CN109747811A - Unmanned aerial vehicle body and vertical tail quick plug - Google Patents
Unmanned aerial vehicle body and vertical tail quick plug Download PDFInfo
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- CN109747811A CN109747811A CN201910222003.2A CN201910222003A CN109747811A CN 109747811 A CN109747811 A CN 109747811A CN 201910222003 A CN201910222003 A CN 201910222003A CN 109747811 A CN109747811 A CN 109747811A
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- vertical tail
- interface
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- peg
- circuit
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- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005194 fractionation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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- 230000004048 modification Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
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Abstract
The present invention relates to unmanned aerial vehicle bodies and vertical tail connecting component technical field, disclose a kind of unmanned aerial vehicle body and vertical tail quick plug, including vertical tail girder and connection-peg, the vertical tail girder is fixedly installed on vertical tail, and it is actively plugged in the connection-peg, the vertical tail girder sequentially passes through upper plate and lower plate, the upper plate and lower plate are arranged in parallel, and it is fixedly installed on vertical tail, the lower plate is equipped with circuit slot, is equipped with circuit plug with circuit slot corresponding position on the connection-peg；The quick plug vertical tail that circuit part plug while vertical tail girder quickly be plugged and fixed to be completed at the same time grafting, and more traditional inserting mode is more convenient.
Description
Technical field
The present invention relates to unmanned aerial vehicle bodies and vertical tail connecting component technical field, and in particular to unmanned aerial vehicle body and hang down
Straight tail quick plug.
Background technique
Unmanned plane is made of wing, fuselage, tailplane, vertical tail etc., vertical tail in unmanned plane cross wind flying,
Vertical tail deflects, to change the flight path of unmanned plane.When unmanned plane is installed, vertical tail is connected with fuselage
It connects, including mechanical connection and circuit connection.And traditional unmanned plane circuit plug is more troublesome by the way of independent grafting.This
Applicant devises this unmanned aerial vehicle body and vertical tail quick plug, so that vertical tail is quickly plugged and fixed in vertical tail
Circuit part plug is completed at the same time grafting while girder, and more traditional inserting mode is more convenient.
Summary of the invention
In view of the deficiencies of the prior art, the present invention intends to provide unmanned aerial vehicle body quickly to insert with vertical tail
Head, the quick plug vertical tail that circuit part plug while vertical tail girder quickly be plugged and fixed to be completed at the same time
Grafting, more traditional inserting mode are more convenient.
To achieve the goals above, the invention provides the following technical scheme:
Unmanned aerial vehicle body and vertical tail quick plug, including vertical tail girder and connection-peg, the vertical tail master
Beam is fixedly installed on vertical tail, and is actively plugged in the connection-peg, and the vertical tail girder sequentially passes through upper plate
And lower plate, the upper plate and lower plate are arranged in parallel, and are fixedly installed on vertical tail, and the lower plate is equipped with circuit slot, institute
It states and is equipped with circuit plug with circuit slot corresponding position on connection-peg.
In the present invention, it is preferred to, the connection-peg is equipped with the first interface, the second interface and third interface,
First interface is for vertical tail girder described in grafting；Second interface is used to dispose the circuit plug, and
The circuit plug penetrates through second interface and is connected to the circuit slot, realizes that fuselage circuit and vertical tail circuit connect
It is logical；The third interface penetrates through the connection-peg.
In the present invention, it is preferred to, circular columns are equipped in the connection-peg, the circular columns and first interface are total
Axis setting, and it is equipped with through-hole corresponding with the third interface；The vertical tail girder is hollow structure, is plugged in
On the outside of the circular columns, and it is equipped with through-hole corresponding with the third interface.
In the present invention, it is preferred to, the connection-peg is arranged with sleeve, and the sleeve is equipped with and the first interface, second
Interface and the corresponding through-hole of third interface.
In the present invention, it is preferred to, the quick plug further includes vertical tail secondary bar, and the vertical tail secondary bar is successively
Across the upper plate and the lower plate, and extend through to the sleeve.
In the present invention, it is preferred to, between the upper plate and the lower plate be equipped with fixed plate, described fixed plate one end with it is described
Upper plate connection, the other end are connect with the lower plate.
Compared with prior art, the beneficial effects of the present invention are:
Quick plug of the invention is fixed by vertical tail girder with vertical tail and connection-peg, the electricity set in connection-peg
Road plug is connected to the circuit slot in vertical tail, and the circuit system for realizing fuselage is connected to the circuit system of vertical tail,
To which the control system of unmanned plane can control vertical tail running and transmit electric power for vertical tail；Pass through vertical tail master again
Beam and vertical tail secondary bar realize the fixation with connection-peg；Vertical tail is plugged and fixed quickly in vertical end in this quick plug
Circuit part plug is completed at the same time grafting while wing girder, and more traditional inserting mode is more convenient.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of unmanned aerial vehicle body and vertical tail quick plug in the present invention.
Fig. 2 is the structure of unmanned aerial vehicle body and vertical tail girder and connection-peg in vertical tail quick plug in the present invention
Schematic diagram.
Fig. 3 is the fractionation structural representation of unmanned aerial vehicle body and vertical tail quick plug in the present invention.
Fig. 4 is the perspective view of the connection-peg of unmanned aerial vehicle body and vertical tail quick plug in the present invention.
Fig. 5 is the side view of Fig. 4.
Fig. 6 is cross-sectional view of the Fig. 5 at the section AA.
Fig. 7 is the main view of Fig. 4.
Fig. 8 is cross-sectional view of the Fig. 7 at the section BB.
Fig. 9 is the partial structural diagram of unmanned aerial vehicle body and vertical tail quick plug use state in the present invention.
In attached drawing: 1- vertical tail girder, 2- connection-peg, the first interface of 201-, the second interface of 202-, 203- third
Interface, 204- circular columns, 3- upper plate, 4- lower plate, 5- circuit slot, 6- circuit plug, 7- sleeve, 8- vertical tail secondary bar,
9- fixed plate.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
It should be noted that it can be directly on another component when component is referred to as " being fixed on " another component
Or there may also be components placed in the middle.When a component is considered as " connection " another component, it, which can be, is directly connected to
To another component or it may be simultaneously present component placed in the middle.When a component is considered as " being set to " another component, it
It can be and be set up directly on another component or may be simultaneously present component placed in the middle.Term as used herein is " vertical
", " horizontal ", "left", "right" and similar statement for illustrative purposes only.
Unless otherwise defined, all technical and scientific terms used herein and belong to technical field of the invention
The normally understood meaning of technical staff is identical.Term as used herein in the specification of the present invention is intended merely to description tool
The purpose of the embodiment of body, it is not intended that in the limitation present invention.Term " and or " used herein includes one or more phases
Any and all combinations of the listed item of pass.
Please referring also to Fig. 1 to Fig. 9, a better embodiment of the invention provide unmanned aerial vehicle body and quickly insert with vertical tail
Head, including vertical tail girder 1 and connection-peg 2, the vertical tail girder 1 are fixedly installed on vertical tail, and activity is inserted
Be connected in the connection-peg 2, the vertical tail girder 1 sequentially passes through upper plate 3 and lower plate 4, be pierced by lower plate 4 be plugged in it is described
In connection-peg 2；The upper plate 3 and lower plate 4 are arranged in parallel, and are fixedly installed on vertical tail, and upper plate 3 and lower plate 4 can be consolidated
The fixed vertical tail girder 1；The lower plate 4 is equipped with circuit slot 5, position corresponding with the circuit slot 5 on the connection-peg 2
It sets place and is equipped with circuit plug 6, the circuit slot 5 is connected to the circuit system of vertical tail, and circuit plug 6 is connected to the circuit of fuselage
System, when circuit plug 6 is plugged in circuit slot 5, the circuit system of fuselage is connected to the circuit system of vertical tail, thus
The control system of unmanned plane can control vertical tail running and transmit electric power for vertical tail.
In the present embodiment, the connection-peg 2 is equipped with the first interface 201, the second interface 202 and third grafting
Mouth 203, first interface 201 is for vertical tail girder 1 described in grafting, to pass through the fixed grafting of vertical tail girder 1
First 2；Second interface 202 is for disposing the circuit plug 6, and the circuit plug 6 penetrates through second interface
202 are connected to the circuit slot 5, realize fuselage circuit and vertical tail circuit communication；The third interface 203 penetrates through institute
Connection-peg 2 is stated, further, circular columns 204, the circular columns 204 and first interface are equipped in the connection-peg 2
201 are coaxially arranged, and are equipped with through-hole corresponding with the third interface 203；The vertical tail girder 1 is hollow knot
Structure is plugged in 204 outside of circular columns, and is equipped with through-hole corresponding with the third interface 203；Pass through third grafting
It is inserted on through-hole corresponding with the third interface 203 and vertical tail girder 1 with the third on mouth 203, circular columns 204
The corresponding through-hole of interface 203, sequentially passing through above-mentioned through-hole with bolt or bolt can be realized vertical tail girder 1 and connection-peg
2 fixation.
In the present embodiment, the connection-peg 2 is arranged with sleeve 7, and the sleeve 7 is equipped with and the first interface 201, the
Two interfaces 202 and the corresponding through-hole of third interface 203,7 inner hollow of sleeve can place the electricity of connection circuit plug 6
Line or other wiring.
In the present embodiment, the quick plug further includes vertical tail secondary bar 8, and the vertical tail secondary bar 8 is successively
It across the upper plate 3 and the lower plate 4, and extends through to the sleeve 7, with fixed vertical empennage and sleeve 7.
In the present embodiment, fixed plate 9, described 9 one end of fixed plate and institute are equipped between the upper plate 3 and the lower plate 4
The connection of upper plate 3 is stated, the other end is connect with the lower plate 4, and fixed plate 9 can be fixedly mounted on the upper plate 3 and the lower plate 4
Between, can also be actively plugged between the upper plate 3 and the lower plate 4, fixed plate 9 be in order to fix the upper plate 3 and it is described under
The position of plate 4 prevents its sliding.
Working principle:
In use, vertical tail girder 1 is fixedly installed on vertical tail first, upper plate 3 and lower plate are sequentially passed through
4, and upper plate 3 and lower plate 4 are fixedly installed on vertical tail, fixed plate 9 is fixedly mounted on the upper plate 3 and the lower plate 4
Between, prevent its sliding；Meanwhile 8 one end of vertical tail secondary bar is fixedly installed on vertical tail, the other end also sequentially passes through described
Upper plate 3 and the lower plate 4；
Then circuit plug 6 is penetrated through into second interface 202, sleeve 7 is arranged connection-peg 2, and circuit plug 6 is pierced by
Sleeve 7；Vertical tail secondary bar 8 is through in the sleeve 7 simultaneously, circuit plug 6 is plugged in circuit slot 5, vertical end
Wing girder 1 is plugged in the first interface 201, and vertical tail girder 1 is completed in three component grafting simultaneously and connection-peg 2 connects,
So that vertical tail is quickly plugged and fixed circuit part plug while vertical tail girder and is completed at the same time grafting, it is more traditional to insert
It is more convenient to connect mode.
Above description is the detailed description for the present invention preferably possible embodiments, but embodiment is not limited to this hair
Bright patent claim, it is all the present invention suggested by technical spirit under completed same changes or modifications change, should all belong to
In the covered the scope of the patents of the present invention.
Claims (6)
1. unmanned aerial vehicle body and vertical tail quick plug, including vertical tail girder (1) and connection-peg (2), the vertical end
Wing girder (1) is fixedly installed on vertical tail, and is actively plugged in the connection-peg (2), which is characterized in that described vertical
Empennage girder (1) sequentially passes through upper plate (3) and lower plate (4), and the upper plate (3) and lower plate (4) are arranged in parallel, and are fixedly installed in
On vertical tail, the lower plate (4) is equipped with circuit slot (5), position corresponding with circuit slot (5) on the connection-peg (2)
It sets place and is equipped with circuit plug (6).
2. unmanned aerial vehicle body according to claim 1 and vertical tail quick plug, which is characterized in that the connection-peg
(2) the first interface (201), the second interface (202) and third interface (203), first interface (201) are equipped with
For vertical tail girder (1) described in grafting；Second interface (202) is used to dispose the circuit plug (6), and described
Circuit plug (6) penetrates through second interface (202) and is connected to the circuit slot (5), realizes fuselage circuit and vertical end
Wing circuit communication；The third interface (203) penetrates through the connection-peg (2).
3. unmanned aerial vehicle body according to claim 2 and vertical tail quick plug, which is characterized in that the connection-peg
(2) circular columns (204) are equipped in, the circular columns (204) are coaxially arranged with first interface (201), and equipped with
The corresponding through-hole of the third interface (203)；The vertical tail girder (1) is hollow structure, is plugged in the circle
On the outside of column (204), and it is equipped with through-hole corresponding with third interface (203).
4. unmanned aerial vehicle body according to claim 1 and vertical tail quick plug, which is characterized in that the connection-peg
(2) it is arranged with sleeve (7), the sleeve (7) is equipped with and the first interface (201), the second interface (202) and third interface
(203) corresponding through-hole.
5. unmanned aerial vehicle body according to claim 4 and vertical tail quick plug, which is characterized in that the quick plug
It further include vertical tail secondary bar (8), the vertical tail secondary bar (8) sequentially passes through the upper plate (3) and the lower plate (4), and
It extends through to the sleeve (7).
6. unmanned aerial vehicle body according to claim 1 and vertical tail quick plug, which is characterized in that the upper plate (3)
And fixed plate (9) are equipped between the lower plate (4), described fixed plate (9) one end is connect with the upper plate (3), the other end and institute
State lower plate (4) connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910222003.2A CN109747811A (en) | 2019-03-22 | 2019-03-22 | Unmanned aerial vehicle body and vertical tail quick plug |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910222003.2A CN109747811A (en) | 2019-03-22 | 2019-03-22 | Unmanned aerial vehicle body and vertical tail quick plug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109747811A true CN109747811A (en) | 2019-05-14 |
Family
ID=66409188
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910222003.2A Pending CN109747811A (en) | 2019-03-22 | 2019-03-22 | Unmanned aerial vehicle body and vertical tail quick plug |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109747811A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110203373A (en) * | 2019-05-24 | 2019-09-06 | 成都飞机工业（集团）有限责任公司 | A kind of vertical horizontal tail detaching structure of unmanned plane |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB457454A (en) * | 1935-05-25 | 1936-11-25 | Leslie Everett Baynes | Improvements in and relating to aircraft controlling surfaces |
| CN206984312U (en) * | 2017-05-09 | 2018-02-09 | 昊翔电能运动科技(昆山)有限公司 | Empennage quick-disassembly structure |
| CN207658034U (en) * | 2017-12-22 | 2018-07-27 | 中科机器人科技有限公司 | A kind of small drone vertical fin quickly disconnects structure |
| CN208007268U (en) * | 2018-03-26 | 2018-10-26 | 北京京东尚科信息技术有限公司 | Aircraft |
| CN208119406U (en) * | 2018-05-02 | 2018-11-20 | 北京京东尚科信息技术有限公司 | Wing installation and aircraft with the wing installation |
| CN208165245U (en) * | 2018-03-22 | 2018-11-30 | 泉州市洛江奎芳保洁有限公司 | A kind of aircraft tail of the aerospace with function easy to disassemble |
| CN209776791U (en) * | 2019-03-22 | 2019-12-13 | 天津天航智远科技有限公司 | quick plug of unmanned aerial vehicle fuselage and perpendicular fin |
-
2019
- 2019-03-22 CN CN201910222003.2A patent/CN109747811A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB457454A (en) * | 1935-05-25 | 1936-11-25 | Leslie Everett Baynes | Improvements in and relating to aircraft controlling surfaces |
| CN206984312U (en) * | 2017-05-09 | 2018-02-09 | 昊翔电能运动科技(昆山)有限公司 | Empennage quick-disassembly structure |
| CN207658034U (en) * | 2017-12-22 | 2018-07-27 | 中科机器人科技有限公司 | A kind of small drone vertical fin quickly disconnects structure |
| CN208165245U (en) * | 2018-03-22 | 2018-11-30 | 泉州市洛江奎芳保洁有限公司 | A kind of aircraft tail of the aerospace with function easy to disassemble |
| CN208007268U (en) * | 2018-03-26 | 2018-10-26 | 北京京东尚科信息技术有限公司 | Aircraft |
| CN208119406U (en) * | 2018-05-02 | 2018-11-20 | 北京京东尚科信息技术有限公司 | Wing installation and aircraft with the wing installation |
| CN209776791U (en) * | 2019-03-22 | 2019-12-13 | 天津天航智远科技有限公司 | quick plug of unmanned aerial vehicle fuselage and perpendicular fin |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110203373A (en) * | 2019-05-24 | 2019-09-06 | 成都飞机工业（集团）有限责任公司 | A kind of vertical horizontal tail detaching structure of unmanned plane |
| CN110203373B (en) * | 2019-05-24 | 2022-04-08 | 成都飞机工业（集团）有限责任公司 | Structure is dismantled to unmanned aerial vehicle tail of hanging down |
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