公开(公告)号：WO2012030300A1

公开(公告)日：2012-03-08

申请号：PCT/SG2011/000268

申请日：2011-07-29

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD ,  TAN, Yio Hock ,  CHAN, Keen Ian

Inventor： TAN, Yio Hock ,  CHAN, Keen Ian

IPC: B64F1/06 ,  B64D3/00

CPC classification number: B64D3/00 ,  B64C39/024 ,  B64C2201/084 ,  B64F1/06

Abstract: Embodiments of the present invention provide a tow hook for use in launching an unmanned aerial vehicle (UAV), the tow hook comprising: a first end capable of releasably engaging a wing of the UAV, a second end capable of being connected to a tow line; and a rigid member connecting the first end to the second end to extend a connection point said tow line below said wing towards a center of gravity of said UAV. Additional embodiments provide for a system and method for launching a UAV using the tow hook.

Abstract translation: 本发明的实施例提供了用于发射无人机（UAV）的牵引钩，牵引钩包括：能够可释放地接合无人机的机翼的第一端，能够连接到牵引线的第二端 ; 以及刚性构件，其将所述第一端连接到所述第二端，以将所述翼片下方的所述牵引线的连接点朝向所述UAV的重心延伸。 另外的实施例提供了使用牵引钩发射无人机的系统和方法。

公开(公告)号：WO2016085404A1

公开(公告)日：2016-06-02

申请号：PCT/SG2014/000563

申请日：2014-11-27

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD

Inventor： CHEN, Xujian ,  TAN, Leon Choon Seng ,  LAM, Chian Poh

IPC: B64F1/10 ,  B64F1/04 ,  B64F1/02

CPC classification number: B64F1/02 ,  B64C2201/021 ,  B64C2201/08 ,  B64C2201/082 ,  B64C2201/182 ,  B64F1/04

Abstract: An apparatus for launch and recovery of an Unmanned Aerial Vehicle (UAV), a method for launching a UAV, a method for recovering a UAV and a kit of parts for launch and recovery of a UAV are disclosed. The apparatus comprises a boom having a center member for receiving the UAV, and first and second arm members extending outwardly and upwardly from the center member, wherein the boom is configured to be lifted to a predetermined height into the air from a reference point; and wherein the boom is movable in the air to an operating position forward of the reference point.

Abstract translation: 公开了一种用于无人机（UAV）的发射和恢复装置，用于发射UAV的方法，用于恢复UAV的方法和用于UAV的发射和恢复的零件的套件。 该装置包括具有用于接收UAV的中心构件的悬臂，以及从中心构件向外和向上延伸的第一和第二臂构件，其中，悬臂构造成从参考点提升到预定高度到空气中; 并且其中所述悬臂可在空中移动到所述参考点的前方的操作位置。

公开(公告)号：WO2014163582A1

公开(公告)日：2014-10-09

申请号：PCT/SG2013/000139

申请日：2013-04-05

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD ,  TENRYU AERO COMPONENT CO., LTD.

Inventor： ZHENG, Guo Ying ,  BAZ, Charles, Fakhri ,  SHIGA, Kazuhiro

IPC: A47C1/023 ,  B60N2/02 ,  B64D11/06

CPC classification number: B64D11/064 ,  B60N2/242 ,  B60N2/686 ,  B64D11/0619 ,  B64D11/0647

Abstract: A seat pan for a passenger seat and a passenger seat. The seat pan is corrugated for partially absorbing a downward loading applied to the seat pan through deformation of a corrugation pattern of the seat pan as a result of a counter force applied by a support structure of the passenger seat.

Abstract translation: 乘客座椅和乘客座椅的座椅平台。 由于由乘客座椅的支撑结构施加的反作用力，座椅盘是波纹形的，以部分地吸收施加到座椅盘的向下的负载，该向下的负载通过座椅盘的波纹图案的变形而被部分吸收。

公开(公告)号：WO2014163580A1

公开(公告)日：2014-10-09

申请号：PCT/SG2013/000137

申请日：2013-04-05

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD ,  TENRYU AERO COMPONENT CO., LTD.

Inventor： ZHENG, Guo Ying ,  BAZ, Charles Fakhri ,  SHIGA, Kazuhiro

IPC: B64D11/06

CPC classification number: B64D11/0648 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/0649 ,  B64D11/0696

Abstract: A seat leg assembly for a passenger seat, a frame for a passenger seat, and a passenger seat. The seat leg assembly comprising a brace member configured to extend from a front end of a base frame of the passenger seat to a rear floor fitting; a front leg configured to extend from a front floor fitting to the brace member and connected to the brace member; a rear leg portion extending from a rear end of the base frame to the brace member; and a first joint structure connecting the rear leg portion to the brace member.

Abstract translation: 用于乘客座椅的座椅支腿组件，乘客座椅的框架和乘客座椅。 所述座椅支腿组件包括支撑构件，所述支撑构件构造成从所述乘客座椅的基架的前端延伸到后地板配件; 前腿，其构造成从前地板配件延伸到支撑构件并连接到支撑构件; 后腿部，其从所述基部框架的后端延伸到所述支撑构件; 以及将后腿部连接到支撑构件的第一接合结构。

公开(公告)号：WO2014163579A1

公开(公告)日：2014-10-09

申请号：PCT/SG2013/000136

申请日：2013-04-05

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD ,  TENRYU AERO COMPONENT CO., LTD.

Inventor： ZHENG, Guo Ying ,  FOONG, Herng Huei ,  SHIGA, Kazuhiro

IPC: B64D11/06

CPC classification number: B64D11/0638 ,  A47B13/16 ,  A47B23/043 ,  B60N3/00 ,  B60N3/001 ,  B60N3/004 ,  B64D11/06

Abstract: A support structure for attachment to a tray table for a passenger seat, a tray table for a passenger seat, and a passenger seat. The support structure comprises a support arm shaped to substantially match at least a first portion of a peripheral contour of the tray table; and a connecting structure for connecting the support arm to the tray table in a manner such that the support arm is configurable into a stowed position in which the support arm extends substantially along said at least first portion of the peripheral contour of the tray table and at least one support position for supporting an item on the tray table in an angled orientation between a surface of the item and the surface of the tray table.

Abstract translation: 用于附接到乘客座椅的托盘台，乘客座椅的托盘台和乘客座椅的支撑结构。 支撑结构包括支撑臂，该支撑臂成形为基本上匹配托盘台的周边轮廓的至少第一部分; 以及用于以支撑臂可配置成收起位置的方式将支撑臂连接到托盘台的连接结构，其中支撑臂基本沿着托盘台的周边轮廓的至少第一部分延伸并且在 至少一个支撑位置，用于在物品的表面和托盘台的表面之间以倾斜的方向支撑托盘桌上的物品。

公开(公告)号：WO2013048339A1

公开(公告)日：2013-04-04

申请号：PCT/SG2012/000336

申请日：2012-09-14

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD ,  CHAN, Keen Ian

Inventor： CHAN, Keen Ian

IPC: B64C29/02 ,  B64C25/32 ,  B64C27/08 ,  B64C39/08 ,  B64C39/10 ,  B64C99/00 ,  B64C11/46 ,  A63H27/133 ,  A63H27/127 ,  A63H27/18

CPC classification number: B64C29/02 ,  A63H27/12 ,  B64C13/24 ,  B64C27/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/165 ,  G05D1/0669 ,  Y10T29/49826

Abstract: An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method for assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises a wing structure comprising elongated equal first and second wings; a support structure comprising first and second sections coupled to a middle position of the wing structure and extending in opposite directions perpendicular to the wing structure; and four propellers, each mounted to a respective one of the first and second wings, and first and second sections, for powering the UAV during both vertical and horizontal flight modes.

Abstract translation: 能够进行垂直和水平飞行模式的无人飞行器（UAV），组装无人机的方法和用于组装无人机的一套零件。 无人机包括翼结构，其包括细长的相等的第一和第二翼; 支撑结构，包括联接到所述机翼结构的中间位置并且在与所述机翼结构垂直的相反方向上延伸的第一和第二部分; 以及四个螺旋桨，每个螺旋桨安装到第一和第二翼中的相应一个以及第一和第二部分，用于在垂直和水平飞行模式期间为无人机提供动力。

公开(公告)号：WO2009075648A1

公开(公告)日：2009-06-18

申请号：PCT/SG2007/000425

申请日：2007-12-10

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD ,  TAY, Milly, Mih Ni ,  YEK, Sing Chee ,  TEO, Guan Kiat ,  HUNTER, Richard, S. ,  LIM, Hoon Sin ,  LER, Hock Seng ,  KONG, Winston, Te Hsiung ,  TAN, Guan Keng

Inventor： TAY, Milly, Mih Ni ,  YEK, Sing Chee ,  TEO, Guan Kiat ,  HUNTER, Richard, S. ,  LIM, Hoon Sin ,  LER, Hock Seng ,  KONG, Winston, Te Hsiung ,  TAN, Guan Keng

IPC: G08G5/06 ,  G01S17/93

CPC classification number: G08G5/0078 ,  G01S17/023 ,  G01S17/026 ,  G01S17/87 ,  G01S17/933 ,  G08G5/0021 ,  G08G5/065

Abstract: A system and method for collision avoidance between an aircraft and surrounding objects on the ground is provided. The system may include a controller interface; a plurality of laser sensors mounted on the aircraft and electrically connected to the controller interface, each of the plurality of laser sensors having a detection area, such that said detection areas cumulatively cover at least a periphery of both a left and a right wing of the aircraft; audio and visual warning means located in a cockpit of the aircraft, each of the audio and visual warning means being electrically connected to the controller interface; and at least one video camera mounted on the aircraft and electrically connected to the controller interface, such that when said at least one video camera is activated, said video camera provides an image of said periphery to said visual warning means; wherein the controller interface receives a signal from at least one of the laser sensors indicating the presence of an object within the detection area and activates at least one of the audio warning means and said at least one video camera to alert an operator of the aircraft that a collision is possible.

Abstract translation: 提供了一种用于飞机和地面周围物体之间的防撞的系统和方法。 该系统可以包括控制器接口; 安装在飞行器上并电连接到控制器接口的多个激光传感器，所述多个激光传感器中的每一个具有检测区域，使得所述检测区域累积地覆盖所述检测区域的左翼和右翼的至少周边 飞机; 音响和视觉警告装置位于飞行器的驾驶舱中，每个音频和视觉警告装置电连接到控制器接口; 以及安装在飞行器上并电连接到控制器接口的至少一个摄像机，使得当所述至少一个摄像机被激活时，所述摄像机向所述视觉警告装置提供所述周边的图像; 其中所述控制器接口接收来自所述激光传感器中的至少一个激光传感器的信号，其指示所述检测区域内存在物体，并且激活所述音频警告装置和所述至少一个摄像机中的至少一个以提醒所述飞行器的操作者， 碰撞是可能的。

公开(公告)号：DE102012215416A1

公开(公告)日：2013-03-14

申请号：DE102012215416

申请日：2012-08-30

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD

Inventor： GAMMELL FRANCIS ROLAND ,  WANG CHANGXIONG

IPC: C09D5/22 ,  C09D163/00 ,  C09K11/64

Abstract: Die Erfindung betrifft eine Epoxid-Leuchtbeschichtung und ein Verfahren zum Herstellen einer Epoxid-Leuchtbeschichtung. Die Epoxid-Leuchtbeschichtung umfasst ein Gemisch, das beim Vermischen von bestimmten Anteilen eines klaren Epoxids und eines Leuchtpulvers erhalten wurde. Das Verfahren umfasst die folgenden Schritte: das Vermischen eines bestimmten Anteils eines klaren Epoxids mit einem Leuchtpulver, um ein viskoses Gemisch herzustellen; das Aufbringen des viskosen Gemisches auf einem bestimmten Bereich; und das Aushärten des Gemisches.

公开(公告)号：SG182017A1

公开(公告)日：2012-07-30

申请号：SG2010093649

申请日：2010-12-16

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD

Inventor： ZHENG GUOYING ,  TAN SOO SIONG RICHARD ,  TAN KUAN SHENG

IPC: B60N2/90

Abstract: Disclosed herein is a single arm adjustment mechanism for supporting an object, thesingle arm adjustment mechanism comprising: a support arm; an upper adjustment assembly coupled to an upper end of said support arm, said upper adjustment assembly capable of being coupled to said object such that said object pivots about a first axis; and a lower adjustment assembly capable of being fixed to a supportand pivotally coupled to a lower end of said support arm such that said support arm pivots about a second axis parallel to said first axis in order to maintain said object in a desired angular orientation with respect to said support.FIG. 1

公开(公告)号：SG182019A1

公开(公告)日：2012-07-30

申请号：SG2010094027

申请日：2010-12-17

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD

Inventor： CHUA BENG CHOON ,  KEK HIAN BENG ,  LIU YONG WEE

Abstract: System and method for measuring static pressure of an aircraft are disclosed. Thesystem comprises: a plurality of static ports mounted on the fuselage of the aircraft, wherein outputs of each of the static ports are connected to a pressure stabilizer, and the pressure stabilizer is operable to provide average pressure from the plurality of the static ports to a static pressure sensor located on a flight control computer(FCC) board of the aircraft.Figure 7b