公开(公告)号：WO2010140082A9

公开(公告)日：2011-03-24

申请号：PCT/IB2010052341

申请日：2010-05-26

Applicant: CAPE PENINSULA UNIVERSITY OF TECHNOLOGY ,  PHILANDER OSCAR ,  RIDDLES MORNAY

Inventor： PHILANDER OSCAR ,  RIDDLES MORNAY

IPC: B64D27/26 ,  B64C1/16 ,  B64C25/06 ,  B64C25/50 ,  B64C25/62 ,  B64D47/08

CPC classification number: B64C39/024 ,  B64C2201/044 ,  B64C2201/127 ,  B64D27/08

Abstract: A UAV with an engine (34) attached to rear (38) of its fuselage by an engine mounting assembly with the rotational axis of the engine generally parallel with the axis (45) of the fuselage. The engine mounting assembly includes a fuselage bulkhead (40) and a parallel, spaced motor mount bulkhead (42) with the engine (34) attached to it. The mounting assembly also includes a number of connectors (64) that extend between the two bulkheads (40, 42) and resiliently compressible material (48) between the bulkheads in the vicinity of each connector. Each connector (64) can pivot relative to the bulkheads (40, 42) and presses on the bulkheads to compress the compressible material (48). The connectors (64) are adjustable to adjust the compressive load exerted on the compressible material (48). An undercarriage assembly (52) for a UAV comprising an upper cylinder (54) which is telescopically displaced relative to a lower cylinder (58) and a spring element (64) connected to both of the cylinders. A support structure (30) mounted in the front of the fuselage for supporting a camera and the support structure is configured to pivot the camera relative to the fuselage between different orientations.

Abstract translation: 具有通过发动机安装组件附接到其机身的后部（38）的发动机（34）的UAV，其中发动机的旋转轴线大体上平行于机身的轴线（45）。 发动机安装组件包括机身隔板（40）和平行间隔开的​​电机安装隔板（42），发动机（34）连接到其上。 安装组件还包括在每个连接器附近的隔板之间在两个隔板（40,42）和弹性压缩材料（48）之间延伸的多个连接器（64）。 每个连接器（64）可以相对于舱壁（40,42）枢转并且压在舱壁上以压缩可压缩材料（48）。 连接器（64）可调节以调节施加在可压缩材料（48）上的压缩载荷。 一种用于UAV的起落架组件（52），包括相对于下部气缸（58）伸缩移位的上部气缸（54）和连接到两个气缸的弹簧元件（64）。 安装在机身前部用于支撑相机的支撑结构（30）和支撑结构被配置为在不同取向之间使相机相对于机身枢转。

公开(公告)号：WO2010140082A1

公开(公告)日：2010-12-09

申请号：PCT/IB2010/052341

申请日：2010-05-26

Applicant: CAPE PENINSULA UNIVERSITY OF TECHNOLOGY ,  PHILANDER, Oscar ,  RIDDLES, Mornay

Inventor： PHILANDER, Oscar ,  RIDDLES, Mornay

IPC: B64D27/26 ,  B64C25/06 ,  B64C25/62 ,  B64C1/16 ,  B64C25/50 ,  B64D47/08

CPC classification number: B64C39/024 ,  B64C2201/044 ,  B64C2201/127 ,  B64D27/08

Abstract: A UAV with an engine (34) attached to rear (38) of its fuselage by an engine mounting assembly with the rotational axis of the engine generally parallel with the axis (45) of the fuselage. The engine mounting assembly includes a fuselage bulkhead (40) and a parallel, spaced motor mount bulkhead (42) with the engine (34) attached to it. The mounting assembly also includes a number of connectors (64) that extend between the two bulkheads (40,42) and resiliently compressible material (48) between the bulkheads in the vicinity of each connector. Each connector (64) can pivot relative to the bulkheads (40,42) and presses on the bulkheads to compress the compressible material (48). The connectors (64) are adjustable to adjust the compressive load exerted on the compressible material (48).

Abstract translation: 具有通过发动机安装组件附接到其机身的后部（38）的发动机（34）的UAV，其中发动机的旋转轴线大致平行于机身的轴线（45）。 发动机安装组件包括机身隔板（40）和与发动机（34）连接在其上的平行隔开的马达安装隔板（42）。 安装组件还包括在每个连接器附近的隔板之间的两个隔板（40,42）和弹性可压缩材料（48）之间延伸的多个连接器（64）。 每个连接器（64）可相对于舱壁（40,42）枢转并且压在舱壁上以压缩可压缩材料（48）。 连接器（64）可调节以调节施加在可压缩材料（48）上的压缩载荷。