CN107972871A - A kind of unmanned plane undercarriage and unmanned plane for launching crawl object - Google Patents
A kind of unmanned plane undercarriage and unmanned plane for launching crawl object Download PDFInfo
- Publication number
- CN107972871A CN107972871A CN201711428578.7A CN201711428578A CN107972871A CN 107972871 A CN107972871 A CN 107972871A CN 201711428578 A CN201711428578 A CN 201711428578A CN 107972871 A CN107972871 A CN 107972871A
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- Prior art keywords
- unmanned plane
- branch
- brace
- launching
- control mechanism
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- 230000007246 mechanism Effects 0.000 claims abstract description 45
- 238000009434 installation Methods 0.000 claims abstract description 15
- 238000004891 communication Methods 0.000 claims abstract description 6
- 230000009471 action Effects 0.000 claims abstract description 5
- 230000010365 information processing Effects 0.000 claims description 5
- 235000008429 bread Nutrition 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 8
- 230000008569 process Effects 0.000 description 5
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manipulator (AREA)
Abstract
The invention discloses a kind of unmanned plane undercarriage and unmanned plane for launching crawl object, unmanned plane undercarriage includes：Master arm, linkage mechanism, lockable mechanism and control mechanism, master arm include branch's brace of more than three, and for installing the mounting portion of each branch's brace, each branch's brace is movably connected on mounting portion；Linkage mechanism is embedded in each branch's brace, is connected with control mechanism, the digital signal that control mechanism is sent is converted into action command, so that each branch's brace open or close；Lockable mechanism is embedded in each branch's brace, is connected with control mechanism, and after each branch's brace has performed order, lockable mechanism is by each branch's brace locking；Control mechanism is embedded in mounting portion, carries out wireless communication with ground control station, and then control each branch's brace open or close.Unmanned plane includes：Unmanned plane body, Fast Installation face, and two above-mentioned unmanned plane undercarriages.Unmanned plane is the method can be widely used in rescue, deliver, taking the fields such as thing.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of landing gear that takes off can be used for the quick nothing launched and capture object
It is man-machine.
Background technology
Unmanned plane industry develops rapidly, and unprecedented facility is brought to industry-by-industry.With widely using for unmanned plane
There is the indeterminable problem of many aircrafts, such as Fast Fixed-point crawl, which is thrown, throws.
Existing unmanned machine equipment can only rely on binding, the mode such as fixed gondola, with can achieve the goal but because preparing
Time is grown, heavy, substantially reduces work efficiency.
The content of the invention
The defects of work efficiency is low during in order to overcome existing unmanned plane fixed point to take the thing to jettisoning, the present invention provides one kind and can throw
The unmanned plane undercarriage and unmanned plane of crawl object are put, versatile, easy to carry, a key prepares, and rapidly and efficiently solves fixed point
The problem of throwing is thrown in crawl, be can be widely used for unmanned plane and is rescued, delivers, taking the fields such as thing.
The technical solution that the present invention solves above-mentioned technical problem is as follows：A kind of unmanned plane for launching crawl object rises and falls
Frame, including：Master arm, linkage mechanism, lockable mechanism and control mechanism, wherein, the master arm includes three or more
In three branch's braces, and for installing the mounting portion of each branch's brace, each branch's brace is movably connected on the mounting portion；Institute
State linkage mechanism to be embedded in each branch's brace, be connected with the control mechanism, the numeral that the control mechanism is sent is believed
Number action command is converted into, so that each branch's brace open or close；The lockable mechanism is embedded in each branch's brace, with institute
State control mechanism to be connected, after each branch's brace has performed order, lockable mechanism is by each branch's brace locking；The control machine
Structure is embedded in the mounting portion, and wireless communication is carried out with ground control station, sends and receives data, and then control each sub-support
Arm open or close.
Based on the above technical solutions, the present invention can also be improved as follows.
Preferably, the unmanned plane undercarriage further includes information process unit, and described information processing unit is embedded at described
In mounting portion, it is connected with the control mechanism, also carries out wireless communication with ground control station.
Preferably, the accessible information of described information processing unit includes：Positional information, audio/video information, data message
And sound, Qiang Guang, smog and the intercommunication information of emergency.
Preferably, the end of each branch's brace of the master arm is also equipped with anti-slip rubber.
The present invention also provides a kind of unmanned plane for launching crawl object, including：Unmanned plane body, Fast Installation face, and
Two above-mentioned unmanned plane undercarriages for launching crawl object, wherein, the Fast Installation face is used to connect the unmanned plane
Undercarriage and the unmanned plane body.
Preferably, the Fast Installation face includes：Sliding supporting bar and foot stool on the sliding supporting bar are fast
Connection device, the face of the upside of the sliding supporting bar are equipped with slide, and the body of rod is offered to be adapted to the mounting portion of unmanned plane undercarriage
Mounting hole；The foot stool quick access device is the bar of more than two, slideably, is vertically arranged on the cunning in the horizontal direction
On the slide of dynamic supporting rod, so that unmanned plane body is installed.
Compared with prior art, the present invention has the following technical effect that：
1st, undercarriage crawl throw throw it is quick and convenient, it is versatile, be mountable on the market it is most it is industrial nobody
Machine；
2nd, unmanned plane can be widely applied to the every profession and trades such as public security, fire-fighting, rescue and electric power.
Brief description of the drawings
Fig. 1 a are the Unclosing structure schematic diagram of the unmanned plane undercarriage for launching crawl object of the present invention；
Fig. 1 b are the closing structure schematic diagram of the unmanned plane undercarriage for launching crawl object of the present invention；
Fig. 2 is the structure diagram in the Fast Installation face of the unmanned plane undercarriage for launching crawl object of the present invention；
Fig. 3 is the structure diagram of the unmanned plane for launching crawl object of the present invention；
In the accompanying drawings, the list of designations represented by each label is as follows：
1 master arm
2 linkage mechanisms
3 lockable mechanisms
4 sliding supporting bars
5 foot stool quick access devices
6 unmanned plane bodies
Embodiment
The principle and features of the present invention will be described below with reference to the accompanying drawings, and the given examples are served only to explain the present invention, and
It is non-to be used to limit the scope of the present invention.
It refer to shown in Fig. 1 a and 1b, wherein, Fig. 1 a are the unmanned plane undercarriage for launching crawl object of the present invention
Unclosing structure schematic diagram, Fig. 1 b are the closing structure schematic diagram of the unmanned plane undercarriage for launching crawl object of the present invention.Institute
Stating unmanned plane undercarriage includes：Master arm 1, linkage mechanism 2, lockable mechanism 3, control mechanism and information process unit (figure
Do not show), wherein,
The master arm 1 preferably includes three branch's braces, can also be more than three according to the actual requirements；The main support
Arm 1 further includes the mounting portion for installing each branch's brace, and each branch's brace is movably connected on the mounting portion, thus, each point
It is used for supporting ground when support arm is opened and decontrols object, be used for during closure capturing object, can be adjusted according to crawl article size
Opening degree；
The linkage mechanism 2 is embedded in each branch's brace, is connected with the control mechanism, for control mechanism to be sent out
The digital signal sent is converted into action command；
The lockable mechanism 3 is embedded in each branch's brace, is connected with the control mechanism, for ensureing master arm
The reliability of Zhong Ge branches brace folding, after master arm has performed order, lockable mechanism, will be each by master arm locking
Branch's brace locking；
The control mechanism is embedded in the mounting portion of the master arm 1, is used to carry out with ground control station after energization
Communication, sends and receives data, to control the folding of master arm；
Described information processing unit is the prior art, and information therein can include：Positional information, audio/video information, data
The sound of information and emergency, Qiang Guang, smog and intercommunication etc., it is full-featured；It is independent that information can both pass ground back after processing
Control uses, and also linkage unmanned plane uses.Ground control station can be analyzed according to the data that information process unit is sent, so
After send commands to information process unit, ground order is sent to control mechanism by information process unit again, and then is sent to joining
Motivation structure, linkage mechanism 2 are performed according to order, are controlled the action of master arm to carry out crawl and are launched object.
Thus, the unmanned plane undercarriage for launching crawl object of the invention can be not only used for crawl, object-throwing after taking off,
Ground is supported when can also be used for taking off landing；To ensure supporting ＆ stablizing, undercarriage is preferably to use in pairs, according to actual need
Three or more undercarriage collocation can be also set to by, which asking, uses.
Preferably, the end of each branch's brace of the master arm is also equipped with anti-slip rubber, thus, in undercarriage branch
Anti-skidding during support, stability maintenance, increases frictional force, crawl firmly when launching crawl object.
It refer to shown in Fig. 2, it is the Fast Installation face for launching the unmanned plane undercarriage for capturing object of the invention
Structure diagram；The Fast Installation face includes：Sliding supporting bar 4 and the foot stool on the sliding supporting bar are hinged with soon
5 are put, wherein,
The face of the upside of the sliding supporting bar 4 is equipped with slide, and the body of rod is offered fits with the mounting portion of unmanned plane undercarriage
The mounting hole matched somebody with somebody, thus, the sliding supporting bar 4 is connected to for the unmanned plane undercarriage；
The foot stool quick access device 5 is two or plurality of rods, slideably, is vertically arranged on the cunning in the horizontal direction
Above dynamic supporting rod 4.
It refer to shown in Fig. 3, it is the structure diagram for launching the unmanned plane for capturing object of the invention；It is described nobody
Machine includes：Above-mentioned undercarriage, above-mentioned Fast Installation face and unmanned plane body 6, the Fast Installation face are used to connect described rise
Fall frame and the unmanned plane body 6, the mounting portion on the master arm of the undercarriage is installed to the slip branch in Fast Installation face
Mounting hole on strut, the unmanned plane body are then installed to the foot stool quick access device.Treated in use, unmanned plane is powered to entering
Machine state, the arrangement of unmanned plane undercarriage rung level is positioned on Fast Installation face, and alignment Fast Installation interface firmly presses
Unmanned plane undercarriage and device can be pinned.
The foregoing is merely presently preferred embodiments of the present invention, is not intended to limit the invention, it is all the present invention spirit and
Within principle, any modification, equivalent replacement, improvement and so on, should all be included in the protection scope of the present invention.
Claims (6)
- A kind of 1. unmanned plane undercarriage for launching crawl object, it is characterised in that including：Master arm, linkage mechanism, locking Mechanism and control mechanism, wherein,The master arm includes three or more than three branch's braces, and for installing the mounting portion of each branch's brace, each point Support arm is movably connected on the mounting portion；The linkage mechanism is embedded in each branch's brace, is connected with the control mechanism, and the control mechanism is sent Digital signal is converted into action command, so that each branch's brace open or close；The lockable mechanism is embedded in each branch's brace, is connected with the control mechanism, and life has been performed in each branch's brace After order, lockable mechanism is by each branch's brace locking；The control mechanism is embedded in the mounting portion, is carried out wireless communication with ground control station, is sent and received data, into And control each branch's brace open or close.
- 2. the unmanned plane undercarriage according to claim 1 for launching crawl object, it is characterised in that further include at information Manage unit, described information processing unit is embedded in the mounting portion, is connected with the control mechanism, also with ground control station Carry out wireless communication.
- 3. the unmanned plane undercarriage according to claim 2 for launching crawl object, it is characterised in that described information processing The accessible information of unit includes：Positional information, audio/video information, the sound of data message and emergency, Qiang Guang, smog and right Say information.
- 4. the unmanned plane undercarriage of crawl object can be launched according to claims 1 to 3 any one of them, it is characterised in that institute The end for stating each branch's brace of master arm is also equipped with anti-slip rubber.
- A kind of 5. unmanned plane for launching crawl object, it is characterised in that including：Unmanned plane body, Fast Installation face, and two As Claims 1 to 4 any one of them can launch the unmanned plane undercarriage of crawl object, wherein, the Fast Installation face is used In the connection unmanned plane undercarriage and the unmanned plane body.
- 6. the unmanned plane according to claim 5 for launching crawl object, it is characterised in that the Fast Installation bread Include：Sliding supporting bar and the foot stool quick access device on the sliding supporting bar, the face of the upside of the sliding supporting bar Equipped with slide, the body of rod offers the mounting hole being adapted to the mounting portion of unmanned plane undercarriage；The foot stool quick access device is two Bar above, is vertically arranged on the slide of the sliding supporting bar, for unmanned plane body slideably, in the horizontal direction Installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711428578.7A CN107972871A (en) | 2017-12-26 | 2017-12-26 | A kind of unmanned plane undercarriage and unmanned plane for launching crawl object |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711428578.7A CN107972871A (en) | 2017-12-26 | 2017-12-26 | A kind of unmanned plane undercarriage and unmanned plane for launching crawl object |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107972871A true CN107972871A (en) | 2018-05-01 |
Family
ID=62007556
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711428578.7A Pending CN107972871A (en) | 2017-12-26 | 2017-12-26 | A kind of unmanned plane undercarriage and unmanned plane for launching crawl object |
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| Country | Link |
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| CN (1) | CN107972871A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109279022A (en) * | 2018-10-12 | 2019-01-29 | 中国民航大学 | A kind of fusion undercarriage and the unmanned plane grabbing device with adaptive ability |
| CN109665102A (en) * | 2018-12-20 | 2019-04-23 | 保定维特瑞交通设施工程有限责任公司 | A kind of unmanned plane loading is fixed and throwing mechanism |
| CN113031116A (en) * | 2021-04-16 | 2021-06-25 | 成都锦天联华科技有限责任公司 | Unmanned aerial vehicle throwing type rainfall emergency observation system |
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| CN105014687A (en) * | 2015-08-07 | 2015-11-04 | 东北电力大学 | Mechanical arm with multi-rotor-wing unmanned aerial vehicle |
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| CN106081111A (en) * | 2016-08-28 | 2016-11-09 | 张玉华 | A kind of rescue unmanned plane |
| CN107458577A (en) * | 2016-06-03 | 2017-12-12 | 比亚迪股份有限公司 | Folding device and unmanned plane |
| CN207631476U (en) * | 2017-12-26 | 2018-07-20 | 烟台欣飞智能系统有限公司 | A kind of unmanned plane undercarriage and unmanned plane for launching crawl object |
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2017
- 2017-12-26 CN CN201711428578.7A patent/CN107972871A/en active Pending
Patent Citations (6)
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| CN105014687A (en) * | 2015-08-07 | 2015-11-04 | 东北电力大学 | Mechanical arm with multi-rotor-wing unmanned aerial vehicle |
| CN205652365U (en) * | 2016-05-04 | 2016-10-19 | 上海钛灵盾无人机技术有限公司 | Plant protection unmanned plane |
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| CN207631476U (en) * | 2017-12-26 | 2018-07-20 | 烟台欣飞智能系统有限公司 | A kind of unmanned plane undercarriage and unmanned plane for launching crawl object |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109279022A (en) * | 2018-10-12 | 2019-01-29 | 中国民航大学 | A kind of fusion undercarriage and the unmanned plane grabbing device with adaptive ability |
| CN109665102A (en) * | 2018-12-20 | 2019-04-23 | 保定维特瑞交通设施工程有限责任公司 | A kind of unmanned plane loading is fixed and throwing mechanism |
| CN113031116A (en) * | 2021-04-16 | 2021-06-25 | 成都锦天联华科技有限责任公司 | Unmanned aerial vehicle throwing type rainfall emergency observation system |
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