WO2023241432A1 - 一种无人机 - Google Patents

一种无人机 Download PDF

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Publication number
WO2023241432A1
WO2023241432A1 PCT/CN2023/098871 CN2023098871W WO2023241432A1 WO 2023241432 A1 WO2023241432 A1 WO 2023241432A1 CN 2023098871 W CN2023098871 W CN 2023098871W WO 2023241432 A1 WO2023241432 A1 WO 2023241432A1
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WO
WIPO (PCT)
Prior art keywords
lens
axis
arms
fuselage
drone
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Application number
PCT/CN2023/098871
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English (en)
French (fr)
Inventor
张桂林
高飞
Original Assignee
影石创新科技股份有限公司
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
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Application filed by 影石创新科技股份有限公司 filed Critical 影石创新科技股份有限公司
Publication of WO2023241432A1 publication Critical patent/WO2023241432A1/zh

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Classifications

    • 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
    • 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

Definitions

  • the utility model belongs to the technical field of panoramic lenses for unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle.
  • the top fisheye lens 1a and the bottom fisheye lens 2a are usually coaxially arranged and fixed in the vertical direction 100.
  • the angle of view of the two lenses is easily blocked by the blades, landing gear 3a or the aircraft body, and the blocking range is wide, affecting the shooting.
  • the lens is generally raised and moved away from the body.
  • this method often sacrifices appearance.
  • the elevated lens increases the air resistance of the drone during flight, and it is easy for the protruding lens to be bumped or the lens to be scratched.
  • This utility model is to overcome the above-mentioned shortcomings of the prior art and provide a drone that effectively reduces the blocked range of the first lens and the second lens, and also reduces the range of the lens protruding from the body, which is better Protect the lens from scratches and wear.
  • the technical solution of the present utility model is: a drone, including:
  • the drone body includes a fuselage, a first set of arms located on one side of the fuselage length direction, and a second set of arms on the other side.
  • the first set of arms is relative to the
  • the second set of arms is located close to the top of the fuselage;
  • the lens assembly includes a first lens and a second lens, the first lens is protruding from the top of the fuselage so that the first set of arms is located outside the viewing angle of the first lens ;
  • the second lens is protruding from the bottom end of the fuselage, so that the second set of arms is located outside the viewing angle of the second lens.
  • the drone body has a longitudinal axis along the height direction of the fuselage, and the axis of the first lens or/and the axis of the second lens is relatively tilted from the longitudinal axis. , so that the drone body is located outside the viewing angle of the first lens and the second lens.
  • the axis of the first lens and the axis of the second lens are coaxially arranged, and the axis of the first lens is directed by the first group of arms relative to the longitudinal axis.
  • the direction of the second set of machine arms is tilted.
  • the angle between the axis of the first lens or the axis of the second lens and the longitudinal axis is 2-10 degrees.
  • the axis of the first lens and the axis of the second lens are arranged asynchronously, and the axis of the first lens is directed by the first group of arms relative to the longitudinal axis.
  • the direction of the second set of machine arms is tilted.
  • the axis of the second lens is arranged along the longitudinal axis direction.
  • the axis of the first lens and the axis of the second lens are arranged asynchronously, and the axis of the second lens is directed by the first group of arms relative to the longitudinal axis.
  • the direction of the second set of machine arms is tilted.
  • the axis of the first lens is arranged along the longitudinal axis direction.
  • the drone body has a longitudinal axis along the height direction of the fuselage, the axis of the first lens and the axis of the second lens are both parallel to the longitudinal axis, and the The first lens and the second lens are spaced apart along the plane direction of the drone body, so that the drone body is located outside the viewing angles of the first lens and the second lens.
  • the viewing angle boundary of the first lens is tangent to the drone body; or/and, the viewing angle boundary of the second lens is tangent to the drone body.
  • the first set of arms is closer to the top of the fuselage relative to the second set of arms; by arranging a first lens and a second lens, the third set of arms is A lens is provided on the top of the UAV body, and the second lens is provided on the bottom of the UAV body, so that the UAV body is located between the first lens and the second lens. Outside the viewing angle; the first lens protrudes from the upper end of the fuselage, the first lens is closer to the first set of arms than the second lens, and the second lens protrudes from the fuselage.
  • the lower end of the body, and the second lens is close to the second set of arms; the first set of arms and the second set of arms are not flush, and the first lens and the second lens are changed relative to the first set of arms.
  • the specific positions of the arms and the second set of arms are such that the drone body is located outside the viewing angles of the first lens and the second lens, so that the viewing angles of the first lens and the second lens are not blocked. Blocking, or can minimize the blocked range, and also reduce the range of the lens (the first lens and the second lens) protruding from the body (the drone body), better protecting the lens so that it is not easy to Bump and wear.
  • Figure 1 is a schematic structural diagram of a drone in the background technology
  • Figure 2 is a schematic structural diagram of a drone provided by an embodiment of the present utility model
  • Figure 3 is a schematic structural diagram of a drone provided by another embodiment of the present invention.
  • setting and connection should be understood in a broad sense. For example, they can be directly set and connected, or they can be set and connected indirectly through centered components and centered structures.
  • a drone provided by an embodiment of the present invention includes a drone body and a lens assembly.
  • the drone body includes a fuselage 6 and a third lens located on one side of the fuselage 6.
  • the first set of arms 4 is closer to the upper end of the fuselage 6 relative to the second set of arms 5, so The first lens 1 protrudes from the upper end of the body 6, and the first lens 1 is closer to the first set of arms 4 relative to the second lens 2; the second lens 2 protrudes from the upper end of the body 6.
  • the lower end of the fuselage 6 is close to the second group of arms 5 .
  • the lens assembly includes a first lens Head 1 and second lens 2, the first lens 1 is arranged on the top of the drone body, and the second lens 2 is arranged on the bottom of the drone body, so that the drone body Located outside the viewing angles of the two panoramic lenses; through the reasonable layout of the first set of arms 4 and the second set of arms 5, on the premise of ensuring smooth and reliable flight, the viewing angles of the first lens 1 and the second lens 2 are Not blocked, or the scope of blocked areas is minimized.
  • the UAV body has a longitudinal axis 200 along the height direction of the fuselage 6. It can be understood that when the UAV body flies horizontally relative to the horizontal plane or is placed horizontally, the longitudinal axis 200 will be perpendicular to level.
  • the axis of the first lens 1 or the axis of the second lens 2 is relatively tilted to the longitudinal axis 200 so that the drone body is located between the first lens 1 and the second lens 2 outside the viewing angle; or, the axis of the first lens 1 and the axis of the second lens 2 are both tilted relative to the longitudinal axis 200, so that the drone body is located between the first lens 1 and the second lens 2. outside the viewing angle of the second lens 2.
  • the utility model provides a drone that changes the relative position and arrangement of the first lens 1 and the second lens 2 so that the drone body is positioned between the first lens 1 and the second lens 2.
  • it can effectively reduce the blocked range of the viewing angles of first lens 1 and second lens 2, and also make the lenses (first lens 1 and the second lens 2) protrude from the body (drone body) ) range is reduced to better protect the lens and make it less likely to be bumped and worn.
  • the first lens 1 and the second lens 2 are coaxially arranged, and the axis of the first lens 1 and the axis of the second lens 2 They are all inclined relative to the longitudinal axis 200 .
  • the axis of the first lens 1 is inclined relative to the longitudinal axis 200 from the first set of arms 4 to the direction of the second set of arms 5 .
  • the angle between the axis of the first lens 1 or the axis of the second lens 2 and the longitudinal axis 200 is 2-10 degrees.
  • the drone may include a connecting component, one end of which is connected to the first lens 1 , and the other end of which is connected to the second lens 2 .
  • the connecting component may include a connecting shaft and a positioning piece.
  • Both ends of the connecting shaft are connected to the first lens 1 and the second lens 2 respectively; the positioning piece is provided on the drone body, And used to fix the connecting shaft.
  • the positioning member is a threaded structural member, and the threaded structural member is used to offset the connecting shaft; the drone body has a through hole, and the threaded structure components can pass through the vias.
  • the connecting component is used to make the first lens 1 and the second lens 2 coaxial, and the limiting effect of the positioning member is used to make the connecting axis relative to the longitudinal axis 200
  • the inclination angle ⁇ is fixed.
  • the threaded structural members are bolts. The bolts pass through the through holes and are against the connecting shaft.
  • the inclination angle ⁇ is adjustable (3.2° in this embodiment), effectively reducing the The angle of view of the first lens 1 and the second lens 2 is blocked, and the adjustment is easy.
  • the axis of the first lens 1 and the axis of the second lens 2 are arranged asynchronously, and the axis of the first lens 1 is formed by the first lens 1 relative to the longitudinal axis 200 .
  • the assembly arm 4 is tilted toward the second assembly arm 5 .
  • the axis of the second lens 2 is arranged along the direction of the longitudinal axis 200 .
  • the tilt direction is the direction in which the first group of arms 4 is tilted toward the second group of arms 5; the axis of the first lens 1 and the longitudinal axis 200 are relatively tilted, and the second lens 2 is tilted relative to the longitudinal axis 200.
  • the axis is arranged along the direction of the longitudinal axis 200; in another embodiment, the axis of the first lens 1 and the longitudinal axis 200 are relatively tilted, and the axis of the second lens 2 is tilted relative to the longitudinal axis 200. 200 relative tilt; in specific applications, it can be adjusted according to actual needs so that the viewing angles of the first lens 1 and the second lens 2 are not blocked or the blocked range is minimized.
  • the axis of the first lens 1 and the axis of the second lens 2 are arranged asynchronously, and the axis of the second lens 2 is formed by the first lens 2 relative to the longitudinal axis 200 .
  • the assembly arm 4 is tilted toward the second assembly arm 5 .
  • the axis of the first lens 1 is arranged along the direction of the longitudinal axis 200 . In specific applications, adjustments can be made according to actual needs so that the angles of view of the first lens 1 and the second lens 2 are not blocked or the blocked range is minimized.
  • the UAV body has a longitudinal axis 200 along the height direction of the fuselage 6. It can be understood that when the UAV body flies horizontally relative to the horizontal plane or is placed horizontally, the longitudinal axis 200 will be perpendicular to level.
  • the axis of the first lens 1 and the axis of the second lens 2 are both parallel to the longitudinal axis 200, and the first lens 1 and the second lens 2 are along the plane direction of the drone body. (ie, the plane direction perpendicular to the longitudinal axis 200) is spaced apart so that the drone body is located outside the viewing angle of the first lens 1 and the second lens 2. As shown in FIG.
  • the first lens 1 and the second lens 2 are spaced apart in a direction perpendicular to the longitudinal axis 200 .
  • the direction perpendicular to the longitudinal axis 200 is the length direction along the fuselage when the drone body flies horizontally relative to the horizontal plane or is placed horizontally.
  • the axis of the first lens 1 and the axis of the second lens 2 are both parallel to the longitudinal axis 200 .
  • the distance between the first lens 1 and the second lens 2 can be flexibly set to ensure that the angles of view of the first lens 1 and the second lens 2 are not blocked or the blocked range is minimized. .
  • the drone body includes a retractable landing gear 3.
  • the landing gear 3 When retracted, the landing gear 3 is located outside the viewing angles of the first lens 1 and the second lens 2. Specifically, the retracted landing gear 3 does not affect the shooting angle.
  • the drone body includes paddles, and the paddles are also located between the first lens 1 and the second lens 2 In addition to the viewing angle, it meets the needs of more shooting scenes.
  • the viewing angle boundary of the first lens 1 is tangent to the drone body; or, the viewing angle boundary of the second lens 2 is tangent to the drone body.
  • the boundary of the viewing angle of the first lens 1 refers to the boundary of the maximum viewing angle of the first lens 1
  • the boundary of the viewing angle of the second lens 2 refers to the boundary of the maximum viewing angle of the second lens 2; in this embodiment, by changing the first lens 1
  • the relative position and arrangement of the first lens 1 and the second lens 2 are such that the maximum viewing angle boundary of the first lens 1 is tangent to the drone body, and the maximum viewing angle boundary of the second lens 2 is tangent to the UAV body.
  • the drone body is tangential to obtain the maximum viewing angle without being blocked by the drone body.
  • the first set of arms 4 is closer to the top of the fuselage relative to the second set of arms 5; by arranging the first lens 1 and the second Lens 2.
  • the first lens 1 is set on the top of the drone body, and the second lens 2 is set on the bottom of the drone body, so that the drone body is positioned between the two panoramic lenses.
  • the first lens 1 protrudes from the upper end of the fuselage, and the first lens 1 is closer to the second lens 2
  • the first set of arms 4, the second lens 2 protrudes from the lower end of the fuselage, and the second lens 2 is close to the second set of arms 5; through the first set of arms 4 and The second set of arms 5 is not arranged flush, and the specific positions of the first lens 1 and the second lens 2 relative to the first set of arms 4 and the second set of arms 5 are changed so that the drone body is located where outside the viewing angles of the first lens 1 and the second lens 2, so that the viewing angles of the first lens 1 and the second lens 2 are not is blocked, or can minimize the blocked range, and also reduce the range of the lens (the first lens 1 and the second lens 2) protruding from the body (the drone body), better protecting the lens Make it less likely to be bumped and worn.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)
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Abstract

一种无人机，包括无人机本体和镜头组件，无人机本体包括机身（6）、位于机身（6）长度方向一侧的第一组机臂（4）和另一侧的第二组机臂（5），第一组机臂（4）相对于第二组机臂（5）靠近于机身（6）的顶端；镜头组件包括第一镜头（1）和第二镜头（2），所述第一镜头（1）凸出于所述机身（6）顶端设置，以使所述第一组机臂（4）位于所述第一镜头（1）的视角之外；所述第二镜头（2）凸出于所述机身（6）底端设置，以使所述第二组机臂（5）位于所述第二镜头（2）的视角之外。上述无人机有效减少第一镜头和第二镜头的视角被遮挡的范围，也使得镜头凸出机体的范围缩小，较好地保护镜头使其不易磕碰磨损。

Description

一种无人机 技术领域
本实用新型属于无人机的全景镜头技术领域，尤其涉及一种无人机。
背景技术
一般单鱼眼镜头的无人机，拍摄的视角比较局限，为了实现全景成像，采用了多个鱼眼镜头。但是由于无人机机身结构的特殊性(机身一般设置有四个机臂、多个桨叶)，使得机身容易遮挡镜头，影响全景成像的质量。
现有技术中，如图1所示，搭载鱼眼镜头的无人机，通常是将顶部鱼眼镜头1a和底部鱼眼镜头2a同轴设置且固定于竖直方向100。如此设置，两个镜头的视角很容易受桨叶、起落架3a或机体遮挡，遮挡范围较广，影响拍摄。为了避免以上遮挡，一般通过将镜头抬高并使其远离机体。但这种方式往往牺牲外观，抬高的镜头加大了无人机在飞行中的空气阻力，且容易发生凸出的镜头被磕碰或镜片被磨花的情况。
实用新型内容
本实用新型的目的在于克服上述现有技术的不足，提供了一种无人机，有效减少第一镜头和第二镜头的视角被遮挡的范围，也使得镜头凸出机体的范围缩小，较好地保护镜头使其不易磕碰磨损。
本实用新型的技术方案是：一种无人机，包括：
无人机本体，所述无人机本体包括机身、位于机身长度方向一侧的第一组机臂和另一侧的第二组机臂，所述第一组机臂相对于所述第二组机臂靠近于所述机身的顶端；
镜头组件，所述镜头组件包括第一镜头和第二镜头，所述第一镜头凸出于所述机身顶端设置，以使所述第一组机臂位于所述第一镜头的视角之外；所述第二镜头凸出于所述机身底端设置，以使所述第二组机臂位于所述第二镜头的视角之外。
作为本技术方案的进一步改进，所述无人机本体具有沿机身高度方向的纵向轴，所述第一镜头的轴线或/和所述第二镜头的轴线与所述纵向轴之间相对倾斜，以使所述无人机本体位于所述第一镜头和所述第二镜头的视角之外。
作为本技术方案的进一步改进，所述第一镜头的轴线和所述第二镜头的轴线同轴设置，且所述第一镜头的轴线相对所述纵向轴由所述第一组机臂向所述第二组机臂方向倾斜设置。
作为本技术方案的进一步改进，所述第一镜头的轴线或所述第二镜头的轴线与所述纵向轴之间的夹角为2-10度。
作为本技术方案的进一步改进，所述第一镜头的轴线和所述第二镜头的轴线不同轴设置，所述第一镜头的轴线相对所述纵向轴由所述第一组机臂向所述第二组机臂方向倾斜设置。
作为本技术方案的进一步改进，且所述第二镜头的轴线沿所述纵向轴方向设置。
作为本技术方案的进一步改进，所述第一镜头的轴线和所述第二镜头的轴线不同轴设置，所述第二镜头的轴线相对所述纵向轴由所述第一组机臂向所述第二组机臂方向倾斜设置。
作为本技术方案的进一步改进，所述第一镜头的轴线沿所述纵向轴方向设置。
作为本技术方案的进一步改进，所述无人机本体具有沿机身高度方向的纵向轴，所述第一镜头的轴线、所述第二镜头的轴线均与所述纵向轴平行，且所述第一镜头与所述第二镜头沿所述无人机本体的平面方向间隔设置，以使所述无人机本体位于所述第一镜头和所述第二镜头的视角之外。
作为本技术方案的进一步改进，所述第一镜头的视角边界与所述无人机本体相切；或/和，所述第二镜头的视角边界与所述无人机本体相切。
本实用新型所提供的一种无人机，所述第一组机臂相对于所述第二组机臂靠近于所述机身的顶端；通过设置第一镜头和第二镜头，所述第一镜头设置于所述无人机本体的顶部，所述第二镜头设置于所述无人机本体的底部，以使所述无人机本体位于所述第一镜头和所述第二镜头的视角之外；所述第一镜头凸出于所述机身上端，所述第一镜头相对所述第二镜头靠近于所述第一组机臂，所述第二镜头凸出于所述机身下端，且所述第二镜头靠近于所述第二组机臂；通过第一组机臂和第二组机臂不平齐设置，以及改变第一镜头和第二镜头相对于第一组机臂和第二组机臂的具体位置，以使所述无人机本体位于所述第一镜头和所述第二镜头的视角之外，从而可以使第一镜头和第二镜头的视角不被遮挡，或可以使得被遮挡的范围得到最大限度地减少，也使得镜头(第一镜头与所述第二镜头)凸出机体(无人机本体)的范围缩小，较好地保护镜头使其不易磕碰磨损。
附图说明
为了更清楚地说明本实用新型实施例中的技术方案，下面将对实施例中所需要使用的附图作简单地介绍，显而易见地，下面描述中的附图仅仅是本实用新型的一些实施例，对于本领域普通技术人员来讲，在不付出创造性劳动的前提下，还可以根据这些附图获得其他的附图。
图1是背景技术中的无人机的结构示意图；
图2是本实用新型实施例提供的一种无人机的结构示意图；
图3是本实用新型另一个实施例提供的一种无人机的结构示意图。
图中标号：
1a-顶部鱼眼镜头，2a-底部鱼眼镜头，100-竖直方向；
1-第一镜头，2-第二镜头，3-起落架，4-第一组机臂，5-第二组机臂，6-
机身，200-纵向轴。
具体实施方式
为了使本实用新型的目的、技术方案及优点更加清楚明白，以下结合附图及实施例，对本实用新型进行进一步详细说明。应当理解，此处所描述的具体实施例仅仅用以解释本实用新型，并不用于限定本实用新型。
需要说明的是，术语“设置”、“连接”应做广义理解，例如，可以是直接设置、连接，也可以通过居中元部件、居中结构间接设置、连接。
另外，本实用新型实施例中若有“纵向”、“横向”、“长度”、“宽度”、“厚度”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”“内”、“外”等指示的方位或位置关系的用语，其为基于附图所示的方位或位置关系或常规放置状态或使用状态，其仅是为了便于描述本实用新型和简化描述，而不是指示或暗示所指的结构、特征、装置或元件必须具有特定的方位或位置关系、也不是必须以特定的方位构造和操作，因此不能理解为对本实用新型的限制。在本实用新型的描述中，除非另有说明，“多个”的含义是两个或两个以上。
在具体实施方式中所描述的各个具体技术特征和各实施例，在不矛盾的情况下，可以通过任何合适的方式进行组合，例如通过不同的具体技术特征/实施例的组合可以形成不同的实施方式，为了避免不必要的重复，本实用新型中各个具体技术特征/实施例的各种可能的组合方式不再另行说明。
如图2和图3所示，本实用新型实施例提供的一种无人机，包括无人机本体和镜头组件，所述无人机本体包括机身6、位于机身6一侧的第一组机臂4和位于机身6另一侧的第二组机臂5，所述第一组机臂4相对于所述第二组机臂5靠近于所述机身6的上端，所述第一镜头1凸出于所述机身6上端，且所述第一镜头1相对所述第二镜头2靠近于所述第一组机臂4；所述第二镜头2凸出于所述机身6下端，且靠近所述第二组机臂5。所述镜头组件包括第一镜 头1和第二镜头2，所述第一镜头1设置于所述无人机本体的顶部，所述第二镜头2设置于所述无人机本体的底部，以使所述无人机本体位于两个全景镜头的视角之外；通过第一组机臂4和第二组机臂5的合理布局，在保证飞行平稳可靠的前提下，以使第一镜头1和第二镜头2的视角不被遮挡，或被遮挡的范围最大限度地减少。
作为一种可选的实施例，所述无人机本体具有沿机身6高度方向的纵向轴200，可以理解地，无人机本体相对水平面平飞或水平放置时，纵向轴200将垂直于水平面。所述第一镜头1的轴线或所述第二镜头2的轴线与所述纵向轴200之间相对倾斜，以使所述无人机本体位于所述第一镜头1和所述第二镜头2的视角之外；或，所述第一镜头1的轴线和所述第二镜头2的轴线均与所述纵向轴200相对倾斜，以使所述无人机本体位于所述第一镜头1和所述第二镜头2的视角之外。本实用新型所提供的一种无人机，通过改变第一镜头1和第二镜头2的相对位置、设置方式，以使所述无人机本体位于所述第一镜头1和所述第二镜头2的视角之外，能有效减少第一镜头1和第二镜头2的视角被遮挡的范围，也使得镜头(第一镜头1与所述第二镜头2)凸出机体(无人机本体)的范围缩小，较好地保护镜头使其不易磕碰磨损。
作为一种可选的实施例，如图2所示，所述第一镜头1和所述第二镜头2同轴设置，且所述第一镜头1的轴线、所述第二镜头2的轴线均与所述纵向轴200相对倾斜，所述第一镜头1的轴线相对所述纵向轴200由所述第一组机臂4向所述第二组机臂5方向倾斜设置。所述第一镜头1的轴线或所述第二镜头2的轴线与所述纵向轴200之间的夹角为2-10度。具体应用中，所述无人机可包括连接部件，所述连接部件的一端连接于所述第一镜头1，所述连接部件的另一端连接于所述第二镜头2。具体地，所述连接部件可以包括连接轴和定位件，连接轴的两端分别与所述第一镜头1和所述第二镜头2连接；所述定位件设置于所述无人机本体，并用于固定所述连接轴。所述定位件为螺纹结构件，所述螺纹结构件用于与所述连接轴相抵；所述无人机本体具有过孔，所述螺纹结构 件可穿过所述过孔。具体应用中，通过所述连接部件以使所述第一镜头1和所述第二镜头2同轴，并通过定位件的限位作用，以使所述连接轴相对所述纵向轴200之间的倾斜角θ固定，本实施例中，所述螺纹结构件为螺栓，螺栓穿过所述过孔并抵于连接轴，倾斜角θ可调(本实施例中为3.2°)，有效减少第一镜头1和第二镜头2的视角被遮挡的范围，且调节便利。
作为一种可选的实施例，所述第一镜头1的轴线和所述第二镜头2的轴线不同轴设置，所述第一镜头1的轴线相对所述纵向轴200由所述第一组机臂4向所述第二组机臂5方向倾斜设置。在一个实施例中，所述第二镜头2的轴线沿所述纵向轴200方向设置。具体地，倾斜方向为所述第一组机臂4偏向所述第二组机臂5方向；所述第一镜头1的轴线与所述纵向轴200之间相对倾斜，所述第二镜头2的轴线沿所述纵向轴200方向设置；在另一个实施例中，所述第一镜头1的轴线与所述纵向轴200之间相对倾斜，所述第二镜头2的轴线与所述纵向轴200之间相对倾斜；具体应用中，可以根据实际的需求进行调节，以使第一镜头1和第二镜头2的视角不被遮挡或被遮挡的范围最大限度地减少。
作为一种可选的实施例，所述第一镜头1的轴线和所述第二镜头2的轴线不同轴设置，所述第二镜头2的轴线相对所述纵向轴200由所述第一组机臂4向所述第二组机臂5方向倾斜设置。所述第一镜头1的轴线沿所述纵向轴200方向设置。具体应用中，可以根据实际的需求进行调节，以使第一镜头1和第二镜头2的视角不被遮挡或被遮挡的范围最大限度地减少。
作为一种可选的实施例，所述无人机本体具有沿机身6高度方向的纵向轴200，可以理解地，无人机本体相对水平面平飞或水平放置时，纵向轴200将垂直于水平面。所述第一镜头1的轴线、所述第二镜头2的轴线均与所述纵向轴200平行，而且所述第一镜头1与所述第二镜头2沿所述无人机本体的平面方向(即垂直于所述纵向轴200的平面方向)间隔设置，以使所述无人机本体位于所述第一镜头1和所述第二镜头2的视角之外。如图3所示，所述第一镜头1与所述第二镜头2沿垂直于所述纵向轴200的方向间隔设置，可以理解地， 垂直于所述纵向轴200的方向，即所述无人机本体相对水平面平飞或水平放置时沿机身的长度方向。且所述第一镜头1的轴线、所述第二镜头2的轴线均与所述纵向轴200平行。具体应用中，所述第一镜头1与所述第二镜头2之间的间距可以灵活设置，以满足第一镜头1和第二镜头2的视角不被遮挡或被遮挡的范围最大限度地减少。
具体应用中，所述无人机本体包括可以收起的起落架3，所述起落架3收起时位于所述第一镜头1与所述第二镜头2的视角之外。具体地，收起的起落架3也不影响拍摄视角，本实施例中，所述无人机本体包括桨叶，所述桨叶也位于所述第一镜头1与所述第二镜头2的视角之外，满足更多拍摄场景的需要。
作为一种可选的实施例，所述第一镜头1的视角边界与所述无人机本体相切；或，所述第二镜头2的视角边界与所述无人机本体相切。可以理解地，所述第一镜头1的视角边界指第一镜头1最大视角的边界，所述第二镜头2的视角边界指第二镜头2最大视角的边界；本实施例中，通过改变第一镜头1和第二镜头2的相对位置和设置方式，以使所述第一镜头1的最大视角边界与所述无人机本体相切，并且，所述第二镜头2的最大视角边界与所述无人机本体相切，以获得最大的视角，而不被无人机本体遮挡。
本实用新型实施例所提供的一种无人机，所述第一组机臂4相对于所述第二组机臂5靠近于所述机身的顶端；通过设置第一镜头1和第二镜头2，所述第一镜头1设置于所述无人机本体的顶部，所述第二镜头2设置于所述无人机本体的底部，以使所述无人机本体位于两个全景镜头(所述第一镜头1和所述第二镜头2)的视角之外；所述第一镜头1凸出于所述机身上端，所述第一镜头1相对所述第二镜头2靠近于所述第一组机臂4，所述第二镜头2凸出于所述机身下端，且所述第二镜头2靠近于所述第二组机臂5；通过第一组机臂4和第二组机臂5不平齐设置，以及改变第一镜头1和第二镜头2相对于第一组机臂4和第二组机臂5的具体位置，以使所述无人机本体位于所述第一镜头1和所述第二镜头2的视角之外，从而可以使第一镜头1和第二镜头2的视角不 被遮挡，或可以使得被遮挡的范围得到最大限度地减少，也使得镜头(第一镜头1与所述第二镜头2)凸出机体(无人机本体)的范围缩小，较好地保护镜头使其不易磕碰磨损。
以上所述仅为本实用新型的较佳实施例而已，并不用以限制本实用新型，凡在本实用新型的精神和原则之内所作的任何修改、等同替换或改进等，均应包含在本实用新型的保护范围之内。

Claims (10)

  1. 一种无人机，其特征在于，包括：
    无人机本体，所述无人机本体包括机身、位于机身长度方向一侧的第一组机臂和另一侧的第二组机臂，所述第一组机臂相对于所述第二组机臂靠近于所述机身的顶端；
    镜头组件，所述镜头组件包括第一镜头和第二镜头，所述第一镜头凸出于所述机身顶端设置，以使所述第一组机臂位于所述第一镜头的视角之外；所述第二镜头凸出于所述机身底端设置，以使所述第二组机臂位于所述第二镜头的视角之外。
  2. 如权利要求1所述的无人机，其特征在于，所述无人机本体具有沿机身高度方向的纵向轴，所述第一镜头的轴线或/和所述第二镜头的轴线与所述纵向轴之间相对倾斜，以使所述无人机本体位于所述第一镜头和所述第二镜头的视角之外。
  3. 如权利要求2所述的无人机，其特征在于，所述第一镜头的轴线和所述第二镜头的轴线同轴设置，且所述第一镜头的轴线相对所述纵向轴由所述第一组机臂向所述第二组机臂方向倾斜设置。
  4. 如权利要求3所述的无人机，其特征在于，所述第一镜头的轴线或所述第二镜头的轴线与所述纵向轴之间的夹角为2-10度。
  5. 如权利要求2所述的无人机，其特征在于，所述第一镜头的轴线和所述第二镜头的轴线不同轴设置，所述第一镜头的轴线相对所述纵向轴由所述第一组机臂向所述第二组机臂方向倾斜设置。
  6. 如权利要求5所述的无人机，其特征在于，所述第二镜头的轴线沿所述纵向轴方向设置。
  7. 如权利要求2所述的无人机，其特征在于，所述第一镜头的轴线和所述第二镜头的轴线不同轴设置，所述第二镜头的轴线相对所述纵向轴由所述第一组机臂向所述第二组机臂方向倾斜设置。
  8. 如权利要求7所述的无人机，其特征在于，所述第一镜头的轴线沿所述纵向轴方向设置。
  9. 如权利要求1所述的无人机，其特征在于，所述无人机本体具有沿机身高度方向的纵向轴，所述第一镜头的轴线、所述第二镜头的轴线均与所述纵向轴平行，且所述第一镜头与所述第二镜头沿所述无人机本体的平面方向间隔设置，以使所述无人机本体位于所述第一镜头和所述第二镜头的视角之外。
  10. 如权利要求1至9中任一项所述的无人机，其特征在于，所述第一镜头的视角边界与所述无人机本体相切；或/和，所述第二镜头的视角边界与所述无人机本体相切。
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