CN112363529B - Unmanned aerial vehicle navigation system terminal with protect function - Google Patents
Unmanned aerial vehicle navigation system terminal with protect function Download PDFInfo
- Publication number
- CN112363529B CN112363529B CN202011143518.2A CN202011143518A CN112363529B CN 112363529 B CN112363529 B CN 112363529B CN 202011143518 A CN202011143518 A CN 202011143518A CN 112363529 B CN112363529 B CN 112363529B
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- terminal
- side wall
- box
- terminal box
- fixedly connected
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- 238000007789 sealing Methods 0.000 claims abstract description 23
- 238000009434 installation Methods 0.000 claims description 17
- 229910000963 austenitic stainless steel Inorganic materials 0.000 claims description 5
- 239000004743 Polypropylene Substances 0.000 claims description 3
- 239000000835 fiber Substances 0.000 claims description 3
- -1 polypropylene Polymers 0.000 claims description 3
- 229920001155 polypropylene Polymers 0.000 claims description 3
- 239000000428 dust Substances 0.000 description 4
- 238000001914 filtration Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000004078 waterproofing Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Navigation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses an unmanned aerial vehicle navigation system terminal with a protection function, which comprises a terminal box, a first display screen, a terminal processor, a control box, a second display screen and a WIFI emitter, wherein a positioning groove is formed in the outer side wall of the terminal box, the control box is fixedly arranged on the inner side wall of the terminal box, a plurality of buffer springs are fixedly connected to the inner bottom of the terminal box, the tail ends of the buffer springs are fixedly connected with a mounting frame, the terminal processor is arranged on the inner bottom of the mounting frame, the first display screen is arranged on the inner side wall of the mounting frame, the mounting frame penetrates through the positioning groove, a fixing box is rotationally connected to the outer side wall of the terminal box, and the fixing box drives a sealing plate to move rightwards through a connecting rod when the fixing box rotates downwards, so that the sealing plate is tightly attached to the inner side wall of the filter groove, and moisture is prevented from entering the inside of the terminal box through the filter groove, and the components inside the sealing plate are prevented from being shorted, and the terminal box is prevented from being damaged.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle navigation system terminal with a protection function.
Background
Unmanned aircraft is simply referred to as "unmanned aircraft" and is a unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programmed control device. Unmanned aerial vehicle needs to carry out WIFI with the terminal and is connected, for unmanned aerial vehicle appointed flight route through the terminal to carry out real-time supervision to the picture that unmanned aerial vehicle took through the terminal, unmanned aerial vehicle is in fact unmanned aerial vehicle's generic term, defines from technical angle and can divide into: unmanned fixed wing aircraft, unmanned vertical takeoff and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parachute wing aircraft, and the like. Compared with the manned plane, the unmanned plane has the advantages of small volume, low manufacturing cost and convenient use, and can be applied to disaster area rescue, agriculture and forestry plant protection, meteorological observation and film and television drama shooting.
The traditional unmanned aerial vehicle navigation system terminal is in the use because be in the open air probably to take place to collide with, owing to lack preceding shock mitigation system, collide with and probably lead to the display device at terminal impaired to can't real-time supervision unmanned aerial vehicle shooting's content, and when not using, moisture can flow into inside the terminal through the louvre on the terminal and not lead to terminal inside to take place the short circuit, consequently need one kind to have protect function unmanned aerial vehicle navigation system terminal.
Disclosure of Invention
The invention aims to solve the defects in the prior art, and provides an unmanned aerial vehicle navigation system terminal with a protection function.
In order to achieve the above purpose, the present invention adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle navigation terminal with protect function, includes the terminal box, first display screen, terminal treater, control the case, the second display screen, the WIFI transmitter, set up the constant head tank on the lateral wall of terminal box, control case fixed mounting on the inside wall of terminal box, a plurality of buffer springs of interior bottom fixedly connected with of terminal box, buffer spring's end fixedly connected with installing frame, terminal treater installs on the interior bottom of installing frame, first display screen is installed on the inside wall of installing frame, the installing frame runs through the constant head tank, rotate on the lateral wall of terminal box and be connected with the fixed box, second display screen fixed mounting is on the lateral wall of fixed box, WIFI transmitter fixed connection is on the inside wall of fixed box, the filter tank has been seted up to the bottom of terminal box, the installation chamber has been seted up on the inside wall of terminal box, the installation chamber links to each other with the sliding tray, fixedly connected with waterproofing mechanism on the inside wall of installation chamber, waterproofing mechanism offsets with the inside wall of terminal box and the inside wall of fixed establishment of locking mechanism, the terminal box offsets the inside wall of terminal box and the fixed connection has the fixed establishment of locking mechanism.
Preferably, the waterproof mechanism comprises a first pressure spring fixedly connected to the inner side wall of the installation cavity, a sealing plate is fixedly connected to the tail end of the first pressure spring, the tail end of the sealing plate penetrates through the installation cavity, the tail end of the sealing plate abuts against the inner side wall of the filter tank, a connecting rod is connected to the outer side wall of the installation cavity in a rotating mode, the connecting rod penetrates through the sliding groove, and the tail end of the connecting rod is connected with the outer side wall of the fixed box in a rotating mode.
Preferably, a filter screen is fixedly arranged on the inner side wall of the filter tank, and the filter screen is made of polypropylene fibers.
Preferably, the opening and closing mechanism comprises a second pressure spring fixedly connected to the inner side wall of the positioning cavity, the tail end of the second pressure spring is fixedly connected with a positioning block, the positioning block penetrates through the positioning cavity, a pull rod is fixedly connected to the outer side wall of the positioning block, a pulling groove is formed in the outer side wall of the terminal box, the pull rod penetrates through the pulling groove, and the outer side wall of the positioning block abuts against the locking block.
Preferably, the pulling groove communicates with the inside of the fixing groove.
Preferably, the sealing plate is tightly attached to the inner side wall of the filter tank.
Preferably, the positioning block and the locking block are made of austenitic stainless steel, and the positioning block and the locking block are in barb shapes.
Preferably, the outer side wall of the terminal box is symmetrically and fixedly connected with a rocker and a button.
Compared with the prior art, the invention has the beneficial effects that:
1. when the terminal box is required to be used, the pull rod is pushed leftwards, the pull rod drives the positioning block to move leftwards, the positioning block moves leftwards, the positioning block is enabled to lose the limiting function of the locking block, the fixing box is rotated upwards, the fixing box is opened, the fixing box drives the connecting rod to start moving upwards in the process of rotating upwards, the connecting rod drives the sealing plate to move leftwards, the sealing plate moves leftwards to open the filtering tank, a filter screen is arranged on the inner side wall of the filtering tank, the filter screen can filter external dust, the dust is prevented from entering the inside of the terminal box, the service life of the internal components of the terminal box is reduced, after the use is finished, the fixing box is rotated downwards, the locking block is driven to rotate downwards until the locking block abuts against the outer side wall of the positioning block, the terminal box and the fixing box are locked, the fixing box is rotated downwards, and simultaneously, the fixing box drives the sealing plate to move rightwards through the connecting rod, so that the sealing plate is tightly attached to the inner side wall of the filtering tank, the terminal box is prevented from being damaged, and the terminal box is prevented from being damaged.
2. When the terminal box carelessly bumps, the mounting frame can move downwards due to gravity, and the buffer spring can play a damping role on the mounting frame, so that vibration received by the mounting frame is reduced, the safety of the mounting frame is ensured, the locking block is made of austenitic stainless steel, the austenitic stainless steel is stable in structure, and the terminal box can be used for a long time without replacement.
Drawings
Fig. 1 is a perspective view of an unmanned aerial vehicle navigation system terminal with a protection function provided by the invention;
FIG. 2 is a schematic diagram of the structure of the present invention;
FIG. 3 is an enlarged view of part A of the present invention;
FIG. 4 is an enlarged view of part B of the present invention;
FIG. 5 is an enlarged view of part C of the present invention;
fig. 6 is a system block diagram of the present invention.
In the figure: 1 terminal box, 2 constant head tanks, 3 installing frame, 4 first display screen, 5 terminal processor, 6 buffer spring, 7 control case, 8 second display screen, 9 WIFI transmitter, 10 filter tank, 11 filter screen, 12 installation chamber, 13 first pressure spring, 14 closing plate, 15 connecting rod, 16 sliding groove, 17 fixed slot, 18 locating piece, 19 positioning chamber, 20 second pressure spring, 21 pull rod, 22 pulling groove, 23 locking piece, 24 fixed case, 25 terminal central processing module, 26 display module, 27 control module, 28 WIFI transmitting module, 29 WIFI receiving module, 30 unmanned aerial vehicle central processing module, 31 navigation positioning module, 32 ultrasonic ranging module, 33 shooting storage module.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments.
Referring to fig. 1-6, an unmanned aerial vehicle navigation system terminal with a protection function comprises a terminal box 1, a first display screen 4, a terminal processor 5, a control box 7, a second display screen 8, a WIFI emitter 9, a positioning groove 2 formed in the outer side wall of the terminal box 1, the control box 7 fixedly installed on the inner side wall of the terminal box 1, a plurality of buffer springs 6 fixedly connected with the inner bottom of the terminal box 1, a mounting frame 3 fixedly connected with the tail end of the buffer springs 6, the terminal processor 5 installed on the inner bottom of the mounting frame 3, the first display screen 4 installed on the inner side wall of the mounting frame 3, the mounting frame 3 penetrating through the positioning groove 2, a fixing box 24 rotationally connected with the outer side wall of the terminal box 1, the second display screen 8 fixedly installed on the outer side wall of the fixing box 24, the WIFI emitter 9 fixedly connected with the inner side wall of the fixing box 24, a filter tank 10 formed in the bottom of the terminal box 1, a filter screen 11 fixedly installed on the inner side wall of the filter tank 10, a polypropylene fiber formed in the filter screen 11, a mounting cavity 12 formed in the inner side wall of the terminal box 1, a sliding cavity 16 formed in the inner side wall of the terminal box 1, and a sliding cavity 16 formed in the sliding cavity 16 communicated with the sliding cavity 16;
the waterproof mechanism is fixedly connected to the inner side wall of the installation cavity 12, the tail end of the waterproof mechanism is abutted against the inner side wall of the filter tank 10, the waterproof mechanism comprises a first pressure spring 13 fixedly connected to the inner side wall of the installation cavity 12, the tail end of the first pressure spring 13 is fixedly connected with a sealing plate 14, the tail end of the sealing plate 14 penetrates through the installation cavity 12, the tail end of the sealing plate 14 is abutted against the inner side wall of the filter tank 10, the sealing plate 14 is tightly attached to the inner side wall of the filter tank 10, a connecting rod 15 is rotationally connected to the outer side wall of the installation cavity 12, the connecting rod 15 penetrates through a sliding groove 16, the tail end of the connecting rod 15 is rotationally connected with the outer side wall of a fixed box 24, a fixed groove 17 is formed in the outer side wall of the terminal box 1, and a positioning cavity 19 is formed in the terminal box 1;
the inside wall fixedly connected with mechanism that opens and shuts of location chamber 19, the mechanism that opens and shuts includes the second compression spring 20 of fixed connection on the inside wall of location chamber 19, the terminal fixedly connected with locating piece 18 of second compression spring 20, locating piece 18 runs through location chamber 19, fixedly connected with pull rod 21 on the lateral wall of locating piece 18, set up pulling groove 22 on the lateral wall of terminal box 1, pulling groove 22 is linked together with the inside of fixed slot 17, pull rod 21 runs through pulling groove 22, the lateral wall of locating piece 18 offsets tightly with locking piece 23, fixedly connected with locking piece 23 on the lateral wall of fixed box 24, it is tight with the lateral wall of locking piece 23 to open and mechanism, the material of locating piece 18 and locking piece 23 is austenitic stainless steel, the shape of locating piece 18 and locking piece 23 is the barb form, the locking piece 23 of being convenient for offsets tightly with locating piece 18 more, realize locking effect, symmetrical fixedly connected with rocker and button on the lateral wall of terminal box 1.
The control module 27 is installed in the control box 7, the display module 26 is installed in the first display screen 4 and the second display screen 8, the terminal central processing module 25 is installed in the terminal processor 5, the WIFI transmitting module 28 is installed in the WIFI transmitter 9, the terminal processor 5 is electrically connected with the WIFI transmitter 9, the rocker on the outer side wall of the terminal box 1 is electrically connected with the control box 7, the first display screen 4 and the second display screen 8 are electrically connected with the terminal processor 5, the WIFI receiving module 29, the unmanned aerial vehicle central processing module 30, the navigation positioning module 31, the ultrasonic ranging module 32 and the shooting storage module 33 are all installed in the unmanned aerial vehicle, the WIFI transmitting module 28 is connected with the WIFI receiving module 29 in the unmanned aerial vehicle, the shooting storage module 33 stores the shot image, the navigation positioning module 31 transmits the position of the WIFI transmitting module to the unmanned aerial vehicle central processing module 30, the unmanned aerial vehicle central processing module 30 transmits the signals to the WIFI transmitting module 28 through the WIFI receiving module 29, transmits the signals to the terminal central processing module 25 through the WIFI transmitting module 28, finally transmits the signals to the display module 26 through the terminal central processing module 25, displays the self positioning of the unmanned aerial vehicle on the surface of the first display screen 4, transmits the image signals of the shooting storage module 33 to the unmanned aerial vehicle central processing module 30, the unmanned aerial vehicle central processing module 30 transmits the signals to the WIFI transmitting module 28 through the WIFI receiving module 29, transmits the signals to the terminal central processing module 25 through the WIFI transmitting module 28, finally transmits the signals to the display module 26 through the terminal central processing module 25, displays the shot images on the second display screen 8 in real time, the ultrasonic ranging module 32 can identify the obstacle in front of the unmanned aerial vehicle, when the obstacle is encountered in front of the unmanned aerial vehicle, the ultrasonic ranging module 32 transmits signals to the unmanned aerial vehicle central processing module 30, the unmanned aerial vehicle central processing module 30 transmits signals to the terminal central processing module 25 through the WIFI receiving module 29 and the WIFI transmitting module 28, the terminal central processing module 25 transmits signals to the display module 26, the display module is displayed on the first display screen 4, at the moment, the rocker on the outer side wall of the terminal box 1 is controlled, the rocker transmits signals to the control module 27 in the control box 7, the control module 27 transmits signals to the terminal central processing module 25, the terminal central processing module 25 sequentially transmits signals to the unmanned aerial vehicle central processing module 30 through the WIFI transmitting module 28 and the WIFI receiving module 29, and the unmanned aerial vehicle central processing module 30 performs emergency obstacle avoidance on the control power system.
In the invention, when the terminal box is used, the pull rod 21 is pushed leftwards, the pull rod 21 drives the positioning block 18 to move leftwards, the positioning block 18 moves leftwards to compress the second pressure spring 20, the positioning block 18 loses the limit function on the locking block 23, then the fixing box 24 is rotated upwards, the fixing box 24 is rotated to drive the connecting rod 15 to rotate upwards, the connecting rod 15 is rotated upwards and simultaneously drives the sealing plate 14 to move leftwards, the sealing plate 14 is moved leftwards to open the filter tank 10, the situation that heat generated during the operation of components in the terminal box 1 cannot be timely discharged is avoided, external dust can be filtered through the terminal box 1, the external dust is prevented from entering the inside of the terminal box 1, after the flying is finished, the fixing box 24 is rotated downwards to drive the sealing plate 14 to move rightwards through the connecting rod 15 until the sealing plate 14 is tightly attached to the inner side wall of the filter tank 10, moisture is prevented from entering the inside of the terminal box 1 through the filter tank 10, and further the components inside the terminal box 1 are short-circuited, the fixing box 24 drives the locking block 23 to rotate downwards, the locking block 23 is tightly abutted against the outer side wall of the fixing box 18, and the locking of the terminal box 1 and the terminal box 24 are realized.
The foregoing is only a preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art, who is within the scope of the present invention, should make equivalent substitutions or modifications according to the technical scheme of the present invention and the inventive concept thereof, and should be covered by the scope of the present invention.
Claims (8)
1. The utility model provides an unmanned aerial vehicle navigation system terminal with protect function, includes terminal box (1), first display screen (4), terminal treater (5), control case (7), second display screen (8), WIFI transmitter (9), its characterized in that, locating slot (2) have been seted up on the lateral wall of terminal box (1), control case (7) fixed mounting on the inside wall of terminal box (1), the interior bottom fixedly connected with a plurality of buffer spring (6) of terminal box (1), the terminal fixedly connected with installing frame (3) of buffer spring (6), terminal treater (5) are installed on the interior bottom of installing frame (3), install frame (3) run through constant head tank (2) on the inside wall of installing frame (3), rotate on the lateral wall of terminal box (1) and be connected with fixed box (24), second display screen (8) fixed mounting is on the lateral wall of fixed box (24), install on the inside wall (16) of terminal box (1) are seted up on the inside wall of terminal box (1) of filter chamber (9) fixed connection on the inside wall (24), the utility model discloses a waterproof device for the filter tank of the filter tank, including installation cavity (12), fixed slot (17), positioning cavity (19) have been seted up to the inside of terminal box (1), the inside wall fixedly connected with mechanism that opens and shuts of positioning cavity (19), fixedly connected with locking piece (23) on the lateral wall of fixed box (24), the outside wall of mechanism and locking piece (23) that opens and shuts offsets tightly on the lateral wall of terminal box (1), installation cavity (12) are linked together with sliding tray (16), fixedly connected with waterproof mechanism on the inside wall of installation cavity (12), terminal end and the inside wall of filter tank (10) are offset tightly.
2. The unmanned aerial vehicle navigation system terminal with the protection function according to claim 1, wherein the waterproof mechanism comprises a first pressure spring (13) fixedly connected to the inner side wall of the installation cavity (12), the tail end of the first pressure spring (13) is fixedly connected with a sealing plate (14), the tail end of the sealing plate (14) penetrates through the installation cavity (12), the tail end of the sealing plate (14) abuts against the inner side wall of the filter tank (10), a connecting rod (15) is rotationally connected to the outer side wall of the installation cavity (12), the connecting rod (15) penetrates through the sliding groove (16), and the tail end of the connecting rod (15) is rotationally connected with the outer side wall of the fixed box (24).
3. The unmanned aerial vehicle navigation system terminal with the protection function according to claim 1, wherein a filter screen (11) is fixedly arranged on the inner side wall of the filter tank (10), and the filter screen (11) is made of polypropylene fibers.
4. The unmanned aerial vehicle navigation system terminal with the protection function according to claim 1, wherein the opening and closing mechanism comprises a second pressure spring (20) fixedly connected to the inner side wall of the positioning cavity (19), the tail end of the second pressure spring (20) is fixedly connected with a positioning block (18), the positioning block (18) penetrates through the positioning cavity (19), a pull rod (21) is fixedly connected to the outer side wall of the positioning block (18), a pulling groove (22) is formed in the outer side wall of the terminal box (1), the pull rod (21) penetrates through the pulling groove (22), and the outer side wall of the positioning block (18) abuts against the locking block (23).
5. The unmanned aerial vehicle navigation system terminal with the protection function according to claim 4, wherein the pulling groove (22) is communicated with the inside of the fixing groove (17).
6. The unmanned aerial vehicle navigation system terminal with the protection function according to claim 2, wherein the sealing plate (14) is tightly attached to the inner side wall of the filter tank (10).
7. The unmanned aerial vehicle navigation system terminal with the protection function according to claim 4, wherein the positioning block (18) and the locking block (23) are made of austenitic stainless steel, and the positioning block (18) and the locking block (23) are in barb shapes.
8. The unmanned aerial vehicle navigation system terminal with the protection function according to claim 1, wherein a rocker and a button are symmetrically and fixedly connected on the outer side wall of the terminal box (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011143518.2A CN112363529B (en) | 2020-10-23 | 2020-10-23 | Unmanned aerial vehicle navigation system terminal with protect function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011143518.2A CN112363529B (en) | 2020-10-23 | 2020-10-23 | Unmanned aerial vehicle navigation system terminal with protect function |
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| Publication Number | Publication Date |
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| CN112363529A CN112363529A (en) | 2021-02-12 |
| CN112363529B true CN112363529B (en) | 2024-02-02 |
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| CN202011143518.2A Active CN112363529B (en) | 2020-10-23 | 2020-10-23 | Unmanned aerial vehicle navigation system terminal with protect function |
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| CN112363529A (en) | 2021-02-12 |
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