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公开(公告)号：KR20180026373A
公开(公告)日：2018-03-12
申请号：KR20177033320
申请日：2016-04-20
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL , COOK JONATHAN EDWARD , COOK MICHAEL KEVIN
IPC: B64C39/02
CPC classification number: B64C13/28 , B64C1/061 , B64C3/56 , B64C13/30 , B64C31/02 , B64C39/024 , B64C2001/0054 , B64C2201/021 , B64C2201/102 , B64C2201/128 , B64C2201/141 , B64C2211/00
Abstract: 목표장소에화물을자율적으로수송하기위한항공수송용어셈블리(10)에있어서, 상기어셈블리는, 본체(12), 절첩된위치와전개된위치사이에서이동가능한적어도하나의전개가능한양력제공구조체(30), 및절첩된위치와전개된위치사이에서이동가능하고어셈블리의비행을제어하는적어도하나의전개가능하고조정가능한제어구조체(34, 36, 38, 39)를포함하는기체를포함한다. 본체(12)는수송될화물을수용하기위한격실을포함한다. 어셈블리는제어구조체(34, 36, 38, 39)를조정하는데 사용하기위한작동모듈을포함하는제어유닛(20)을추가로포함하며, 제어유닛은기체에해제가능하게연결되어, 상이한기체를갖는항공이송용어셈블리에재사용가능하다.
Abstract translation: 一种用于将货物自主运送到目标位置的空中运输组件（10），所述组件包括主体（12），至少一个可展开的提升提供结构（30），所述结构可在折叠位置和展开位置之间移动 以及至少一个可展开和可调整的控制结构（34,36,38,39），其可在折叠位置和展开位置之间移动并控制组件的飞行。 主体12包括用于接收待运输货物的隔间。 该组件还包括控制单元（20），该控制单元（20）包括用于调节控制结构（34,36,38,39）的操作模块，其中控制单元可释放地连接到气体， 空气可以在运输组件中重复使用。
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公开(公告)号：KR20180026374A
公开(公告)日：2018-03-12
申请号：KR20177033321
申请日：2016-04-20
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL , COOK JONATHAN EDWARD , COOK MICHAEL KEVIN
IPC: B64C39/02
CPC classification number: B64C13/28 , B64C1/061 , B64C3/56 , B64C13/30 , B64C31/02 , B64C39/024 , B64C2001/0054 , B64C2201/021 , B64C2201/102 , B64C2201/128 , B64C2201/141 , B64C2211/00
Abstract: 목표장소로의화물의자율적인항공수송을위한항공기(10)에있어서, 상기항공기는, 항공기의비행을제어하기위한적어도하나의조정가능한제어구조체(36, 38, 39), 및화물을수용하도록구성된본체(12)를구비하는기체, 기체에해제가능하게연결되며, 제어구조체(36, 38, 39)를조정하기위한액추에이터및 액추에이터를제어하기위한전기구동신호를생성하기위한제어기를포함하는자납형제어모듈(20), 및제어모듈로부터적어도하나의조정가능한제어구조체까지연장되어제어모듈(20)을적어도하나의조정가능한제어구조체(36, 38, 39)에작동가능하게연결하는적어도하나의링크기구(24)를포함하며, 제어모듈(20)의액추에이터는적어도하나의링크기구(24)를사용하여적어도하나의조정가능한제어구조체(36, 38, 39)를조정함으로써항공기(10)의비행을제어하고항공기를목표장소로조종하도록구성된다.
Abstract translation: 一种用于将货物自动空中运送到目标位置的飞机（10），所述飞机包括：至少一个用于控制飞机的飞行的可调整的控制结构（36,38,39） 气体包括构造成可移除地连接到气体并且包括用于产生用于控制致动器的电驱动信号的控制器的主体12以及用于调节控制结构36的致动器， 至少一个无引导控制模块（20）从控制模块延伸到至少一个可调节控制结构并且可操作地将控制模块（20）连接到至少一个可调节控制结构（36,38,39） 其中，控制模块（20）的致动器包括连杆机构（24），用于使用至少一个连杆机构（36,38,39）调节至少一个可调控制结构 控制飞行并设置飞机 它被配置为。
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公开(公告)号：AU2016251397A1
公开(公告)日：2017-12-07
申请号：AU2016251397
申请日：2016-04-20
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL , COOK JONATHAN EDWARD , COOK MICHAEL KEVIN
IPC: B64C39/02
Abstract: An aerial delivery assembly (10) for autonomously delivering a load to a target location, the assembly comprising an airframe which comprises a main body (12), at least one deployable lift providing structure (30), the lift providing structure being moveable between a stowed position and a deployed position; and at least one deployable and adjustable control structure (34, 36, 38, 39) for controlling the flight of the assembly and moveable between a stowed position and a deployed position. The main body (12) comprises a compartment for receiving a load to be delivered. The assembly further comprises a control unit (20) comprising an actuation module for use in adjusting the control structure (34,36, 38, 39), wherein the control unit is releaseably connected to the airframe such that it is reusable in an aerial delivery assembly having a different airframe.
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Patent Agency Ranking
公开(公告)号：GB2525619A
公开(公告)日：2015-11-04
申请号：GB201407526
申请日：2014-04-29
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL , COOK JONATHAN EDWARD , COOK MICHAEL
Abstract: A self contained alarm unit 10 is provided for use in a network 102,120 having a plurality of similar alarm units 10 together with at least one sensor unit 114 for sensing an alarm event, and a remote control unit 104,106. The alarm unit comprises an enclosure incorporating: an audible/visual alert generator; a power supply; a receiver for communication with the sensor unit, another self contained alarm unit, or the remote control unit; a transmitter for communication with another self contained alarm unit or the remote control unit; and a control module for controlling: the alert generator to generate an alert based on an alarm signal being received by the receiver, and to stop an alert based on a disarm signal being received by the receiver; and to control the transmitter to transmit an alert signal in response to an alarm signal being received by the receiver, and to transmit a disarm signal in response to the disarm signal being received by the receiver.
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公开(公告)号：AU2016251396A1
公开(公告)日：2017-12-07
申请号：AU2016251396
申请日：2016-04-20
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL , COOK JONATHAN EDWARD , COOK MICHAEL KEVIN
IPC: B64C39/02
Abstract: An aircraft (10) for the autonomous aerial delivery of a load to a target location, the aircraft comprising an airframe having at least one adjustable control structure (36, 38, 39) for controlling the flight of the aircraft and a main body (12) adapted to receive a load, a self-contained control module (20) releaseably connected to the airframe, the control module (20) containing an actuator (for adjusting the control structure (36, 38, 39) and a controller for producing an electrical drive signal for controlling the actuator; and at least one linkage (24) extending from the control module to the at least one adjustable control structure so as to operably connect the control module (20) to the at least one adjustable control structure (36, 38, 39), wherein the actuator of the control module (20) is adapted to adjust the at least one adjustable control structure (36, 38, 39) using the at least one linkage (24) so as to control the flight of the aircraft (10) and to steer the aircraft to the target location.
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公开(公告)号：CA2983097A1
公开(公告)日：2016-10-27
申请号：CA2983097
申请日：2016-04-20
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL , COOK JONATHAN EDWARD , COOK MICHAEL KEVIN
Abstract: An aerial delivery assembly (10) for autonomously delivering a load to a target location, the assembly comprising an airframe which comprises a main body (12), at least one deployable lift providing structure (30), the lift providing structure being moveable between a stowed position and a deployed position; and at least one deployable and adjustable control structure (34, 36, 38, 39) for controlling the flight of the assembly and moveable between a stowed position and a deployed position. The main body (12) comprises a compartment for receiving a load to be delivered. The assembly further comprises a control unit (20) comprising an actuation module for use in adjusting the control structure (34,36, 38, 39), wherein the control unit is releaseably connected to the airframe such that it is reusable in an aerial delivery assembly having a different airframe.
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公开(公告)号：CA2983095A1
公开(公告)日：2016-10-27
申请号：CA2983095
申请日：2016-04-20
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL , COOK JONATHAN EDWARD , COOK MICHAEL KEVIN
Abstract: An aircraft (10) for the autonomous aerial delivery of a load to a target location, the aircraft comprising an airframe having at least one adjustable control structure (36, 38, 39) for controlling the flight of the aircraft and a main body (12) adapted to receive a load, a self-contained control module (20) releaseably connected to the airframe, the control module (20) containing an actuator (for adjusting the control structure (36, 38, 39) and a controller for producing an electrical drive signal for controlling the actuator; and at least one linkage (24) extending from the control module to the at least one adjustable control structure so as to operably connect the control module (20) to the at least one adjustable control structure (36, 38, 39), wherein the actuator of the control module (20) is adapted to adjust the at least one adjustable control structure (36, 38, 39) using the at least one linkage (24) so as to control the flight of the aircraft (10) and to steer the aircraft to the target location.
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公开(公告)号：GB2337967A
公开(公告)日：1999-12-08
申请号：GB9805742
申请日：1998-03-19
Applicant: COOK GEORGE MICHAEL
Inventor： COOK GEORGE MICHAEL
IPC: B60G21/05 , B60G21/055
Abstract: An anti-roll system is provided for a wheeled land vehicle. A torsional coupling is arranged to couple unsprung masses of suspension units positioned on opposite sides of the vehicle. The coupling comprises torsion bar components 10A, 10B which extend inwardly from each unsprung mass, and a torsion bar coupling means 14A, 14B, 16 coupling the two torsion bars. Upon lateral acceleration of the vehicle body torsional stresses are induced in the coupling which further comprises means 18, 20 whereby equal and opposite torque can be induced into the torsion bars by way of the torsion bar coupling means 14A, 14B, 16.
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