CN214690238U - Double-light video holder and unmanned aerial vehicle - Google Patents

Double-light video holder and unmanned aerial vehicle Download PDF

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Publication number
CN214690238U
CN214690238U CN202023285380.8U CN202023285380U CN214690238U CN 214690238 U CN214690238 U CN 214690238U CN 202023285380 U CN202023285380 U CN 202023285380U CN 214690238 U CN214690238 U CN 214690238U
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China
Prior art keywords
assembly
quick release
control box
function control
optical
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CN202023285380.8U
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Chinese (zh)
Inventor
黄黎明
张焱
古文仁
盛志刚
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Shenzhen Pegasus Robotics Co ltd
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Shenzhen Feima Robotics Co ltd
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Abstract

The utility model discloses a double-light video holder, which comprises a quick-release component, a vibration-damping component, an antenna component, an optical equipment component and a rotating component, wherein the quick-release component is used for quickly and accurately disassembling the holder and an unmanned aerial vehicle; the vibration reduction assembly comprises a vibration reduction frame and an elastic body positioned below the vibration reduction frame; the quick release assembly is arranged on the vibration damping frame; the antenna assembly comprises a function control box and antennas extending out of the left side wall and the right side wall of the function control box; the function control box is arranged below the elastic body; the upper end of the rotating assembly is connected with the function control box body, and the lower end of the rotating assembly is connected with the optical equipment assembly; the optical equipment assembly is a bifocal lens. The utility model discloses a double-light video holder, which is provided with a left antenna and a right antenna, and can reduce the weight of an unmanned aerial vehicle when the holder load is not used; the optical equipment assembly adopts double lenses, and different shooting requirements can be met. The utility model also discloses an unmanned aerial vehicle.

Description

Double-light video holder and unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a two light video cloud platforms and unmanned aerial vehicle.
Background
The pan-tilt is mounted on the bearing member as a supporting device for mounting and fixing electrical equipment such as a camera, and is widely applied to the fields of photography, monitoring and the like. In the unmanned aerial vehicle technical field, the optical equipment that current cloud platform carried on only has a camera lens, can't satisfy the shooting demand to different scenes, and current cloud platform does not take the antenna, and the antenna need add the unmanned aerial vehicle body on, can increase unmanned aerial vehicle weight when not using the cloud platform. In addition, current antenna assembly is on unmanned aerial vehicle, and the signal line overlength, the signal weakens greatly.
Present cloud platform and unmanned aerial vehicle fixed connection adopt the screw to lock fixedly mostly, and the dismouting operation is complicated, inefficiency. And the unmanned aerial vehicle that the tradition carried on optical equipment has very big vibrations because air disturbance and self power when normal flight, shoots the image and rocks, can not clear see the image of shooing, seriously influences optical equipment's shooting effect.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a two light video cloud platforms and unmanned aerial vehicle just in order to solve above-mentioned problem.
The utility model discloses a following technical scheme realizes above-mentioned purpose:
a dual-optical video holder comprises a quick release assembly, a vibration reduction assembly, an antenna assembly, an optical equipment assembly and a rotating assembly, wherein the quick release assembly is used for quickly and accurately dismounting the holder and an unmanned aerial vehicle; the vibration reduction assembly comprises a vibration reduction frame and an elastic body positioned below the vibration reduction frame; the quick release assembly is arranged on the vibration damping frame; the antenna assembly comprises a function control box and antennas extending out of the left side wall and the right side wall of the function control box; the function control box is arranged below the elastic body; the upper end of the rotating assembly is connected with the function control box body, and the lower end of the rotating assembly is connected with the optical equipment assembly; the optical device assembly includes a bifocal lens.
Preferably, the bifocal lens includes either or both of a visible optical device or a non-visible optical imaging device.
Preferably, the visible light device is a visible light camera; the invisible optical imaging device is an infrared thermal imager.
Preferably, the visible optical devices are binocular cameras having different focal lengths.
Preferably, the elastic body is a rubber body or a spring.
Preferably, the quick release assembly comprises a quick release device cover, a hollow quick release button, a quick release button bracket, a second spring sleeved inside the quick release button, a quick release socket interface communicated with the unmanned aerial vehicle and a quick release device shell used for accommodating the quick release assembly; the quick release button comprises a clamping tongue part and a pressing part, and two ends of the second spring are respectively abutted with the lower end of the clamping tongue part and a boss on the quick release socket interface.
Preferably, the rotating assembly comprises a heading motor, a first connecting arm, a rolling motor, a second connecting arm and a pitching motor; the course motor is arranged at the bottom of the function control box; the two ends of the first connecting arm are respectively connected with a course motor and a rolling motor; two ends of the second connecting arm are respectively connected with the roll motor and the pitching motor; the pitching motor is connected with the optical equipment assembly.
Preferably, a guide block is arranged on the outer side wall of the quick release device shell.
Preferably, the outside of the side wall of the function control box is provided with a lug, the vibration reduction frame is provided with a connecting hole, the elastic body is of a hollow structure, and the vibration reduction frame, the elastic body and the function control box body are sequentially connected through the connecting hole and the lug.
The utility model also provides an unmanned aerial vehicle, including foretell two optical video cloud platforms.
Has the advantages that: the cloud platform is from taking the antenna, can alleviate unmanned aerial vehicle's weight, is equipped with two left and right sides antennas, can ensure that the signal does not have the dead angle. The holder optical equipment is provided with the twin-lens, so that different shooting requirements can be met, and different shooting environments can be adapted. Meanwhile, the double-light video cradle head provided by the utility model has a quick-release structure and a vibration damping structure, the quick-release structure can realize the quick disassembly of the cradle head and the unmanned aerial vehicle, the structural design is simple, the operation is convenient, and the continuity performance is reliable; the vibration reduction structure can improve the shooting stability of the optical equipment and improve the shooting effect, and is simple in structure and low in cost.
Drawings
Fig. 1 is a schematic perspective view of a dual-optical video pan/tilt head according to the present invention.
Fig. 2 is a schematic view of a first viewing angle of the dual-optical video platform according to the present invention.
Fig. 3 is a schematic view of a second viewing angle of the dual-optical video platform according to the present invention.
Fig. 4 is a schematic structural diagram of a quick release assembly in a dual-optical video pan/tilt head according to an embodiment of the present invention.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings, and obviously, the described embodiments are some, but not all embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it is to be noted that the terms "mounted" and "connected" are to be construed broadly and, for example, may be fixedly connected, detachably connected, or integrally connected unless otherwise explicitly stated or limited. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1 to 4, a dual-optical video platform comprises a quick release assembly 100, a vibration damping assembly 200, an antenna assembly 300, an optical device assembly 400 and a rotation assembly 500, wherein the quick release assembly 100 comprises a quick release cover 111, a hollow quick release button 112, a quick release button bracket 113, a second spring 114 sleeved inside the quick release button, a quick release socket interface 115 communicated with an unmanned aerial vehicle, and a quick release housing 116 for accommodating the quick release assembly; quick release cover 111 and quick release housing 116 form a housing that houses quick release assembly 100. The quick release button 112 includes a latch 1121 and a pressing portion 1122, the latch 1121 protrudes outward from the upper surface of the quick release button 112, and the pressing portion 1122 protrudes outward from a side wall of the quick release button 112. The upper end of the second spring 114 abuts against the lower end of the latch 1121, and the lower end of the second spring 114 abuts against a boss 1151 on the quick release socket interface 115. The quick release cover 111 and the quick release button bracket 113 have a first opening 1111 and a second opening 1131 on the upper surface thereof for the latch 1121 to extend out. The quick release button support 113 is disposed on the quick release button 112, and the latch portion 1121 protrudes from the second opening 1131 of the upper surface. The side wall of the quick release device housing 116 is provided with a third opening 1161 for the pressing portion 1122 to extend. And guide blocks 1162 are arranged on the other two side walls intersecting with the direction of the third opening 1161. When installing with unmanned aerial vehicle, block tongue portion 1121 receives the extrusion, and second spring 114 contracts, and block tongue portion 1121 removes to the direction that is close to second spring 114, and when the draw-in groove of unmanned aerial vehicle installation face slided to block tongue portion 1121 top, second spring 114 obtained the release, and block tongue portion 1121 stretches out and blocks with the unmanned aerial vehicle draw-in groove. When the cloud platform is dismantled with unmanned aerial vehicle, press and press portion 1122, block tongue portion 1121 removes to the direction that is close to second spring 114, and second spring 114 atress shrink breaks away from with the unmanned aerial vehicle draw-in groove. When the clamping tongue portion 1121 is not squeezed, the protruding state is kept, and the clamping tongue portion 1121 is conveniently clamped with the unmanned aerial vehicle clamping groove quickly and accurately again.
The damping module 200 includes a damping frame 210 and an elastic body 220 located below the damping frame, wherein the elastic body 220 is a hollow and soft sphere. The quick release assembly 100 is disposed on the vibration damping frame 210; the antenna assembly 300 includes a function control box 310 and antennas 320 protruding from left and right sidewalls of the function control box 310; four lugs 311 are arranged on the outer side of the side wall of the function control box 310, four connecting holes 211 are correspondingly arranged on the vibration damping frame 210, and the vibration damping frame 210, the elastic body 220 and the function control box 310 are sequentially connected through the connecting holes 211 and the lugs 311 by parts such as bolts or bolts; when the cloud platform carries on unmanned aerial vehicle, because factor damping subassembly 200 such as gravity is in by tensile state, when unmanned aerial vehicle self vibration or air interference caused the vibration, by tensile elastomer 220 can absorb the vibration, guarantee optical equipment's steady shooting effect. The function control box 310 accommodates therein electronic components for controlling the rotation of the motor and for photographing by the optical device.
The rotating assembly 500 comprises a heading motor 510, a first connecting arm 520, a rolling motor 530, a second connecting arm 540 and a pitching motor 550; the heading motor 510 is arranged at the bottom of the function control box 310; two ends of the first connecting arm 520 are respectively connected with a heading motor 510 and a rolling motor 530; the two ends of the second connecting arm 540 are respectively connected with the roll motor 530 and the pitch motor 550; the two tilting motors 550 are connected to the left and right ends of the optical device module 400, respectively. The rotation assembly 500 may help the optical device assembly to perform photographing at different angles.
The optical device assembly 400 includes a bifocal lens 410. The bifocal lens 410 can be a visible camera equipped with two lenses of different focal lengths, can also be two thermal infrared imagers, and can also be a visible camera and a thermal infrared imager. The embodiment adopts the visible light camera with two lenses with different focal lengths, and can meet the shooting requirements of different distances and different scenes.
Finally, it should be noted that: the above embodiments are merely illustrative of the technical solutions, not restrictive; although described in detail with reference to the foregoing embodiments, those of ordinary skill in the art will understand that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions.

Claims (10)

1. A double-optical video holder is characterized by comprising a quick-release assembly, a vibration reduction assembly, an antenna assembly, an optical equipment assembly and a rotating assembly, wherein the quick-release assembly is used for quickly and accurately dismounting the holder and an unmanned aerial vehicle; the vibration reduction assembly comprises a vibration reduction frame and an elastic body positioned below the vibration reduction frame; the quick release assembly is arranged on the vibration damping frame; the antenna assembly comprises a function control box and antennas extending out of the left side wall and the right side wall of the function control box; the function control box is arranged below the elastic body; the upper end of the rotating assembly is connected with the function control box body, and the lower end of the rotating assembly is connected with the optical equipment assembly; the optical device assembly includes a bifocal lens.
2. A bi-optic video head as claimed in claim 1 wherein said bi-optic lens comprises either or both of a visible optical device or an invisible optical imaging device.
3. A dual-light video pan/tilt head as claimed in claim 2, wherein the visible light device is a visible light camera; the invisible optical imaging device is an infrared thermal imager.
4. A dual-light video head as claimed in claim 2 wherein the visible optical devices are binocular cameras having different focal lengths.
5. A dual-light video head as claimed in claim 1, wherein the elastomer is a rubber or spring.
6. A dual optical video pan/tilt head as claimed in claim 1, wherein the quick release assembly comprises a quick release cover, a hollow quick release button, a quick release button bracket, a second spring fitted inside the quick release button, a quick release socket interface communicating with the unmanned aerial vehicle, and a quick release housing for accommodating the quick release assembly; the quick release button comprises a clamping tongue part and a pressing part, and two ends of the second spring are respectively abutted with the lower end of the clamping tongue part and a boss on the quick release socket interface.
7. A dual-optic video head as claimed in claim 1 wherein the rotational assembly comprises a heading motor, a first link arm, a roll motor, a second link arm, a pitch motor; the course motor is arranged at the bottom of the function control box; the two ends of the first connecting arm are respectively connected with a course motor and a rolling motor; two ends of the second connecting arm are respectively connected with the roll motor and the pitching motor; the pitching motor is connected with the optical equipment assembly.
8. A dual-optic video holder as claimed in claim 6 wherein guide blocks are provided on the outer side walls of the quick release housing.
9. A dual-optical video platform according to claim 1, wherein a lug is disposed on an exterior of a sidewall of the function control box, the damping frame is provided with a connecting hole, the elastic body is a hollow structure, and the damping frame, the elastic body and the function control box body are sequentially connected through the connecting hole and the lug.
10. A drone, comprising a bifocal video head according to claims 1 to 9.
CN202023285380.8U 2020-12-29 2020-12-29 Double-light video holder and unmanned aerial vehicle Active CN214690238U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202023285380.8U CN214690238U (en) 2020-12-29 2020-12-29 Double-light video holder and unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202023285380.8U CN214690238U (en) 2020-12-29 2020-12-29 Double-light video holder and unmanned aerial vehicle

Publications (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114596506A (en) * 2022-03-04 2022-06-07 北京理工大学 Unmanned aerial vehicle inspection equipment and image fusion method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114596506A (en) * 2022-03-04 2022-06-07 北京理工大学 Unmanned aerial vehicle inspection equipment and image fusion method

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Address after: 518000, 13th Floor, Building A4, Nanshan Zhiyuan, No. 1001 Xueyuan Avenue, Changyuan Community, Taoyuan Street, Nanshan District, Shenzhen, Guangdong Province

Patentee after: Shenzhen Pegasus Robotics Co.,Ltd.

Country or region after: China

Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province

Patentee before: SHENZHEN FEIMA ROBOTICS Co.,Ltd.

Country or region before: China

CP03 Change of name, title or address