WO2018068375A1 - 感测组件及具有该感测组件的电子装置、无人机 - Google Patents

感测组件及具有该感测组件的电子装置、无人机 Download PDF

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Publication number
WO2018068375A1
WO2018068375A1 PCT/CN2016/109274 CN2016109274W WO2018068375A1 WO 2018068375 A1 WO2018068375 A1 WO 2018068375A1 CN 2016109274 W CN2016109274 W CN 2016109274W WO 2018068375 A1 WO2018068375 A1 WO 2018068375A1
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Prior art keywords
sensing assembly
sensor
substrate
shielding layer
light shielding
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PCT/CN2016/109274
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English (en)
French (fr)
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冯建刚
唐尹
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深圳市大疆创新科技有限公司
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Publication of WO2018068375A1 publication Critical patent/WO2018068375A1/zh

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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D3/00—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups
    • G01D3/028—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups mitigating undesired influences, e.g. temperature, pressure
    • G01D3/036—Indicating or recording apparatus with provision for the special purposes referred to in the subgroups mitigating undesired influences, e.g. temperature, pressure on measuring arrangements themselves
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L11/00—Measuring steady or quasi-steady pressure of a fluid or a fluent solid material by means not provided for in group G01L7/00 or G01L9/00
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L19/00—Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
    • G01L19/14—Housings
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01W—METEOROLOGY
    • G01W1/00—Meteorology
    • G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed

Definitions

  • the invention relates to a sensing component and an electronic device and a drone having the same.
  • sensing components For the purpose of intelligent control, environmental monitoring and human-computer interaction, many existing devices, such as sensing components, are equipped with sensing components and/or electronic devices having sensing components to obtain an environment or a state thereof. information.
  • sensing components such as barometers
  • the sensing components are sensitive to the light, temperature, airflow, etc., and the sensing components will be difficult to function properly or even cause equipment failure. Or damaged.
  • a sensing assembly includes a substrate and a sensor disposed on the substrate.
  • the sensing component further includes a light shielding layer and a cover.
  • the light shielding layer covers the sensor and can prevent the influence of illumination on the sensor.
  • the cover is disposed outside the sensor and the light shielding layer.
  • the sensing component has a slit or a through hole, and the slit or the through hole can make the inner and outer sides of the outer cover breathable.
  • the slit is formed between the outer cover and the substrate.
  • the slit is formed on the outer cover.
  • the outer cover is an opaque outer cover.
  • the substrate includes a mounting surface and a side surface
  • the sensor is disposed on the mounting surface
  • the cover covers the sensor and the light shielding layer and is coupled to the mounting surface
  • the substrate is provided with a connecting hole recessed from the mounting surface, and the outer cover forms a connecting portion corresponding to the connecting hole, and the connecting hole and the connecting portion cooperate to position the outer cover On the substrate.
  • the side has a plurality of engaging portions, and the engaging portion can be engaged with other structures to position the sensing assembly.
  • the engaging portion is a groove
  • the engaging portion is a protrusion.
  • the substrate is a circuit board, and the sensor is electrically connected to the surface of the substrate.
  • the substrate is any one of a hard circuit board, a flexible circuit board, or a hard and soft circuit board.
  • the light shielding layer covers a surface of the side of the sensor facing away from the substrate;
  • the light shielding layer simultaneously covers a side of the sensor and a side surface facing away from the substrate.
  • the light shielding layer is a gas permeable light shielding layer or a sponge light shielding layer.
  • the sensing component is a barometer.
  • An electronic device comprising at least a sensing component as described above.
  • a drone comprising at least a sensing component as described above.
  • the drone is an unmanned aerial vehicle, an unmanned vehicle or an unmanned vehicle.
  • the sensing component adopts the cover to reduce the influence of airflow, temperature and illumination on the sensing accuracy, thereby ensuring accurate acquisition of data of the electronic device and the drone having the sensing component and Play a predetermined function.
  • FIG. 1 is an exploded view of a sensing assembly provided by an embodiment of the present invention.
  • FIG. 2 is a cross-sectional view of the sensing assembly of FIG. 1 assembled.
  • a component when referred to as being “fixed” to another component, it can be directly on the other component or the component can be present.
  • a component When a component is considered to "connect” another component, it can be directly connected to another component or possibly a central component.
  • a component When a component is considered to be “set to” another component, it can be placed directly on another component or possibly with a centered component.
  • the terms “vertical,” “horizontal,” “left,” “right,” and the like, as used herein, are for illustrative purposes only.
  • an embodiment of the present invention provides a sensing component 100 for acquiring data of an environment in which the sensing component 100 can be a device such as a drone.
  • Functions such as intelligent control, environmental monitoring, and human-computer interaction provide parameters.
  • the sensing component 100 can be a sensing component of the type of sight, hearing, touch, and the like.
  • the sensing component 100 is a barometer for acquiring air pressure data of the environment in which it is located to provide the required parameters for the drone.
  • the UAV may be an unmanned aerial vehicle, an unmanned vehicle, an unmanned vehicle, or the like, which is not operated by an airborne person.
  • the UAV is an unmanned aerial vehicle, and the UAV may be a rotor.
  • Aircraft eg, single-rotor, twin-rotor, three-rotor, quad-rotor, six-rotor, and eight-rotor aircraft
  • the sensing component 100 can be disposed in the Any suitable position of the drone is set, for example, inside, above, below, behind, behind, etc. of the drone.
  • the sensing assembly 100 includes a substrate 10, a sensor 20, a light shielding layer 30, and a cover 40.
  • the sensor 20 is disposed on the substrate 10
  • the light shielding layer 30 covers the sensor 20
  • the cover 40 is disposed outside the sensor 20 and the light shielding layer 30 .
  • the substrate 10 is used to carry the sensor 20, the light shielding layer 30, and the outer cover 40.
  • the substrate 10 is a circuit board that is electrically connected to the sensor 20 and is capable of transmitting the sensed data of the sensor 20 to other electronic components (eg, a processor).
  • the substrate 10 may be a rigid circuit board, a flexible circuit board, or a hard and soft combined circuit board.
  • the substrate 10 includes a mounting surface 11 and a side surface 12.
  • the mounting surface 11 is a surface facing the sensor 20, and the side surface 12 is located on the circumferential side of the substrate 10 and is connected to the mounting surface 11.
  • a connecting hole 111 recessed from the mounting surface 11 is opened on the substrate 10, and the connecting hole 111 is used to connect the outer cover 40.
  • the number of the connection holes 111 is one piece, and both are round holes. It can be understood that the number and shape of the connecting holes 111 can be appropriately changed according to actual needs, and is not limited to the illustrated embodiment.
  • the side surface 12 has a plurality of engaging portions 121 for engaging with other structures to position the sensing assembly 100.
  • the engaging portion 121 is a groove. It can be understood that the engaging portion 121 can also be a protrusion as long as the sensing component 100 can be positioned.
  • the sensor 20 is a part of the sensing component 100 that collects environmental information, and can convert the data of the environmental information into a corresponding electrical signal.
  • the sensor 20 is typically used to sense information about a certain aspect of the environment (eg, air pressure, temperature, altitude, etc.), while the sensor 20 senses certain aspects of the information while being susceptible to other factors of the environment. The impact of the sensor 20 is therefore minimized or eliminated.
  • the sensor 20 is capable of collecting air pressure information, and the sensing accuracy of the sensor 20 is susceptible to changes in illumination, airflow, and temperature.
  • the senor 20 is electrically connected to the mounting surface 11 .
  • the sensor 20 is disposed on the mounting surface 11 by using a surface mount technology (SMT). It can be understood that the sensor 20 can also be disposed on the mounting surface 11 by any other suitable technique.
  • SMT surface mount technology
  • the light shielding layer 30 covers the sensor 20 to prevent the sensor 20 from being subjected to non- The effect of the expected illumination ensures the sensing accuracy of the sensor 20.
  • the light shielding layer 30 is a gas permeable light shielding layer to enable the sensor 20 to correctly sense a change in air pressure.
  • the light shielding layer 30 is a sponge. It can be understood that the light shielding layer 30 can also adopt other suitable gas permeable materials, such as foam, fabric, and the like.
  • the light shielding layer 30 covers a surface of the sensor 20 facing away from the substrate 10 .
  • the light shielding layer 30 may simultaneously cover the side surface of the sensor 20 and the side surface facing away from the substrate 10.
  • the cover 40 covers the sensor 20 and the light shielding layer 30 is connected to the substrate 10 for preventing external airflow from affecting the sensing accuracy of the sensor 20, and the inside of the outer cover 40 can maintain a relatively stable temperature. Environment, reducing the effect of temperature changes on the sensor 20.
  • the outer cover 40 is made of an opaque material that further reduces the effects of illumination on the sensor 20.
  • the cover 40 includes a cover 41 and a connecting portion 42.
  • the cover body 41 has a substantially square shape. It can be understood that in other embodiments, the cover body 41 may have other regular or irregular shapes such as a circular shape and a polygonal shape.
  • the connecting portion 42 corresponds to the connecting hole 111 on the substrate 10, and the outer cover 40 can be positioned and fixed in cooperation with the connecting hole 111.
  • the connecting portion 42 is a column protruding from the cover 41, and the connecting portion 42 can be interference-fitted with the corresponding connecting hole 111.
  • the structure of the connecting hole 111 and the connecting portion 42 may be interchanged, that is, a structure similar to the connecting portion 42 may be formed on the substrate 10, and the outer cover 40 may be formed like the connecting hole 111.
  • the substrate 10 may have a structure similar to the connecting portion 42 and the connecting hole 111.
  • the outer cover 40 is also formed with a corresponding connecting hole and a connecting portion.
  • a gap 50 is formed between the outer cover 40 and the mounting surface 11 for venting the sensor 20 to properly sense the change in air pressure.
  • the outer cover 40 is formed by the connecting portion 42 separating the cover 41 from the mounting surface 11.
  • the slit 50 may also be a recess formed on a side surface of the cover 41 facing the substrate 10.
  • the slit 50 can also be formed at other positions of the cover 41.
  • the slit 50 is a slit formed at the top or the side of the cover 41.
  • the sensing assembly adopts the cover to reduce airflow, temperature and illumination to sensing accuracy The influence can thus ensure accurate acquisition of data and play a predetermined function of the electronic device and the drone having the sensing component.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Atmospheric Sciences (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Ecology (AREA)
  • Environmental Sciences (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)

Abstract

一种感测组件（100），包括基板（10）以及设置于所述基板（10）上的传感器（20）；所述感测组件（100）还包括遮光层（30）以及外罩（40）；所述遮光层（30）覆盖所述传感器（20），能够防止光照对所述传感器（20）的影响；所述外罩（40）罩设于所述传感器（20）以及所述遮光层（30）外；所述感测组件（100）采用所述外罩（40）能够减少气流、温度以及光照对感测精度的影响，因此能够确保具有所述感测组件（100）的电子设备及无人机的准确获取数据及发挥预定的功能。

Description

感测组件及具有该感测组件的电子装置、无人机 技术领域
本发明涉及一种感测组件及具有该感测组件的电子装置、无人机。
背景技术
为实现智能控制、环境监测及人机交互等目的，现有很多设备，例如感测组件等，都配置有感测组件及/或具有感测组件的电子装置，以获得环境或者自身的状态的信息。但是，很多感测组件，例如气压计等，其感测精度容易受到光、温度、气流等的影响，一旦受到上述因素的影响，所述感测组件将难以正确发挥功能，甚至或造成设备失灵或者损坏。
发明内容
有鉴于此，有必要提供一种能够避免上述问题的感测组件及具有所述感测组件的电子装置、无人机。
一种感测组件，包括基板以及设置于所述基板上的传感器。所述感测组件还包括遮光层以及外罩。所述遮光层覆盖所述传感器，能够防止光照对所述传感器的影响。所述外罩罩设于所述传感器以及所述遮光层外。
进一步地，所述感测组件具有缝隙或者通孔，所述缝隙或者通孔能够使所述外罩的内外透气。
进一步地，所述缝隙形成于所述外罩与所述基板之间；或者，
所述缝隙形成于所述外罩上。
进一步地，所述外罩为不透明外罩。
进一步地，所述基板包括装配面以及侧面，所述传感器设置于所述装配面上，所述外罩罩设所述传感器以及所述遮光层并连接于所述装配面。
进一步地，所述基板上开设有从所述装配面凹陷的连接孔，所述外罩上形成对应于所述连接孔的连接部，所述连接孔与所述连接部相互配合将所述外罩定位于所述基板上。
进一步地，所述侧面上具有多个卡合部，所述卡合部能够与其他结构卡合，以定位所述感测组件。
进一步地，所述卡合部为凹槽；或者，
所述卡合部为凸起。
进一步地，所述基板为电路板，所述传感器电连接地设置于所述基板表面。
进一步地，所述基板为硬质电路板、柔性电路板或者软硬结合电路板中的任意一种。
进一步地，所述遮光层覆盖所述传感器背离所述基板的一侧表面设置；或者，
所述遮光层同时覆盖所述传感器的侧面以及背离所述基板的一侧表面。
进一步地，所述遮光层为透气遮光层或海绵遮光层。
进一步地，所述感测组件为气压计。
一种电子装置，至少包括如上所述的感测组件。
一种无人机，至少包括如上所述的感测组件。
进一步地，所述无人机为无人飞行器、无人车或者无人船。
相对于现有技术，所述感测组件采用所述外罩能够减少气流、温度以及光照对感测精度的影响，因此能够确保具有所述感测组件的电子设备及无人机的准确获取数据及发挥预定的功能。
附图说明
图1是本发明实施方式提供的一种感测组件的分解图。
图2是图1的感测组件组装完成后的剖视图。
主要元件符号说明
感测组件                       100
基板                           10
装配面                         11
连接孔                         111
侧面                           12
卡合部                         121
传感器                         20
遮光层                         30
外罩                           40
罩体                           41
连接部                          42
缝隙                            50
如下具体实施方式将结合上述附图进一步说明本发明。
具体实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅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。
需要说明的是，当组件被称为“固定于”另一个组件，它可以直接在另一个组件上或者也可以存在居中的组件。当一个组件被认为是“连接”另一个组件，它可以是直接连接到另一个组件或者可能同时存在居中组件。当一个组件被认为是“设置于”另一个组件，它可以是直接设置在另一个组件上或者可能同时存在居中组件。本文所使用的术语“垂直的”、“水平的”、“左”、“右”以及类似的表述只是为了说明的目的。
除非另有定义，本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的，不是旨在于限制本发明。本文所使用的术语“及/或”包括一个或多个相关的所列项目的任意的和所有的组合。
请参阅图1及图2，本发明实施方式提供一种感测组件100，所述感测组件100用于获取所处的环境的数据，所述感测组件100能够为无人机等设备的智能控制、环境监测及人机交互等功能提供参数。所述感测组件100可以为视觉、听觉、触觉等类型的感测组件。本实施方式中，所述感测组件100为气压计，用于获取所处环境的气压数据，以为所述无人机提供所需的参数。所述无人机可以为无人飞行器、无人车、无人船等没有机载人员操纵的设备，本实施方式中，所述无人机为无人飞行器，所述无人飞行器可以为旋翼飞行器(例如单旋翼、双旋翼、三旋翼、四旋翼、六旋翼及八旋翼飞行器等)固定翼飞行器或固定翼与旋翼混合的飞行器。所述感测组件100可以设置于所 述无人机的任意合适的位置，例如，设置于无人机内部、上方、下方、前方、后方等。
所述感测组件100包括基板10、传感器20、遮光层30以及外罩40。所述传感器20设置于所述基板10上，所述遮光层30覆盖所述传感器20，所述外罩40罩设于所述传感器20以及所述遮光层30外。
所述基板10用于承载所述传感器20、所述遮光层30以及所述外罩40。本实施方式中，所述基板10为电路板，其与所述传感器20电连接，能够将所述传感器20的所感测到的数据传送至其他电子元件(例如处理器)。具体地，所述基板10可以为硬质电路板、柔性电路板或者软硬结合电路板。
具体到图示的实施方式中，所述基板10包括装配面11以及侧面12。所述装配面11为朝向所述传感器20的表面，所述侧面12位于所述基板10周侧且与所述装配面11相连。所述基板10上开设有从所述装配面11凹陷的连接孔111，所述连接孔111用于连接所述外罩40。本实施方式中，所述连接孔111的数量为连个，且均为圆孔。可以理解，所述连接孔111的数量和形状可以依据实际需求作合适的变化，并不限于图示的实施方式。所述侧面12上具有多个卡合部121，所述卡合部121用于与其他结构卡合，以定位所述感测组件100。本实施方式中，所述卡合部121为凹槽，可以理解，所述卡合部121也可以为凸起，只要能够定位所述感测组件100即可。
所述传感器20为所述感测组件100的采集环境信息的部分，能够将环境信息的数据转换为相应的电信号。所述传感器20通常用于感测环境的某一方面的信息(例如，气压、温度、高度等)，所述传感器20感测某一方面的信息的同时，还容易受所述环境的其他因素的影响，因此需要尽量减小或者消除其他因素对所述传感器20的影响。本实施方式中，所述传感器20能够采集气压信息，所述传感器20的感测精度易受光照、气流、温度变化的影响。
本实施方式中，所述传感器20电连接地设置于所述装配面11上，具体地，所述传感器20采用表面贴装技术(SMT)设置于所述装配面11上。可以理解，所述传感器20还可以采用其他任意合适的技术设置于所述装配面11上。
所述遮光层30覆盖所述传感器20设置，以避免所述传感器20受到非 预期的光照的影响，确保所述传感器20的感测精度。所述遮光层30为透气遮光层，以使所述传感器20能够正确感测气压的变化。本实施方式中，所述遮光层30为海绵，可以理解，所述遮光层30也可以采用其他合适的透气材料，例如泡棉、织物等。
本实施方式中，所述遮光层30覆盖所述传感器20背离所述基板10的一侧表面设置。在其他的实施方式中，所述遮光层30也可以同时覆盖所述传感器20的侧面以及背离所述基板10的一侧表面。
所述外罩40罩设所述传感器20以及所述遮光层30连接于所述基板10，用于避免外部气流影响所述传感器20的感测精度，同时所述外罩40内部可以维持相对稳定的温度环境，减少温度变化对所述传感器20的影响。优选地，所述外罩40由不透明材料制成，可以进一步减少光照对所述传感器20的影响。
所述外罩40包括罩体41以及连接部42。本实施方式中，所述罩体41大致呈方形，可以理解，在其他的实施方式中，所述罩体41也可以为圆形、多边性等其他规则或者不规则的形状。所述连接部42与所述基板10上的连接孔111对应，能够与所述连接孔111配合定位并固定所述外罩40。本实施方式中，所述连接部42为凸出于所述罩体41的柱体，所述连接部42能够与对应的所述连接孔111过盈配合。可以理解，所述连接孔111以及所述连接部42的结构可以互换，即，所述基板10上可以形成类似所述连接部42的结构，所述外罩40可以形成类似所述连接孔111的结构；另外，所述基板10上可以既有类似所述连接部42及类似所述连接孔111的结构，此时，所述外罩40也形成有对应的连接孔及连接部的结构。
所述外罩40与所述装配面11之间具有缝隙50，所述缝隙50用于透气，以使所述传感器20能够正确感测气压的变化。本实施方式中，所述外罩40由所述连接部42将所述罩体41支离所述装配面11而形成。
可以理解，所述缝隙50也可以为形成于所述罩体41朝向所述基板10的一侧表面上的凹陷。
可以理解，所述缝隙50也可以形成于罩体41的其他位置，例如，所述缝隙50为开设于罩体41的顶部或者侧部的狭槽。
所述感测组件采用所述外罩能够减少气流、温度以及光照对感测精度的 影响，因此能够确保具有所述感测组件的电子设备及无人机的准确获取数据及发挥预定的功能。
另外，对于本领域的普通技术人员来说，可以根据本发明的技术构思做出其它各种相应的改变与变形，而所有这些改变与变形都应属于本发明权利要求的保护范围。

Claims (16)

  1. 一种感测组件，包括基板以及设置于所述基板上的传感器，其特征在于：所述感测组件还包括遮光层以及外罩，所述遮光层覆盖所述传感器，能够防止光照对所述传感器的影响，所述外罩罩设于所述传感器以及所述遮光层外。
  2. 如权利要求1所述的感测组件，其特征在于：所述感测组件具有缝隙或通孔，所述缝隙或通孔能够使所述外罩的内外透气。
  3. 如权利要求2所述的感测组件，其特征在于：所述缝隙或通孔形成于所述外罩与所述基板之间；或者，
    所述缝隙或通孔形成于所述外罩上。
  4. 如权利要求1所述的感测组件，其特征在于：所述外罩为不透明外罩。
  5. 如权利要求1所述的感测组件，其特征在于：所述基板包括装配面以及侧面，所述传感器设置于所述装配面上，所述外罩罩设所述传感器以及所述遮光层并连接于所述装配面。
  6. 如权利要求5所述的感测组件，其特征在于：所述基板上开设有从所述装配面凹陷的连接孔，所述外罩上形成对应于所述连接孔的连接部，所述连接孔与所述连接部相互配合将所述外罩定位于所述基板上。
  7. 如权利要求5所述的感测组件，其特征在于：所述侧面上具有多个卡合部，所述卡合部能够与其他结构卡合，以定位所述感测组件。
  8. 如权利要求7所述的感测组件，其特征在于：所述卡合部为凹槽；或者，
    所述卡合部为凸起。
  9. 如权利要求1所述的感测组件，其特征在于：所述基板为电路板，所述传感器电连接地设置于所述基板表面。
  10. 如权利要求9所述的感测组件，其特征在于：所述基板为硬质电路板、柔性电路板或者软硬结合电路板中的任意一种。
  11. 如权利要求1所述的感测组件，其特征在于：所述遮光层覆盖所述传感器背离所述基板的一侧表面设置；或者，
    所述遮光层同时覆盖所述传感器的侧面以及背离所述基板的一侧表面。
  12. 如权利要求1所述的感测组件，其特征在于：所述遮光层为透气遮光层或海绵遮光层。
  13. 如权利要求1所述的感测组件，其特征在于：所述感测组件为气压计。
  14. 一种电子装置，至少包括如权利要求1-13任意一项所述的感测组件。
  15. 一种无人机，至少包括如权利要求1-13任意一项所述的感测组件。
  16. 如权利要求15所述的无人机，其特征在于：所述无人机为无人飞行器、无人车或者无人船。
PCT/CN2016/109274 2016-10-13 2016-12-09 感测组件及具有该感测组件的电子装置、无人机 WO2018068375A1 (zh)

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CN206926829U (zh) * 2017-05-19 2018-01-26 深圳市大疆创新科技有限公司 气压计组件及无人机
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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5014100A (en) * 1987-12-18 1991-05-07 Semiconductor Energy Laboratory Co., Ltd. Image sensor free from undesirable incident light rays which have not been reflected in the surface bearing the image to be sensed
CN101030015A (zh) * 2006-03-03 2007-09-05 富士通株式会社 图像采集装置
CN101750934A (zh) * 2008-12-05 2010-06-23 柯尼卡美能达商用科技株式会社 感光单元和成像设备
CN204439984U (zh) * 2015-02-06 2015-07-01 东莞佰鸿电子有限公司 一种具有黑色光阻的微型相机模组
CN204946029U (zh) * 2015-06-23 2016-01-06 天津市卓扬世纪科技发展有限公司 一种新型指纹识别传感器

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5014100A (en) * 1987-12-18 1991-05-07 Semiconductor Energy Laboratory Co., Ltd. Image sensor free from undesirable incident light rays which have not been reflected in the surface bearing the image to be sensed
CN101030015A (zh) * 2006-03-03 2007-09-05 富士通株式会社 图像采集装置
CN101750934A (zh) * 2008-12-05 2010-06-23 柯尼卡美能达商用科技株式会社 感光单元和成像设备
CN204439984U (zh) * 2015-02-06 2015-07-01 东莞佰鸿电子有限公司 一种具有黑色光阻的微型相机模组
CN204946029U (zh) * 2015-06-23 2016-01-06 天津市卓扬世纪科技发展有限公司 一种新型指纹识别传感器

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