CN204750579U - Unmanned aerial vehicle of battery power display is equipped with to inside - Google Patents

Unmanned aerial vehicle of battery power display is equipped with to inside Download PDF

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Publication number
CN204750579U
CN204750579U CN201520341911.0U CN201520341911U CN204750579U CN 204750579 U CN204750579 U CN 204750579U CN 201520341911 U CN201520341911 U CN 201520341911U CN 204750579 U CN204750579 U CN 204750579U
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CN
China
Prior art keywords
controller
unmanned plane
groove
wire
support plate
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Expired - Fee Related
Application number
CN201520341911.0U
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Chinese (zh)
Inventor
李楠
邓开连
尚建华
卢学民
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Donghua University
National Dong Hwa University
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Donghua University
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Priority to CN201520341911.0U priority Critical patent/CN204750579U/en
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Publication of CN204750579U publication Critical patent/CN204750579U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to an unmanned aerial vehicle of battery power display is equipped with to inside, including the unmanned aerial vehicle main part, set up the recess in the unmanned aerial vehicle main part, the automatic turnover door device of installation on the recess, be equipped with drive mechanism in the recess, the last motor that links to each other with the controller through the wire of installing of drive mechanism, installing the diaphragm on the output shaft of motor, installing two pillars under the diaphragm, install the spin under the pillar, it is nevertheless fixed with drive mechanism that the spin is located the drive mechanism upper surface, install the electric putter who links to each other through wire and controller on the diaphragm, the last fisheye bearing that installs of electric putter, fisheye bearing install under quick -witted case, quick -witted incasement installation display circuit board, display circuit board pass through the wire respectively with inside battery of unmanned aerial vehicle and quick -witted case on the display of installation link to each other, the controller is located that drive mechanism goes up and by remote controller control. The utility model discloses can solve the battery power display installs in the easy problem of damaging of casing surface.

Description

The unmanned plane of electric quantity indicator is equipped with in a kind of inside
Technical field
The utility model relates to the battery electric quantity technique of display field of unmanned plane, particularly relates to the unmanned plane that electric quantity indicator is equipped with in a kind of inside.
Background technology
In recent years, along with the downward of unmanned plane price, and the fast development of unmanned plane industry, domestic unmanned plane market is in continuous expansion, and storage battery is the power supply of every frame unmanned plane indispensability, when the battery of unmanned plane is in low state of charge for a long time, storage battery is easily made to scrap, reduce the service life of storage battery, in order to know that the electricity of storage battery needs to install battery indicator, the electric quantity indicator of prior art is all mounted on unmanned plane casing outer surface, although convenient electric quantity data in unmanned plane during flying on reading displayed device, but be mounted in casing outer surface and easily make display damage.
Utility model content
The utility model provides a kind of inside that the unmanned plane of electric quantity indicator is housed, and can solve electric quantity indicator and be arranged on casing outer surface and hold damageable problem.
The utility model solves the technical scheme that its technical matters adopts: provide a kind of inside that the unmanned plane of electric quantity indicator is housed, comprise unmanned plane main body, described unmanned plane main body arranges groove, described groove is installed automatic turning door gear; Transmission device is provided with in described groove; Described transmission device is provided with the motor be connected with controller by wire; The output shaft of described motor installs transverse slat, and install two pillars under transverse slat, install spin under described pillar, described spin is positioned at transmission device upper surface but does not fix with transmission device; Described transverse slat is provided with the electric pushrod be connected with controller by wire, described electric pushrod is installed flake bearing, under described flake bearing is arranged on cabinet, install display circuit board in described cabinet, described display circuit board is connected with the telltale that the storage battery of unmanned plane inside and cabinet are installed respectively by wire; Described controller to be positioned on transmission device and to be controlled by remote controller.
Described transmission device comprises the first support plate and the second support plate; Described second support plate to be arranged in groove and to be provided with the second hollow out, and described second hollow out is provided with two the second bearing pins, wherein, second bearing pin is connected with the piston rod of the cylinder being positioned at groove, described cylinder internal solenoid valve; Described two the second bearing pins are connected with the left and right sides, scissor arm lower end respectively, the left and right sides, described scissor arm upper end is arranged on two the first bearing pins respectively, described two the first bearing pins are arranged in the first hollow out, described first hollow out is arranged on the first support plate, one end of first support plate is provided with slide block, and slide block is arranged on the slide rail that is positioned at inside groove; The energising of described electromagnetic valve or power-off are controlled by described controller.
Described transverse slat is provided with annunciator; Described annunciator is connected with controller by wire.
Beneficial effect
Owing to have employed above-mentioned technical scheme, the utility model compared with prior art, there is following advantage and good effect: the utility model is by the unlatching of first on remote controller by key control automatic turning door gear, by energising or the power-off of the second button control cylinder internal solenoid valve on remote controller, the piston rod carrying out control cylinder does stretching routine, piston rod promotes the second bearing pin makes scissor arm extend, and telltale is moved up and shifts out groove; The 3rd button on remote controller controls motor forward or reverse, makes transverse slat forward or reverse, telltale is rotated, rotated to by telltale in face of telltale, does not need user to walk about and just can see telltale; The 4th button on remote controller controls electric pushrod and does fore and aft motion, make to be positioned at two front-seat electric pushrods and do contractile motion, make two electric pushrods being positioned at rear row do stretching routine, cabinet is tilted to down, telltale is tilted to down, and person easy to use checks telltale; When the accumulator electric-quantity of unmanned plane inside is too low, controller controls annunciator and sends chimes of doom, reminds people to charge in time; When not checking telltale, make telltale be positioned at groove, avoid telltale to be exposed to wind and rain.
Accompanying drawing explanation
Fig. 1 is integral structure figure of the present utility model;
Fig. 2 is the partial enlarged drawing of a in Fig. 1;
Fig. 3 is the birds-eye view of b in Fig. 2;
Fig. 4 is remote controller structure schematic diagram;
In figure, 1, automatic turning door gear 2, unmanned plane main body 3, display circuit board 4, transverse slat 5, pillar 6, spin 7, slide block 8, first hollow out 9, first support plate 10, first bearing pin 11, scissor arm 12, slide rail 13, second support plate 14, second hollow out 15, second bearing pin 16, telltale 17, cabinet 18, flake bearing 19, electric pushrod 20, annunciator 21, motor 22, controller 23, groove 24, cylinder 25, remote controller 26, first button 27, second button 28, the 3rd button 29, the 4th button.
Detailed description of the invention
Below in conjunction with specific embodiment, set forth the utility model further.Should be understood that these embodiments are only not used in restriction scope of the present utility model for illustration of the utility model.In addition should be understood that those skilled in the art can make various changes or modifications the utility model, and these equivalent form of values fall within the application's appended claims limited range equally after the content of having read the utility model instruction.
Embodiment of the present utility model relates to the unmanned plane that electric quantity indicator is equipped with in a kind of inside, as Figure 1-3, comprise automatic turning door gear 1, unmanned plane main body 2, display circuit board 3, transverse slat 4, pillar 5, spin 6, slide block 7, first hollow out 8, first support plate 9, first bearing pin 10, scissor arm 11, slide rail 12, second support plate 13, second hollow out 14, second bearing pin 15, telltale 16, cabinet 17, flake bearing 18, electric pushrod 19, annunciator 20, motor 21, controller 22, groove 23, cylinder 24 and remote controller 25, on in described unmanned plane main body 2, groove 23 is set, groove 23 is installed automatic turning door gear 1, by the unlatching of first on remote controller 25 by key control automatic turning door gear 1, in groove 23, second support plate 13 is installed, second support plate 13 is provided with the second hollow out 14, second hollow out 14 installs two the second bearing pins 15, the second bearing pin 15 being positioned at right-hand member is connected with the piston rod of cylinder 24, cylinder 24 is arranged in groove 23, cylinder 24 internal solenoid valve, the left and right sides, scissor arm 11 lower end is arranged on two the second bearing pins 15 respectively, the left and right sides, scissor arm 11 upper end is arranged on two the first bearing pins 10 respectively, first bearing pin 10 is arranged in the first hollow out 8, first hollow out 8 is arranged on the first support plate 9, first support plate 9 left end installs slide block 7, slide block 7 is arranged on slide rail 12, slide rail 12 is arranged on left side in groove 23, by energising or the power-off of the second button 27 control cylinder 24 internal solenoid valve on remote controller 25, the piston rod carrying out control cylinder 24 does stretching routine, piston rod promotes the second bearing pin 15 makes scissor arm 11 extend, telltale 16 is moved up and shifts out groove 23, mount controller 22 on first support plate 9, controller 22 is connected with remote controller 25 signal, remote controller 25 comprises the first button, second button 27, 3rd button 28 and the 4th button 29, first by key control automatic turning door gear 1, second button 27 Controlling solenoid valve, 3rd button 28 controls motor 21, 4th button 29 controls electric pushrod 19, controller 22 is connected with electromagnetic valve with automatic turning door gear 1 respectively by wire, mounted motor 21 on first support plate 9, motor 21 is connected with controller 22 by wire, the output shaft of motor 21 is installed transverse slat 4, the 3rd button 28 on remote controller 25 controls motor 21 forward or reverse, make transverse slat 4 forward or reverse, telltale 16 is rotated, telltale 16 is rotated in face of telltale 16, do not need user to walk about and just can see telltale 16, transverse slat installs two pillars 54 times, pillar installs spin 65 times, spin 6 is positioned on the first support plate 9, do not interfix with the first support plate 9 bottom spin 6, transverse slat 4 is installed annunciator 20, annunciator 20 is connected with controller 22 by wire, when the accumulator electric-quantity of unmanned plane inside is too low, controller 22 controls annunciator 20 and sends chimes of doom, reminds people to charge in time, transverse slat 4 installs four electric pushrods 19, electric pushrod 19 is connected with controller 22 by wire, the 4th button 29 on remote controller 25 controls electric pushrod 19 and does fore and aft motion, make to be positioned at two front-seat electric pushrods 19 and do contractile motion, two electric pushrods 19 being positioned at rear row are made to do stretching routine, cabinet 17 is tilted to down, and telltale 16 is tilted to down, and person easy to use checks telltale 16, electric pushrod 19 is installed flake bearing 18, flake bearing 18 is arranged on cabinet 17 times, in cabinet 17, display circuit board 3 is installed, display circuit board 3 is connected with the storage battery of unmanned plane inside respectively by wire, cabinet 17 is installed telltale 16, telltale 16 is connected with display circuit board 3 by wire, when not checking telltale 16, make telltale 16 be positioned at groove 23, avoid telltale 16 to be exposed to wind and rain.
As shown in Figure 4, described remote controller is provided with the first button 26, second button 27, the 3rd button 28 and the 4th button 29.The utility model using method: by the unlatching of first on remote controller 25 by key control automatic turning door gear 1; By energising or the power-off of the second button 27 control cylinder 24 internal solenoid valve on remote controller 25, the piston rod carrying out control cylinder 24 does stretching routine, and piston rod promotes the second bearing pin 15 makes scissor arm 11 extend, and telltale 16 is moved up and shifts out groove 23; The 3rd button 28 on remote controller 25 controls motor 21 forward or reverse, makes transverse slat 4 forward or reverse, and telltale 16 is rotated, and is rotated to by telltale 16 in face of telltale 16, does not need user to walk about and just can see telltale 16; The 4th button 29 on remote controller 25 controls electric pushrod 19 and does fore and aft motion, make to be positioned at two front-seat electric pushrods 19 and do contractile motion, two electric pushrods 19 being positioned at rear row are made to do stretching routine, cabinet 17 is tilted to down, telltale 16 is tilted to down, and person easy to use checks telltale 16; When the accumulator electric-quantity of unmanned plane inside is too low, controller 22 controls annunciator 20 and sends chimes of doom, reminds people to charge in time; When not checking telltale 16, make telltale 16 be positioned at groove 23, avoid telltale 16 to be exposed to wind and rain.

Claims (3)

1. the unmanned plane of electric quantity indicator is equipped with in an inside, comprise unmanned plane main body (2), it is characterized in that, described unmanned plane main body (2) arranges groove (23), and described groove (23) is upper installs automatic turning door gear (1); Described groove is provided with transmission device in (23); Described transmission device is provided with the motor (21) be connected with controller (22) by wire; The output shaft of described motor (21) is installed transverse slat (4), under transverse slat (4), two pillars (5) are installed, install spin (6) under described pillar (5), described spin (6) is positioned at transmission device upper surface but does not fix with transmission device; Described transverse slat (4) is provided with the electric pushrod (19) be connected with controller (22) by wire, described electric pushrod (19) is upper installs flake bearing (18), under described flake bearing (18) is arranged on cabinet (17), install display circuit board (3) in described cabinet (17), described display circuit board (3) is connected with the upper telltale (16) installed of cabinet (17) with the storage battery of unmanned plane inside respectively by wire; Described controller (22) to be positioned on transmission device and to be controlled by remote controller.
2. the unmanned plane of electric quantity indicator is equipped with in inside according to claim 1, it is characterized in that, described transmission device comprises the first support plate (9) and the second support plate (13); Described second support plate (13) to be arranged in groove (23) and to be provided with the second hollow out (14), described second hollow out (14) is provided with two the second bearing pins (15), wherein, second bearing pin (15) is connected with the piston rod of the cylinder (24) being positioned at groove (23), described cylinder (24) internal solenoid valve; Described two the second bearing pins (15) are connected with scissor arm (11) left and right sides, lower end respectively, described scissor arm (11) left and right sides, upper end is arranged on two the first bearing pins (10) respectively, described two the first bearing pins (10) are arranged in the first hollow out (8), described first hollow out (8) is arranged on the first support plate (9), one end of first support plate (9) is provided with slide block (7), slide block (7) be arranged on be positioned at groove (23) inner side slide rail (12) on; The energising of described electromagnetic valve or power-off are controlled by described controller (22).
3. the unmanned plane of electric quantity indicator is equipped with in inside according to claim 1, it is characterized in that, described transverse slat (4) is provided with annunciator (20); Described annunciator (20) is connected with controller (22) by wire.
CN201520341911.0U 2015-05-25 2015-05-25 Unmanned aerial vehicle of battery power display is equipped with to inside Expired - Fee Related CN204750579U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520341911.0U CN204750579U (en) 2015-05-25 2015-05-25 Unmanned aerial vehicle of battery power display is equipped with to inside

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520341911.0U CN204750579U (en) 2015-05-25 2015-05-25 Unmanned aerial vehicle of battery power display is equipped with to inside

Publications (1)

Publication Number Publication Date
CN204750579U true CN204750579U (en) 2015-11-11

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105398550A (en) * 2015-12-21 2016-03-16 浙江海洋学院 Control console for ship
CN105415269A (en) * 2015-11-13 2016-03-23 舟山长宏国际船舶修造有限公司 Universal marine rudder blade mounting platform
CN108172067A (en) * 2016-12-07 2018-06-15 浙江海洋大学 A kind of new teaching management equipment
CN109459701A (en) * 2018-10-26 2019-03-12 浙江海洋大学 A kind of electric quantity indicator

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105415269A (en) * 2015-11-13 2016-03-23 舟山长宏国际船舶修造有限公司 Universal marine rudder blade mounting platform
CN105415269B (en) * 2015-11-13 2017-07-28 舟山长宏国际船舶修造有限公司 A kind of universal ship rudder blade mounting platform
CN105398550A (en) * 2015-12-21 2016-03-16 浙江海洋学院 Control console for ship
CN108172067A (en) * 2016-12-07 2018-06-15 浙江海洋大学 A kind of new teaching management equipment
CN109459701A (en) * 2018-10-26 2019-03-12 浙江海洋大学 A kind of electric quantity indicator

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20151111

Termination date: 20160525