CN212354376U - But quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting - Google Patents
But quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting Download PDFInfo
- Publication number
- CN212354376U CN212354376U CN202020665255.0U CN202020665255U CN212354376U CN 212354376 U CN212354376 U CN 212354376U CN 202020665255 U CN202020665255 U CN 202020665255U CN 212354376 U CN212354376 U CN 212354376U
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- wing
- fuselage
- aerial vehicle
- unmanned aerial
- motor
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Abstract
The utility model relates to a for military use unmanned aerial vehicle technical field specifically is a but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting, the reciprocating impact tunnel drilling machine comprises a machine body, the fuselage left and right sides all can be dismantled to connect and be provided with the wing, the fuselage front side is provided with the motor, the motor passes through the screw and is connected with the fuselage, motor front side output is connected with the screw, the fuselage rear side is provided with vertical tail and horizontal tail, vertical tail and horizontal tail all are connected with the fuselage through the connecting piece, the utility model discloses, through setting up wing fixing bolt and wing constant head tank, conveniently carry out the dismouting to the wing, when the wing receives the damage and the fuselage is intact, but the intact wing of quick replacement improves work efficiency, through setting up wing bracing piece and mounting groove, can strengthen the fastness of wing installation, the holistic stability of reinforcing unmanned.
Description
Technical Field
The utility model relates to a for military use unmanned air vehicle technical field specifically is a but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting.
Background
Unmanned Aircraft (Pilotless Aircraft), colloquially known as: unmanned planes, unmanned aerial vehicles, unmanned combat airplanes, and bee-type machines; the airplane is a wide-range remote control aircraft which does not need a pilot to pilot, and generally refers to an unmanned reconnaissance airplane in the military. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar.
Along with military unmanned aerial vehicle's development, the demand of each country in the world to military unmanned aerial vehicle increases fast, and traditional unmanned aerial vehicle volume is great relatively, and the unable adjustment of wing length causes conveying efficiency poor, and inconvenient single transportation is carried, consequently, to above current situation, but the urgent need develops a but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting to overcome not enough in the current practical application.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides a but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting, includes the fuselage, the fuselage left and right sides all can be dismantled and connect and be provided with the wing, the fuselage front side is provided with the motor, the motor passes through the screw and is connected with the fuselage, motor front side output is connected with the screw, the fuselage rear side is provided with vertical fin and horizontal tail, vertical fin and horizontal tail all are connected with the fuselage through the connecting piece.
As a further aspect of the present invention: the wing fixing bolt is rotatably connected to the left side and the right side of the fuselage, external threads are arranged on the outer side of the wing fixing bolt, wing positioning grooves corresponding to the wing fixing bolts are formed in the inner side of the wing, and internal threads are arranged on the inner side of the wing positioning grooves.
As a further aspect of the present invention: the front side of the wing fixing bolt is provided with a wing supporting rod fixedly connected with the fuselage, and the inner side of the wing is provided with a wing mounting groove corresponding to the wing supporting rod.
As a further aspect of the present invention: the wings, the fuselage, the horizontal tails and the vertical tails are all made of basswood plates.
As a further aspect of the present invention: the wing supporting rod and the wing fixing bolt are both made of carbon tubes.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the wing fixing bolts and the wing positioning grooves are arranged, so that the wings can be conveniently disassembled and assembled, when the wings are damaged and the body is intact, the intact wings can be quickly replaced, and the working efficiency is improved;
2. through setting up wing bracing piece and wing mounting groove, can strengthen the fastness of wing installation process, strengthen the holistic stability of unmanned aerial vehicle.
Drawings
Fig. 1 is a schematic structural view of a rapidly detachable individual combat unmanned aerial vehicle.
Fig. 2 is an exploded view of a rapidly detachable individual combat unmanned aerial vehicle.
In the figure: 1-wing, 2-fuselage, 3-motor, 4-propeller, 5-wing support rod, 6-wing fixing bolt, 7-horizontal tail, 8-vertical tail, 9-wing positioning groove and 10-wing mounting groove.
Detailed Description
The technical solution of the present patent will be described in further detail with reference to the following embodiments.
Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.
Example 1
Please refer to fig. 1-2, in the embodiment of the present invention, a fast detachable unmanned aerial vehicle for individual combat, comprises a body 2, the left and right sides of the body 2 are detachably connected to form wings 1, the front side of the body 2 is provided with a motor 3, the motor 3 is connected with the body 2 through screws, the output end of the front side of the motor 3 is connected with a propeller 4, the rear side of the body 2 is provided with a vertical tail 8 and a horizontal tail 7, and the vertical tail 8 and the horizontal tail 7 are both connected with the body 2 through connecting pieces.
Example 2
In this embodiment, 2 left and right sides of fuselage all rotate to connect and are provided with wing fixing bolt 6, the wing fixing bolt 6 outside is provided with the external screw thread, 1 inboard of wing is provided with the wing constant head tank 9 corresponding with wing fixing bolt 6, wing constant head tank 9 inboard is provided with the internal thread, through setting up wing fixing bolt 6 and wing constant head tank 9, conveniently carries out the dismouting to wing 1, when wing 1 received the damage and fuselage 2 is intact, but the intact wing 1 of quick replacement improves work efficiency.
In this embodiment, 6 front sides of wing fixing bolts are provided with the wing bracing piece 5 with fuselage 2 fixed connection, 1 inboard of wing is provided with the wing mounting groove 10 corresponding with wing bracing piece 5, through setting up wing bracing piece 5 and wing mounting groove 10, can strengthen the fastness of 1 installation of wing, strengthens the holistic stability of unmanned aerial vehicle.
In this embodiment, the wing 1, the fuselage 2, the horizontal tail 7 and the vertical tail 8 are all made of basswood boards.
In this embodiment, the wing support rod 5 and the wing fixing bolt 6 are both made of carbon tubes.
In this embodiment, be equipped with the spread groove on the connecting piece, the connecting piece passes through the spread groove and is connected with fuselage 2.
This but quick assembly disassembly's individual combat unmanned aerial vehicle through setting up wing fixing bolt 6 and wing constant head tank 9, conveniently carries out the dismouting to wing 1, when wing 1 receives the damage and fuselage 2 is intact, but intact wing 1 of quick replacement improves work efficiency, through setting up wing bracing piece 5 and wing mounting groove 10, can strengthen the fastness of 1 installation of wing, strengthens the holistic stability of unmanned aerial vehicle.
The utility model discloses a theory of operation is: the vertical tail 8 and the horizontal tail 7 are connected with the fuselage 2 through connecting grooves in a connecting piece, the wing positioning groove 9 in the wing 1 is connected with the wing fixing bolt 6 in the fuselage 2, the wing fixing bolt 6 is provided with external threads, the inner side of the wing positioning groove 9 is provided with internal threads corresponding to the external threads, when the wing 1 is installed, the wing supporting rod 5 is partially inserted into the wing mounting groove 10, then the wing fixing bolt 6 is rotated to be screwed into the wing positioning groove 9 until the wing supporting rod is locked, at the moment, the wing supporting rod 5 is completely inserted into the wing mounting groove 10, when the wing 1 is installed, the wing 1 is disassembled, the wing fixing bolt 6 is reversely rotated to be screwed out of the wing positioning groove 9, when the wing fixing bolt 6 and the wing positioning groove 9 are completely separated, the wing supporting rod 5 is pulled out from the wing mounting groove 10, and the.
The above is only the preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, without departing from the concept of the present invention, several modifications and improvements can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent.
Claims (5)
1. The utility model provides a but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting, includes fuselage (2), its characterized in that, fuselage (2) the left and right sides all can be dismantled to connect and be provided with wing (1), fuselage (2) front side is provided with motor (3), motor (3) are connected with fuselage (2) through the screw, motor (3) front side output is connected with screw (4), fuselage (2) rear side is provided with vertical fin (8) and horizontal tail (7), vertical fin (8) and horizontal tail (7) all are connected with fuselage (2) through the connecting piece.
2. The individual combat unmanned aerial vehicle capable of being rapidly disassembled and assembled as claimed in claim 1, wherein wing fixing bolts (6) are rotatably connected to the left side and the right side of the fuselage (2), external threads are arranged on the outer sides of the wing fixing bolts (6), wing positioning grooves (9) corresponding to the wing fixing bolts (6) are arranged on the inner sides of the wings (1), and internal threads are arranged on the inner sides of the wing positioning grooves (9).
3. The individual combat unmanned aerial vehicle capable of being rapidly disassembled and assembled as claimed in claim 2, wherein a wing support rod (5) fixedly connected with the fuselage (2) is arranged on the front side of the wing fixing bolt (6), and a wing mounting groove (10) corresponding to the wing support rod (5) is arranged on the inner side of the wing (1).
4. The individual combat unmanned aerial vehicle capable of being rapidly disassembled and assembled as claimed in claim 1, wherein the wings (1), the fuselage (2), the horizontal tail (7) and the vertical tail (8) are all made of basswood plates.
5. The individual combat unmanned aerial vehicle capable of being rapidly disassembled and assembled as claimed in claim 3, wherein the wing support rods (5) and the wing fixing bolts (6) are made of carbon tubes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020665255.0U CN212354376U (en) | 2020-04-27 | 2020-04-27 | But quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020665255.0U CN212354376U (en) | 2020-04-27 | 2020-04-27 | But quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212354376U true CN212354376U (en) | 2021-01-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020665255.0U Expired - Fee Related CN212354376U (en) | 2020-04-27 | 2020-04-27 | But quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212354376U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2759299C1 (en) * | 2021-03-12 | 2021-11-11 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Long-range unmanned aerial vehicle with drop wing |
-
2020
- 2020-04-27 CN CN202020665255.0U patent/CN212354376U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2759299C1 (en) * | 2021-03-12 | 2021-11-11 | Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Long-range unmanned aerial vehicle with drop wing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210115 Termination date: 20210427 |
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| CF01 | Termination of patent right due to non-payment of annual fee |