WO2021129778A1 - 电子设备 - Google Patents

电子设备 Download PDF

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Publication number
WO2021129778A1
WO2021129778A1 PCT/CN2020/139211 CN2020139211W WO2021129778A1 WO 2021129778 A1 WO2021129778 A1 WO 2021129778A1 CN 2020139211 W CN2020139211 W CN 2020139211W WO 2021129778 A1 WO2021129778 A1 WO 2021129778A1
Authority
WO
WIPO (PCT)
Prior art keywords
camera
electronic device
flying
driving mechanism
casing
Prior art date
Application number
PCT/CN2020/139211
Other languages
English (en)
French (fr)
Inventor
成东村
王微
朱丽君
罗政军
张小南
Original Assignee
维沃移动通信有限公司
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 维沃移动通信有限公司 filed Critical 维沃移动通信有限公司
Priority to EP20906442.7A priority Critical patent/EP4087227A4/en
Publication of WO2021129778A1 publication Critical patent/WO2021129778A1/zh
Priority to US17/849,585 priority patent/US20220324568A1/en

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Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/02—Constructional features of telephone sets
    • H04M1/0202—Portable telephone sets, e.g. cordless phones, mobile phones or bar type handsets
    • H04M1/026—Details of the structure or mounting of specific components
    • H04M1/0264—Details of the structure or mounting of specific components for a camera module assembly
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/50—Constructional details
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • 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
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/40—Modular UAVs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/26—Ducted or shrouded rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/50—Launching from storage containers, e.g. from submarine missile tubes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/10—Transport or storage specially adapted for UAVs with means for moving the UAV to a supply or launch location, e.g. robotic arms or carousels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/20—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV
    • B64U80/25—Transport or storage specially adapted for UAVs with arrangements for servicing the UAV for recharging batteries; for refuelling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/60—Transport or storage specially adapted for UAVs by wearable objects, e.g. garments or helmets
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/02—Constructional features of telephone sets
    • H04M1/0202—Portable telephone sets, e.g. cordless phones, mobile phones or bar type handsets
    • H04M1/0254—Portable telephone sets, e.g. cordless phones, mobile phones or bar type handsets comprising one or a plurality of mechanically detachable modules
    • H04M1/0256—Portable telephone sets, e.g. cordless phones, mobile phones or bar type handsets comprising one or a plurality of mechanically detachable modules wherein the modules are operable in the detached state, e.g. one module for the user interface and one module for the transceiver
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/50—Constructional details
    • H04N23/54—Mounting of pick-up tubes, electronic image sensors, deviation or focusing coils
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/57—Mechanical or electrical details of cameras or camera modules specially adapted for being embedded in other devices
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
    • H04N23/90—Arrangement of cameras or camera modules, e.g. multiple cameras in TV studios or sports stadiums
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/02—Constructional features of telephone sets
    • H04M1/0202—Portable telephone sets, e.g. cordless phones, mobile phones or bar type handsets
    • H04M1/0206—Portable telephones comprising a plurality of mechanically joined movable body parts, e.g. hinged housings
    • H04M1/0208—Portable telephones comprising a plurality of mechanically joined movable body parts, e.g. hinged housings characterized by the relative motions of the body parts
    • H04M1/0235—Slidable or telescopic telephones, i.e. with a relative translation movement of the body parts; Telephones using a combination of translation and other relative motions of the body parts

Definitions

  • the present invention relates to the technical field of communication equipment, and in particular to an electronic device.
  • the screen ratio of electronic devices is increasing.
  • current electronic equipment usually adopts a camera module that can be raised and lowered.
  • the camera module protrudes out of the device housing of the electronic device; when the camera module is completed, the camera module retracts into the device housing of the electronic device, so as to realize the Hidden within the body.
  • the camera module with this structure can avoid the influence on the display screen area, so that the screen occupying ratio of the electronic device can be increased.
  • the current camera module can only take images when it extends out of the device housing, and can only take pictures within the limited working distance of the camera module, and cannot achieve longer-distance shooting.
  • the current camera module requires the user to grasp the electronic device during shooting, and adjust the shooting angle by adjusting the body posture, so there is a problem of poor shooting flexibility.
  • the invention discloses an electronic device to solve the problem of poor shooting flexibility of the current lifting camera of the electronic device.
  • the present invention adopts the following technical solutions:
  • An electronic device comprising a device housing and a flying camera, the device housing having an opening and an inner cavity, the opening is in communication with the inner cavity, and the flying camera is movably arranged on the device housing ,
  • the flying camera can be extended out of the equipment housing or retracted into the equipment housing through the opening, in the case that the flying camera is located outside the equipment housing ,
  • the flying camera can be separated from the device housing.
  • the electronic device disclosed in the embodiment of the present invention improves the structure of the electronic device in the prior art, so that the electronic device is equipped with a flying camera, the flying camera is detachably connected to the device housing, and the flying camera can be returned through the opening. It is retracted into the equipment housing to realize the concealment in the equipment housing.
  • the flying camera extends out of the equipment housing and is separated from the equipment housing, so that the flying camera can perform flight shooting and flight shooting.
  • the camera can adjust its position in flight, so as to achieve more flexible shooting. It can be seen that the electronic device disclosed in the embodiment of the present invention can improve the flexibility of shooting of the electronic device.
  • Fig. 1 is a schematic structural diagram of an electronic device disclosed in an embodiment of the present invention
  • Fig. 2 is a schematic diagram of Fig. 1 in the extended state of the flying camera
  • FIG. 3 is a schematic diagram of a part of the structure of an electronic device disclosed in an embodiment of the present invention.
  • Figure 4 is a schematic diagram of the explosive structure of the flying camera
  • Fig. 5 is an enlarged schematic diagram of a part of the structure in Fig. 4;
  • FIG. 6 is a schematic structural diagram of the flying camera disclosed in the embodiment of the present invention from another perspective.
  • 100-device housing 210-mounting bracket, 220-flight camera, 221-chassis, 2211-shell body, 2211a-mounting hole, 2212-cover, 221a-first shooting window, 221b-second shooting window , 222-first camera, 223-battery, 224-propeller, 225-second camera, 226-device bracket, 227-infrared proximity sensor, 228-cover, 300-first drive mechanism.
  • an embodiment of the present invention discloses an electronic device.
  • the disclosed electronic device includes a device housing 100 and a flying camera 220.
  • the device housing 100 is a basic component of the electronic device, and the device housing 100 can provide an installation location for other components of the electronic device.
  • the device housing 100 has an opening and an inner cavity, and the opening is in communication with the inner cavity. The opening can allow the flight camera 220 to enter and exit the device housing 100, so that the position of the flight camera 220 can be changed.
  • the flying camera 220 is movably disposed in the equipment housing 100, and the flying camera 220 can be extended out of the equipment housing 100 or retracted into the equipment housing 100 through the opening.
  • the flying camera 220 can be hidden and installed in the device housing 100.
  • the flying camera 220 is detachably connected to the equipment housing 100.
  • the flying camera 220 can be separated from the equipment housing 100 to realize the flying camera.
  • 220 is separated from the device housing 100 to fly.
  • the flight camera 220 can adjust its position in the air to realize shooting in various directions, and finally achieve more flexible shooting.
  • the electronic device disclosed in the embodiment of the present invention improves the structure of the electronic device in the prior art, so that the electronic device is equipped with a flight camera 220, which is detachably connected to the device housing 100, and the flight camera 220 It can be retracted into the device housing 100 through the opening, thereby achieving concealment in the device housing 100.
  • the flying camera 220 extends out of the device housing 100 and is separated from the device housing 100. In this way, the flight camera 220 can perform flight shooting, and the flight camera 220 can adjust its position in the flight state, thereby achieving more flexible shooting. It can be seen that the electronic device disclosed in the embodiment of the present invention can improve the flexibility of shooting of the electronic device.
  • the flight camera 220 when the flight camera 220 is located in the equipment housing 100, the flight camera 220 and the equipment housing 100 are in a detachable assembly state. Specifically, the flying camera 220 can be assembled with the device housing 100 in a detachable manner such as magnetic attraction and snap connection.
  • an electromagnetic component may be provided in the equipment housing 100. When the flying camera 220 is retracted into the equipment housing 100 through the opening, the electromagnetic component can be energized, thereby generating an impact on the flying camera. 220 adsorption magnetic force, so as to achieve assembly. When the electromagnetic component is powered off, the magnetic attraction between the flying camera 220 and the device housing 100 is released.
  • the device housing 100 may be provided with a first buckle, and the flight camera 220 may be provided with a second buckle, and the flight camera 220 is retracted into the device housing 100 through the opening.
  • the first buckle is matched with the second buckle, so as to realize the detachable assembly between the flying camera 220 and the device housing 100.
  • the flight camera 220 and the device housing 100 may be detachably assembled in other ways.
  • the movement of the flight camera 220 can be realized by the user's manual manipulation.
  • the device housing 100 can be provided with a sliding button, which can cooperate with the flight camera 220.
  • the sliding button slides.
  • the flight camera 220 can be moved to extend out of the device housing 100 through the opening.
  • the flight camera 220 can be released from the equipment housing 100 (for example, the first buckle and the second buckle occur). Tripping), and further prepare for the separation of the flying camera 220 from the equipment housing 100 when the flying camera 220 is located outside the equipment housing 100.
  • the electronic device disclosed in the embodiment of the present invention may further include a mounting bracket 210.
  • the flight camera 220 is arranged on the mounting bracket 210, and the flight camera 220 can be attached with the mounting bracket. 210 extends out of the device housing 100 or retracts into the device housing 100 through the opening.
  • the flying camera 220 is detachably connected to the equipment housing 100 through the mounting bracket 210.
  • the flying camera 220 can be separated from the mounting bracket 210, thereby achieving separation from the device housing 100.
  • the configuration of the mounting bracket 210 facilitates the assembly between the flight camera 220 and the device housing 100.
  • the mounting bracket 210 may be provided with a storage space, and the flight camera 220 may be placed in the installation space.
  • the installation space may be an installation slot.
  • the electronic device disclosed in the embodiment of the present invention may further include a first driving mechanism 300, and the first driving mechanism 300 is disposed in the device housing 100.
  • the first driving mechanism 300 is connected to the flying camera 220, and the first driving mechanism 300 drives the flying camera 220 to extend out of the equipment housing 100 or retract into the equipment housing 100 through the opening.
  • the first driving mechanism 300 is detachably connected to the flight camera 220, so as to indirectly realize the detachable connection with the equipment housing 100, so that when the flight camera 220 extends out of the equipment housing 100 , Can be separated from the first driving mechanism 300 to further realize the separation from the device housing 100.
  • the first driving mechanism 300 can make the movement and control of the flight camera 220 more convenient and intelligent, thereby facilitating the user's use.
  • the first driving mechanism 300 may be a driving device such as a lead screw driving mechanism, a hydraulic telescopic element, a pneumatic telescopic element, a linear motor, etc.
  • the embodiment of the present invention does not limit the specific type of the first driving mechanism 300.
  • the first driving mechanism 300 and the flying camera 220 may be connected by magnetic attraction.
  • the part that the first driving mechanism 300 drives the flying camera 220 to move may include an electromagnetic component, and the flying camera is provided with a magnet or a magnetic attraction member that is magnetically attracted.
  • the electromagnetic element When the electromagnetic element is energized, the first drive mechanism 300 is connected to the flight camera 220 through magnetic adsorption.
  • the electromagnetic element When the electromagnetic element is de-energized, the first drive mechanism 300 is demagnetized by the electromagnetic element, thereby canceling the connection with the flying camera 220. The connection between the flight camera 220.
  • the first driving mechanism 300 may be drivingly connected to the mounting bracket 210, and the first driving mechanism 300 drives the mounting bracket 210 to drive the flying camera 220 to extend out of the device housing 100 through the opening or Retract into the device housing 100.
  • the first driving mechanism 300 drives the mounting bracket 210 to drive the flying camera 220 in and out of the equipment housing 100.
  • the flight camera 220 can fly away directly without directly setting a detachable structure between the flight camera 220 and the equipment housing 100. This undoubtedly simplifies the user's operation and facilitates the user’s operation. use.
  • the mounting bracket 210 may also be provided with at least one of a light supplement module, a receiver, a fingerprint recognition module, and a USB interface. .
  • the above-mentioned functional device can be extended out of the equipment housing 100 through the opening along with the mounting bracket 210. After the work is completed, the above-mentioned functional device can be retracted into the equipment housing 100 through the opening along with the mounting bracket 210. , Thereby achieving concealment within the device housing 100.
  • the mounting bracket 210 is slidably connected to the equipment housing 100 through a sliding rail.
  • the opening of the equipment housing 100 is provided with a limiting structure.
  • the limiting structure of the opening restricts the mounting bracket 210 from sliding out further, and the mounting bracket 210 is not separated from the equipment housing 100 .
  • the flying camera 220 is supported on the mounting bracket, and the user can manually take out the flying camera 220.
  • the structure of the flying camera 220 may be various.
  • the flight camera 220 includes a casing 221, a first camera 222, a battery 223, a propeller 224, and a second driving mechanism disposed in the casing 221.
  • the second driving mechanism is drivingly connected to the propeller 224 and drives the propeller. 224 rotates, and the battery 223 is connected to the first camera 222 and the second driving mechanism for power supply.
  • the propeller 224 is driven by the second driving mechanism to rotate, thereby driving the entire flight camera 220 to fly.
  • the flight camera 220 can adjust its position to realize the first camera. 222 takes more flexible shooting.
  • the casing 221 disclosed in the embodiment of the present invention may include a top wall, a bottom wall, and a side wall connecting the top wall and the bottom wall.
  • the side wall is provided with a first shooting window 221a, and the first camera 222 is installed in the machine.
  • the lens of the first camera 222 is arranged opposite to the first shooting window 221a.
  • the first camera 222 can realize the lateral shooting of the flying camera 220 through the first shooting window 221a opened on the side wall, which undoubtedly can satisfy the flying camera 220 to shoot from the side.
  • the first camera 222 is arranged in the casing 221 so as to be protected by the casing 221 to avoid damage caused by collisions during flight.
  • the flying camera 220 disclosed in the embodiment of the present invention may further include a second camera 225.
  • the second camera 225 is arranged in the casing 221, and the bottom wall is provided with a second shooting window 221b.
  • the lens of the second camera 225 and the second shooting The windows 221b are arranged relatively.
  • the second camera 225 of the flying camera 220 can perform overhead shooting through the second shooting window 221b.
  • the second camera 225 is disposed in the casing 221 so as to be protected by the casing 221.
  • the second camera 225 can be used to shoot from a bird's-eye view, thereby realizing the detection of object height data.
  • the flying camera 220 disclosed in the embodiment of the present invention may further include a device bracket 226 which is arranged in the casing 221, and the first camera 222, the second camera 225 and the battery 223 are all mounted on the device bracket 226.
  • the first camera 222, the second camera 225, and the battery 223 can be pre-installed on the device holder 226, and then form a modular structure together with the device holder 226, and then be installed into the casing 221 as a whole.
  • the assembly efficiency can be improved.
  • the side wall of the casing 221 is provided with a first shooting window 221a.
  • the number of side walls may be four, the first shooting window 221a is provided on one side wall, and the other
  • the proximity sensor may be an infrared proximity sensor 227. This can undoubtedly improve the flight safety of the flight camera 220.
  • the top wall can also be provided with proximity sensors.
  • the flight camera 220 disclosed in the embodiment of the present invention may include a third camera and a fourth camera, and the third camera and the fourth camera may be respectively disposed in the housing 221.
  • the third camera and the fourth camera can be distributed opposite to each other. Both the third camera and the fourth camera are spherically hinged to the casing 221. By adjusting the angle of the third camera and the fourth camera, a larger field of view shooting can be achieved. Of course, more shooting angles can be achieved.
  • the flying camera 220 may be one propeller 224 or may include multiple propellers 224.
  • the multiple propellers 224 are arranged at intervals, and the multiple propellers 224 work together to make the flight of the flying camera 220 more stable.
  • the number of the propellers 224 is four, and the four propellers 224 are sequentially arranged at the four corners of the casing 221, and the two propellers 224 are diagonally distributed and the other two are diagonally distributed.
  • the direction of rotation of the propeller 224 can be reversed, so as to achieve a balanced drive, so that the flight camera 220 can better maintain the position.
  • the number of the second driving mechanism may be one or multiple.
  • the second driving mechanism may drive all the propellers 224 to rotate through the transmission mechanism.
  • the number of the second driving mechanisms and the propellers 224 are equal, and each second driving mechanism is drivingly connected to one propeller 224.
  • each propeller 224 is separately configured with a second driving mechanism, so that the flight camera 220 does not need a more complicated power transmission mechanism, which is beneficial to simplify the overall structure of the flight camera 220.
  • the number of the second driving mechanism is multiple, and the continuous flight of the flying camera 220 can be maintained due to the driving of the other second driving mechanism when part of the second driving mechanism fails and stops operation.
  • the casing 221 may include a casing body 2211 and a cover body 2212.
  • the cover body 2212 is fixed on the opening of the casing body 2211, and the propeller 224 and the second driving mechanism are both installed on the casing body.
  • the cover body 2212 is provided with an escape gap, and the escape gap is arranged along a part of the edge of the propeller 224.
  • the propeller 224 and the second driving mechanism are both installed on the housing main body 2211, which is more convenient to realize the assembly between the two on the same installation basis.
  • the cover 2212 can be fixed on the shell main body 2211 by a fixing method such as a snap connection or a screw connection.
  • the side wall of the casing main body 2211 may be provided with a mounting hole 2211a
  • the casing 221 may also include a cover 228, and the cover 228 may A charging contact is provided, and the charging contact is electrically connected to the battery 223, so as to charge the flying camera 220.
  • a separate cover 228 is undoubtedly more convenient to provide a charging connection structure on it.
  • the cover 228 can be detachably connected to the mounting hole 2211a, so as to facilitate the user to remove the cover 228 to overhaul the local structure of the flying camera 220. .
  • the electronic devices disclosed in the embodiments of the present invention may be smart phones, tablet computers, e-book readers, wearable devices (such as smart watches), game consoles and other devices.
  • the electronic devices disclosed in the embodiments of the present invention may also be of other types.
  • the embodiments of the present invention do not limit the specific types of electronic devices.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Signal Processing (AREA)
  • Mechanical Engineering (AREA)
  • Multimedia (AREA)
  • Transportation (AREA)
  • Automation & Control Theory (AREA)
  • Human Computer Interaction (AREA)
  • Robotics (AREA)
  • Studio Devices (AREA)

Abstract

本发明公开一种电子设备，其包括设备壳体和飞行拍摄器，设备壳体具有开口与内腔，开口与内腔连通，飞行拍摄器可移动地设置于设备壳体，飞行拍摄器可通过开口伸出至设备壳体之外或回缩至设备壳体之内，在飞行拍摄器位于设备壳体之外的情况下，飞行拍摄器可与设备壳体分离。

Description

电子设备
相关申请的交叉引用
本申请主张在2019年12月27日在中国提交的中国专利申请号No.201911376440.6的优先权，其全部内容通过引用包含于此。
技术领域
本发明涉及通信设备技术领域，尤其涉及一种电子设备。
背景技术
随着用户需求的提升，电子设备的性能持续在优化，其中，较为突出的表现为：电子设备的屏幕占比越来越大。为了进一步增大电子设备的屏幕占比，目前的电子设备通常采用能够升降的摄像模组。当需要摄像模组工作时，摄像模组伸出电子设备的设备壳体之外；当摄像模组工作完成之后，摄像模组回缩到电子设备的设备壳体之内，从而实现在设备壳体之内的隐藏。此种结构的摄像模组由于能够避免对显示屏面积的影响，从而能够使得电子设备的屏幕占比得到提高。
但是，目前的摄像模组只能在伸出设备壳体之外的状态下进行图像的拍摄，只能在摄像模组有限的工作距离内进行拍摄，无法实现更远距离的拍摄。与此同时，目前的摄像模组在拍摄的过程中需要用户抓握电子设备，通过调整身体姿势实现拍摄角度的调整，因此存在拍摄灵活性较差的问题。
发明内容
本发明公开一种电子设备，以解决目前的电子设备的升降式摄像头存在拍摄灵活性较差的问题。
为了解决上述问题，本发明采用下述技术方案：
一种电子设备，包括设备壳体和飞行拍摄器，所述设备壳体具有开口与内腔，所述开口与所述内腔连通，所述飞行拍摄器可移动地设置于所述设备壳体，所述飞行拍摄器可通过所述开口伸出至所述设备壳体之外或回缩至所 述设备壳体之内，在所述飞行拍摄器位于所述设备壳体之外的情况下，所述飞行拍摄器可与所述设备壳体分离。
本发明采用的技术方案能够达到以下有益效果：
本发明实施例公开的电子设备通过对现有技术中的电子设备的结构进行改进，使得电子设备配置有飞行拍摄器，飞行拍摄器可拆卸地与设备壳体相连，飞行拍摄器能够通过开口回缩至设备壳体内，从而实现在设备壳体内的隐藏，在需要拍摄时，飞行拍摄器伸出至设备壳体之外，并与设备壳体分离，从而使得飞行拍摄器进行飞行拍摄，飞行拍摄器能够在飞行状态下调节自身的位置，从而实现更为灵活地拍摄。可见，本发明实施例公开的电子设备能够提高电子设备的拍摄的灵活性。
附图说明
此处所说明的附图用来提供对本发明的进一步理解，构成本发明的一部分，本发明的示意性实施例及其说明用于解释本发明，并不构成对本发明的不当限定。在附图中：
图1为本发明实施例公开的电子设备的结构示意图；
图2为图1在飞行拍摄器在伸出状态下的示意图；
图3为本发明实施例公开的电子设备的部分结构示意图；
图4为飞行拍摄器的爆炸结构示意图；
图5为图4中部分结构的放大示意图；
图6为本发明实施例公开的飞行拍摄器在另一视角下的结构示意图。
附图标记说明：
100-设备壳体、210-安装支架、220-飞行拍摄器、221-机壳、2211-壳主体、2211a-安装孔、2212-盖体、221a-第一拍摄视窗、221b-第二拍摄视窗、222-第一摄像头、223-电池、224-螺旋桨、225-第二摄像头、226-器件支架、227-红外靠近传感器、228-封盖、300-第一驱动机构。
具体实施方式
为使本发明的目的、技术方案和优点更加清楚，下面将结合本发明具体实施例及相应的附图对本发明技术方案进行清楚、完整地描述。显然，所描述的实施例仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。
以下结合附图，详细说明本发明各个实施例公开的技术方案。
请参考图1～图6，本发明实施例公开一种电子设备，所公开的电子设备包括设备壳体100和飞行拍摄器220。
设备壳体100为电子设备的基础构件，设备壳体100能够为电子设备的其它构件提供安装位置。在本发明实施例中，设备壳体100具有开口和内腔，开口与内腔连通。开口可以供飞行拍摄器220进出设备壳体100，从而实现飞行拍摄器220位置的变化。
在本发明实施例中，飞行拍摄器220可移动地设置于设备壳体100，飞行拍摄器220可通过开口伸出至设备壳体100之外或回缩至设备壳体100之内。在飞行拍摄器220通过开口回缩至设备壳体100之内的情况下，飞行拍摄器220能够实现在设备壳体100内的隐藏及安装。
飞行拍摄器220与设备壳体100可拆卸相连，在飞行拍摄器220通过开口伸出至设备壳体100之外的情况下，飞行拍摄器220可与设备壳体100分离，从而实现飞行拍摄器220脱离设备壳体100而进行飞行，在飞行过程中，飞行拍摄器220能够通过调整自身在空中的位置，从而实现多种方位的拍摄，最终实现更灵活地拍摄。
本发明实施例公开的电子设备通过对现有技术中的电子设备的结构进行改进，使得电子设备配置有飞行拍摄器220，飞行拍摄器220可拆卸地与设备壳体100相连，飞行拍摄器220能够通过开口回缩至设备壳体100内，从而实现在设备壳体100内的隐藏，在需要拍摄时，飞行拍摄器220伸出至设备壳体100之外，并与设备壳体100分离，从而使得飞行拍摄器220进行飞行拍摄，飞行拍摄器220能够在飞行状态下调节自身的位置，从而实现更为灵活地拍摄。可见，本发明实施例公开的电子设备能够提高电子设备的拍摄的灵活性。
在本发明实施例中，飞行拍摄器220位于设备壳体100之内的情况下，飞行拍摄器220与设备壳体100处于能够拆卸的装配状态。具体的，飞行拍摄器220可以与设备壳体100之间可以通过磁吸、卡扣连接等可拆卸的方式实现装配。一种具体的实施方式中，设备壳体100内可以设置有电磁件，在飞行拍摄器220通过开口回缩至设备壳体100之内的情况下，电磁件可以通电，进而产生对飞行拍摄器220吸附的磁力，从而实现装配。在电磁件断电的情况下，飞行拍摄器220与设备壳体100之间的磁吸解除。
在另一种具体的实施方式中，设备壳体100可以设置有第一卡扣，飞行拍摄器220可以设置有第二卡扣，在飞行拍摄器220通过开口回缩至设备壳体100之内的情况下，第一卡扣与第二卡扣配合，从而实现飞行拍摄器220与设备壳体100之间的可拆卸装配。当然，飞行拍摄器220与设备壳体100之间可以通过其他方式实现可拆卸装配。
飞行拍摄器220的移动可以通过用户的手动操控实现，例如，设备壳体100可以设置有滑动按键，滑动按键可以与飞行拍摄器220配合，用户在操控滑动按键滑动的过程中，滑动按键的滑动能够拨动飞行拍摄器220通过开口伸出至设备壳体100之外，此过程中，飞行拍摄器220可以与设备壳体100之间的配合解除(例如第一卡扣与第二卡扣发生脱扣)，进而为飞行拍摄器220位于设备壳体100之外的情况下与设备壳体100的分离进行准备。
为了方便飞行拍摄器220的装配，在较为优选的方案中，本发明实施例公开的电子设备还可以包括安装支架210，飞行拍摄器220设置于安装支架210上，飞行拍摄器220可随安装支架210通过开口伸出至设备壳体100之外或回缩至设备壳体100之内。在飞行拍摄器220随安装支架210回缩至设备壳体100之内的情况下，飞行拍摄器220通过安装支架210与设备壳体100可拆卸相连。在飞行拍摄器220随安装支架210伸出至设备壳体100之外的情况下，飞行拍摄器220可与安装支架210分离，从而实现与设备壳体100之间的分离。安装支架210的配置更方便飞行拍摄器220与设备壳体100之间的装配。
一种可选的方案中，安装支架210可以设置有安放空间，飞行拍摄器220可以放置在安装空间内，在飞行拍摄器220伸出至设备壳体100之外的情况 下，飞行拍摄器220直接飞走。具体的，安放空间可以为安装槽。
为了方便操控飞行拍摄器220的移动，可选地方案中，本发明实施例公开的电子设备还可以包括第一驱动机构300，第一驱动机构300设置在设备壳体100之内。第一驱动机构300与飞行拍摄器220相连，第一驱动机构300驱动飞行拍摄器220通过开口伸出至设备壳体100之外或回缩至设备壳体100之内。当然，第一驱动机构300与飞行拍摄器220可拆卸相连，从而间接实现与设备壳体100之间的可拆卸相连，从而在飞行拍摄器220在伸出至设备壳体100之外的情况下，能够通过与第一驱动机构300之间的分离，进而实现与设备壳体100之间的分离。第一驱动机构300能够使得飞行拍摄器220的移动操控更加方便、智能化，进而方便用户的使用。
在本发明实施例中，第一驱动机构300可以为丝杠驱动机构、液压伸缩件、气压伸缩件、直线电机等驱动装置，本发明实施例不限制第一驱动机构300的具体种类。
一种具体的实施方式中，第一驱动机构300与飞行拍摄器220之间可以通过磁吸相连。具体的，第一驱动机构300带动飞行拍摄器220移动的部分可以包括电磁件，飞行拍摄器上设有磁铁或被磁性相吸的磁吸件。在电磁件通电的情况下，第一驱动机构300通过磁性吸附实现与飞行拍摄器220之间的连接，在电磁件断电的情况下，第一驱动机构300由于电磁件的消磁，从而解除与飞行拍摄器220之间的连接。
在电子设备包括安装支架210的情况下，第一驱动机构300可以与安装支架210驱动相连，第一驱动机构300驱动安装支架210带动飞行拍摄器220通过开口伸出至设备壳体100之外或回缩至设备壳体100之内。如上文所述，由于飞行拍摄器220可以放置在安装支架210带动安放空间，因此，第一驱动机构300驱动安装支架210驱动飞行拍摄器220进出设备壳体100即可，在飞行拍摄器220位于设备壳体100之外的情况下，飞行拍摄器220可以直接飞走，无需在飞行拍摄器220与设备壳体100之间直接设置可拆卸结构，这无疑能够简化用户的操作，同时方便用户的使用。
一种可选的方案中，本发明实施例公开的电子设备包括安装支架210的情况下，安装支架210还可以设置有补光模组、受话器、指纹识别模组和USB 接口中的至少一者。在此种情况下，能够避免上述功能器件的设置对电子设备的显示屏的布设面积的影响，从而能够进一步提高电子设备的屏幕占比。在使用的过程中，上述功能器件可随安装支架210通过开口伸出至设备壳体100之外，在工作完成之后，上述功能器件可随安装支架210通过开口回缩至设备壳体100之内，从而实现在设备壳体100之内的隐藏。
一种可选方案，安装支架210通过滑轨与设备壳体100滑动连接。设备壳体100的开口设有限位结构，在安装支架210的主体滑出设备壳体100的开口时，开口的限位结构限制安装支架210进一步滑出，安装支架210与设备壳体100不分离。此时，飞行拍摄器220承托在安装支架上，用户可以手动取出飞行拍摄器220。
本发明实施例公开的电子设备中，飞行拍摄器220的结构可以有多种。可选的方案中，飞行拍摄器220包括机壳221以及设置于机壳221的第一摄像头222、电池223、螺旋桨224和第二驱动机构，第二驱动机构与螺旋桨224驱动相连，且驱动螺旋桨224转动，电池223与第一摄像头222和第二驱动机构供电连接。在具体的工作过程中，螺旋桨224在第二驱动机构的驱动下旋转，进而带动整个飞行拍摄器220飞行，在飞行的过程中，飞行拍摄器220能够通过调整自己的位置，从而实现第一摄像头222进行较为灵活地拍摄。
可选的方案中，本发明实施例公开的机壳221可以包括顶壁、底壁和连接顶壁与底壁的侧壁，侧壁开设有第一拍摄视窗221a，第一摄像头222设置在机壳221之内，且第一摄像头222的镜头与第一拍摄视窗221a相对设置。在此种情况下，第一摄像头222能够通过开设于侧壁的第一拍摄视窗221a，从而实现向飞行拍摄器220的侧向的拍摄，这无疑能够满足飞行拍摄器220从侧向进行拍摄。第一摄像头222设置于机壳221之内，从而能够得到机壳221的防护，避免飞行过程中发生磕碰而发生的损坏。
本发明实施例公开的飞行拍摄器220还可以包括第二摄像头225，第二摄像头225设置在机壳221之内，底壁开设有第二拍摄视窗221b，第二摄像头225的镜头与第二拍摄视窗221b相对设置。在此种情况下，飞行拍摄器220的第二摄像头225能够通过第二拍摄视窗221b进行俯视拍摄。与此同时，第二摄像头225设置于机壳221之内，从而能够得到机壳221的防护。在此 种情况下，第二摄像头225可以用于通过俯视拍摄，进而来实现物体高度数据的检测。
本发明实施例公开的飞行拍摄器220还可以包括器件支架226，器件支架226设置在机壳221之内，第一摄像头222、第二摄像头225和电池223均安装在器件支架226上。在此种装配方式下，可以先将第一摄像头222、第二摄像头225和电池223预先安装在器件支架226上，然后连同器件支架226形成模块化结构，再整体向机壳221内安装，这无疑能够提高组装效率。
如上文所述，机壳221的侧壁开设有第一拍摄视窗221a，一种具体的实施方式中，侧壁的数量可以为四个，第一拍摄视窗221a设置在一个侧壁上，其他的三个侧壁和底壁均可以设置有靠近传感器，靠近传感器能够避免飞行拍摄器220在飞行的过程中与其它物体发生碰撞。具体的，靠近传感器可以为红外靠近传感器227。这无疑能够提高飞行拍摄器220飞行的安全性。当然，顶壁也可以设置有靠近传感器。
为了实现更为灵活地拍摄，在较为优选的方案中，本发明实施例公开的飞行拍摄器220可以包括第三摄像头和第四摄像头，第三摄像头和第四摄像头可以分别设置于机壳221之外，第三摄像头和第四摄像头可以相背分布，第三摄像头和第四摄像头均与机壳221球面铰接，通过调节第三摄像头和第四摄像头的角度，从而实现更大视场的拍摄，当然也能够实现更多的拍摄视角。
在本发明实施例中，飞行拍摄器220可以一个螺旋桨224，也可以包括多个螺旋桨224，多个螺旋桨224间隔设置，多个螺旋桨224共同作用从而能够使得飞行拍摄器220的飞行更加平稳。一种具体的实施方式中，螺旋桨224的数量为四个，四个螺旋桨224依次设置在机壳221的四个角部，成对角分布的两个螺旋桨224与成对角分布的另外两个螺旋桨224的转动方向可以相反，从而实现驱动的均衡性，使得飞行拍摄器220能够更好地实现位置的维持。
具体的，第二驱动机构的数量可以为一个，也可以为多个，在第二驱动机构的数量为一个的情况下，第二驱动机构可以通过传动机构实现对所有的螺旋桨224旋转的驱动。一种可选的方案中，第二驱动机构与螺旋桨224的 数量相等，每个第二驱动机构与一个螺旋桨224驱动相连。此种为每个螺旋桨224单独配置一个第二驱动机构的情况，使得飞行拍摄器220无需较为复杂的动力传输机构，有利于简化飞行拍摄器220的整体结构。与此同时，第二驱动机构的数量为多个，能够在部分第二驱动机构发生故障而停止运行的情况下，由于其它的第二驱动机构的驱动，能够维持飞行拍摄器220的持续飞行。
请再次参考图4，一种可选方案中，机壳221可以包括壳主体2211和盖体2212，盖体2212固定在壳主体2211的开口上，螺旋桨224和第二驱动机构均安装在壳主体2211上，盖体2212开设有避让豁口，避让豁口沿螺旋桨224的部分边缘设置。此种情况下，螺旋桨224和第二驱动机构均安装于壳主体2211，较方便实现在同一安装基础上实现两者之间的装配。与此同时，方便用户在维修的过程中打开盖体2212，进而方便对机壳221内的配件进行检修。一种具体的实施方式中，盖体2212可以通过卡接、螺纹连接件等固定方式固定在壳主体2211上。
请再次参考图4，一种具体的实施方式中，壳主体2211的侧壁(即机壳221的侧壁)可以开设有安装孔2211a，机壳221还可以包括封盖228，封盖228可以设置有充电触点，充电触点与电池223电连接，进而实现对飞行拍摄器220进行充电。当然，单独的封盖228无疑更方便在其上设置充电连接结构，具体的，封盖228可以与安装孔2211a可拆卸相连，进而方便用户拆卸封盖228对飞行拍摄器220的局部结构进行检修。
本发明实施例公开的电子设备可以是智能手机、平板电脑、电子书阅读器、可穿戴设备(例如智能手表)、游戏机等设备，当然，本发明实施例公开的电子设备还可以为其他种类，本发明实施例不限制电子设备的具体种类。
本发明上文实施例中重点描述的是各个实施例之间的不同，各个实施例之间不同的优化特征只要不矛盾，均可以组合形成更优的实施例，考虑到行文简洁，在此则不再赘述。
以上所述仅为本发明的实施例而已，并不用于限制本发明。对于本领域技术人员来说，本发明可以有各种更改和变化。凡在本发明的精神和原理之 内所作的任何修改、等同替换、改进等，均应包含在本发明的权利要求范围之内。

Claims (10)

  1. 一种电子设备，包括设备壳体和飞行拍摄器，所述设备壳体具有开口与内腔，所述开口与所述内腔连通，所述飞行拍摄器可移动地设置于所述设备壳体，所述飞行拍摄器可通过所述开口伸出至所述设备壳体之外或回缩至所述设备壳体之内，在所述飞行拍摄器位于所述设备壳体之外的情况下，所述飞行拍摄器可与所述设备壳体分离。
  2. 根据权利要求1所述的电子设备，其中，所述电子设备还包括安装支架，所述安装支架可移动地设置于所述设备壳体，所述飞行拍摄器设置于所述安装支架上，所述飞行拍摄器可随所述安装支架通过所述开口伸出至所述设备壳体之外或回缩至所述设备壳体之内，在所述飞行拍摄器伸出至所述设备壳体之外的情况下，所述飞行拍摄器可与所述安装支架分离。
  3. 根据权利要求2所述的电子设备，其中，所述电子设备还包括第一驱动机构，所述第一驱动机构与所述安装支架驱动相连，所述第一驱动机构驱动所述安装支架带动所述飞行拍摄器，通过所述开口伸出至所述设备壳体之外或回缩至所述设备壳体之内。
  4. 根据权利要求1所述的电子设备，其中，所述飞行拍摄器包括机壳以及设置于所述机壳的第一摄像头、电池、螺旋桨和第二驱动机构，所述第二驱动机构与所述螺旋桨驱动相连，且驱动所述螺旋桨转动，所述电池与所述第一摄像头和所述第二驱动机构供电连接。
  5. 根据权利要求4所述的电子设备，其中，所述机壳包括顶壁、底壁和连接所述顶壁与所述底壁的侧壁，所述侧壁开设有第一拍摄视窗，所述第一摄像头设置在所述机壳之内，且所述第一摄像头的镜头与所述第一拍摄视窗相对设置。
  6. 根据权利要求5所述的电子设备，其中，所述飞行拍摄器还包括第二摄像头，所述第二摄像头设置在所述机壳之内，所述底壁开设有第二拍摄视窗，所述第二摄像头的镜头与所述第二拍摄视窗相对设置。
  7. 根据权利要求6所述的电子设备，其中，所述飞行拍摄器还包括器件支架，所述器件支架设置在所述机壳之内，所述第一摄像头、所述第二摄像 头和所述电池均安装在所述器件支架上。
  8. 根据权利要求5所述的电子设备，其中，所述侧壁为四个，所述第一拍摄视窗设置在一个所述侧壁上，其他的三个所述侧壁和所述底壁均设置有红外靠近传感器。
  9. 根据权利要求4所述的电子设备，其中，所述螺旋桨的数量为四个，四个所述螺旋桨依次设置在所述机壳的四个角部，成对角分布的两个所述螺旋桨与成对角分布的另外两个所述螺旋桨的转动方向相反，所述第二驱动机构与所述螺旋桨的数量相等，每个所述第二驱动机构与一个所述螺旋桨驱动相连。
  10. 根据权利要求4所述的电子设备，其中，所述机壳包括壳主体及盖体，所述盖体固定在所述壳主体的开口上，所述螺旋桨和所述第二驱动机构均安装在所述壳主体上，所述盖体开设有避让豁口，所述避让豁口沿所述螺旋桨的部分边缘设置。
PCT/CN2020/139211 2019-12-27 2020-12-25 电子设备 WO2021129778A1 (zh)

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