CN206833126U - Camera, head assembly and unmanned plane - Google Patents

Camera, head assembly and unmanned plane Download PDF

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Publication number
CN206833126U
CN206833126U CN201720584316.9U CN201720584316U CN206833126U CN 206833126 U CN206833126 U CN 206833126U CN 201720584316 U CN201720584316 U CN 201720584316U CN 206833126 U CN206833126 U CN 206833126U
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CN
China
Prior art keywords
camera
lens barrel
flange
head
fore shell
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201720584316.9U
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Chinese (zh)
Inventor
马天航
宾朋
赵喜峰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SZ DJI Osmo Technology Co Ltd
Original Assignee
SZ DJI Osmo Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SZ DJI Osmo Technology Co Ltd filed Critical SZ DJI Osmo Technology Co Ltd
Priority to CN201720584316.9U priority Critical patent/CN206833126U/en
Application granted granted Critical
Publication of CN206833126U publication Critical patent/CN206833126U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of camera, including circuit board, lens barrel on circuit boards and the lens assembly being installed with the lens barrel are set, the camera includes camera fore shell, camera rear shell, the camera fore shell is fixedly connected with the camera rear shell to be enclosed to set to form accommodation space, the circuit board, the lens barrel and the lens assembly are installed with the accommodation space, the camera fore shell inwall is formed with cylindrical circumferential wall, the lens barrel periphery wall is arranged with flange, sealing ring is provided with the flange, the cylindrical circumferential wall aligns with the flange, supports the sealing ring jointly.The camera, head assembly and unmanned plane prevent steam from entering head camera cavity inside, reduce the possibility that steam is condensed under chilling environment on head eyeglass by sealing structure.

Description

Camera, head assembly and unmanned plane
Technical field
It the utility model is related to a kind of camera, head assembly and unmanned plane.
Background technology
With the development of unmanned air vehicle technique, unmanned plane is widely applied multi-field.Unmanned plane can carry head and hold Carry various portable cameras to use, be widely used in TV, film, reality TV show, moving camera shooting, take photo by plane, the scene such as safety monitoring.
In airtight condition, at a certain temperature, claim with solid or liquid in pressure possessed by the steam to balance each other For saturated vapour pressure.Same substance has different saturated vapour pressures at different temperatures, and increases with the rise of temperature.It is pure The saturated vapour pressure of solvent is more than the saturated vapour pressure of solution;For same substance, the saturated vapour pressure of solid-state is less than liquid Saturated vapour pressure.Glass often produces mist under the conditions of temperature is high, difference variation is significant, this be due to glass surface compared with Existing steam is not accommodated, unnecessary steam is in glass after rapid cooling containing the oversaturated air of saturation under high-temperature Glass surface condenses into very thin dewdrop due to the effect of heterogeneous nucleation, makes light that diffusing reflection occur, impermeable so as to form atomization Bright shape.
Head camera internal element increases with usage time, and component temperature gradually rises, and camera internal cavity can produce Raw high temperature saturated steam, after aircraft enters low-temperature region, camera outermost layer eyeglass cools rapidly at first, saturation in cavity Vapour pressure is reduced, and vapor can condense in low temperature lens area and form water smoke, and shooting is caused greatly to perplex.This phenomenon exists Become apparent on miniaturization head camera.
Utility model content
In view of this, it is necessary to which a kind of camera, head assembly and unmanned plane with lens antifogging structure are provided.
A kind of camera, including circuit board, lens barrel on circuit boards and the lens assembly being installed with the lens barrel are set, The camera include camera fore shell, camera rear shell, the camera fore shell be fixedly connected with the camera rear shell enclose set to be formed it is accommodating Space, the circuit board, the lens barrel and the lens assembly are installed with the accommodation space, the camera fore shell inwall Formed with cylindrical circumferential wall, the lens barrel periphery wall is arranged with flange, and sealing ring, the cylindrical shape are provided with the flange Perisporium aligns with the flange, supports the sealing ring jointly.
Further, the flange includes being set in the cylindrical portion of the lens barrel periphery wall and from the cylindrical portion away from institute The side for stating circuit board radially extends the flange to be formed, the sealing ring support the cylindrical circumferential wall and the flange it Between.
Further, the cylindrical circumferential wall encloses the space of the receiving lens assembly set with the lens barrel as vacuum.
Further, the cylindrical circumferential wall encloses the space filling-foam of the receiving lens assembly set with the lens barrel Material.
Further, the lens assembly sets heating arrangement, and the heating arrangement can give the one of the lens assembly Individual or multiple eyeglass heating.
Further, the sealing ring is quality of rubber materials.
Further, the camera also includes closure, and the closure is fixedly connected with the camera fore shell and the phase Machine rear shell.
Further, connecting hole is provided with the closure, the connecting hole is used to be connected with a head bearing structure To carry in the camera and the head bearing structure.
Further, the closure is generally circular, and the camera fore shell and the camera rear shell are mutually permanently connected When, the side of the camera fore shell and the camera rear shell is generally circular, and the closure just covers the camera fore shell With the side of the camera rear shell.
A kind of head assembly, including head bearing structure and the camera that is carried in the head bearing structure, the phase Machine is upper described camera.
Further, the head bearing structure includes the first rotational structure, the supporting construction of the carrying camera and the Two rotational structures, first rotational structure can drive the supporting construction to be rotated around first direction, the second rotation knot Structure can drive the camera to be rotated relative to the supporting construction around second direction, and the first direction and the second direction are just Hand over.
Further, the head bearing structure includes shock-damping structure, and connecting the head by the shock-damping structure holds Structure is carried in the fuselage of unmanned plane.
A kind of unmanned plane, including fuselage and the head assembly that is connected on the fuselage, the head assembly are upper described Head assembly.
The upper camera, head assembly and unmanned plane prevent steam from entering head camera cavity inside by sealing structure, Reduce the possibility that steam is condensed under chilling environment on head eyeglass.
Brief description of the drawings
Fig. 1 is a kind of stereogram for unmanned plane that the utility model embodiment provides.
Fig. 2 is a kind of stereogram for head assembly that the utility model embodiment provides.
Fig. 3 is a kind of stereogram for camera that the utility model embodiment provides.
Fig. 4 is a kind of stereogram at another visual angle for camera that the utility model embodiment provides.
Fig. 5 is sectional view of the camera along V-V lines shown in Fig. 4.
Fig. 6 is the blast disassembly diagram of the camera shown in Fig. 3.
Main element symbol description
Unmanned plane 1000
Fuselage 1
Head assembly 2
Head bearing structure 20
Shock-damping structure 200
Vibration damper plate 2000
Shock-absorbing ball 2002
First rotational structure 202
First rotating shaft portion 2022
Supporting construction 204
First support arm 2040
Second support arm 2042
Second rotational structure 206
Camera 22
Camera fore shell 220
Through hole 2200
Transparent glasses lens 2202
Cylindrical circumferential wall 2204
First fixing hole 2206
Camera rear shell 221
Second fixing hole 2210
Circuit board 222
Lens barrel 223
Lens assembly 224
Flange 225
Cylindrical portion 2250
Flange 2252
Sealing ring 226
Closure 227
3rd fixing hole 2270
Connecting hole 2272
Fixing device 228
Following embodiment will further illustrate the utility model with reference to above-mentioned accompanying drawing.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belong to the scope of the utility model protection.
It should be noted that when component is referred to as " being fixed on " another component, it can be directly on another component Or there may also be component placed in the middle.When a component is considered as " connection " another component, it can be directly connected to To another component or it may be simultaneously present component placed in the middle.When a component is considered as " being arranged at " another component, it Can be set directly on another component or may be simultaneously present component placed in the middle.Term as used herein is " vertical ", " horizontal ", "left", "right" and similar statement for illustrative purposes only.
Unless otherwise defined, all of technologies and scientific terms used here by the article is led with belonging to technology of the present utility model The implication that the technical staff in domain is generally understood that is identical.It is simply in term used in the description of the present utility model herein The purpose of description specific embodiment, it is not intended that in limitation the utility model.Term as used herein " and/or " include The arbitrary and all combination of one or more related Listed Items.The first, the second grade word is used for representing title, and simultaneously Any specific order is not indicated that.
The utility model provides a kind of unmanned plane, and the unmanned plane can be used for any suitable environment, such as (example in the air The aircraft that is mixed such as depopulated helicopter, rotor craft, Fixed Wing AirVehicle or fixed-wing with rotor, unmanned airship, nobody Parasol), in water (example, ship or submarine), on the ground (example, motorcycle, automobile, truck, bus, train etc.), too (example, space shuttle, satellite or detector) in the air, or in underground (such as subway), or any combination of above-mentioned environment.In this reality Apply in example, the unmanned plane is rotor craft, wherein the rotor can be single rotor, DCB Specimen, three rotors, four rotors, six Rotor and eight rotors etc..For ease of description, the unmanned plane in following examples illustrates by taking quadrotor as an example.
Below in conjunction with the accompanying drawings, some embodiments of the present utility model are elaborated.In the case where not conflicting, under Feature in the embodiment and embodiment stated can be mutually combined.
Referring to Fig. 1, the unmanned plane 1000 includes fuselage 1 and is arranged on the head assembly 2 of the lower section of fuselage 1.Institute Stating head assembly 2 includes head bearing structure 20 and the camera 22 being carried in the head bearing structure 20.
The camera 22 is used to shoot the environmental images of unmanned plane 1000, its can built-in high-definition camera with shoot picture and Video, it can operate with TV, film, reality TV show, moving camera shooting, take photo by plane, the scene such as safety monitoring.
The head bearing structure 20 is used to carry the camera 22, while to realize the pose stabilization control of camera 22 Device, in other words, the camera is kept the static of its posture during exercise.The head bearing structure 20 can So that the camera 22 shoots stable picture during motion.It can be set on the support arm of the head bearing structure 20 Put one or more servomotors, be responsible for around, the rotation in upper inferior one or more directions.The head carrying knot Structure 20 can be two axles (such as:Roll (Roll) axle, pitching (Pitch) axle), three axles (such as:Driftage (YAW) axle, roll (Roll) axle, pitching (Pitch) axle.), the rotation bearing structure such as four axles, for ease of description, rotated in following examples with two axles Illustrated exemplified by bearing structure.
Refer to shown in Fig. 2, be the structural representation of the head bearing structure 20 of the embodiment of the utility model one.Institute State head bearing structure 20 include shock-damping structure 200, be fixedly connected on the shock-damping structure 200 the first rotational structure 202 and It is rotationally connected with the supporting construction 204 of first rotational structure 202 and is arranged in the supporting construction 204 away from described the Second rotational structure 206 of one end of one rotational structure 202.First rotational structure 202 can drive the supporting construction 204 are rotated in a first direction, and second rotational structure 206 can drive the camera 22 being carried in the supporting construction 204 Rotate in a second direction, the first direction is orthogonal with the second direction.In the illustrated embodiment, first rotation Rotation structure 202 is R axles (roll axles) rotational structure of control roll motion, and second rotational structure 206 is control pitching fortune Dynamic P axles (pitch) rotational structure.
The shock-damping structure 200 is used to be connected with the fuselage 1 of the unmanned plane 1000, and can be in the unmanned plane 1000 it is mobile when reduce the fuselage 1 of the unmanned plane 1000 shadow of the caused vibrations to the camera 22 in moving process Ring.The shock-damping structure 200 includes vibration damper plate 2000 and the shock-absorbing ball 2002 being arranged on the vibration damper plate 2000.The damping Plate 2000 and the shock-absorbing ball 2002 may be provided inside the fuselage 1, and the shock-absorbing ball 2002 is away from the vibration damper plate 2000 One end can be fixedly connected on inside the fuselage 1, the vibration damper plate 2000 is movably set in inside the fuselage 1.It can manage Solution, the shock-absorbing ball 2002 and the vibration damper plate 2000 may also be arranged on the outside of fuselage 1, and the shock-absorbing ball 2002 is remote One end from the vibration damper plate 2000 is fixedly connected on the outside of the fuselage 1.
Described one end of first rotational structure 202 is fixedly connected with the shock-damping structure 200, and the other end is connected to the support Structure 204.First rotational structure 202, including the first motor section being fixedly connected on the shock-damping structure 200, it is described First motor section is substantially in cylindrical type, including first rotating shaft portion 2022 (shown in ginseng Fig. 4), the first rotating shaft portion 2022 with it is described Supporting construction 204 is fixedly connected, and it is described so as to drive that first motor section can drive the first rotating shaft portion 2022 to rotate Supporting construction 204 rotates.
The supporting construction 204 is substantially u-shaped, including the first support arm 2040 and from first support arm 2040 two Opposite end is to be roughly parallel to the direction of the axis of the rotating shaft of first motor section to away from first support arm 2040 Two second support arms 2042 of direction extension.The axis of rotation of first motor section is connected to first support arm 2040 On, two second support arm 2042 is connected to two opposite ends of the camera 22.The rotating shaft of first motor section Axis is approximately perpendicular to first support arm 2042.
Second rotational structure 206 is arranged on wherein on one second support arm 2042 of the supporting construction 204, can The camera 22 is driven to be rotated relative to the supporting construction 204, the direction of rotation of the camera 22 and the supporting construction 204 Direction of rotation is orthogonal.The structure of second rotational structure 206 is roughly the same with the structure of first rotational structure 202, bag The second motor section being fixedly installed on second support arm 2042 is included, second motor section is generally cylindrical, including Second shaft, second shaft are fixedly connected with the camera 22, and second motor section drives second rotating shaft Portion is rotated so as to drive the camera 22 to rotate.The second support arm 2042 and 22 turns of the camera away from second motor section Dynamic connection.
It is understood that first rotational structure 202, second rotational structure 206 be also not necessarily limited to it is described Structure, as long as the supporting construction 204 and the camera 22 can be caused to be rotated around different axles.The supporting construction 204 Described structure is also not necessarily limited to, as long as the camera 22 can be carried and cause the relatively described supporting construction 204 of the camera 22 Rotation, for example, the supporting construction 204 can be camera 22 described in single arm support, i.e., described supporting construction 204 only with One end of the camera 22 is connected.
Refer to shown in Fig. 3 to Fig. 6, be the structure chart of the camera 22 of the utility model embodiment.The camera 22 includes Camera fore shell 220, camera rear shell 221, circuit board 222, lens barrel 223, lens assembly 224.The camera fore shell 220 and the phase Machine rear shell 221 can separably interfix sets a receiving space so as to enclose, the circuit board 222, the lens barrel 223 and institute Lens assembly 224 is stated to be housed in the receiving space.The position of the lens assembly 224 is corresponded on the camera fore shell 220 The place of putting is provided with through hole 2200 and transparent glasses lens 2202, and the through hole 2200 and the lens assembly 224 are relatively just, described transparent Eyeglass 2202 covers the through hole 2200, can be obtained around the camera 22 by the through hole 2200 and the transparent glasses lens 2202 Image.The transparent glasses lens 2202 can be the eyeglass that glass lens or other transparent materials make, and be set as long as can cover The through hole 2200 and can cause light be incident to from the transparent glasses lens 2202 on the lens assembly 224.
The lens barrel 223 is generally cylindrical, is fixedly installed on the circuit board 222, and the lens assembly 224 is installed with In the lens barrel 223, including one or more optical mirror slips, imaging sensor (such as electricity is integrated with the circuit board 222 Lotus coupling element Charge Coupled Device, CCD), sample circuit, the electronic component such as analog to digital conversion circuit, work as outside Light enters the lens assembly 224 by the through hole 2200, is sensed by described image sensor, optical signalling is changed For charge signal, then digitized video is converted into through over-sampling circuit and analog to digital conversion circuit.
The camera 22 also includes the flange 225 being set on the lens barrel 223 and is arranged on the He of camera fore shell 220 Sealing ring 226 between the camera rear shell 221.The flange 225 is in substantially cylinder barrel shaped, can be set in the lens barrel On 223.The flange 225 includes the cylindrical portion 2250 being set on the lens barrel 223 and from the cylindrical portion 2250 away from institute The one end for stating circuit board 222 radially extends a flange 2252, and the external diameter of the flange 2252 is more than the outer of the cylindrical portion 2250 Footpath.The sealing ring 226 is supported between the flange 2252 and the camera fore shell 220 of the flange 225.Preferably, it is described Sealing ring 226 is made of flexible material, such as rubber, when the sealing ring 226 is supported in the camera fore shell 220 When between the flange 2252, the sealing ring 226 is extruded, and its elastic-restoring force causes the sealing ring 226 to seal institute State camera fore shell 220 and the flange 225, the lens barrel 223 enclose the inner space set.
The inwall of camera fore shell 220 is to be roughly parallel to the direction of the axis of the lens barrel 223 to away from described transparent The direction of eyeglass 2202 extends to form cylindrical circumferential wall 2204, and the cylindrical circumferential wall 2204, which encloses, sets an accommodation space, to house The lens assembly 224.The cylindrical circumferential wall 2204 aligns setting with the flange 225, supports the sealing ring jointly 226 so that the sealing ring 226 closely supported the flange 2252 of the camera fore shell 220 and the flange 225 it Between.
The camera 22 also includes being arranged on the camera fore shell 220 and the closure of the side of camera rear shell 221 227.Be respectively arranged with the camera fore shell 220, the camera rear shell 221 and the closure 227 first fixing hole 2216, Second fixing hole 2200 and the 3rd fixing hole 2270, the closure 227 can be worn by fixing device 228 (such as screw etc.) Corresponding fixing hole and be fixed on the camera fore shell 220 and the camera rear shell 221.It is understood that in other realities Apply in example, the closure 227 can also be fixed to the camera fore shell 220 and the camera rear shell by other fixed forms 221, for example, buckle, screw thread, interference, form fit etc., as long as the closure 227 can be caused to be fixed to the camera fore shell 220 and the side of the camera rear shell 221.The camera fore shell 220 and the side of camera rear shell 221 are substantially in half Circle, the closure 227 is generally circular, after the closure 227 is fixed on the camera fore shell 220 and the camera When on shell 221, the closure 227 just covers the side for setting and covering the camera fore shell 220 and the camera rear shell 221. The closure 227 offers connecting hole 2272, for installing the rotating shaft of the supporting construction 204, so that the rotating shaft It is fixedly connected with the closure 227, and is rotated with the rotation of the rotating shaft.
When assembling the camera 22, lens barrel 223 is fixed on the circuit board 222 first, then by the lens group Part 224 is installed in the lens barrel 223, and then flange 225 is set on the lens barrel 223, sealing ring 226 is placed in described On the flange 2252 of flange 225, then the camera fore shell 220 is located on the lens assembly 224 so that the camera The cylindrical circumferential wall 2204 of fore shell 220 is supported on the sealing ring 226, then by the closure 227 by the camera Fore shell 220 and the camera rear shell 221 are fixed together, before the transparent glasses lens 2202 lid finally is located at into the camera On the through hole 2200 of shell 220.Formed after being completed, between the cylindrical circumferential wall 2204 and the lens assembly 224 free Chamber 2205, can be before lid sets the transparent glasses lens 2202 by the vacuumize process of cavity 2205, so that the lens group Part 224 is in vacuum tightness environment.
In certain embodiments, the cavity 2205 can absorb water with filling-foam material, the expanded material Vapour, so as to further reduce the possibility that hazes.
In certain embodiments, the lens assembly 224 can also set heating arrangement, for example, eyeglass and eyeglass it Between or eyeglass on connect thermo electric material, powered by the circuit board 222 to heat the eyeglass of the lens assembly 224, so as to Further reduce the possibility that hazes.The heating arrangement can also be arranged on the position of any suitable in lens barrel (such as in lens barrel Wall), as long as the lens assembly 224 can be given to heat.
It is understood that the flange 225 can omit, the periphery wall of the lens barrel 223 radially outward from a flange, The cylindrical circumferential wall 2204 of the camera fore shell 220 is relative with the flange of the lens barrel just, and the sealing ring 226 is held in institute State between the cylindrical circumferential wall 2204 of camera fore shell 220 and the flange of the lens barrel 223.It is understood that the sealing ring 226 are held between the camera fore shell 220 and the lens barrel 223 and can also have other suitable structures, as long as can cause The sealing ring 226 can seal the camera fore shell 220 and the lens barrel 223 and enclose the accommodating lens assembly set when being supported 224 space.
The sealing ring 226 and the closure 227 are set up in the camera 22, completely cuts off extraneous steam and enters, reduce nothing It is man-machine in possibility of the condensation vapor on head eyeglass under chilling environment, so as to play anti-fog effect.
In addition, for the person of ordinary skill of the art, it can be made according to technical concept of the present utility model Its various corresponding changes and deformation, and all these changes and deformation should all belong to the protection model of the utility model claims Enclose.

Claims (13)

1. a kind of camera, including circuit board, lens barrel on circuit boards is set and is installed with the lens barrel lens assembly, its It is characterised by:The camera includes camera fore shell, camera rear shell, and the camera fore shell is fixedly connected to enclose and set with the camera rear shell Accommodation space is formed, the circuit board, the lens barrel and the lens assembly are installed with the accommodation space, the camera Fore shell inwall is arranged with flange formed with cylindrical circumferential wall, the lens barrel periphery wall, and sealing ring is provided with the flange, described Cylindrical circumferential wall aligns with the flange, supports the sealing ring jointly.
2. camera as claimed in claim 1, it is characterised in that:The flange includes the cylinder for being set in the lens barrel periphery wall Portion and the flange to be formed is radially extended from side of the cylindrical portion away from the circuit board, the sealing ring is supported in the circle Between cylindrical periphery-wall and the flange.
3. camera as claimed in claim 1, it is characterised in that:The cylindrical circumferential wall is enclosed described in the receiving set with the lens barrel The space of lens assembly is vacuum.
4. camera as claimed in claim 1, it is characterised in that:The cylindrical circumferential wall is enclosed described in the receiving set with the lens barrel The space filling-foam material of lens assembly.
5. camera as claimed in claim 1, it is characterised in that:The lens assembly sets heating arrangement, the heating arrangement One or more eyeglasses of the lens assembly can be given to heat.
6. camera as claimed in claim 1, it is characterised in that:The sealing ring is quality of rubber materials.
7. camera as claimed in claim 1, it is characterised in that:The camera also includes closure, and the closure, which is fixed, to be connected Connect the camera fore shell and the camera rear shell.
8. camera as claimed in claim 7, it is characterised in that:Connecting hole is provided with the closure, the connecting hole is used In being connected with a head bearing structure to carry in the camera and the head bearing structure.
9. camera as claimed in claim 7, it is characterised in that:The closure is generally circular, the camera fore shell and institute When stating camera rear shell and being mutually permanently connected, the side of the camera fore shell and the camera rear shell is generally circular, the sealing Lid just covers the side of the camera fore shell and the camera rear shell.
10. a kind of head assembly, including head bearing structure and the camera that is carried in the head bearing structure, its feature exist In the camera is the camera described in any one of claim 1 to 9.
11. head assembly as claimed in claim 10, it is characterised in that the head bearing structure includes the first rotation and tied The supporting construction and the second rotational structure of structure, the carrying camera, first rotational structure can drive the supporting construction Rotated around first direction, second rotational structure can drive the relatively described supporting construction of the camera to be revolved around second direction Turn, the first direction is orthogonal with the second direction.
12. head assembly as claimed in claim 10, it is characterised in that:The head bearing structure includes shock-damping structure, leads to Cross the shock-damping structure and connect the head bearing structure in the fuselage of unmanned plane.
13. a kind of unmanned plane, including fuselage and the head assembly that is connected on the fuselage, the head assembly are held including head Carry the camera of structure and bearer connection in the head bearing structure, it is characterised in that the camera is claim 1 to 9 Camera described in any one.
CN201720584316.9U 2017-05-23 2017-05-23 Camera, head assembly and unmanned plane Expired - Fee Related CN206833126U (en)

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Application Number Priority Date Filing Date Title
CN201720584316.9U CN206833126U (en) 2017-05-23 2017-05-23 Camera, head assembly and unmanned plane

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Application Number Priority Date Filing Date Title
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Publication Number Publication Date
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CN108791924A (en) * 2018-06-04 2018-11-13 广州市华科尔科技股份有限公司 A kind of mixed dynamic unmanned plane head assembly of oil electricity
WO2018214030A1 (en) * 2017-05-23 2018-11-29 深圳市大疆灵眸科技有限公司 Camera, camera mount assembly, and unmanned aerial vehicle
CN109639943A (en) * 2018-12-17 2019-04-16 中国科学院西安光学精密机械研究所 A kind of space camera
CN112154372A (en) * 2019-07-29 2020-12-29 深圳市大疆创新科技有限公司 Shooting equipment, cloud platform device and unmanned aerial vehicle
CN112166375A (en) * 2019-07-29 2021-01-01 深圳市大疆创新科技有限公司 Shooting equipment, cloud platform device and unmanned aerial vehicle
CN113508324A (en) * 2020-05-29 2021-10-15 深圳市大疆创新科技有限公司 Optical system, precision device and electronic apparatus
CN113678059A (en) * 2020-06-30 2021-11-19 深圳市大疆创新科技有限公司 Cloud platform camera and casing, movable platform thereof
CN114047661A (en) * 2019-06-05 2022-02-15 广东弘景光电科技股份有限公司 Miniaturized self-heating module of making a video recording
CN117429645A (en) * 2023-12-21 2024-01-23 南京拓恒航空科技有限公司 High-altitude terrain surveying and measuring device and method using unmanned aerial vehicle
CN109639943B (en) * 2018-12-17 2024-06-04 中国科学院西安光学精密机械研究所 Space camera

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Publication number Priority date Publication date Assignee Title
WO2018214030A1 (en) * 2017-05-23 2018-11-29 深圳市大疆灵眸科技有限公司 Camera, camera mount assembly, and unmanned aerial vehicle
CN108791924A (en) * 2018-06-04 2018-11-13 广州市华科尔科技股份有限公司 A kind of mixed dynamic unmanned plane head assembly of oil electricity
CN108791924B (en) * 2018-06-04 2024-02-13 广州市华科尔科技股份有限公司 Oil-electricity hybrid unmanned aerial vehicle holder assembly
CN109639943A (en) * 2018-12-17 2019-04-16 中国科学院西安光学精密机械研究所 A kind of space camera
CN109639943B (en) * 2018-12-17 2024-06-04 中国科学院西安光学精密机械研究所 Space camera
CN114047661B (en) * 2019-06-05 2024-01-02 广东弘景光电科技股份有限公司 Miniaturized self-heating camera module
CN114047661A (en) * 2019-06-05 2022-02-15 广东弘景光电科技股份有限公司 Miniaturized self-heating module of making a video recording
CN112154372A (en) * 2019-07-29 2020-12-29 深圳市大疆创新科技有限公司 Shooting equipment, cloud platform device and unmanned aerial vehicle
CN112166375A (en) * 2019-07-29 2021-01-01 深圳市大疆创新科技有限公司 Shooting equipment, cloud platform device and unmanned aerial vehicle
WO2021016816A1 (en) * 2019-07-29 2021-02-04 深圳市大疆创新科技有限公司 Photographing apparatus, gimbal device, and unmanned aerial vehicle
CN113508324A (en) * 2020-05-29 2021-10-15 深圳市大疆创新科技有限公司 Optical system, precision device and electronic apparatus
CN113678059B (en) * 2020-06-30 2023-05-16 深圳市大疆创新科技有限公司 Tripod head camera and shell and movable platform thereof
CN113678059A (en) * 2020-06-30 2021-11-19 深圳市大疆创新科技有限公司 Cloud platform camera and casing, movable platform thereof
CN117429645A (en) * 2023-12-21 2024-01-23 南京拓恒航空科技有限公司 High-altitude terrain surveying and measuring device and method using unmanned aerial vehicle
CN117429645B (en) * 2023-12-21 2024-03-19 南京拓恒航空科技有限公司 High-altitude terrain surveying and measuring device and method using unmanned aerial vehicle

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