CN109562834A - Reconfigurable modular assembly type unmanned vehicle - Google Patents
Reconfigurable modular assembly type unmanned vehicle Download PDFInfo
- Publication number
- CN109562834A CN109562834A CN201780046980.0A CN201780046980A CN109562834A CN 109562834 A CN109562834 A CN 109562834A CN 201780046980 A CN201780046980 A CN 201780046980A CN 109562834 A CN109562834 A CN 109562834A
- Authority
- CN
- China
- Prior art keywords
- mentioned
- aircraft
- body portion
- machine body
- assembly type
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/40—Modular UAVs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2211/00—Modular constructions of airplanes or helicopters
Abstract
The present invention relates to reconfigurable modular assembly type unmanned vehicles, in more detail, it is related to be in meet the shape of multiple-task by making the shape of multiple components of aircraft, to be reconfigurable into the reconfigurable modular assembly type unmanned vehicle of the aircraft of various shapes.Reconfigurable modular assembly type unmanned vehicle of the invention is characterised by comprising: center main body section plays the role of the fuselage of aircraft；Flank section, it is in a variety of shapes, in conjunction with the two sides for being set to above-mentioned center machine body portion；Empennage portion is set to the rear in above-mentioned center machine body portion；Promotion part is set to the front in above-mentioned center machine body portion, for providing thrust to above-mentioned aircraft；And interconnecting piece, for connecting above-mentioned center machine body portion and empennage portion, above-mentioned center machine body portion, flank section, empennage portion, promotion part and interconnecting piece are formed with modular assembly type, so as to be reconstructed into the aircraft of variform.An embodiment according to the present invention, the present invention provides can be by keeping multiple components of aircraft in a variety of shapes, to be reconfigurable into the reconfigurable modular assembly type unmanned vehicle of the aircraft in the shape for meeting multiple-task purpose.Also, the present invention provides the Modular assembled unmanned vehicle that the global shape of aircraft can be made to be deformed into various shapes by making all parts modularization.
Description
Technical field
The present invention relates to reconfigurable modular assembly type unmanned vehicles, and in more detail, being related to can be by making aircraft
Multiple components are in the shape for meeting multiple-task, to be reconfigurable into the reconfigurable modular assembly type of the aircraft of various shapes
Unmanned vehicle.
Background technique
In general, putting into a large amount of time in order to make aircraft that just there is the shape of optimization since development phase and exerting
Power, and after specified specific shape, change shape and is severely limited.In order to realize operation aspect convenience and
Mobility, the unmanned vehicle researched and developed recently reach miniaturization or realize modularization in a manner of removable particular device.But
Existing way belongs to the method for the purpose of improving mobility or operability mostly, exist can not change of flight device global shape
The problem of.
Summary of the invention
Technical problem
The present invention proposes that the purpose of the present invention is to provide can pass through in order to solve prior art problem as described above
Keep multiple components of aircraft in a variety of shapes, thus be reconfigurable into shape meet multiple-task purpose aircraft it is restructural
Modular assembled unmanned vehicle.
Also, the purpose of the present invention is to provide aircraft global shape can be made to deform by making all parts modularization
At the Modular assembled unmanned vehicle of various shapes.
Problem to be solved by this invention is not limited to problem mentioned above, the technical field of the invention it is general
Logical technical staff will be clearly understood that the other problems to be solved by this invention not referred in the present specification.
The means solved the problems, such as
Reconfigurable modular assembly type unmanned vehicle of the invention is characterised by comprising: center main body section plays winged
The effect of the fuselage of row device；Flank section, it is in a variety of shapes, in conjunction with the two sides for being set to above-mentioned center machine body portion；Empennage portion, setting
In the rear in above-mentioned center machine body portion；Promotion part is set to the front in above-mentioned center machine body portion, for providing to above-mentioned aircraft
Thrust；And interconnecting piece, for connecting above-mentioned center machine body portion and empennage portion, above-mentioned center machine body portion, flank section, empennage portion,
Promotion part and interconnecting piece are formed with modular assembly type, so as to be reconstructed into the aircraft of variform.
The effect of invention
An embodiment according to the present invention, the present invention provide can by keeping multiple components of aircraft in a variety of shapes, from
And it is reconfigurable into the reconfigurable modular assembly type unmanned vehicle that shape meets the aircraft of multiple-task purpose.
Also, present invention offer can make aircraft global shape be deformed into various shapes by making all parts modularization
Modular assembled unmanned vehicle.
Detailed description of the invention
Fig. 1 is the figure for showing the shape of reconfigurable modular assembly type unmanned vehicle of first embodiment of the invention.
Fig. 2 is a variety of shapes for showing the flank of reconfigurable modular assembly type unmanned vehicle of first embodiment of the invention
The figure of shape.
Fig. 3 is the figure for showing the shape of reconfigurable modular assembly type unmanned vehicle of second embodiment of the invention.
Fig. 4 is the figure for showing the shape of reconfigurable modular assembly type unmanned vehicle of third embodiment of the invention.
Fig. 5 is the lower shape for showing the reconfigurable modular assembly type unmanned vehicle of second embodiment of the invention
Figure.
Fig. 6 is the shape for showing the task device of reconfigurable modular assembly type unmanned vehicle of second embodiment of the invention
The figure of shape.
Specific embodiment
Below by the examples and drawings of record enumerate by technical problem present invention as described above, technical solution,
The details that The effect of invention is included.Referring to the embodiment being described in detail together with attached drawing, it will be expressly understood that arriving this hair
Bright advantage, feature and the method for realizing these advantages and features.
Hereinafter, will be explained in more detail with reference to the drawing the present invention.
As shown in Figures 1 to 6, the reconfigurable modular assembly type unmanned vehicle of the embodiment of the present invention includes center fuselage
Portion 10, flank section 20, empennage portion 30, promotion part 40 and interconnecting piece 50.
Firstly, the present invention is provided with center main body section 10.
Specifically, above-mentioned center machine body portion 10 is located at the center of aircraft, plays the role of fuselage.In above-mentioned center machine body portion
The 10 multiple important components for being internally provided with flight-control computer and battery etc..Above-mentioned center machine body portion 10 is as following
The part at the center that the multiple components that will be enumerated combine.Above-mentioned center machine body portion 10 includes task device dismounting portion 11.
Above-mentioned task device dismounting portion 11 is set to the downside in above-mentioned center machine body portion 10, can be to following of various shapes
Business equipment 60 is dismounted.
Then, the two sides in above-mentioned center machine body portion 10 are provided with flank section 20.It can make above-mentioned side according to the purpose of task
Alar part 20 is in a variety of shapes, and combines the two sides for being set to above-mentioned center machine body portion 10.
First embodiment
Specifically, as shown in Figure 1, above-mentioned flank section 20 is in the wing shapes of standard aircraft.
As shown in Fig. 2, the above-mentioned flank section 20 of the wing shapes with standard aircraft can be set to front and back
It is mode shown in part (a) such as Fig. 2 that length direction width becomes narrow gradually towards outside, only wide in front formation length direction
Spend mode shown in part (b) such as Fig. 2 of variation and only at (c) of rear formation length direction change width such as Fig. 2
Mode shown in part.
Second embodiment
Specifically, as shown in figure 3, above-mentioned flank section 20 for the quadrotor portion 70 of quadrotor type aircraft by forming.On
Stating quadrotor portion 70 is in form the shape of rotor in the two sides front and back in above-mentioned center machine body portion 10, in above-mentioned center machine body portion 10
Above-mentioned quadrotor portion 70 is set, for executing being suitable for vertical flight etc. of the task.
Then, empennage portion 30 is set at the rear in above-mentioned center machine body portion 10.
Specifically, the empennage of standard aircraft is played the role of in above-mentioned empennage portion 30.
Then, promotion part 40 is set in the front in above-mentioned center machine body portion 10.
Specifically, above-mentioned promotion part 40 provides thrust to above-mentioned aircraft, so as to make above-mentioned aircraft flight.
3rd embodiment
As shown in figure 4, above-mentioned promotion part 40 may be disposed at the rear in above-mentioned empennage portion 30.By the way that above-mentioned promotion part 40 is set
It is placed in the rear in above-mentioned empennage portion 30, can only be flown by above-mentioned promotion part 40 and empennage portion 30 to be reconstructed into.It is pushed away by above-mentioned
In the case where the rear for being set to above-mentioned empennage portion 30 into portion 40, the hole in the above-mentioned empennage portion 30 combined with following interconnecting pieces 50
It will be plugged.
In above-mentioned 3rd embodiment include above-mentioned empennage portion 30 and promotion part 40 aircraft be arranged it is small-sized following
Task device 60, for executing task.
Also, above-mentioned empennage portion 30 is set to the front of above-mentioned promotion part 40, so as to realize reconstruct.
Then, interconnecting piece 50 is set between above-mentioned center machine body portion 10 and empennage portion 30.
Specifically, as shown in Figure 1, above-mentioned interconnecting piece 50 is for connecting above-mentioned center machine body portion 10 and empennage portion 30.
Then, task device 60 is set in the lower part in above-mentioned center machine body portion 10.
Specifically, as shown in fig. 6, above-mentioned task device 60 is in a variety of shapes, and it is set to above-mentioned task device dismounting portion
11.Above-mentioned task device 60 setting in a variety of shapes according to the purpose of task is incorporated into above-mentioned task device dismounting portion
11.Above-mentioned task device 60 is mainly set to the flight in shape shown in above-mentioned first embodiment and second embodiment
Device.
Then, the present invention is provided with integrated type connector.
Specifically, the portion that above-mentioned integrated type connector is respectively formed in above-mentioned center machine body portion 10 and flank section 20 combines
The power supply and control signal of above-mentioned aircraft are played the role of while being transmitted in position.
Reconfigurable modular assembly type unmanned vehicle of the invention can be by making multiple components of above-mentioned aircraft in more
Kind shape, to be reconfigurable into the aircraft that shape meets multiple-task purpose.
Also, aircraft global shape can be made to be deformed into various shapes by making all parts modularization.
As described above, general technical staff of the technical field of the invention is not it is understood that changing skill of the invention
In the case where art thought or essential feature, technology knot present invention as described above can be realized with other specific embodiments
Structure.
It it will thus be appreciated that the embodiment described above is all illustrative in structure at all levels, and is not limited
, relative to detailed description, range is claimed by aftermentioned invention to embody in the scope of the present invention, is claimed from invention
The meaning of range, range and equivalents are derived to have altered and variant embodiment should be construed to include in model of the invention
Within enclosing.
The explanation of appended drawing reference
10: center main body section
11: task device dismounting portion
20: flank section
30: empennage portion
40: promotion part
50: interconnecting piece
60: task device
70: quadrotor portion
Claims (5)
1. a kind of reconfigurable modular assembly type unmanned vehicle, which is characterized in that
Include:
Center main body section plays the role of the fuselage of aircraft；
Flank section, it is in a variety of shapes, in conjunction with the two sides for being set to above-mentioned center machine body portion；
Empennage portion is set to the rear in above-mentioned center machine body portion；
Promotion part is set to the front in above-mentioned center machine body portion, for providing thrust to above-mentioned aircraft；And
Interconnecting piece, for connecting above-mentioned center machine body portion and empennage portion,
Above-mentioned center machine body portion, flank section, empennage portion, promotion part and interconnecting piece are formed with modular assembly type, so as to
It is reconstructed into the aircraft of variform.
2. reconfigurable modular assembly type unmanned vehicle according to claim 1, which is characterized in that
Task device including lower part that is in a variety of shapes and being set to above-mentioned center machine body portion,
The above-mentioned task device of setting can be replaced according to the purpose of task.
3. reconfigurable modular assembly type unmanned vehicle according to claim 1, which is characterized in that
Above-mentioned center machine body portion and flank section include the integrated type connector for being respectively formed at binding site,
Above-mentioned integrated type connector transmits the power supply and control signal of above-mentioned aircraft simultaneously.
4. reconfigurable modular assembly type unmanned vehicle according to claim 1, which is characterized in that various shapes it is upper
One of flank section shape is stated in quadrotor shape.
5. reconfigurable modular assembly type unmanned vehicle according to claim 1, which is characterized in that in above-mentioned center machine
It further include the task device dismounting portion for being dismounted to above-mentioned task device on the downside of body portion.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1020160097241A KR101883986B1 (en) | 2016-07-29 | 2016-07-29 | Reconfigurable Modular Prefabricated UAV |
| KR10-2016-0097241 | 2016-07-29 | ||
| PCT/KR2017/005943 WO2018021679A2 (en) | 2016-07-29 | 2017-06-08 | Reconfigurable module-type prefabricated unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109562834A true CN109562834A (en) | 2019-04-02 |
Family
ID=61017126
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780046980.0A Withdrawn CN109562834A (en) | 2016-07-29 | 2017-06-08 | Reconfigurable modular assembly type unmanned vehicle |
Country Status (3)
| Country | Link |
|---|---|
| KR (1) | KR101883986B1 (en) |
| CN (1) | CN109562834A (en) |
| WO (1) | WO2018021679A2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102012149B1 (en) * | 2019-01-16 | 2019-08-20 | 강동훈 | Module combination type radio control toy |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030066932A1 (en) * | 2001-09-27 | 2003-04-10 | Carroll Ernest A. | Miniature, unmanned aircraft with interchangeable data module |
| CN2923517Y (en) * | 2006-04-22 | 2007-07-18 | 深圳市京信通工贸有限公司 | Aircraft |
| US20080149758A1 (en) * | 2006-04-21 | 2008-06-26 | Colgren Richard D | Modular unmanned air-vehicle |
| CN202728576U (en) * | 2012-02-10 | 2013-02-13 | 田瑜 | Transformable composite aircraft formed by fixed wing and electric multi-propeller |
| CN102923296A (en) * | 2012-11-16 | 2013-02-13 | 中国航空工业集团公司西安飞机设计研究所 | Modularized unmanned aerial vehicle |
| CN204173154U (en) * | 2014-10-09 | 2015-02-25 | 中国航天空气动力技术研究院 | A kind of modularized combination type unmanned plane |
| CN204548499U (en) * | 2015-02-01 | 2015-08-12 | 范磊 | Modularization combined type many rotors hybrid power aircraft |
| WO2015157114A1 (en) * | 2014-04-11 | 2015-10-15 | Sada-Salinas Jaime G | Modular nacelles to provide vertical takeoff and landing (vtol) capabilities to fixed wing aerial vehicles, and associated systems and methods |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IL199009A (en) * | 2009-05-27 | 2013-11-28 | Israel Aerospace Ind Ltd | Air vehicle |
| KR20120082394A (en) | 2009-07-22 | 2012-07-23 | 에어로바이론먼트, 인크. | Reconfigurable aircraft |
| WO2011149544A1 (en) * | 2010-05-26 | 2011-12-01 | Aerovironment Inc. | Reconfigurable battery-operated vehicle system |
-
2016
- 2016-07-29 KR KR1020160097241A patent/KR101883986B1/en active IP Right Grant
-
2017
- 2017-06-08 WO PCT/KR2017/005943 patent/WO2018021679A2/en active Application Filing
- 2017-06-08 CN CN201780046980.0A patent/CN109562834A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030066932A1 (en) * | 2001-09-27 | 2003-04-10 | Carroll Ernest A. | Miniature, unmanned aircraft with interchangeable data module |
| US20080149758A1 (en) * | 2006-04-21 | 2008-06-26 | Colgren Richard D | Modular unmanned air-vehicle |
| CN2923517Y (en) * | 2006-04-22 | 2007-07-18 | 深圳市京信通工贸有限公司 | Aircraft |
| CN202728576U (en) * | 2012-02-10 | 2013-02-13 | 田瑜 | Transformable composite aircraft formed by fixed wing and electric multi-propeller |
| CN102923296A (en) * | 2012-11-16 | 2013-02-13 | 中国航空工业集团公司西安飞机设计研究所 | Modularized unmanned aerial vehicle |
| WO2015157114A1 (en) * | 2014-04-11 | 2015-10-15 | Sada-Salinas Jaime G | Modular nacelles to provide vertical takeoff and landing (vtol) capabilities to fixed wing aerial vehicles, and associated systems and methods |
| CN204173154U (en) * | 2014-10-09 | 2015-02-25 | 中国航天空气动力技术研究院 | A kind of modularized combination type unmanned plane |
| CN204548499U (en) * | 2015-02-01 | 2015-08-12 | 范磊 | Modularization combined type many rotors hybrid power aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| KR101883986B1 (en) | 2018-07-31 |
| WO2018021679A3 (en) | 2018-03-15 |
| KR20180013464A (en) | 2018-02-07 |
| WO2018021679A2 (en) | 2018-02-01 |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190402 |
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| WW01 | Invention patent application withdrawn after publication |