KR20170040877A - Drone which can be disassembled - Google Patents
Drone which can be disassembled Download PDFInfo
- Publication number
- KR20170040877A KR20170040877A KR1020150140079A KR20150140079A KR20170040877A KR 20170040877 A KR20170040877 A KR 20170040877A KR 1020150140079 A KR1020150140079 A KR 1020150140079A KR 20150140079 A KR20150140079 A KR 20150140079A KR 20170040877 A KR20170040877 A KR 20170040877A
- Authority
- KR
- South Korea
- Prior art keywords
- frame
- corner member
- rod
- rods
- subframe
- Prior art date
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Classifications
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- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
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- B64C2201/024—
-
- B64C2201/108—
-
- B64C2201/162—
Abstract
The present invention relates to a main frame, A subframe detachably coupled to the main frame, the subframe configured to swing relative to the main frame; And a rotor detachably mounted to the sub-frame.
Description
The present invention relates to a dron which is easy to disassemble and assemble.
Generally, a drone is a generic term for an unmanned aerial vehicle (UAV) or a helicopter-type aeronautical vehicle (UAV) capable of flying and steerable by induction of radio waves without a pilot.
The drones are used for military purposes, as targets for practice shooting, or for reconnaissance, surveillance and anti-submarine attacks. Before and after the 2010 period, it has been used in various civilian and military applications.
In the private sector, there are courier services using drones, broadcast photography using drones, hobby video shooting using drones, and training on drones.
During these uses, it is also possible to train and hobbies that the drones are made by the general public and students themselves. However, in order to produce the drones, a tool for coupling between the parts is necessary.
It is an object of the present invention to provide a disassembly and assembly type dron that can be easily assembled and disassembled without tools.
According to an aspect of the present invention, there is provided a disassembled and assembled type dron comprising: a main frame; A subframe detachably coupled to the main frame, the subframe configured to swing relative to the main frame; And a rotor detachably installed in the subframe.
Wherein the main frame includes an upper frame and a side frame, the sub frame being swingably coupled to the upper frame such that the swing between a first state parallel to the side frame and a second state parallel to the upper frame, . ≪ / RTI >
Here, the side frame may be configured to define a receiving space, and the subframe may be located in the receiving space in the first state.
Here, the receiving space may be an open area.
Here, a plurality of side frames may be provided, and the plurality of side frames may be provided to correspond to the plurality of side frames.
Here, the plurality of side frames may be arranged to form a polygon.
Here, the subframe may include a side stopper that hung on the side frame in the first state, causing the subframe to stop in the first state.
Here, the upper frame may include a top stopper that catches the subframe in the second state, and stops the subframe in the second state.
Here, the sub-frame may further include a fixing module for fixing the sub-frame to the side frame as the sub-frame is swung from the second state to the first state.
Here, the fixing module may include: a metal piece installed on the side frame; And a magnet installed in the subframe and corresponding to the metal piece.
The fixing module may further include an elastic body provided on the side frame and elastically supporting the metal piece.
The fixing module may further include a housing that houses the elastic body and is installed in the side frame.
Here, the upper frame includes a plurality of upper rods; And an upper corner member to which two adjacent upper rods of the plurality of upper rods are fixed, respectively.
Here, the upper corner member may include two upper insertion holes into which the two adjacent upper rods are inserted, respectively.
Here, the upper corner member may include a coupling protrusion, and the upper frame may further include a mounting board having a coupling groove for coupling the coupling protrusion.
Here, the subframe may include a base having a rotary tube rotatably receiving the upper rod; A duct connected to the base; And a mounting base which is located in the duct and on which the rotor is mounted.
Here, the subframe may further include a link extending from the duct to the mount for connecting the mount to the duct.
Here, the rotary tubes are provided in pairs on the upper rods, and the connecting rods include a reference bar extending from the lower region side of the side frame to the mounting; And a pair of reinforcing bars extending from the mounting at positions corresponding to the pair of rotating tubes and thicker than the mover bars.
Here, the side frame may include a first side rod arranged in a direction intersecting with an arrangement direction of the upper rods, and the upper corner member may further include a side insertion hole into which the first side rod is inserted have.
Here, the side frame may include: a second side rod arranged in a direction crossing the arrangement direction of the first side rods; And a side corner member for fixing the first side rod and the second side rod.
Here, the side corner member may include a coupling groove which is opened downward.
The upper corner member may include a fastening protrusion formed in a size to be inserted into the fastening groove and projecting upward at a position corresponding to the fastening groove.
According to the disassembly and assembly type dron according to the present invention, the dron can be easily assembled and disassembled without tools.
By doing this, students can build up and break down the drones, strengthening their understanding of the drones.
1 is a perspective view showing a first state of a disassembly and
FIG. 2 is a perspective view showing a state in which the disassembled and assembled
3 is an exploded perspective view of the disassembly and
4 is a perspective view for explaining a state in which the disassembly and
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, a disassembled and assembled drone according to a preferred embodiment of the present invention will be described in detail with reference to the accompanying drawings. In the present specification, the same or similar reference numerals are given to different embodiments in the same or similar configurations.
FIG. 1 is a perspective view showing a first state of a disassembled and assembled
Referring to these drawings, the disassembled and assembled
The
The
And the
The
The
The
The
The
The
The
The space defined by the
The
The
Specifically, the
The
The
The mounting
The connecting
The
The fixing
The
The
The
The
According to this configuration, when power is applied to the
At this time, while the
As the
When power supply to the
Since the
Further, while the
The disassembling and assembling process of the above disassembly and
3 is an exploded perspective view of the disassembly and assembly type drones 100 of FIG.
Referring to this figure, the
The
The
An engaging
The configuration of the
According to this configuration, the
The other end of the
The mounting
This completes assembly of the
In order to assemble the
The
Next, a structure for stacking the
4 is a perspective view for explaining a state in which the disassembly and assembly type drones 100 of FIG. 1 are stacked.
Referring to this figure, the upper surface of the
Corresponding to the
The
According to this construction, when the plurality of
Thereby, the
The disassembly and assembly type drones as described above are not limited to the construction and the operation of the embodiments described above. The embodiments may be configured so that all or some of the embodiments may be selectively combined so that various modifications may be made.
100: disassembled and assembled type drone 110: main frame
111: upper frame 112: upper rod
113: upper corner member 115: mounting board
121: side frame 122: first side load
123: second side rod 125: side corner member
130: Subframe 131: Base
133: duct 135: mounting base
137: connecting rod 150: rotor
170: fixed module 171: metal piece
173: Magnet 175: Elastic body
177: Housing
Claims (12)
A subframe detachably coupled to the main frame, the subframe configured to swing relative to the main frame; And
And a rotor detachably mounted to the sub-frame.
The main frame includes an upper frame and a side frame,
Wherein the subframe is swingably coupled to the upper frame such that it is swingable between a first condition parallel to the side frame and a second condition parallel to the upper frame.
Wherein the upper frame comprises:
A plurality of upper rods; And
And an upper corner member to which two adjacent upper rods of the plurality of upper rods are fixed, respectively.
The upper corner member
And two upper insertion holes into which the two adjacent upper rods are respectively inserted.
Wherein the upper corner member includes an engaging projection,
Wherein the upper frame further comprises a mounting board having an engaging groove for engaging the engaging projection.
The sub-
A base having a rotary tube rotatably receiving the upper rod;
A duct connected to the base; And
And a mounting base located within the duct and on which the rotor is mounted.
The sub-
Further comprising a link extending from the duct to the mounting to connect the mounting bracket to the duct.
Wherein the rotary tube is provided in a pair in the upper rod,
The connecting rod includes:
A reference bar extending from the lower region side of the side frame to the mounting; And
And a pair of reinforcing bars extending from the mounting at positions corresponding to the pair of rotating tubes and thicker than the mover bars.
The side frame includes a first side rod arranged in a direction intersecting with an arrangement direction of the upper rods,
Wherein the upper corner member further comprises a side insertion hole into which the first side rod is inserted.
The side frame
A second side rod arranged in a direction intersecting with an arrangement direction of the first side rods; And
And a side corner member for fixing the first side rod and the second side rod.
The side corner member
And a fastening groove that is opened toward the lower side,
The upper corner member
And a fastening protrusion formed in a size to be inserted into the fastening groove and protruding upward at a position corresponding to the fastening groove.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150140079A KR20170040877A (en) | 2015-10-06 | 2015-10-06 | Drone which can be disassembled |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150140079A KR20170040877A (en) | 2015-10-06 | 2015-10-06 | Drone which can be disassembled |
Publications (1)
Publication Number | Publication Date |
---|---|
KR20170040877A true KR20170040877A (en) | 2017-04-14 |
Family
ID=58579510
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020150140079A KR20170040877A (en) | 2015-10-06 | 2015-10-06 | Drone which can be disassembled |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR20170040877A (en) |
-
2015
- 2015-10-06 KR KR1020150140079A patent/KR20170040877A/en active IP Right Grant
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