection structure 2 in a second direction, easy to disassemble and install.
The above embodiment is only the preferred embodiment of the present invention, and the scope of protection of the present invention is not limited thereto,
The variation and replacement for any unsubstantiality that those skilled in the art is done on the basis of the present invention belong to institute of the present invention
Claimed range.
Claims (13)
1. a kind of unmanned plane, which is characterized in that including fuselage and connection structure, the fuselage is equipped with for installing the connection
The mounting groove of structure, the mounting groove is interior to be equipped with the first holding section and the first fixed part；The connection structure includes the first installation
Portion and the second mounting portion extended from the inclination of one end of first mounting portion, first mounting portion are equipped with the second holding section,
Second mounting portion is equipped with the second fixed part far from one end of first mounting portion；First holding section and described second
Holding section is matched to fix the connection structure in a first direction, and second fixed part is fixed to first fixed part
On to fix the connection structure in a second direction, the first direction is vertical with the second direction.
2. unmanned plane as described in claim 1, which is characterized in that first holding section be from the side wall of the mounting groove to
First protrusion of interior extension, second holding section are from outwardly extending second protrusion in the side of first mounting portion.
3. unmanned plane as described in claim 1, which is characterized in that be formed in first mounting portion and second mounting portion
Between angle be obtuse angle.
4. unmanned plane as described in claim 1, which is characterized in that the unmanned plane further includes fastener, and described first is fixed
Portion is equipped with the first mounting hole, and second fixed part is equipped with the second mounting hole, and the fastener is arranged in the first mounting hole
With the second mounting hole second fixed part to be fixed on first fixed part.
5. unmanned plane as described in claim 1, which is characterized in that second fixed part is and second mounting portion is movable
The elastic card fastener of connection, first fixed part are the card slot matched with the elastic card fastener.
6. unmanned plane as described in claim 1, which is characterized in that the unmanned plane further includes being installed in the connection structure
For installing the holder of photographic device.
7. unmanned plane as claimed in claim 6, which is characterized in that the connection structure further includes for installing the holder
Third mounting portion, the third mounting portion is set to first mounting portion and second mounting portion is formed by the interior of angle
Side, one end of the third mounting portion are installed on the one end of first mounting portion far from second mounting portion, the third
The other end of mounting portion is installed on the one end of second mounting portion far from first mounting portion.
8. unmanned plane as claimed in claim 7, which is characterized in that the connector further includes being connected to third mounting portion and institute
Second for stating the first shock absorber part between the first mounting portion and being connected between the third mounting portion and second mounting portion
Shock absorber part.
9. unmanned plane as claimed in claim 8, which is characterized in that the quantity of first shock absorber part be two, described second
The quantity of shock absorber part is two；The third mounting portion includes mounting portion ontology and four connectors, four connectors by
To extending to form on the outside of the mounting portion ontology, two of them connector passes through two respectively at the both ends of the mounting portion ontology
First shock absorber part is installed on the two sides of first mounting portion, other two connector passes through two described second respectively and subtracts
Shake part is installed on the two sides of second mounting portion.
10. unmanned plane as claimed in claim 7, which is characterized in that the connector further includes being set to first mounting portion
Third shock absorber part away from the side of the third mounting portion.
11. unmanned plane as described in claim 1, which is characterized in that be equipped with and the first mounting portion phase in the mounting groove
The guide groove of adaptation.
12. a kind of assemble method of unmanned plane as described in claim 1 characterized by comprising
First mounting portion of the connection structure is installed in the mounting groove so that first holding section with it is described
Second holding section is not overlapped in this second direction；
Make moving to the slot bottom of the mounting groove until described close to one end of second mounting portion for first mounting portion
Second holding section and first holding section be not be overlapped in said first direction；
Along the second direction push second mounting portion so that second holding section with first holding section described
It is least partially overlapped in second direction；
Second fixed part is fixed on first fixed part.
13. assemble method as claimed in claim 12, which is characterized in that pacify first mounting portion of the connection structure
Loaded on including: in the mounting groove
First mounting portion of the connection structure is slided along the second direction to the head of the unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910576816.1A CN110329525A (en) | 2019-06-28 | 2019-06-28 | A kind of unmanned plane and its assemble method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910576816.1A CN110329525A (en) | 2019-06-28 | 2019-06-28 | A kind of unmanned plane and its assemble method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110329525A true CN110329525A (en) | 2019-10-15 |
Family
ID=68143619
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910576816.1A Pending CN110329525A (en) | 2019-06-28 | 2019-06-28 | A kind of unmanned plane and its assemble method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110329525A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022095209A1 (en) * | 2020-11-09 | 2022-05-12 | 深圳市大疆创新科技有限公司 | Mounting bracket, bump assembly, and mechanical device |
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| CN106068226A (en) * | 2015-05-19 | 2016-11-02 | 深圳市大疆创新科技有限公司 | Vibration absorber, The Cloud Terrace and apply the unmanned vehicle of this The Cloud Terrace |
| CN106029503A (en) * | 2015-07-02 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Stop device and unmanned aerial vehicle having the same |
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| WO2022095209A1 (en) * | 2020-11-09 | 2022-05-12 | 深圳市大疆创新科技有限公司 | Mounting bracket, bump assembly, and mechanical device |
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Address after: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Applicant after: Shenzhen daotong intelligent Aviation Technology Co.,Ltd. Address before: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Applicant before: AUTEL ROBOTICS Co.,Ltd. |