CN110171575A - A kind of unmanned plane with multi-faceted defencive function - Google Patents
A kind of unmanned plane with multi-faceted defencive function Download PDFInfo
- Publication number
- CN110171575A CN110171575A CN201910331005.5A CN201910331005A CN110171575A CN 110171575 A CN110171575 A CN 110171575A CN 201910331005 A CN201910331005 A CN 201910331005A CN 110171575 A CN110171575 A CN 110171575A
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- main body
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- 230000035939 shock Effects 0.000 abstract description 9
- 230000006870 function Effects 0.000 description 17
- 238000000034 method Methods 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000009993 protective function Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Studio Devices (AREA)
Abstract
The invention belongs to unmanned plane fields, especially a kind of unmanned plane with multi-faceted defencive function, once there is accidental falling situation for existing unmanned plane, camera will be faced with the misfortune of damage, the problem of causing damages to user, now propose following scheme, it includes unmanned plane main body, the four sides of the unmanned plane main body is fixedly installed with wing, one end of the wing is fixedly installed with propeller cabin, the bottom of the unmanned plane main body is provided with camera, the configuration of the present invention is simple, shock sensor, which detects, can pass to driving motor for signal when vibration, driving motor can be detached from the first L-type plate with moving cam, tension spring can cover on camera in cylindrical box, two rotor plates on the same wing can open simultaneously, so that when falling, camera can be effectively protected, it avoids causing damages to user, It realizes to the multi-faceted defencive function of unmanned plane main body, it is easy to use.
Description
Technical field
The present invention relates to air vehicle technique field more particularly to a kind of unmanned planes with multi-faceted defencive function.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation.Unmanned plane+industrial application is that unmanned plane has really just needed.Currently, unmanned plane is logical
The function camera for carrying every different size is crossed, to be widely used in various fields, for example take photo by plane, field search and rescue, video display bat
Take the photograph etc. field.
Wherein camera is extremely important component on unmanned plane, while being also that damage is easiest to when unmanned plane falls
Component often will appear due to occurring interrupting etc. powerup issue and communication system in the use process of unmanned plane
Accidental falling, and once there is accidental falling situation in unmanned plane, camera will be faced with the misfortune of damage, cause to user
Loss, so it is proposed that a kind of unmanned plane with multi-faceted defencive function, to solve the problems, such as above-mentioned be previously mentioned.
Summary of the invention
The purpose of the present invention is to solve unmanned plane exists in the prior art accidental falling situation, camera once occur
It will be faced with the misfortune of damage, the shortcomings that cause damages to user, and proposed a kind of with multi-faceted defencive function
Unmanned plane.
A kind of unmanned plane with multi-faceted defencive function proposed by the present invention, including unmanned plane main body, the unmanned plane
The four sides of main body is fixedly installed with wing, and one end of the wing is fixedly installed with propeller cabin, the unmanned plane main body
Bottom is provided with camera, and the side of the unmanned plane main body is fixedly installed with shock sensor, the bottom of the unmanned plane main body
Portion is fixedly installed with the first slide bar and the second slide bar respectively, and first slide bar and the second slide bar are located at the two of camera
Side slidably connects the first L-type plate and the second L-type plate on the outer wall of first slide bar and on the outer wall of the second slide bar respectively,
Be arranged with tension spring on the outer wall of first slide bar, the top and bottom end of the tension spring respectively with the bottom of unmanned plane main body and
The top of one L-type plate is mutually welded, and the first L-type plate and the second L-type plate side close to each other are fixedly installed with the same circle
Ring, the camera are located in annulus, and the bottom of the annulus is fixedly installed with cylindrical box, and the cylindrical box is located at camera
Underface, the side of the unmanned plane main body are fixedly installed with driving motor, vertical welding on the output shaft of the driving motor
There is cam, is in contact at the top of the bottom of the cam and the first L-type plate；
Guide rod is welded in the side that the first L-type plate and the second L-type plate are located remotely from each other, and the top of two guide rods is passed through respectively
It wears two wings and extends respectively to the top of two wings, the side of two wings is symmetrically rotatablely connected there are two shaft,
One end of the shaft is welded with gear, and two gears being located on the same wing are meshed, the side weldering of the shaft
It is connected to rotor plate, and two rotor plates being located on same wing side close to each other is fixedly installed with the first magnet respectively
With the second magnet, first magnet and the second magnet mutually attract, and the bottom side of the underlying rotor plate is fixed to be connected
It is connected to drawstring, two drawstrings one end close to each other is fixedly connected with the outer wall of two guide rods respectively, and the bottom of two wings is equal
It is rotatably connected to sheave, the top of the drawstring is in contact with the inner wall of sheave.
Preferably, the first L-type plate and the second L-type plate side close to each other are welded with mounting post, two installations
Column one end close to each other is mutually welded with the two sides of annulus respectively, can by mounting post by annulus be fixed on the first L-type plate and
On second L-type plate.
Preferably, the two sides of the bottom of the annulus are welded with support rod, the bottom of the support rod and the top of cylindrical box
Portion is mutually welded, and cylindrical box can be fixed on annulus by support rod.
Preferably, the bottom of first slide bar and the bottom of the second slide bar are welded with limit plate, two limit plates point
Not Wei Yu the lower section of the first L-type plate and the lower section of the second L-type plate, two limit plates can be respectively to the first slide bar and the second slide bar
It is limited.
Preferably, the bottom of two wings is fixedly installed with cylinder, and the side of the sheave is welded with rotation axis, described
One end of rotation axis and the side of cylinder are rotatablely connected, and the cylinder can be supported sheave.
Preferably, baffle is welded at the top of the guide rod, the baffle is located at the top of wing, and the baffle can be right
Guide rod is limited.
Preferably, the top of the first L-type plate and the top of the second L-type plate are welded with stiffening plate, the stiffening plate
Side and the side of guide rod mutually weld, the stiffening plate can increase by the first L-type plate and the connection of the second L-type plate and guide rod is strong
Degree.
Preferably, sponge is fixedly installed in the bottom interior wall of the cylindrical box, the side of the rotor plate is welded with bullet
Spring, one end of the spring are fixedly installed with ball, and the spring and ball can play the role of buffering.
The beneficial effects of the present invention are: shock sensor can work and signal is passed to driving motor when falling, drive
Dynamic motor can be detached from the first L-type plate with moving cam, and tension spring can pull the first L-type plate, the first L to the direction of drone body
Template can drive annulus and the second L-type plate to be moved to the direction of drone body, and annulus can drive support rod to carry out
Mobile, support rod can drive cylindrical box to carry out mobile to the direction of camera and can cover on camera in cylindrical box；
The first L-type plate and the second L-type plate can drive two guide rods to move up respectively simultaneously, and guide rod can pull
Rope, drawstring can pull rotor plate and rotate backward two gears, and then two rotor plate meetings being located on the same wing
It opens, then rotor plate can be when falling with ground face contact, and in addition rubber ball and spring can play when contacting ground
Buffer function.
The configuration of the present invention is simple, shock sensor, which detects, can pass to signal driving motor, driving motor when vibration
It can be detached from the first L-type plate with moving cam, tension spring can cover on camera in cylindrical box, while two on the same wing
Rotor plate can open, so that camera can be effectively protected when falling, avoid causing damages to user, realize pair
The multi-faceted defencive function of unmanned plane main body, it is easy to use.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of the unmanned plane with multi-faceted defencive function proposed by the present invention；
Fig. 2 is a kind of enlarged drawing of the part A of the unmanned plane with multi-faceted defencive function proposed by the present invention；
Fig. 3 is a kind of structural schematic diagram of the rotor plate of the unmanned plane with multi-faceted defencive function proposed by the present invention；
Fig. 4 is a kind of top view of the rotor plate of the unmanned plane with multi-faceted defencive function proposed by the present invention；
Fig. 5 is a kind of three-dimensional figure of the cylindrical box of the unmanned plane with multi-faceted defencive function proposed by the present invention.
In figure: 1 unmanned plane main body, 2 wings, 3 baffles, 4 rotor plates, 5 propeller cabins, 6 drawstrings, 7 sheaves, 8 first L-types
Plate, 9 guide rods, 10 shock sensors, 11 driving motors, 12 cams, 13 second L-type plates, 14 stiffening plates, 15 tension springs, 16 first are slided
Bar, 17 second slide bars, 18 mounting posts, 19 cylinders, 20 cylindrical box, 21 sponges, 22 cameras, 23 support rods, 24 annulus, 25 limits
Plate, 26 gears, 27 first magnet, 28 second magnet, 29 balls, 30 shafts, 31 springs.
Specific embodiment
Combined with specific embodiments below the present invention is made further to explain.
Embodiment
The present embodiment proposes a kind of unmanned plane with multi-faceted defencive function, including unmanned plane main body 1, unmanned owner
The four sides of body 1 is fixedly installed with wing 2, and one end of wing 2 is fixedly installed with propeller cabin 5, and the bottom of unmanned plane main body 1 is set
It is equipped with camera 22, the side of unmanned plane main body 1 is fixedly installed with shock sensor 10, and the bottom of unmanned plane main body 1 is solid respectively
Dingan County is equipped with the first slide bar 16 and the second slide bar 17, and the first slide bar 16 and the second slide bar 17 are located at the two sides of camera 22,
The first L-type plate 8 and the second L-type plate 13 are slidably connected on the outer wall of first slide bar 16 and respectively on the outer wall of second slide bar 17,
Be arranged with tension spring 15 on the outer wall of first slide bar 16, the top and bottom end of tension spring 15 respectively with the bottom of unmanned plane main body 1 and
The top of one L-type plate 8 is mutually welded, and the first L-type plate 8 and the second L-type plate 13 side close to each other are fixedly installed with the same circle
Ring 24, camera 22 are located in annulus 24, and the bottom of annulus 24 is fixedly installed with cylindrical box 20, and cylindrical box 20 is located at camera 22
Underface, the side of unmanned plane main body 1 is fixedly installed with driving motor 11, is vertically welded on the output shaft of driving motor 11
Cam 12, the bottom of cam 12 are in contact with the top of the first L-type plate 8；
Weld guide rod 9, the top difference of two guide rods 9 in the side that first L-type plate 8 and the second L-type plate 13 are located remotely from each other
Through two wings 2 and extend respectively to the tops of two wings 2, the side of two wings 2 is symmetrically there are two rotation connections
Shaft 30, one end of shaft 30 is welded with gear 26, and two gears 26 being located on the same wing 2 are meshed, shaft 30
Side be welded with rotor plate 4, and two rotor plates 4 being located on the same wing 2 side close to each other fixed peace respectively
Equipped with the first magnet 27 and the second magnet 28, the first magnet 27 mutually attracts with the second magnet 28, the bottom of underlying rotor plate 4
Portion side is fixedly connected with drawstring 6, and two drawstrings 6 one end close to each other is fixedly connected with the outer wall of two guide rods 9 respectively, and two
The bottom of a wing 2 is rotatably connected to sheave 7, and the top of drawstring 6 is in contact with the inner wall of sheave 7, and when falling, vibration is passed
Signal is simultaneously passed to driving motor 11 by the meeting work of sensor 10, and driving motor 11 can be detached from the first L-type plate 8 with moving cam 12,
Tension spring 15 can pull the first L-type plate 8 to the direction of drone body 1, and the first L-type plate 8 can drive annulus 24 and the second L-type
Plate 13 is moved to the direction of drone body 1, and annulus 24 can drive support rod 23 to be moved, and support rod 23 can band
Dynamic cylindrical box 20 carries out mobile and can cover on camera 22 in cylindrical box 20 to the direction of camera 22, while the first L-type plate 8
Two guide rods 9 can be driven to move up respectively with the second L-type plate 13, guide rod 9 can pull drawstring 6, and drawstring 6, which can pull, to be turned
Movable plate 4 simultaneously rotates backward two gears 26, and then two rotor plates 4 being located on the same wing 2 can open, then rotor plate
4 can be when falling with ground face contact, and in addition ball 29 and spring 31 can play buffer function when contacting ground,
The configuration of the present invention is simple, shock sensor 10, which detects, can pass to signal driving motor 11 when vibration, driving motor 11 can
It is detached from the first L-type plate 8 with band moving cam 12, tension spring 15 can cover on camera 22 in cylindrical box 20, while the same wing 2
On two rotor plates 4 can open so that camera 22 can be effectively protected when falling, avoid causing to damage to user
It loses, realizes to the multi-faceted defencive function of unmanned plane main body 1, easy to use, the wherein model SW- of shock sensor 10
1801P。
In the present embodiment, the first L-type plate 8 and the second L-type plate 13 side close to each other are welded with mounting post 18, and two
The one end close to each other of mounting post 18 is mutually welded with the two sides of annulus 24 respectively, can be fixed on annulus 24 by mounting post 18
On first L-type plate 8 and the second L-type plate 13.
In the present embodiment, the two sides of the bottom of annulus 24 are welded with support rod 23, the bottom of support rod 23 and cylindrical box 20
Top mutually weld, cylindrical box 20 can be fixed on annulus 24 by support rod 23.
In the present embodiment, the bottom of the bottom of the first slide bar 16 and the second slide bar 17 is welded with limit plate 25, two limits
Position plate 25 is located at the lower section of the first L-type plate 8 and the lower section of the second L-type plate 13, and two limit plates 25 can be respectively to first
Slide bar 16 and the second slide bar 17 are limited.
In the present embodiment, the bottom of two wings 2 is fixedly installed with cylinder 19, and the side of sheave 7 is welded with rotation axis,
One end of rotation axis and the side of cylinder 19 are rotatablely connected, and cylinder 19 can be supported sheave 7.
In the present embodiment, the top of guide rod 9 is welded with baffle 3, and baffle 3 is located at the top of wing 2, and baffle 3 can be to leading
Bar 9 is limited.
In the present embodiment, the top of the top of the first L-type plate 8 and the second L-type plate 13 is welded with stiffening plate 14, stiffening plate
14 side and the side of guide rod 9 are mutually welded, and stiffening plate 14 can increase the first L-type plate 8 and the second L-type plate 13 and guide rod 9
Bonding strength.
In the present embodiment, sponge 21 is fixedly installed in the bottom interior wall of cylindrical box 20, the side of rotor plate 4 is welded with bullet
Spring 31, one end of spring 31 are fixedly installed with ball 29, and spring 31 and ball 29 can play the role of buffering.
In the present embodiment, power on, when falling, signal is simultaneously passed to driving motor by the meeting work of shock sensor 10
11, driving motor 11 is rotated with moving cam 12, and when cam 12 is detached from the first L-type plate 8, tension spring 15 can be to unmanned plane sheet
The direction of body 1 pulls the first L-type plate 8, and the first L-type plate 8 drives annulus 24 to be moved to the direction of drone body 1, annulus
24 the second L-type plates 13 of drive are moved to the direction of drone body 1, then the second L-type plate 13 can be enterprising in the second slide bar 17
Row sliding, in addition annulus 24 will drive support rod 23 and be moved, and support rod 23 drives cylindrical box 20 to the direction of camera 22
It carries out mobile and camera 22 can be covered in cylindrical box 20, while the first L-type plate 8 and the second L-type plate 13 can drive respectively
Two guide rods 9 move up, and guide rod 9 will pull drawstring 6, and drawstring 6 can slide on sheave 7, and drawstring 6 will pull rotor plate 4
And rotor plate 4 is rotated, rotor plate 4 can be such that the first magnet 27 and the second magnet 28 separates, and in addition rotor plate 4 can make
Two gears 26 rotate backward, and then two rotor plates 4 being located on the same wing 2 can open, then rotor plate 4 can fall
With ground face contact when falling, in addition ball 29 and spring 31 can play buffer function when contacting ground, so that falling
When falling, camera 22 can be effectively protected, avoid causing damages to user, realize to the multi-faceted guarantor of unmanned plane main body 1
Protective function, it is easy to use.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (8)
1. a kind of unmanned plane with multi-faceted defencive function, including unmanned plane main body (1), the four of the unmanned plane main body (1)
Face is fixedly installed with wing (2), and one end of the wing (2) is fixedly installed with propeller cabin (5), the unmanned plane main body
(1) bottom is provided with camera (22), which is characterized in that the side of the unmanned plane main body (1) is fixedly installed with vibration and passes
Sensor (10), the bottom of the unmanned plane main body (1) is fixedly installed with the first slide bar (16) and the second slide bar (17) respectively, described
First slide bar (16) and the second slide bar (17) are located at the two sides of camera (22), on the outer wall of first slide bar (16) and
The first L-type plate (8) and the second L-type plate (13), first slide bar are slidably connected on the outer wall of second slide bar (17) respectively
(16) it is arranged on outer wall tension spring (15), the top and bottom end of the tension spring (15) bottom with unmanned plane main body (1) respectively
It is mutually welded with the top of the first L-type plate (8), the first L-type plate (8) and the second L-type plate (13) side close to each other are fixed
It is equipped with the same annulus (24), the camera (22) is located in annulus (24), and the bottom of the annulus (24) is fixedly mounted
Have cylindrical box (20), the cylindrical box (20) is located at the underface of camera (22), and the side of the unmanned plane main body (1) is fixed
It is equipped with driving motor (11), is vertically welded with cam (12) on the output shaft of the driving motor (11), the cam (12)
Bottom and the first L-type plate (8) at the top of be in contact；
The side that the first L-type plate (8) and the second L-type plate (13) are located remotely from each other is welded guide rod (9), two guide rods (9)
Top extends through two wings (2) and extends respectively to the top of two wings (2), and the side of two wings (2) is symmetrical
There are two shaft (30), one end of the shaft (30) to be welded with gear (26) for rotation connection, and is located on the same wing (2)
Two gears (26) be meshed, the side of the shaft (30) is welded with rotor plate (4), and be located at the same wing (2) on
Two rotor plate (4) sides close to each other be fixedly installed with the first magnet (27) and the second magnet (28) respectively, described
One magnet (27) mutually attracts with the second magnet (28), and the bottom side of the underlying rotor plate (4) is fixedly connected with drawing
It restricts (6), two drawstrings (6) one end close to each other is fixedly connected with the outer wall of two guide rods (9) respectively, two wings (2)
Bottom is rotatably connected to sheave (7), and the top of the drawstring (6) is in contact with the inner wall of sheave (7).
2. a kind of unmanned plane with multi-faceted defencive function according to claim 1, which is characterized in that the first L
Template (8) and the second L-type plate (13) side close to each other are welded with mounting post (18), and two mounting posts (18) are close to each other
Two sides of the one end respectively with annulus (24) mutually weld.
3. a kind of unmanned plane with multi-faceted defencive function according to claim 1, which is characterized in that the annulus
(24) two sides of the bottom are welded with support rod (23), and the bottom of the support rod (23) and the top of cylindrical box (20) are mutually welded
It connects.
4. a kind of unmanned plane with multi-faceted defencive function according to claim 1, which is characterized in that described first is sliding
The bottom of bar (16) and the bottom of the second slide bar (17) are welded with limit plate (25), and two limit plates (25) are located at first
The lower section of the lower section of L-type plate (8) and the second L-type plate (13).
5. a kind of unmanned plane with multi-faceted defencive function according to claim 1, which is characterized in that two wings
(2) bottom is fixedly installed with cylinder (19), and the side of the sheave (7) is welded with rotation axis, one end of the rotation axis
It is rotatablely connected with the side of cylinder (19).
6. a kind of unmanned plane with multi-faceted defencive function according to claim 1, which is characterized in that the guide rod
(9) it is welded at the top of baffle (3), the baffle (3) is located at the top of wing (2).
7. a kind of unmanned plane with multi-faceted defencive function according to claim 1, which is characterized in that the first L
The top of template (8) and the top of the second L-type plate (13) are welded with stiffening plate (14), the side of the stiffening plate (14) with lead
It mutually welds the side of bar (9).
8. a kind of unmanned plane with multi-faceted defencive function according to claim 1, which is characterized in that the cylindrical box
(20) it is fixedly installed in bottom interior wall sponge (21), the side of the rotor plate (4) is welded with spring (31), the spring
(31) one end is fixedly installed with ball (29).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910331005.5A CN110171575B (en) | 2019-04-23 | 2019-04-23 | Unmanned aerial vehicle with diversified protect function |
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|---|---|---|---|
| CN201910331005.5A CN110171575B (en) | 2019-04-23 | 2019-04-23 | Unmanned aerial vehicle with diversified protect function |
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| CN110171575A true CN110171575A (en) | 2019-08-27 |
| CN110171575B CN110171575B (en) | 2022-10-04 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113816232A (en) * | 2021-09-30 | 2021-12-21 | 本溪市特种设备监督检验所 | Monitoring device for special equipment inspection and use method thereof |
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