CN209472853U - A kind of ground control system of unmanned plane, unmanned plane - Google Patents
A kind of ground control system of unmanned plane, unmanned plane Download PDFInfo
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- CN209472853U CN209472853U CN201821583212.7U CN201821583212U CN209472853U CN 209472853 U CN209472853 U CN 209472853U CN 201821583212 U CN201821583212 U CN 201821583212U CN 209472853 U CN209472853 U CN 209472853U
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- 230000006835 compression Effects 0.000 claims description 9
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- 230000000007 visual effect Effects 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 24
- 238000000034 method Methods 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000004069 differentiation Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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Abstract
The utility model provides a kind of ground control system of unmanned plane, it include: cabinet, it includes main box and auxiliary box body, the side of main box is connected with the side of auxiliary box body by connector, main box and auxiliary box body is set around the axis rotation perpendicular to top of the box, to realize the open state and conjunction state of cabinet;Main screen panel, is embedded in main box, and main screen panel is equipped with main display, charging interface, main screen power button, USB interface, earth station's power switch;Vice screen panel, is embedded in auxiliary box body, and vice screen panel is equipped with secondary display screen, data-link antenna;First display is opposite with secondary display screen set on the back side of vice screen panel;Second display is opposite with main display set on the back side of main screen panel.The ground control system of the utility model is light-weight, visual field is wide, the angle between two display screens is adjustable, battery life is long.
Description
Technical field
The utility model relates to air vehicle technique field more particularly to a kind of ground control systems of unmanned plane, unmanned plane.
Background technique
With the progress of science and technology, the maturation and large-scale application of unmanned air vehicle technique, a large amount of manpowers are much needed originally
Operation mode replaced unmanned plane, improve safety and the working efficiency of operating personnel.
UAV system is divided into flying platform and ground control system (ground control system is also named earth station), unmanned plane
Command and control center of the face station as UAV system is an important component of UAV system.
And current earth station on the market, volume is big, and cruise duration is short, and screen uses single screen or upper and lower double screen layout side
Formula, single-screen show that content is limited, and double screen is influenced by observation visual angle, is unfavorable for two operators while being watched display
Screen, affects the synchronism of work.
Utility model content
(1) technical problems to be solved
In view of above-mentioned technical problem, the utility model provides the ground control system and unmanned plane of a kind of unmanned plane.This
The ground control system of utility model is light-weight, visual field is wide, the angle between two display screens is adjustable, battery life
It is long, the portability of ground control system is improved, the convenience of ground control system is optimized, increases ground control system
Reliability has widened field of view.
(2) technical solution
One aspect according to the present utility model provides a kind of ground control system of unmanned plane, comprising:
Cabinet comprising main box and auxiliary box body, the side of main box are connected by connector with the side of auxiliary box body, made
Main box and auxiliary box body realize the open state and conjunction state of cabinet around the axis rotation perpendicular to top of the box;
Main screen panel, is embedded in main box, main screen panel be equipped with main display, charging interface, main screen power button,
USB interface, earth station's power switch;
Vice screen panel, is embedded in auxiliary box body, and vice screen panel is equipped with secondary display screen, data-link antenna;
First display is opposite with secondary display screen set on the back side of vice screen panel;
Second display is opposite with main display set on the back side of main screen panel.
In some embodiments of the utility model, the folding angle between main box and auxiliary box body is adjustable.
In some embodiments of the utility model, the main screen power button includes:
Connecting rod,
First end in contact of compression bar, first end and connecting rod, second end is by the through-hole on main screen panel by main screen panel
The back side extend the front of main screen panel;
Switch main body, first end are rotatablely connected by the second end of link pin and connecting rod;
The second end of triggering pin, first end and switch main body is close, and the switch of second end and second display is close;
Return spring covers on triggering pin;
By the second end of moulded rod, under the drive of connecting rod, switch main body rotation, switch main body pin contacts and is pushed away with triggering
Dynamic triggering pin, triggering sell the switch contact with second display and trigger the switch of second display;The second end of compression bar is unclamped,
Triggering pin return under the elastic force of return spring, completes a trigger action.
In some embodiments of the utility model, further includes:
One, for installing the apparatus mounting plate of control panel, is embedded in main box, positioned at the back side of main screen panel.
In some embodiments of the utility model, further includes:
One winder, in embedded equipment mounting plate, the power supply line for charging for ground control system is received within winder
Interior, the charging plug of power supply line is exposed at except winder.
In some embodiments of the utility model,
Power cord wrap in the winder becomes multiple concentric circles, and plane is perpendicular to equipment where concentric diameter of a circle
Mounting plate, the winder are fastened by a L-type part.
In some embodiments of the utility model,
The L-type part includes size identical parallel opposite the first L structure and the 2nd L structure, the head of the first L structure
End, the 2nd L structure head end be each attached to the back side of apparatus mounting plate, end, the end of the 2nd L structure of the first L structure are equal
Far from apparatus mounting plate the back side and be attached by a cross bar;The winder is pressed from both sides by the first L structure, the 2nd L structure
Tightly.
In some embodiments of the utility model, vice screen panel, main screen panel, apparatus mounting plate the back side be provided with
Multiple columns.
In some embodiments of the utility model, the first display, second display pass through U-shaped card part respectively and fasten;
Control panel is fixed on the back side of apparatus mounting plate by U-shaped card part.
Other side according to the present utility model additionally provides a kind of unmanned plane, including above-mentioned ground control system.
(3) beneficial effect
It can be seen from the above technical proposal that the ground control system and unmanned plane of the utility model unmanned plane at least have
One of following beneficial effect:
(1) the utility model is by the horizontal layout of double-display screen or so, and the folding angle between two display screens can be with
Adjustment, expands observation visual angle, is conducive to the simultaneously operating to two display screens;
(2) the utility model uses high capacity cell, and uses extendible charger interface, duplicate supply mode, improves
Cruise duration of ground control system and the convenience for optimizing ground control system;
(3) ground control system of the utility model is small in size, light-weight, improves the portability of ground control system.
Detailed description of the invention
Fig. 1 is the box structure diagram of the ground control system of the utility model embodiment unmanned plane, wherein (a) is
Front view, (b) are top view.
Fig. 2 is the cabinet unfolded state schematic diagram of Fig. 1, and (a) is front view, (b) is top view.
(a), (b) of Fig. 3 is respectively the schematic diagram of the different folding angles of cabinet.
Fig. 4 is the structural schematic diagram of the main screen panel of the utility model embodiment ground control system, vice screen panel.
The Facad structure of the structure schematic diagram for the vice screen panel that (a) of Fig. 5 is Fig. 4, the vice screen panel that (b) is Fig. 4
Schematic diagram.
The back side and positive structural schematic diagram of the Fig. 6 for the main screen panel of Fig. 4.
Fig. 7 is the structural schematic diagram of main screen power button in Fig. 6.
(a) of Fig. 8 is the top view of main screen power button, the side view that (b) is main screen power button.
Fig. 9 is the structural schematic diagram of the apparatus mounting plate of the utility model embodiment ground control system.
Figure 10 is the back side of apparatus mounting plate and positive structural schematic diagram in Fig. 9.
Figure 11 is the structural schematic diagram of the column of the utility model embodiment ground control system.
Figure 12 is the structural schematic diagram that the utility model embodiment main screen panel and apparatus mounting plate are fixed together,
In, (a) is main view, (b) is side view, (c) is back side main view, (d) is front plan view.
[main element]
1- main box;
2- auxiliary box body;
3- hinge;
4- handle;
5- foot pad;
6- vice screen panel;
7- main screen panel;
8- apparatus mounting plate;
9- data-link antenna;
The first fan of 10-;
10 '-the second fans;
11- electric-quantity display device;
12- earth station power switch;
13-USB interface;
14- main screen power button;
15- charging interface;
16- main screen speaker hole;
17- main display;
18- pair display screen;
19- the first U-shaped card part;
The first display of 20-;
20 '-second displays;
21- connecting rod;
22- compression bar;
23- switch main body;
24- triggering pin;
25- return spring;
26- link pin;
27- the second U-shaped card part;
28- control panel;
29- winder;
30- column.
Specific embodiment
For the purpose of this utility model, technical solution and advantage is more clearly understood, below in conjunction with specific embodiment, and
Referring to attached drawing, the utility model is further described.
In the exemplary embodiment of the utility model, a kind of ground control system of unmanned plane is provided.Fig. 1 is this reality
With the box structure diagram of the ground control system of new embodiment unmanned plane, wherein (a) is front view, (b) is to overlook
Figure.Fig. 2 is the cabinet unfolded state schematic diagram of Fig. 1, and (a) is front view, (b) is top view.(a), (b) of Fig. 3 is respectively case
The schematic diagram of the different folding angles of body.Fig. 4 is main screen panel, the vice screen panel of the utility model embodiment ground control system
Structural schematic diagram.The front of the structure schematic diagram for the vice screen panel that (a) of Fig. 5 is Fig. 4, the vice screen panel that (b) is Fig. 4
Structural schematic diagram.The back side and positive structural schematic diagram of the Fig. 6 for the main screen panel of Fig. 4.As shown in figures 1 to 6, the utility model
The ground control system of unmanned plane includes: cabinet, main screen panel 7, vice screen panel 6, the first display 20, second display 20 '.
Cabinet includes main box 1 and auxiliary box body 2, and the side of main box 1 is connected with the side of auxiliary box body 2 by connector,
Main box 1 and auxiliary box body 2 is set around the axis rotation perpendicular to top of the box, to realize the open state and conjunction state of cabinet.It is preferred that
Ground, connector can be hinge 3.In addition, cabinet can be carbon fibre material.
Main screen panel 7 is embedded in main box 1, and main screen panel 7 is equipped with main display 17, charging interface 15, main screen power supply
Key 14, usb 13, main screen speaker hole 16, the first fan 10, earth station's power switch 12, electric-quantity display device 11.
Vice screen panel 6 is embedded in auxiliary box body 2, and vice screen panel 6 is equipped with secondary display screen 18, the second fan 10 ', data-link day
Line 9.
First display 20 is set to the back side of vice screen panel 6, opposite with secondary display screen 18;Second display 20 ' is set to master
The back side of panel plate 7, it is opposite with main display 17.
In the present invention, the Biscreen display layout type horizontal using left and right, observation visual angle is big, is conducive to multiple
Operator watches display screen simultaneously, facilitates the synchronism of work.
Again as shown in Figure 1, being provided with handle 4 at the top of cabinet, so that guiding and supporting conveniently, the bottom of cabinet is additionally provided with foot pad
5。
Again as shown in figure 3, the folding angle between main box 1 and auxiliary box body 2 is adjustable, for example folding angle is big
In 90 degree, as shown in (a) of Fig. 3;For another example folding angle is 90 degree, can according to the actual situation certainly as shown in (b) of Fig. 3
Row adjustment, it is easy to use.
Again as shown in figure 5, the first display 20 is fastened by the first U-shaped card part 19, the first U-shaped card part 19 includes U-type groove
With the lug of U-type groove opening, U-type groove is open towards the back side of vice screen panel 6, is fastened on the first display 20 in U-type groove,
U-type groove is connected by the lug of its opening and the back side of vice screen panel 6.
Again as shown in fig. 6, second display 20 ' is fastened by identical U-shaped card part as shown in Figure 5, herein not
It repeats again.
Fig. 7 is the structural schematic diagram of main screen power button in Fig. 6.(a) of Fig. 8 is top view, (b) of main screen power button
For the side view of main screen power button.As shown in Figure 7,8, main screen power button 14 includes: connecting rod 21, compression bar 22, switch main body
23, pin 24, return spring 25, the first end of compression bar 22 and the first end in contact of connecting rod 21 are triggered, the second end of compression bar 22 passes through
Through-hole on main screen panel 7 is extended the front of main screen panel 7 by the back side of main screen panel 7;The first end of switch main body 23 is logical
The second end for crossing link pin 26 and connecting rod 21 is rotatablely connected;The first end for triggering pin 24 and the second end of switch main body 23 are close,
The second end for triggering pin 24 and the switch of second display 20 ' are close;25 sets of return spring on triggering pin 24.
The operating process of switching on and shutting down is carried out to second display 20 ' using main screen power button 14 are as follows: by moulded rod 22
Second end, under the drive of connecting rod 21, switch main body 23 is rotated, and switch main body 23 contacts with triggering pin 24 and triggering is pushed to sell
24, it triggers the switch contact of pin 24 and second display 20 ' and triggers the switch of second display 20 ';Unclamp the of compression bar 22
Two ends trigger the return under the elastic force of return spring 25 of pin 24, complete a trigger action.
By the above structure of the utility model, the power switch on 20 ' side of second display is transferred to main screen face
The front of plate 7 when switching on and shutting down, need to only press the main screen power button 14 on 7 front of main screen panel, easy to operate.
Fig. 9 is the structural schematic diagram of the apparatus mounting plate of the utility model embodiment ground control system.As shown in figure 9,
Ground control system further includes an apparatus mounting plate 8, and for installing control panel 28, apparatus mounting plate 8 is embedded in main box 1,
Positioned at the back side of main screen panel 7.
Figure 10 is the back side of apparatus mounting plate and positive structural schematic diagram in Fig. 9.As shown in Figure 10, ground control system
It further include a winder 29, the power supply line receiving in 29 embedded equipment mounting plate 8 of winder, for charging for ground control system
In winder 29, the charging plug of power supply line is exposed at except winder 29, and the power cord wrap in winder 29 becomes multiple
Concentric circles, plane is perpendicular to apparatus mounting plate 8 where concentric diameter of a circle.Winder 29 is fastened by a L-type part, L-type part packet
Size identical parallel opposite the first L structure and the 2nd L structure are included, head end, the head end of the 2nd L structure of the first L structure are equal
Be fixed on the back side of apparatus mounting plate 8, the end of the first L structure, the 2nd L structure back of the end far from apparatus mounting plate 8
It face and is attached by a cross bar;Winder 29 is clamped by the first L structure, the 2nd L structure.
Preferably, a lug is respectively set in the head end of the first L structure, the head end of the 2nd L structure, by lug by the first L
The back side of structure, the 2nd L structure and apparatus mounting plate 8 is connected.Winder 29 is clamped same by the first L structure, the 2nd L structure
When, the cross bar between the end of the first L structure and the end of the 2nd L structure can also apply a upward thrust to winder,
For holding winder.
Control panel 28 is fixed on the back side of apparatus mounting plate 8, the knot of the second U-shaped card part 27 by the second U-shaped card part 27
Structure is identical as the structure of the first U-shaped card part 19, and details are not described herein.
Figure 11 is the structural schematic diagram of the column of the utility model embodiment ground control system.Figure 12 is the utility model
The structural schematic diagram that embodiment main screen panel and apparatus mounting plate are fixed together, wherein (a) is main view, (b) is side view
Figure, (c) are back side main view, (d) is front plan view.As shown in Figure 11,12, vice screen panel 6, main screen panel 7, equipment installation
The back side of plate 8 is provided with multiple columns, between vice screen panel 6 and auxiliary box body 2, main screen panel 7 and apparatus mounting plate 8 it
Between, being connected and fixed between apparatus mounting plate 8 and main box 1.
Again as shown in figure 12, there is an outlet on winder 29, power supply line stretches out winder 29, and power supply by the outlet
Line is freely rolled up by the outlet to be put.The charging plug of power supply line stretches out main screen panel 7 by the charging interface 15 on main screen panel 7
Front.When ground control system works, power supply line is pulled out into winder 29, charging plug access 220V power supply controls ground
System processed is powered, and when without power supply, power supply line is involved in winder 29, charging plug card is placed on charging interface 15.
It is exposed on the front of main screen panel 7 by using winder 29, and by charging plug, it is easy to use.To sum up, main screen panel 7 is carried on the back
The second display 20 ' in face can pass through above-mentioned electricity other than included lithium battery (for example, by using 18650 high energy battery cores) power supply
Source line charges, i.e., the present invention provides duplicate supply mode, improves the cruise duration of ground control system.
In the exemplary embodiment of the utility model, a kind of unmanned plane is additionally provided comprising above-mentioned ground control
System.
So far, attached drawing is had been combined the present embodiment is described in detail.According to above description, those skilled in the art
Should ground control system to the utility model unmanned plane and unmanned plane have clear understanding.
It should be noted that in attached drawing or specification text, the implementation for not being painted or describing is affiliated technology
Form known to a person of ordinary skill in the art, is not described in detail in field.In addition, the above-mentioned definition to each element and method is simultaneously
It is not limited only to various specific structures, shape or the mode mentioned in embodiment, those of ordinary skill in the art can carry out letter to it
It singly changes or replaces.
It should also be noted that, the direction term mentioned in embodiment, for example, "upper", "lower", "front", "rear", " left side ",
" right side " etc. is only the direction with reference to attached drawing, is not used to limit the protection scope of the utility model.
Furthermore the word of ordinal number such as " first ", " second ", " third " etc. used in specification and claim,
To modify corresponding element, itself simultaneously unexpectedly contains and represents the element and have any ordinal number, does not also represent a certain element and another
The sequence or the sequence in manufacturing method of one element, the use of those ordinal numbers are only used to obtain the element with certain name
Clear differentiation can be made with another element with identical name.
It should be noted that running through attached drawing, identical element is indicated by same or similar appended drawing reference.In the following description,
Some specific embodiments are used for description purposes only, and should not be construed to the utility model has any restrictions, and are this reality
With the example of new embodiment.When may cause the understanding to the utility model and cause to obscure, conventional structure or structure will be omitted
It makes.It should be noted that the shape and size of each component do not reflect actual size and ratio in figure, and only illustrate the utility model embodiment
Content.
Particular embodiments described above has carried out into one the purpose of this utility model, technical scheme and beneficial effects
Step is described in detail, it should be understood that being not limited to this foregoing is merely specific embodiment of the utility model
Utility model, within the spirit and principle of the utility model, any modification, equivalent substitution, improvement and etc. done should all wrap
Containing being within the protection scope of the utility model.
Claims (10)
1. a kind of ground control system of unmanned plane characterized by comprising
Cabinet comprising main box (1) and auxiliary box body (2), the side of main box (1) and the side of auxiliary box body (2) pass through connection
Part connection makes main box (1) and auxiliary box body (2) around the axis rotation perpendicular to top of the box, realize the open state of cabinet with
Conjunction state;
Main screen panel (7) is embedded in main box (1), and main screen panel (7) is equipped with main display (17), charging interface (15), master
Shield power button (14), USB interface (13), earth station's power switch (12);
Vice screen panel (6) is embedded in auxiliary box body (2), and vice screen panel (6) is equipped with secondary display screen (18), data-link antenna (9);
First display (20) is set to the back side of vice screen panel (6), opposite with secondary display screen (18);
Second display (20 ') is set to the back side of main screen panel (7), opposite with main display (17).
2. ground control system according to claim 1, which is characterized in that opening between main box (1) and auxiliary box body (2)
Close angle degree is adjustable.
3. ground control system according to claim 1, which is characterized in that the main screen power button (14) includes:
Connecting rod (21),
Compression bar (22), the first end in contact of first end and connecting rod (21), second end is by the through-hole on main screen panel (7) by leading
Extend the front of main screen panel (7) in the back side of panel plate (7);
Switch main body (23), first end are rotatablely connected by the second end of link pin (26) and connecting rod (21);
Triggering pin (24), first end and the second end of switch main body (23) are close, and second end is opened with second display (20 ')
It closes close;
Return spring (25) covers on triggering pin (24);
By the second end of moulded rod (22), under the drive of connecting rod (21), switch main body (23) is rotated, switch main body (23) and touching
Hair pin (24) contacts and pushes triggering pin (24), and the switch contact of triggering pin (24) and second display (20 ') simultaneously triggers second
The switch of display (20 ');The second end of compression bar (22) is unclamped, (24) return under the elastic force of return spring (25) is sold in triggering,
Complete a trigger action.
4. ground control system according to claim 3, which is characterized in that further include:
One, for installing the apparatus mounting plate (8) of control panel (28), is embedded in main box (1), is located at the back of main screen panel (7)
Surface side.
5. ground control system according to claim 3, which is characterized in that further include:
One winder (29), in embedded equipment mounting plate (8), the power supply line for charging for ground control system is received within spiral
In device (29).
6. ground control system according to claim 5, which is characterized in that
Power cord wrap in the winder (29) becomes multiple concentric circles, and plane is perpendicular to equipment where concentric diameter of a circle
Mounting plate (8), the winder (29) are fastened by a L-type part.
7. ground control system according to claim 6, which is characterized in that
The L-type part includes size identical parallel opposite the first L structure and the 2nd L structure, the head end of the first L structure, the
The head end of two L structures is each attached to the back side of apparatus mounting plate (8), and end, the end of the 2nd L structure of the first L structure are remote
It the back side from apparatus mounting plate (8) and is attached by a cross bar;
The winder (29) is clamped by the first L structure, the 2nd L structure.
8. ground control system according to claim 1-7, which is characterized in that
Vice screen panel (6), main screen panel (7), apparatus mounting plate (8) the back side be provided with multiple columns.
9. ground control system according to claim 1-7, which is characterized in that
First display (20), second display (20 ') are fastened by U-shaped card part respectively;
Control panel (28) is fixed on the back side of apparatus mounting plate (8) by U-shaped card part.
10. a kind of unmanned plane, which is characterized in that including the described in any item ground control systems of claim 1-9.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201821583212.7U CN209472853U (en) | 2018-09-27 | 2018-09-27 | A kind of ground control system of unmanned plane, unmanned plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201821583212.7U CN209472853U (en) | 2018-09-27 | 2018-09-27 | A kind of ground control system of unmanned plane, unmanned plane |
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Publication Number | Publication Date |
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CN209472853U true CN209472853U (en) | 2019-10-08 |
Family
ID=68086936
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CN201821583212.7U Expired - Fee Related CN209472853U (en) | 2018-09-27 | 2018-09-27 | A kind of ground control system of unmanned plane, unmanned plane |
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Country | Link |
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2018
- 2018-09-27 CN CN201821583212.7U patent/CN209472853U/en not_active Expired - Fee Related
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Granted publication date: 20191008 |