WO2020062536A1 - 无人机及其插接件 - Google Patents

无人机及其插接件 Download PDF

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Publication number
WO2020062536A1
WO2020062536A1 PCT/CN2018/117921 CN2018117921W WO2020062536A1 WO 2020062536 A1 WO2020062536 A1 WO 2020062536A1 CN 2018117921 W CN2018117921 W CN 2018117921W WO 2020062536 A1 WO2020062536 A1 WO 2020062536A1
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WO
WIPO (PCT)
Prior art keywords
support
support plate
circuit board
connector
casing
Prior art date
Application number
PCT/CN2018/117921
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English (en)
French (fr)
Inventor
刘煜程
高诗经
Original Assignee
深圳市大疆创新科技有限公司
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.)
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Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to CN201880016204.0A priority Critical patent/CN110915074A/zh
Publication of WO2020062536A1 publication Critical patent/WO2020062536A1/zh

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    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/46—Bases; Cases
    • H01R13/502—Bases; Cases composed of different pieces
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/66—Structural association with built-in electrical component

Definitions

  • the embodiment of the present invention relates to a drone and its connector, and belongs to the technical field of drones and their parts.
  • the existing cable connection method not only needs to mechanically connect the functional module to the body of the drone, but also needs to further connect the cable plug of the functional module with the socket configured in the fuselage to complete it.
  • the entire assembly process is not only complicated, but the cables are often exposed outside the fuselage, which greatly affects the aesthetics of the drone.
  • Embodiments of the present invention provide a drone and its connector to solve the above or other potential problems.
  • a plug connector for a movable platform including: a housing, a circuit board, a connector, and a support; the housing for fixing to a mounting portion of a main device;
  • the circuit board is installed in the housing;
  • the connector is welded to one surface of the circuit board for electrical connection with an interface provided in the mounting portion, and the connector protrudes to the housing.
  • the support is disposed in the housing, and one end of the support is fixed to the housing, and the other end of the support is in contact with at least one surface of the circuit board.
  • the supporting member includes a first supporting member and a second supporting member, the first supporting member is in contact with the first surface of the circuit board, and the second supporting member is in contact with the first surface of the circuit board.
  • the second surface of the circuit board abuts, the second surface is opposite to the first surface, and the second support and the joint are located on the same side of the circuit board.
  • the first supporting member includes a first supporting plate and a second supporting plate, and the first supporting plate is fixed to the second supporting plate.
  • first support members there are two first support members, and the two first support members are respectively disposed on opposite sides of the longitudinal axis of the joint; The end is connected to the tail end of the second support plate, and the first support plate is disposed obliquely to the second support plate.
  • the first support member further includes a third support plate, the first support plate and the second support plate are oppositely disposed, and the second support plate is disposed on the first support Between the plate and the third support plate, and both ends of the second support plate are respectively fixed to the first support plate and the third support plate.
  • the first supporting member is one or more supporting posts.
  • the second support member includes two support bosses, and the two support bosses are disposed on opposite sides of the joint.
  • the two supporting bosses are symmetrically disposed on opposite sides of the joint.
  • the plug-in member as described above, wherein the plug-in member further includes two elastic protection pieces, the elastic protection pieces are disposed outside the housing, and the two elastic protection pieces are respectively located at the joints Two sides in the thickness direction; one end of the elastic protective sheet is fixed to the housing, and the other end of the elastic protective sheet extends in a direction away from the circuit board.
  • the plug-in member as described above, wherein the plug-in member further comprises a ring-shaped elastic protective sheet, the elastic protective sheet is disposed outside the casing, and the elastic protective sheet is surrounded by the elastic protective sheet The outside of the connector; one end of the elastic protective sheet is fixed to the housing, and the other end of the elastic protective sheet extends in a direction away from the circuit board.
  • the groove is formed in the mounting portion.
  • the housing includes: an upper case and a lower case, the upper case covers the lower case and forms a receiving space for receiving the circuit board and the support member;
  • the joint protrudes to the outside of the casing through an opening opened by the lower casing.
  • the bottom surface of the lower case is recessed toward the upper case; when the connector is used to electrically connect with the interface, a side surface of the upper case is used for the installation.
  • the portion cooperates to at least shield a portion of the joint protruding to the outside of the housing.
  • a drone includes a fuselage and a plug-in member as described above, and the plug-in member is plugged into a mounting portion of the fuselage.
  • a circuit board is provided in the housing and a connector for electrical connection is welded on the surface of the circuit board, so that when the plug-in is mounted on the mounting portion of the main device, It can be directly connected to the interface provided by the installation part of the main device, thereby avoiding the need to configure cables separately, simplifying the assembly process and improving the aesthetics of the movable platform.
  • the present application also provides a support member in the housing, so that when the plug-in member is installed on or removed from the movable platform, the support member can provide additional support for the circuit board to avoid the circuit board from deforming or occurring. Deformation tends to cause cracks or internal changes at the joint between the connector and the circuit board, thereby ensuring the reliability of the connection between the connector and the circuit board, thereby increasing the service life of the connector.
  • FIG. 1 is a top view of a connector according to an embodiment of the present invention
  • FIG. 2 is a bottom view of the connector in FIG. 1;
  • FIG. 3 is a cross-sectional view taken along A-A in FIG. 1;
  • FIG. 4 is a schematic partial structural diagram of an unmanned aerial vehicle provided by an embodiment of the present invention.
  • Figure 5 is a top view of Figure 4.
  • Fig. 6 is a sectional view taken along the line B-B in Fig. 5;
  • FIG. 7 is an enlarged view of the G position in FIG. 6;
  • FIG. 8 is an enlarged view of the F position in FIG. 3
  • FIG. 9 is a schematic structural diagram of a first support member according to an embodiment of the present invention.
  • FIG. 10 is another schematic structural diagram of a first support member according to an embodiment of the present invention.
  • first and second are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as “first” and “second” may explicitly or implicitly include at least one of the features. In the description of the embodiments of the present invention, the meaning of "a plurality” is at least two, for example, two, three, etc., unless it is specifically and specifically defined otherwise.
  • the terms “installation”, “connected”, “connected”, “fixed” and the like shall be understood in a broad sense unless specified and limited otherwise.
  • the terms may be a fixed connection or a fixed connection. Disassembly and connection, or integration; it can be directly connected or indirectly connected through an intermediate medium, and it can be the internal connection of two elements or the interaction relationship between two elements, unless it is clearly defined otherwise.
  • the specific meanings of the above terms in the embodiments of the present invention may be understood according to specific situations.
  • FIG. 1 is a top view of a plug-in component provided in the present embodiment
  • FIG. 2 is a bottom view of the plug-in component in FIG. 1
  • FIG. 3 is a cross-sectional view taken along the line A-A in FIG. 1.
  • this embodiment provides a plug-in for a movable platform, and the purpose of installing a device with certain functions to the movable platform can be achieved through the plug-in.
  • the device may be, for example, a photographing device, a lighting device, a detection device, a warning device, or other suitable devices.
  • the plug-in member of this embodiment When the plug-in member of this embodiment is fixed to the mounting portion of the movable platform, it can not only be mechanically fixed to the movable platform, but also can realize power supply and / or communication connection with the movable platform.
  • the above-mentioned movable platform may be, for example, various suitable types of mobile tools such as a drone, a car, a ship, and a remote control model.
  • FIG. 4 shows the structure of the drone
  • FIG. 5 is a top view of FIG. 4.
  • FIG. 4 and FIG. 5 only show a part of the structure diagram of the drone that cooperates with the connector 1 of this embodiment, that is, the vicinity of the installation part 21 of the main body 2 of the drone.
  • the structure omits conventional structures such as power components and tripods of the UAV. These conventional structures are basically the same as ordinary UAVs.
  • the main device of the drone in this embodiment, may be a center frame of the drone, for example, it may be a housing of the center frame.
  • FIG. 6 is a cross-sectional view taken along the line B-B in FIG. 5, and FIG. 7 is an enlarged view at a position G in FIG. 6.
  • the top surface of the main device is provided with a mounting portion 21, and an interface 211 mated with a connector 15 hereinafter is provided in the mounting portion 21.
  • the plug connector 1 of this embodiment includes a housing 11, a circuit board 13, a connector 15, and a support member.
  • the casing 11 is used for fixing to the mounting portion 21 of the main device of the drone to be described below;
  • the circuit board 13 is installed in the casing 11, and the upper end of the joint 15 is welded to the lower surface of the circuit board 13.
  • the lower end of the joint 15 extends from the inside of the casing 11 to the outside of the casing 11 so as to be electrically connected to the interface 211 provided in the mounting portion 21;
  • the support member is disposed in the casing 11, and one end thereof is connected to the casing 11. It is fixed, and the other end thereof is in contact with at least one surface of the circuit board 13.
  • the joint 15 in FIG. 3 may be rotated 180 degrees.
  • the lower end of the joint 15 is welded to the upper surface of the circuit board 13, and the upper end of the structure extends from the top of the housing 11. Out.
  • the joint 15 in FIG. 3 may be rotated 180 degrees.
  • the joint 15 can be soldered on any one of two opposite surfaces (the upper surface and the lower surface in FIG. 3) having the largest surface area of the circuit board 13.
  • the casing 11 may be made of plastic through molding, or may be made of a metal material (for example, steel) by molding or forging.
  • the casing 11 can be manufactured by being divided into two parts.
  • the upper shell 111 and the lower shell 113 may be manufactured separately, and then the two are buckled and fixed together to assemble into a complete shell 11.
  • a sealing mechanism may be provided between the upper case 111 and the lower case 113, for example, A seal ring or a labyrinth seal structure can be provided.
  • the upper casing 111 includes a top surface 1111 and a side surface 1113 surrounding the top surface 1111 and extending downward so as to be fixed to the mounting portion 21 of the drone.
  • the side surface 1113 is formed with a bent portion 1113a away from the cavity inside the housing 11, and a bolt 115 for fitting with a bolt hole in the mounting portion 21 may be provided on the bent portion 1113a.
  • a fitting hole 1113 b extending upward is also opened from the bottom of the side surface 1113. The fitting hole 1113 b is used to cooperate with the fitting protrusion formed on the mounting portion 21 so as to connect the plug-in member 1 and the mounting portion 21.
  • the bolt 115 may be provided, and the form of the bolt 115 and the fitting hole 1113b is not limited to the structure shown in FIG. 3, and it may take any suitable form.
  • the bolt 115 and the housing 11 may be designed as separate parts, or the fitting holes 1113b may not be provided in the form of upper narrow and lower width in FIG. Consistent width.
  • the lower shell 113 may be designed as an arc-shaped plate recessed into the cavity of the housing 11 as shown in FIG. 3, and the arc-shaped plate may match the shape of the bottom surface of the mounting portion 21.
  • the connector 15 extends from the inside of the housing 11 to the outside of the housing or Part of it will be blocked by the side of the upper case 111, and because the shape of the arc-shaped plate matches the inner surface of the mounting portion 21, the joint 15 plugged into the interface 211 is completely covered by the side of the housing 11 and the mounting portion 21 Wrapped in the inner surface.
  • the distance between the circuit board 13 and the opening on the arc-shaped plate for the connector 15 to protrude can be reduced, so that a more compact connector 15 can be used in order to make the entire connector 1 more compact.
  • An upwardly extending top portion 1131 and a fixing portion 1133 may be formed on the curved plate.
  • the top portion 1131 may abut a step surface formed by a side surface 1113 of the upper case 111, and the fixing portion 1133 is used to fix the circuit board 13. .
  • an extending edge 1113c is formed on the bent portion 1113a of the side surface 1113 of the upper case 111, and an inner surface of the extending edge 1113c is partially removed, thereby forming a supporting portion for abutting against the supporting portion of the lower case 113. Step surface.
  • Bolt holes are provided at the top of the fixing portion 1133.
  • the circuit board 13 is placed on the top of the fixing portion 1133, and then fixed to the fixing portion 1133 by bolts.
  • the circuit board 13 can be any suitable circuit board 13 capable of realizing corresponding functions.
  • the circuit board 13 for controlling LED lights can be used.
  • an image sensing device needs to be connected to the drone through the plug-in 1
  • a circuit board 13 for implementing image processing and / or image transmission can be used.
  • the connector 15 soldered on the circuit board 13 may be any type of connector 15 used in the prior art, such as a USB connector and an HDMI connector.
  • a Micro-USB connector can be used in order to achieve miniaturization of the connector 1, reduce the impact of its own load on the drone's flight efficiency, and improve any of the drone's flight speed, flight distance, and steering flexibility Or multiple properties.
  • FIG. 8 is a partially enlarged view of the F position in FIG. 3.
  • the supporting member includes a first supporting member 171 and a second supporting member 173, wherein the first supporting member 171 is located above the circuit board 13 in FIG. 3 (hereinafter referred to as “Upper support”), and the second support 173 is located below the circuit board 13 in FIG. 3 (hereinafter referred to as “lower support”).
  • Upper support the first supporting member 171 is located above the circuit board 13 in FIG. 3
  • second support 173 is located below the circuit board 13 in FIG. 3
  • only the upper support or only the lower support may be provided.
  • the upper support member and the upper case 111 are integrally formed, and the bottom end of the upper support member is used to abut the upper surface of the circuit board 13.
  • the upper support member may be provided separately from the upper case 111 and then fixed to the inner surface of the upper case 111 by a conventional fixing method such as welding, bonding, or screwing.
  • FIG. 3 shows that the top end of the upper support member is fixed to the top surface 1111 of the upper case 111, in other examples, the upper support member may be fixed to the side surface 1113 of the upper case 111. Alternatively, the upper support member is fixed to both the top surface 1111 and the side surface 1113 of the upper case 111 at the same time.
  • a first supporting member 171 is provided on two opposite sides of the connector 15 perpendicular to the axis L of the circuit board 13 so as to provide corresponding supporting forces on opposite sides of the connector 15. .
  • two first support members 171 may be symmetrically disposed on both sides of the axis L of the joint 15.
  • the first support 171 may be provided only on one side of the axis L.
  • FIG. 9 is a schematic structural diagram of a first support member 171 provided in this embodiment.
  • the first support member 171 may be a plate-like structure.
  • the first support member 171 may include a first support plate 1711 and a second support plate 1713.
  • the two supporting plates 1713 are fixedly connected together.
  • the first end of the first support plate 1711 and the rear end of the second support plate 1713 are connected, and the first support plate 1711 is disposed obliquely to the second support plate 1713, that is, the first
  • the support 171 is formed in a shape similar to an L shape or a V shape. Among them, as shown in FIG.
  • the ends of the first support plate 1711 and the second support plate 1713 facing away from the paper surface are fixed on the inner surface of the upper case 111, and the first support plate 1711 and the second support plate 1713 face the paper surface.
  • One end abuts against the upper surface of the circuit board 13.
  • the two first supporting members 171 may be disposed facing each other.
  • the two first supporting members 171 may also be provided.
  • a support member 171 forms a closed or near-closed ring shape around the axis L, so that the circuit board 13 can be supported around the axis L.
  • the first end of the first support plate 1711 and the middle portion of the second support plate 1713 located between the head end and the tail end are connected, that is, the first support member 171 is formed similarly. T-shaped shape.
  • FIG. 10 is another schematic structural diagram of the second support member 173 provided in this embodiment.
  • the first support member 171 includes a first support plate 1711, a second support plate 1713, and a third support plate 1715.
  • the third support plate 1715 is disposed between the opposite first support plate 1711 and the second support plate 1713, and both ends of the third support plate 1715 are fixed to the first support plate 1711 and the second support plate 1713, respectively.
  • a shape similar to an I-shape or a chevron shape is formed. Among them, as shown in FIG.
  • the ends of the first support plate 1711, the second support plate 1713, and the third support plate 1715 facing away from the paper surface are fixed on the inner surface of the upper case 111, and the first support plate 1711 and the second support One end of the board 1713 and the third supporting plate 1715 facing the paper surface abuts the upper surface of the circuit board 13.
  • the first support 171 may also be provided in a columnar structure.
  • the first support member 171 is provided as one or more circular or circular truncated support pillars.
  • the first support member 171 is a plurality of support posts, it may be uniformly disposed around the axis L.
  • the second support member 173 is fixed on the inner surface of the lower case 113 to abut the lower surface of the circuit board 13. It should be noted that, in this embodiment, it is assumed that the second supporting member 173 does not directly abut against the lower surface of the circuit board 13 but directly abuts the abutting surface formed on the portion of the joint 15 located in the housing 11. In this case, it is considered that the second supporting member 173 indirectly abuts on the lower surface of the circuit board 13, and the second supporting member 173 in a broad sense abuts on the lower surface of the circuit board 13.
  • the abutting of the second supporting member 173 on the lower surface of the circuit board 13 includes: directly abutting on the lower surface of the circuit board 13 and indirectly abutting on the lower side of the circuit board 13 through the joint 15. surface.
  • the second support member 173 may include two support bosses disposed on two opposite sides of the axis L, so as to provide a supporting effect on both sides of the axis.
  • the two supporting bosses may be symmetrically disposed on both sides of the axis L to balance the force.
  • the second support 173 may also be a support ring surrounding the axis L, so as to provide corresponding support on all sides of the axis L.
  • the second supporting member 173 may be disposed at an opening opened by the lower case 113 for the joint 15 to protrude from the housing 11 as shown in FIG. 8.
  • the second supporting member 173 may also be disposed at any other suitable position of the lower case 113.
  • two elastic protection pieces 19 can be provided on the outside of the lower case 113, and the two elastic protection pieces 19 are respectively along the thickness direction of the joint 15. It is provided on both sides of the joint 15, that is, the two elastic protection pieces 19 are provided on both sides of the axis L, respectively.
  • One end of the elastic protection sheet 19 is fixed to the lower case 113, and the other end extends in a direction away from the circuit board 13.
  • the two elastic protection pieces 19 are to prevent the joint 15 from shaking left and right, the two elastic protection pieces 19 should be disposed near the joint 15 and the elastic protection pieces 19 need to A sufficient length is extended downward, and this length can be set according to the need to prevent the joint 15 from swinging leftward and rightward, which is not specifically limited herein.
  • a ring-shaped elastic protective sheet 19 may be provided outside the joint 15 so as to surround the joint 15 so that the joint 15 can be prevented from shaking around the axis L.
  • the top end of the annular elastic protection sheet 19 is also fixed to the lower case 113, and the bottom end thereof also extends away from the circuit board 13.
  • a groove 213 may be provided on the mounting portion 21, so that when the connector 1 is mounted on the mounting portion 21, the elastic protection sheet 19 and a part of the joint 15 protruding to the outside of the housing 11 may be received in the groove 213.
  • a circuit board 13 is provided in the housing 11 and a connector 15 for electrical connection is welded on the surface of the circuit board 13 so that the plug-in component 1 is mounted to the main body device 2
  • an electrical connection can be directly achieved with the interface 211 provided by the mounting portion 21, thereby avoiding the need to separately configure cables, which can simplify the assembly process and improve the aesthetics of the movable platform.
  • the connector 15 is soldered on one surface of the circuit board 13, when the connector 1 is inserted into or pulled out from the mounting portion 21 of the drone, the connector 15 is connected to the circuit board 13. Compared with the force applied when soldering the connector 15 to the side surface 1113 of the circuit board 13, the applied force is more likely to cause the circuit board 13 to deform or have a tendency to deform. Such deformation or deformation tends to cause the circuit board The welding between 13 and the joint 15 causes cracks or internal changes occur at the joint between the joint 15 and the circuit board 13, resulting in poor contact between the joint 15 and the circuit board 13.
  • the plug connector 1 of this embodiment is provided with a first support member 171 and a second support member 173 in the housing.
  • the circuit board 13 is deformed upward or has a tendency to deform upward due to the effect of the insertion force, so that it can be supported by the first support member 171, thereby avoiding the problem caused by the circuit board.
  • the deformation or deformation tendency of 13 results in the occurrence of cracks at the welding position of the circuit board 13 and the joint 15 or poor contact caused by internal changes, thereby improving the reliability of the plug-in connector 1.
  • the circuit board 13 When the connector 15 is pulled out from the interface 211 of the mounting portion 21, the circuit board 13 may be deformed downward or has a tendency to deform downward due to the pulling force, so it may be supported by the second support member 173, so that Avoiding the occurrence of cracks at the welding position of the circuit board 13 and the joint 15 or poor contact caused by internal changes caused by the deformation or deformation tendency of the circuit board 13, thereby improving the reliability of the plug-in component 1.
  • first support 171 and the second support 173 must be provided at the same time, even if the first support 171 or the second support 173 are separately provided It is also possible to alleviate to a certain extent the possible damage of the joint between the joint 15 and the circuit board 13 when the plug-in connector 1 is inserted and removed, thereby improving the service life of the plug-in connector 1.

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Abstract

一种插接件(1)，其用于可移动平台，包括：壳体(11)、电路板(13)、接头(15)以及支撑件；所述壳体(11)，用于固定到主体设备(2)的安装部(21)；所述电路板(13)安装在所述壳体(11)内；所述接头焊接于所述电路板(13)的一个表面上，用于与所述安装部(21)内设置的接口(211)电连接，且所述接头(15)伸出到所述壳体(11)的外部；所述支撑件设置在所述壳体(11)内，且所述支撑件的一端与所述壳体(11)固定，所述支撑件的另一端与所述电路板(13)的至少一个表面抵接。本发明实施例提供的插接件(1)，通过在壳体(11)内设置电路板(13)并将用于电连接的接头(15)焊接在电路板(13)的表面上，可以直接与主体设备(2)的安装部(21)设置的接口(211)实现电连接而无需再单独配置线缆，可以简化装配并提高可移动平台的美观度。本发明实施例还提供一种无人机。

Description

无人机及其插接件 技术领域
本发明实施例涉及一种无人机及其插接件，属于无人机及其零配件技术领域。
背景技术
随着经济的发展，消费者对于电子设备的功能要求越来越高，故而现在的电子设备开始往模块化方向发展，从而在装配时可以将具有不同功能给的模块组装在一起以实现对电子设备功能的扩展。以无人机为例，为了在飞行表演中通过灯光和/或音效等来增强其表演效果，往往需要为无人机装配音响和/或LED灯等，这时就需要将相应的音响模块或者LED灯模块装配到无人机的机体上。通常来讲，大部分装配到无人机上的功能模块都需要与无人机的飞控系统通信连接，从而接受飞控系统的控制。但是，现有的线缆连接方式不仅需要将该功能模块机械连接到无人机的机身上，而且还需要进一步的将功能模块的线缆插头与机身配置的插口插接到一起才能完成整个装配过程，不仅流程复杂，而且线缆往往都暴露在机身的外面，极大的影响了无人机的美观性。
发明内容
本发明实施例提供一种无人机及其插接件，以解决上述或者其他潜在问题。
根据本发明的一些实施例，提供一种插接件，其用于可移动平台，包括：壳体、电路板、接头以及支撑件；所述壳体，用于固定到主体设备的安装部；所述电路板安装在所述壳体内；所述接头焊接于所述电路板的一个表面上，用于与所述安装部内设置的接口电连接，且所述接头伸出到所述壳体的外部；所述支撑件设置在所述壳体内，且所述支撑件的一端与所述壳体固定，所述支撑件的另一端与所述电路板的至少一个表面抵接。
如上所述的插接件，其中，所述支撑件包括第一支撑件和第二支撑件，所述第一支撑件与所述电路板的第一表面抵接，所述第二支撑件与所述电路板的第二表面抵接，所述第二表面与所述第一表面相对设置，且所述第二支撑件与所述接头位于所述电路板的同一侧。
如上所述的插接件，其中，所述第一支撑件包括第一支撑板和第二支撑板，所述第一支撑板与所述第二支撑板固定。
如上所述的插接件，其中，所述第一支撑件为两个，两个所述第一支撑件分别设置在所述接头的纵向轴线相对的两侧；所述第一支撑板的首端和第二支撑板的尾端相连，且所述第一支撑板倾斜于所述第二支撑板设置。
如上所述的插接件，其中，所述第一支撑件还包括第三支撑板，所述第一支撑板和第二支撑板相对设置，所述第二支撑板设置于所述第一支撑板和所述第三支撑板之间，并且所述第二支撑板的两端分别与所述第一支撑板和第三支撑板固定。
如上所述的插接件，其中，所述第一支撑件为一个或者多个支撑柱。
如上所述的插接件，其中，所述第二支撑件包括两个支撑凸台，两个所述支撑凸台设置在所述接头相对的两侧。
如上所述的插接件，其中，两个所述支撑凸台对称设置在所述接头相对的两侧。
如上所述的插接件，其中，所述插接件还包括两个弹性保护片，所述弹性保护片设置在所述壳体的外部，且两个所述弹性保护片分别位于所述接头的厚度方向的两侧；所述弹性保护片的一端与壳体固定，所述弹性保护片的另一端往远离所述电路板的方向延伸。
如上所述的插接件，其中，所述插接件还包括一呈环形的弹性保护片，所述弹性保护片设置在所述壳体的外部，且所述弹性保护片围设在所述接头的外侧；所述弹性保护片的一端与壳体固定，所述弹性保护片的另一端往远离所述电路板的方向延伸。
如上所述的插接件，其中，当所述插接件安装于所述安装部上时，所述弹性保护片和所述接头伸出于所述壳体的外部的一部分用于容纳于所述安装部形成的凹槽内。
如上所述的插接件，其中，所述壳体包括：上壳和下壳，所述上壳盖合在下壳上并形成用于容纳所述电路板和所述支撑件的容纳空间；所述接头穿过所述下壳开设的开口伸出到所述壳体的外部。
如上所述的插接件，其中，所述下壳的底面往所述上壳方向凹陷；当所述接头用于与所述接口电连接时，所述上壳的侧面用于与所述安装部配合以至少遮挡所述接头伸出到所述壳体的外部的一部分。
根据本发明的一些实施例，提供一种无人机，所述无人机包括机身以及如上所述的插接件，所述插接件插接在所述机身的安装部上。
如上所述的无人机，其中，所述机身的顶部部分内凹形成所述安装部。
本发明实施例提供的插接件，通过在壳体内设置电路板并将用于电连接的接头焊接在电路板的表面上，从而当将该插接件安装到主体设备的安装部上时，就可以直接与主体设备的安装部设置的接口实现电连接，从而避免再单独配置线缆，以简化装配的流程并使可移动平台的美观度提高。而且，本申请还在壳体内设置支撑件，使得将插接件安装到可移动平台或者从可移动平台拔出时，支撑件可以为电路板提供额外的支撑力，避免电路板产生变形或者发生变形趋势导致接头与电路板的焊接处产生裂缝或者内部变化，从而保证接头和电路板的连接可靠性，进而提高插接件的使用寿命。
本发明实施例的附加方面的优点将在下面的描述中部分给出，部分将从下面的描述中变得明显，或通过本发明实施例的实践了解到。
附图说明
通过参照附图的以下详细描述，本发明实施例的上述和其他目的、特征和优点将变得更容易理解。在附图中，将以示例以及非限制性的方式对本发明实施例的多个实施例进行说明，其中：
图1为本发明实施例实施提供的一种插接件的俯视图；
图2为图1中插接件的仰视图；
图3为图1中A-A向的剖视图；
图4为本发明实施例提供的无人机的局部结构示意图；
图5为图4的俯视图；
图6为图5中B-B向的剖视图；
图7为图6中G位置的放大图；
图8为图3中F位置的放大图
图9为本发明实施例提供的第一支撑件的一种结构示意图；
图10为本发明实施例提供的第一支撑件的另一种结构示意图。
图中：
1-插接件；         11-壳体；         111-上壳；
1111-顶面；        1113-侧面；       1113a-弯折部；
1113b-嵌合孔；       1113c-延伸边；      113-下壳；
1131-抵顶部；        1133-固定部；       115-螺栓；
13-电路板；          15-接头；           171-第一支撑件；
1711-第一支撑板；    1713-第二支撑板；   1715-第三支撑板；
173-第二支撑件；     19-弹性保护片；     2-主体设备；
21-安装部；          211-接口；          213-凹槽。
具体实施方式
下面详细描述本发明的实施例，所述实施例的示例在附图中示出，其中自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。下面通过参考附图描述的实施例是示例性的，旨在用于解释本发明，而不能理解为对本发明的限制。
在本发明实施例的描述中，需要理解的是，术语“厚度”、“上”、“下”、“左”、“右”、“顶”、“底”、“内”、“外”、“顺时针”、“逆时针”等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述本发明实施例和简化描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作，因此不能理解为对本发明实施例的限制。
此外，术语“第一”、“第二”仅用于描述目的，而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此，限定有“第一”、“第二”的特征可以明示或者隐含地包括至少一个该特征。在本发明实施例的描述中，“多个”的含义是至少两个，例如两个，三个等，除非另有明确具体的限定。
在本发明实施例中，除非另有明确的规定和限定，术语“安装”、“相连”、“连接”、“固定”等术语应做广义理解，例如，可以是固定连接，也可以是可拆卸连接，或成一体；可以是直接相连，也可以通过中间媒介间接相连，可以是两个元件内部的连通或两个元件的相互作用关系，除非另有明确的限定。对于本领域的普通技术人员而言，可以根据具体情况理解上述术语在本发明实施例中的具体含义。
在本说明书的描述中，参考术语“一个实施例”、“一些实施例”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明实施例的至少一个实施例或示 例中。在本说明书中，对上述术语的示意性表述不必须针对的是相同的实施例或示例。而且，描述的具体特征、结构、材料或者特点可以在任一个或多个实施例或示例中以合适的方式结合。此外，在不相互矛盾的情况下，本领域的技术人员可以将本说明书中描述的不同实施例或示例以及不同实施例或示例的特征进行结合和组合。
图1为本实施提供的一种插接件的俯视图；图2为图1中插接件的仰视图；图3为图1中A-A向的剖视图。如图1至图3所示，本实施例提供一种用于可移动平台的插接件，通过该插接件可以实现将具有某些功能的装置安装到该可移动平台上的目的，上述装置例如可以是拍摄装置、照明装置、探测装置、警示装置或者其他合适的装置。本实施例的插接件，当其固定到可移动平台的安装部上时，不仅能够与可移动平台的机械固定，而且可以实现与可移动平台的供电和/或通信连接。需要说明的是，上述可移动平台例如可以是无人机、汽车、船舶、遥控模型等各种合适类型的移动工具。
为了描述更加简洁，本实施例还提供了一种无人机，下文将结合图4至图7所示的无人机对本实施例的插接件进行说明。其中，图4示出的是无人机的结构示意，图5为图4的俯视图。需要说明的是，图4和图5中仅示意了与本实施例的插接件1配合的无人机的部分结构示意图，也即示意了无人机的主体设备2的安装部21附近的结构，省略了无人机的动力组件、脚架等常规结构，这些常规结构与普通的无人机基本相同，具体可以参考现有技术中各种类型的无人机的相关结构。无人机的主体设备，在本实施例中，可以是无人机的中心架，例如，可以是中心架的外壳。
图6为图5中B-B向的剖视图，图7为图6中G位置的放大图。如图6和图7所示，主体设备的顶面设置有安装部21，在该安装部21内设置有与下文中的接头15配接的接口211。
参见图1、图3和图7，本实施例的插接件1包括：壳体11、电路板13、接头15以及支撑件。其中，壳体11用于固定到下文将要描述到的无人机的主体设备的安装部21上；电路板13则安装在壳体11内，在电路板13的下表面焊接接头15的上端，该接头15的下端则从壳体11的内部伸出到壳体11的外部以便与安装部21内设置的接口211电连接；支撑件设置在壳体11内，并且它的一端与壳体11固定，它的另一端与电路板13的至少一个表面抵接。可以理解的是，虽然图3中示出的是接头15的上端与电路板13的下表面焊接在一 起，该接头15的下端从壳体11的底部伸出，但其仅仅是针对图3中方位进行的描述，并不代表对具体方位的限制。例如，在另一些示例中，可以将图3中的接头15旋转180度，此时，就是接头15的下端与电路板13的上表面焊接在一起，该结构的上端从壳体11的顶部伸出。当然，根据主体设备上的安装部21的位置不同，也可以将图3中的接头15顺时针旋转90度、或者逆时针旋转90度、或者旋转任意合适的角度后与主体设备的安装部21固定。由上可见，本实施例中，接头15可以焊接于电路板13表面积最大的相对的两个表面(图3中的上表面和下表面)中的任意一个上。
具体的，壳体11可以是由塑料经过模塑的方式制备而成，或者也可以是由金属材料(例如钢材)通过模压或者锻造而成。一般而言，为了方便在壳体11内安装电路板13，可以将壳体11分成两部分来制造。例如，可以分别制造上壳111和下壳113，然后再将二者扣合并固定在一起以装配成一个完整的壳体11。可选地，为了提高壳体11的密闭性，避免水汽、灰尘等进入到壳体11的内部，损坏电路板13的寿命，可以在上壳111和下壳113之间设置密封机构，比如，可以设置密封圈或者迷宫式密封结构。
可选地，如图3和图7所示，上壳111包括顶面1111以及围绕该顶面1111并向下延伸以便与无人机的安装部21固定的侧面1113。具体来说，在侧面1113形成有远离壳体11内部空腔的弯折部1113a，在该弯折部1113a上可以设置用于与安装部21上的螺栓孔配合的螺栓115。而且，从侧面1113的底部还开设有往上延伸的嵌合孔1113b，该嵌合孔1113b用于与安装部21上形成的嵌合凸起相配合，以便将插接件1和安装部21卡合在在一起，从而与螺栓115配合使得插接件1和安装部21更牢固的固定在一起。当然，在其他一些示例中，也可以仅设置螺栓115或者嵌合孔1113b，而且螺栓115和嵌合孔1113b的形式也不仅限于图3中示意出的结构形式，其可以采用任意合适的形式。例如，在某些示例中，可以将螺栓115和壳体11设计成分离的零件，或者也可以不将嵌合孔1113b设置成图3中的上窄下宽的形式而将上下设计成具有大约一致的宽度。
继续参考图3，下壳113可以设计成如图3所示的向壳体11的空腔内凹陷的弧形板，该弧形板可以与安装部21的底面的形状相匹配。通过设计弧形板，可以使得当插接件1安装到无人机的安装部21上，接头15与接口211实现电连接的时候，接头15从壳体11内伸出到壳体外的全部或者部分会被上壳111的侧面挡住，且由于弧形板与安装部21的内表面的形状是匹配的，故而插接到 接口211上的接头15就完全被壳体11的侧面和安装部21的内表面所包裹住。此外，通过设置弧形板，也可以减少电路板13与弧形板上供接头15伸出的开口的距离，从而可以使用更加小巧的接头15，以便使得整个插接件1更加小巧。在弧形板上可以形成往上延伸的抵顶部1131以及固定部1133，该抵顶部1131可以抵顶在上壳111的侧面1113所形成的台阶面上，固定部1133则用于固定电路板13。具体来说，在上壳111的侧面1113的弯折部1113a往下延伸形成有延伸边1113c，该延伸边1113c的内表面被部分去除，从而形成了用于与下壳113的支撑部抵顶的台阶面。在固定部1133的顶端开设有螺栓孔，电路板13放置在固定部1133的顶端上，然后通过螺栓固定在该固定部1133上。
电路板13可以选用能够实现相应功能的任意合适电路板13，例如，当需要通过插接件1在无人机上连接照明装置时，则可以使用用于控制LED灯的电路板13，又如，当需要通过插接件1在无人机上连接图像传感装置时，则可以使用用于实现图像处理和/或图像传输的电路板13。
焊接在电路板13上的接头15可以是现有技术中使用的任意类型的接头15，例如USB接头和HDMI接头等。可选地，可以使用Micro-USB接头，以便实现插接件1的小型化，减少自身负重对无人机飞行效能的影响，提高无人机飞行速度、飞行距离、转向灵活性中任意一种或者多种的性能。
图8为图3中F位置的局部放大图。请一并参考图3和图8，在本实施例中，支撑件包括第一支撑件171和第二支撑件173，其中，第一支撑件171位于图3中电路板13的上方(以下称“上支撑件”)，第二支撑件173位于图3中电路板13的下方(以下称“下支撑件”)。当然，在某些示例中，也可以仅设置有上支撑件或者仅设置有下支撑件。
具体来说，如图3所示，在一些示例中，上支撑件和上壳111一体成型，该上支撑件的底端用于抵顶电路板13的上表面。在另一些示例中，上支撑件也可以与上壳111分体设置，然后通过焊接、粘接或者螺接等现有固定方式固定在上壳111的内表面上。需要说明的是，虽然图3中示出的是上支撑件的顶端与上壳111的顶面1111固定，但在其他一些示例中，也可以是上支撑件与上壳111的侧面1113固定，或者上支撑件同时与上壳111的顶面1111和侧面1113均固定。
请继续参考图3，在一些示例中，在接头15垂直于电路板13的轴线L的相对的两侧分别设置有一个第一支撑件171，以便在接头15相对两侧均提供相应 的支撑力。为了使接头15的轴线L两侧的支撑力更加均衡，可以将两个第一支撑件171对称设置在接头15的轴线L的两侧。当然，在另一些示例中，也可以仅在轴线L的一侧设置第一支撑件171。
图9为本实施例提供的第一支撑件171的一种结构示意图。如图9所示，可选地，第一支撑件171可以是板状结构，例如，该第一支撑件171可以包括第一支撑板1711和第二支撑板1713，第一支撑板1711和第二支撑板1713固定连接在一起。例如，在一些可选的示例中，第一支撑板1711的首端和第二支撑板1713的尾端相连，且该第一支撑板1711倾斜于第二支撑板1713设置，也即，第一支撑件171形成为类似L形或者V形的形状。其中，如图9所示，第一支撑板1711与第二支撑板1713背离纸面的一端固定在上壳111的内表面上，而第一支撑板1711与第二支撑板1713朝向纸面的一端抵顶电路板13的上表面。当在轴线L相对的两侧分别设置一个第一支撑件171，且该第一支撑件171为L形的形状时，两个第一支撑件171可以相向设置，当然，也可以使得两个第一支撑件171围绕轴线L形成闭合或者接近闭合的环形，从而在轴线L的四周均可以提供对电路板13的支撑。又如，在另一些可选的示例中，第一支撑板1711的首端与第二支撑板1713位于首端和尾端之间的中间部分连接，也即，第一支撑件171形成为类似T形的形状。
图10为本实施例提供的第二支撑件173的另一种结构示意图。如图10所示，在另一些示例中，第一支撑件171包括第一支撑板1711、第二支撑板1713和第三支撑板1715。其中，第三支撑板1715设置在相对的第一支撑板1711和第二支撑板1713之间，并且该第三支撑板1715的两端分别与第一支撑板1711和第二支撑板1713固定，从而形成类似于工字形或者凵字形的形状。其中，如图10所示，第一支撑板1711、第二支撑板1713和第三支撑板1715背离纸面的一端固定在上壳111的内表面上，而第一支撑板1711、第二支撑板1713和第三支撑板1715朝向纸面的一端抵顶电路板13的上表面。
在其他一些示例中，第一支撑件171还可以设置成柱状结构。例如，将第一支撑件171设置成一个或者多个圆形或者圆台状的支撑柱。当第一支撑件171为多个支撑柱时，其可以围绕轴线L均匀设置。
如图3和8所示，第二支撑件173固定在下壳113的内表面上，用于抵顶电路板13的下表面。需要注意的是，在本实施例中，假设第二支撑件173未直接抵顶在电路板13的下表面而是直接抵顶在接头15位于壳体11内的部分上所 形成的抵接面上，这种情况被认为是第二支撑件173间接抵顶在电路板13的下表面上，属于广义上的第二支撑件173抵顶在电路板13的下表面。也即是说，在本实施例中，第二支撑件173抵接电路板13的下表面包括：直接抵接在电路板13的下表面，以及通过接头15间接抵接在电路板13的下表面。
具体而言，请参照图8，在一些示例中，第二支撑件173可以包括两个设置在轴线L相对的两侧的支撑凸台，以便在轴线的两侧均能提供支撑作用。可选地，这两个支撑凸台可以对称设置在轴线L的两侧，以便平衡受力。在另一些示例中，第二支撑件173也可以是环绕轴线L的支撑环，以便在轴线L的四周均提供相应的支撑作用。
应当理解，在设置第二支撑件173时，可以是如图8所示的将该第二支撑件173设置在下壳113所开设的用于供接头15伸出壳体11的开口处。当然，也可以将第二支撑件173设置在下壳113其他任意合适的位置。
进一步，为了避免在插拔时接头15受到侧向的作用力，也即，为了避免图3中示出的插接件1的接头15在插拔的过程中向左或者向右晃动从而导致接头15与电路板13的焊接处产生裂缝或者内部发生变化，可以如图3所示的在下壳113的外部设置两个弹性保护片19，这两个弹性保护片19沿着接头15的厚度方向分别设置在接头15的两侧，也即，这两个弹性保护片19分别设置轴线L的两侧。其中，弹性保护片19的一端与下壳113固定，另一端则往远离电路板13的方向延伸。可以理解的是，由于上述两个弹性保护片19是为了阻止接头15向左和向右的晃动，故这两个弹性保护片19应该设置在靠近接头15的位置，且弹性保护片19需要往下延伸足够的长度，该长度可以根据需要防止接头15向左和向右晃动的幅度来设置，在此不做具体限定。
当然，在另一些示例中，也可以在接头15外设置环形的弹性保护片19，以便将该接头15包围住，从而在轴线L的四周均可以起到防止接头15晃动的作用。同理的，该环形的弹性保护片19的顶端也与下壳113固定，其底端也往远离电路板13的方向延伸。
此外，请参考图7，为了与插接件1上设置的弹性保护片19配合，可以在安装部21上设置凹槽213，从而当插接件1安装到安装部21上时，弹性保护片19和接头15伸出到壳体11外部的一部分可以容纳在该凹槽213内。
本实施例的插接件1，通过在壳体11内设置电路板13并将用于电连接的接头15焊接在电路板13的表面上，从而当将该插接件1安装到主体设备2的安 装部21上时，就可以直接与安装部21设置的接口211实现电连接，从而避免再单独配置线缆，可以简化装配的流程并使可移动平台的美观度提高。
进一步，由于接头15焊接在电路板13的其中一个表面上，故当该插接件1插接到无人机的安装部21或者从该安装部21拔出时，接头15对电路板13的作用力相比于将接头15焊接在电路板13的侧面1113时所受到的作用力相比，更容易使得电路板13产生变形或者具有变形的趋势，这种变形或者变形趋势往往会导致电路板13与接头15的焊接产生裂缝或者在接头15和电路板13的焊接处产生内部变化，导致接头15和电路板13的接触不良。
有鉴于此，本实施例的插接件1又在壳体内设置了第一支撑件171和第二支撑件173。当接头15插接到安装部21的接口211时，电路板13由于受到插接力的作用而往上变形或者具有往上变形的趋势时可以被第一支撑件171支撑住，从而避免由于电路板13的变形或者变形趋势所导致的电路板13与接头15焊接位置处产生裂纹或者内部变化所出现的接触不良的现象，进而提高插接件1的可靠性。当接头15从安装部21的接口211拔出时，电路板13由于受到拔出力的作用而往下变形或者具有往下变形的趋势时可以被该第二支撑件173支撑住，从而也可以避免由于电路板13的变形或者变形趋势所导致的电路板13与接头15焊接位置处产生裂纹或者内部变化所出现的接触不良的现象，进而提高插接件1的可靠性。当然，基于受力的计算和结构上的差异，在本实施例中并不要求必须同时设置第一支撑件171和第二支撑件173，即使单独设置第一支撑件171或者第二支撑件173也可以在某种程度上缓解插拔插接件1时接头15与电路板13焊接处可能的损坏，从而提高插接件1的使用寿命。
再进一步，本实施例的插接件1即使盲插到无人机的安装部21时，也不用过于担心会损坏接头15与电路板13的焊接，尤其是当上壳111的侧面1113部分或者全部遮挡接头15伸出到壳体11外面的部分时，更无需过于担心插拔力不合适对于接头15与电路板13焊接处的损坏。
最后应说明的是：以上实施方式仅用以说明本发明实施例的技术方案，而非对其进行限制；尽管参照前述实施方式对本发明实施例已经进行了详细的说明，但本领域的普通技术人员应当理解：其依然可以对前述实施方式所记载的技术方案进行修改，或者对其中部分或者全部技术特征进行等同替换；而这些修改或者替换，并不使相应技术方案的本质脱离本发明实施例实施方式技术方案的范围。

Claims (27)

  1. 一种插接件，用于可移动平台，其特征在于，包括：壳体、电路板、接头以及支撑件；
    所述壳体，用于固定到主体设备的安装部；
    所述电路板安装在所述壳体内；
    所述接头焊接于所述电路板的一个表面上，用于与所述安装部内设置的接口电连接，且所述接头伸出到所述壳体的外部；
    所述支撑件设置在所述壳体内，且所述支撑件的一端与所述壳体固定，所述支撑件的另一端与所述电路板的至少一个表面抵接。
  2. 根据权利要求1所述的插接件，其特征在于，所述支撑件包括第一支撑件和第二支撑件，所述第一支撑件与所述电路板的第一表面抵接，所述第二支撑件与所述电路板的第二表面抵接，所述第二表面与所述第一表面相对设置，且所述第二支撑件与所述接头位于所述电路板的同一侧。
  3. 根据权利要求2所述的插接件，其特征在于，所述第一支撑件包括第一支撑板和第二支撑板，所述第一支撑板与所述第二支撑板固定。
  4. 根据权利要求3所述的插接件，其特征在于，所述第一支撑件为两个，两个所述第一支撑件分别设置在所述接头的纵向轴线相对的两侧；所述第一支撑板的首端和第二支撑板的尾端相连，且所述第一支撑板倾斜于所述第二支撑板设置。
  5. 根据权利要求3所述的插接件，其特征在于，所述第一支撑件还包括第三支撑板，所述第一支撑板和第二支撑板相对设置，所述第二支撑板设置于所述第一支撑板和所述第三支撑板之间，并且所述第二支撑板的两端分别与所述第一支撑板和第三支撑板固定。
  6. 根据权利要求2所述的插接件，其特征在于，所述第一支撑件为一个或者多个支撑柱。
  7. 根据权利要求2所述的插接件，其特征在于，所述第二支撑件包括两个支撑凸台，两个所述支撑凸台设置在所述接头相对的两侧。
  8. 根据权利要求7所述的插接件，其特征在于，两个所述支撑凸台对称设置在所述接头相对的两侧。
  9. 根据权利要求1所述的插接件，其特征在于，所述插接件还包括两个弹 性保护片，所述弹性保护片设置在所述壳体的外部，且两个所述弹性保护片分别位于所述接头的厚度方向的两侧；所述弹性保护片的一端与壳体固定，所述弹性保护片的另一端往远离所述电路板的方向延伸。
  10. 根据权利要求1所述的插接件，其特征在于，所述插接件还包括一呈环形的弹性保护片，所述弹性保护片设置在所述壳体的外部，且所述弹性保护片围设在所述接头的外侧；所述弹性保护片的一端与壳体固定，所述弹性保护片的另一端往远离所述电路板的方向延伸。
  11. 根据权利要求9或10所述的插接件，其特征在于，当所述插接件安装于所述安装部上时，所述弹性保护片和所述接头伸出于所述壳体的外部的一部分用于容纳于所述安装部形成的凹槽内。
  12. 根据权利要求1至10任一项所述的插接件，其特征在于，所述壳体包括：上壳和下壳，所述上壳盖合在下壳上并形成用于容纳所述电路板和所述支撑件的容纳空间；所述接头穿过所述下壳开设的开口伸出到所述壳体的外部。
  13. 根据权利要求12所述的插接件，其特征在于，所述下壳的底面往所述上壳方向凹陷；当所述接头用于与所述接口电连接时，所述上壳的侧面用于与所述安装部配合以至少遮挡所述接头伸出到所述壳体的外部的一部分。
  14. 一种无人机，其特征在于，所述无人机包括机身以及插接件；
    所述插接件，用于可移动平台，其特征在于，包括：壳体、电路板、接头以及支撑件；
    所述壳体，用于固定到主体设备的安装部；
    所述电路板安装在所述壳体内；
    所述接头焊接于所述电路板的一个表面上，用于与所述安装部内设置的接口电连接，且所述接头伸出到所述壳体的外部；
    所述支撑件设置在所述壳体内，且所述支撑件的一端与所述壳体固定，所述支撑件的另一端与所述电路板的至少一个表面抵接；
    所述插接件插接在所述机身的安装部上。
  15. 根据权利要求14所述的无人机，其特征在于，所述支撑件包括第一支撑件和第二支撑件，所述第一支撑件与所述电路板的第一表面抵接，所述第二支撑件与所述电路板的第二表面抵接，所述第二表面与所述第一表面相对设置，且所述第二支撑件与所述接头位于所述电路板的同一侧。
  16. 根据权利要求15所述的无人机，其特征在于，所述第一支撑件包括第 一支撑板和第二支撑板，所述第一支撑板与所述第二支撑板固定。
  17. 根据权利要求16所述的无人机，其特征在于，所述第一支撑件为两个，两个所述第一支撑件分别设置在所述接头的纵向轴线相对的两侧；所述第一支撑板的首端和第二支撑板的尾端相连，且所述第一支撑板倾斜于所述第二支撑板设置。
  18. 根据权利要求16所述的无人机，其特征在于，所述第一支撑件还包括第三支撑板，所述第一支撑板和第二支撑板相对设置，所述第二支撑板设置于所述第一支撑板和所述第三支撑板之间，并且所述第二支撑板的两端分别与所述第一支撑板和第三支撑板固定。
  19. 根据权利要求15所述的无人机，其特征在于，所述第一支撑件为一个或者多个支撑柱。
  20. 根据权利要求15所述的无人机，其特征在于，所述第二支撑件包括两个支撑凸台，两个所述支撑凸台设置在所述接头相对的两侧。
  21. 根据权利要求20所述的无人机，其特征在于，两个所述支撑凸台对称设置在所述接头相对的两侧。
  22. 根据权利要求14所述的无人机，其特征在于，所述插接件还包括两个弹性保护片，所述弹性保护片设置在所述壳体的外部，且两个所述弹性保护片分别位于所述接头的厚度方向的两侧；所述弹性保护片的一端与壳体固定，所述弹性保护片的另一端往远离所述电路板的方向延伸。
  23. 根据权利要求14所述的无人机，其特征在于，所述插接件还包括一呈环形的弹性保护片，所述弹性保护片设置在所述壳体的外部，且所述弹性保护片围设在所述接头的外侧；所述弹性保护片的一端与壳体固定，所述弹性保护片的另一端往远离所述电路板的方向延伸。
  24. 根据权利要求22或23所述的无人机，其特征在于，当所述插接件安装于所述安装部上时，所述弹性保护片和所述接头伸出于所述壳体的外部的一部分用于容纳于所述安装部形成的凹槽内。
  25. 根据权利要求14至23任一项所述的无人机，其特征在于，所述壳体包括：上壳和下壳，所述上壳盖合在下壳上并形成用于容纳所述电路板和所述支撑件的容纳空间；所述接头穿过所述下壳开设的开口伸出到所述壳体的外部。
  26. 根据权利要求25所述的无人机，其特征在于，所述下壳的底面往所述上壳方向凹陷；当所述接头用于与所述接口电连接时，所述上壳的侧面用于与 所述安装部配合以至少遮挡所述接头伸出到所述壳体的外部的一部分。
  27. 根据权利要求14至26任一项所述的无人机，其特征在于，所述机身的顶部部分内凹形成所述安装部。
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