CN209776791U - quick plug of unmanned aerial vehicle fuselage and perpendicular fin - Google Patents
quick plug of unmanned aerial vehicle fuselage and perpendicular fin Download PDFInfo
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- CN209776791U CN209776791U CN201920371991.2U CN201920371991U CN209776791U CN 209776791 U CN209776791 U CN 209776791U CN 201920371991 U CN201920371991 U CN 201920371991U CN 209776791 U CN209776791 U CN 209776791U
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- vertical tail
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Abstract
The utility model relates to the technical field of connecting components of an unmanned aerial vehicle body and a vertical tail wing, and discloses a quick plug for the unmanned aerial vehicle body and the vertical tail wing, which comprises a vertical tail wing main beam and a plug connector, wherein the vertical tail wing main beam is fixedly arranged on the vertical tail wing and is movably inserted in the plug connector, the vertical tail wing main beam sequentially passes through an upper plate and a lower plate, the upper plate and the lower plate are arranged in parallel and are fixedly arranged on the vertical tail wing, the lower plate is provided with a circuit slot, and a circuit plug is arranged on the plug connector at a position corresponding to the circuit slot; the quick plug enables the vertical tail to be quickly plugged and fixed on the main beam of the vertical tail, and meanwhile, plugs of a circuit part are plugged simultaneously, so that the quick plug is more convenient and quick compared with a traditional plugging mode.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle fuselage and perpendicular fin adapting unit technical field, concretely relates to unmanned aerial vehicle fuselage and perpendicular fin quick plug.
Background
The unmanned aerial vehicle comprises wing, fuselage, horizontal fin, vertical fin etc. and vertical fin when the unmanned aerial vehicle crosswind flies, vertical fin takes place to deflect to change unmanned aerial vehicle's flight route. When unmanned aerial vehicle installs, its vertical fin is connected with the fuselage, including mechanical connection and circuit connection. And the traditional unmanned aerial vehicle circuit plug adopts the mode of individual grafting, and is comparatively troublesome. The applicant designs the rapid plug for the unmanned aerial vehicle body and the vertical tail wing, so that the vertical tail wing is rapidly inserted and fixed on the main beam of the vertical tail wing, and meanwhile, the plug of a circuit part is inserted and connected simultaneously, and the rapid plug is more convenient and rapid compared with a traditional insertion mode.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art exists, the utility model aims to provide an unmanned aerial vehicle fuselage and perpendicular fin quick plug, this quick plug make perpendicular fin peg graft fast fix in perpendicular fin girder circuit part plug accomplish simultaneously and peg graft, more convenient and fast than traditional grafting mode.
In order to achieve the above object, the present invention provides the following technical solutions:
Quick plug of unmanned aerial vehicle fuselage and perpendicular fin, including perpendicular fin girder and bayonet joint, perpendicular fin girder fixed mounting on perpendicular fin, and the activity peg graft in the bayonet joint, perpendicular fin girder passes upper plate and hypoplastron in proper order, upper plate and hypoplastron parallel arrangement, and fixed mounting are on perpendicular fin, the hypoplastron is equipped with the circuit slot, on the bayonet joint with circuit slot corresponds position department and is equipped with the circuit plug.
in the utility model, preferably, the plug is provided with a first plug interface, a second plug interface and a third plug interface, and the first plug interface is used for plugging the vertical tail girder; the second plug interface is used for arranging the circuit plug, and the circuit plug penetrates through the second plug interface to be communicated with the circuit slot, so that the communication between the body circuit and the vertical tail wing circuit is realized; the third interface is communicated with the plug connector.
In the present invention, preferably, a circular column is disposed in the plug, the circular column and the first plug are coaxially disposed, and a through hole corresponding to the third plug is disposed; the vertical tail wing main beam is of a hollow structure, is inserted outside the circular column and is provided with a through hole corresponding to the third insertion port.
The utility model discloses in, it is preferred, the bayonet joint cover is equipped with the sleeve, the sleeve is equipped with the through-hole that corresponds with first interface, second interface and third interface.
The utility model discloses in, preferably, quick plug still includes the vice pole of vertical fin, the vice pole of vertical fin passes in proper order the upper plate reaches the hypoplastron to extend and run through to in the sleeve.
The utility model discloses in, preferably, the upper plate reaches be equipped with the fixed plate down between the board, fixed plate one end with the upper plate is connected, its other end with the hypoplastron is connected.
Compared with the prior art, the beneficial effects of the utility model are that:
The utility model discloses a quick plug is fixed with vertical fin and connector through vertical fin girder, and the circuit plug that establishes in the connector communicates with the circuit slot in the vertical fin, realizes that the circuit system of fuselage communicates with the circuit system of vertical fin to the control system of unmanned aerial vehicle can control the operation of vertical fin and carry electric power for vertical fin; the fixing with the plug connector is realized through the vertical tail main beam and the vertical tail auxiliary rod; the quick plug enables the vertical tail to be quickly plugged and fixed on the main beam of the vertical tail, and meanwhile, plugs of the circuit part are plugged simultaneously, so that the quick plug is more convenient and quick compared with a traditional plugging mode.
Drawings
Fig. 1 is the utility model discloses well unmanned aerial vehicle fuselage and perpendicular fin quick plug's schematic structure diagram.
Fig. 2 is the utility model discloses in the structure schematic diagram of perpendicular fin girder and bayonet joint in the quick plug of well unmanned aerial vehicle fuselage and perpendicular fin.
Fig. 3 is the utility model discloses well unmanned aerial vehicle fuselage and perpendicular fin quick plug's split structure schematic diagram.
Fig. 4 is the utility model discloses well unmanned aerial vehicle fuselage and perpendicular fin quick plug's stereogram.
Fig. 5 is a side view of fig. 4.
fig. 6 is a cross-sectional view at AA of fig. 5.
Fig. 7 is a front view of fig. 4.
Fig. 8 is a cross-sectional view of fig. 7 at BB section.
Fig. 9 is the utility model discloses well unmanned aerial vehicle fuselage and perpendicular fin quick plug user state's local structure schematic diagram.
In the drawings: 1-vertical tail main beam, 2-plug connector, 201-first plug interface, 202-second plug interface, 203-third plug interface, 204-circular column, 3-upper plate, 4-lower plate, 5-circuit slot, 6-circuit plug, 7-sleeve, 8-vertical tail auxiliary rod and 9-fixing plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When a component is referred to as being "connected" to another component, it can be directly connected to the other component or intervening components may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Referring to fig. 1 to 9, a preferred embodiment of the present invention provides a fast plug for a fuselage and a vertical tail of an unmanned aerial vehicle, including a vertical tail girder 1 and a plug 2, wherein the vertical tail girder 1 is fixedly mounted on the vertical tail and movably plugged into the plug 2, the vertical tail girder 1 sequentially passes through an upper plate 3 and a lower plate 4, and penetrates out of the lower plate 4 to be plugged into the plug 2; the upper plate 3 and the lower plate 4 are arranged in parallel and fixedly arranged on the vertical tail, and the vertical tail main beam 1 can be fixed by the upper plate 3 and the lower plate 4; the lower plate 4 is provided with a circuit slot 5, a circuit plug 6 is arranged at a position, corresponding to the circuit slot 5, of the plug connector 2, the circuit slot 5 is communicated with a circuit system of the vertical tail fin, the circuit plug 6 is communicated with a circuit system of the machine body, when the circuit plug 6 is plugged into the circuit slot 5, the circuit system of the machine body is communicated with the circuit system of the vertical tail fin, and therefore a control system of the unmanned aerial vehicle can control the operation of the vertical tail fin and transmit electric power for the vertical tail fin.
In this embodiment, the plug 2 is provided with a first plug interface 201, a second plug interface 202 and a third plug interface 203, where the first plug interface 201 is used to plug the vertical tail girder 1, so as to fix the plug 2 through the vertical tail girder 1; the second jack 202 is used for arranging the circuit plug 6, and the circuit plug 6 penetrates through the second jack 202 to be communicated with the circuit slot 5, so that a machine body circuit is communicated with a vertical tail wing circuit; the third socket 203 penetrates through the plug 2, further, a circular column 204 is arranged in the plug 2, the circular column 204 and the first socket 201 are coaxially arranged, and a through hole corresponding to the third socket 203 is formed in the circular column 204; the vertical tail main beam 1 is of a hollow structure, is inserted outside the circular column 204 and is provided with a through hole corresponding to the third insertion port 203; through the third interface 203, the through hole corresponding to the third interface 203 on the circular column 204 and the through hole corresponding to the third interface 203 on the vertical tail main beam 1, the vertical tail main beam 1 and the plug 2 can be fixed by sequentially penetrating the through holes through bolts or bolts.
In this embodiment, the plug connector 2 is sleeved with a sleeve 7, the sleeve 7 is provided with through holes corresponding to the first plug port 201, the second plug port 202 and the third plug port 203, and the sleeve 7 is hollow and can accommodate an electric wire or other connection wires of the circuit plug 6.
In this embodiment, the quick connector further comprises a vertical tail auxiliary rod 8, and the vertical tail auxiliary rod 8 sequentially penetrates through the upper plate 3 and the lower plate 4 and extends into the sleeve 7 to fix the vertical tail and the sleeve 7.
In this embodiment, a fixing plate 9 is disposed between the upper plate 3 and the lower plate 4, one end of the fixing plate 9 is connected to the upper plate 3, and the other end thereof is connected to the lower plate 4, the fixing plate 9 may be fixedly installed between the upper plate 3 and the lower plate 4, or may be movably inserted between the upper plate 3 and the lower plate 4, and the fixing plate 9 is for fixing the positions of the upper plate 3 and the lower plate 4 to prevent the sliding thereof.
The working principle is as follows:
When in use, the main beam 1 of the vertical tail wing is fixedly arranged on the vertical tail wing, sequentially passes through the upper plate 3 and the lower plate 4, the upper plate 3 and the lower plate 4 are fixedly arranged on the vertical tail wing, and the fixing plate 9 is fixedly arranged between the upper plate 3 and the lower plate 4 to prevent the sliding; meanwhile, one end of the vertical tail auxiliary rod 8 is fixedly arranged on the vertical tail, and the other end of the vertical tail auxiliary rod sequentially penetrates through the upper plate 3 and the lower plate 4;
Then, the circuit plug 6 penetrates through the second jack 202, the sleeve 7 is sleeved with the plug connector 2, and the circuit plug 6 penetrates out of the sleeve 7; meanwhile, the vertical tail auxiliary rod 8 penetrates into the sleeve 7, the circuit plug 6 is plugged into the circuit slot 5, the vertical tail main beam 1 is plugged into the first plugging port 201, the three components are simultaneously plugged to complete connection of the vertical tail main beam 1 and the plugging head 2, so that the vertical tail is quickly plugged and fixed on the vertical tail main beam, and meanwhile, plugging of partial plugs of the circuit is simultaneously completed, and the method is more convenient and faster than a traditional plugging method.
The above description is for the detailed description of the preferred possible embodiments of the present invention, but the embodiments are not intended to limit the scope of the present invention, and all equivalent changes or modifications accomplished under the technical spirit suggested by the present invention should fall within the scope of the present invention.
Claims (6)
1. Quick plug of unmanned aerial vehicle fuselage and perpendicular fin, including perpendicular fin girder (1) and bayonet joint (2), perpendicular fin girder (1) fixed mounting is on perpendicular fin, and the activity peg graft in bayonet joint (2), its characterized in that, upper plate (3) and hypoplastron (4) are passed in proper order in perpendicular fin girder (1), upper plate (3) and hypoplastron (4) parallel arrangement, and fixed mounting is on perpendicular fin, hypoplastron (4) are equipped with circuit slot (5), on bayonet joint (2) with circuit slot (5) correspond position department and are equipped with circuit plug (6).
2. The unmanned aerial vehicle fuselage and vertical tail quick plug according to claim 1, characterized in that a first interface (201), a second interface (202) and a third interface (203) are provided on the plug (2), the first interface (201) is used for plugging the vertical tail main beam (1); the second plug interface (202) is used for accommodating the circuit plug (6), and the circuit plug (6) penetrates through the second plug interface (202) to be communicated with the circuit slot (5), so that a machine body circuit is communicated with a vertical tail wing circuit; the third interface (203) penetrates through the plug connector (2).
3. The unmanned aerial vehicle fuselage and vertical tail fin quick plug as claimed in claim 2, wherein a circular column (204) is provided in the plug connector (2), the circular column (204) is coaxial with the first plug port (201), and a through hole corresponding to the third plug port (203) is provided; the vertical tail main beam (1) is of a hollow structure, is inserted into the outer side of the circular column (204), and is provided with a through hole corresponding to the third insertion port (203).
4. The unmanned aerial vehicle fuselage and vertical tail fin quick plug as claimed in claim 1, wherein the plug connector (2) is sleeved with a sleeve (7), and the sleeve (7) is provided with through holes corresponding to the first plug interface (201), the second plug interface (202) and the third plug interface (203).
5. The unmanned aerial vehicle fuselage and vertical tail quick plug of claim 4, characterized in that, the quick plug further comprises a vertical tail auxiliary rod (8), the vertical tail auxiliary rod (8) passes through the upper plate (3) and the lower plate (4) in sequence and extends through into the sleeve (7).
6. The unmanned aerial vehicle fuselage and vertical tail fin quick plug according to claim 1, characterized in that a fixing plate (9) is arranged between the upper plate (3) and the lower plate (4), one end of the fixing plate (9) is connected with the upper plate (3), and the other end is connected with the lower plate (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920371991.2U CN209776791U (en) | 2019-03-22 | 2019-03-22 | quick plug of unmanned aerial vehicle fuselage and perpendicular fin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920371991.2U CN209776791U (en) | 2019-03-22 | 2019-03-22 | quick plug of unmanned aerial vehicle fuselage and perpendicular fin |
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| Publication Number | Publication Date |
|---|---|
| CN209776791U true CN209776791U (en) | 2019-12-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920371991.2U Active CN209776791U (en) | 2019-03-22 | 2019-03-22 | quick plug of unmanned aerial vehicle fuselage and perpendicular fin |
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| CN (1) | CN209776791U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
-
2019
- 2019-03-22 CN CN201920371991.2U patent/CN209776791U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109747811A (en) * | 2019-03-22 | 2019-05-14 | 天津天航智远科技有限公司 | Unmanned aerial vehicle body and vertical tail quick plug |
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