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1. 发明申请

US20110139939A1 PERSONAL FLIGHT DEVICE INCORPORATING RADIATOR COOLING PASSAGE 有权
标题翻译：个人飞行器装置散热器冷却通风
公开(公告)号：US20110139939A1
公开(公告)日：2011-06-16
申请号：US13001254
申请日：2009-05-13
申请人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
发明人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
IPC分类号： B64C39/02 , B64C27/20 , F01P1/00
CPC分类号： B64C39/026 , B64D33/10 , F01P3/18
摘要： A personal flight device which includes: a housing which is securable to a pilot; at least one pair of ducted fans, one fan of the pair mounted to one side of the housing, the other fan of the pair mounted to the other side of the housing; wherein each fan rotates about an axis of rotation so as to draw air through the corresponding duct from an entry end of the duct to an exit end of the duct; and wherein the axis of rotation of each fan is fixed relative to the housing; at least one engine mounted on the housing for driving the fans such that both fans rotate in the same direction for producing thrust; the or each engine being cooled by a radiator; the or each radiator being associated with at least one passage having an entry end in communication with one surface of the radiator and an exit end adjacent the entry end of one of said ducts.
摘要翻译：一种个人飞行装置，其包括：可安装到飞行员的壳体; 至少一对导管风扇，一对风扇安装在壳体的一侧，另一个风扇安装在壳体的另一侧; 其中每个风扇围绕旋转轴线旋转，以便将空气从所述管道的入口端引导到所述管道的出口端; 并且其中每个风扇的旋转轴线相对于壳体是固定的; 安装在壳体上的至少一个发动机用于驱动风扇，使得两个风扇沿相同的方向旋转以产生推力; 该发动机或每个发动机由散热器冷却; 所述或每个散热器与至少一个通道相关联，所述至少一个通道具有与所述散热器的一个表面连通的入口端和邻近所述管道之一的入口端的出口端。

2. 发明授权

US07484687B2 Propulsion device 有权
标题翻译：推进装置
公开(公告)号：US07484687B2
公开(公告)日：2009-02-03
申请号：US11259814
申请日：2005-10-26
申请人： Glenn Neil Martin
发明人： Glenn Neil Martin
IPC分类号： B64C29/00 , B64C29/02
CPC分类号： B64D35/04 , B64C15/00 , B64C27/20 , B64C39/026
摘要： A personal flight device which consists of a housing securable to a pilot, at least one pair of fans, and at least one engine mounted on the housing for driving the fans; one fan of the pair is mounted to one side of the housing and the other fan of the pair is mounted to the other side of the housing; in use, both fans rotate in the same direction for producing thrust.
摘要翻译：一种个人飞行装置，其包括可安装到飞行员的壳体，至少一对风扇和安装在壳体上的用于驱动风扇的至少一个引擎; 该对的一个风扇安装在壳体的一侧，另一个风扇安装在壳体的另一侧; 在使用中，两个风扇以相同的方向旋转以产生推力。

3. 发明申请

US20110133037A1 PERSONAL FLIGHT VEHICLE INCLUDING CONTROL SYSTEM 失效
标题翻译：个人航空包括控制系统
公开(公告)号：US20110133037A1
公开(公告)日：2011-06-09
申请号：US13001319
申请日：2009-05-13
申请人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
发明人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
IPC分类号： B64C39/02 , B64C27/20 , B64C29/00 , B64C11/00 , B64C9/02 , B64C13/00 , B64C15/02
CPC分类号： B64C39/026 , B64C15/02
摘要： A personal flight device including: a housing securable to the pilot; at least one pair of ducted fans, one fan of each pair mounted to each side of the housing; wherein each fan rotates about an axis of rotation to draw air through the corresponding duct; wherein the axis of rotation of each fan is fixed relative to the housing; at least one engine mounted on the housing for driving the fans, wherein both fans rotate in the same direction for producing thrust; three pairs of control surfaces, with one control surface of each pair mounted below each fan of the one or each pair of fans; such that air leaving said fan impact on said control surface; one pair of control surfaces being configured to control yaw, one pair to control pitch, and one pair to control roll; control means for controlling the orientation of said control surfaces relative to said fans.
摘要翻译：一种个人飞行装置，包括：可以安装到飞行员的房屋; 至少一对导风扇，每对的一个风扇安装在壳体的每一侧; 其中每个风扇围绕旋转轴线旋转以吸入空气通过相应的管道; 其中每个风扇的旋转轴线相对于壳体是固定的; 至少一个发动机安装在壳体上用于驱动风扇，其中两个风扇沿相同的方向旋转以产生推力; 三对控制面，每对的一个控制面安装在一对或每对风扇的每个风扇下方; 使得离开所述风扇的空气冲击所述控制表面; 一对控制表面被配置为控制偏航，一对控制俯仰，一对控制滚动; 用于控制所述控制表面相对于所述风扇的取向的控制装置。

4. 发明授权

US09171479B2 Training system of a powered vehicle 有权
标题翻译：动力车辆的训练系统
公开(公告)号：US09171479B2
公开(公告)日：2015-10-27
申请号：US13383833
申请日：2010-07-15
申请人： Glenn Neil Martin , Vanessa Louise Martin
发明人： Glenn Neil Martin , Vanessa Louise Martin
IPC分类号： G09B19/16 , G09B9/042 , G09B9/052 , G09B9/02 , G09B9/048 , G09B9/08
CPC分类号： G09B9/042 , G09B9/02 , G09B9/048 , G09B9/052 , G09B9/08 , G09B19/165 , G09B19/167
摘要： A training system for the solo operation of a powered vehicle, wherein the system includes: —providing means for electronic control of the speed and orientation of a ground vehicle or of the speed, orientation and height of a flying vehicle; —providing a virtual enclosure training area delineated by a plurality of spaced sensors; —providing means associated with said vehicle for communicating with, and receiving instructions from, each of said sensors; —whereby instructions received from said sensors may be used to control said means for electronic control such that movement of said vehicle is restricted to said virtual enclosure training area, and within said virtual enclosure training area, the speed and orientation of a ground vehicle or the speed, orientation and height of a flying vehicle controlled within preset parameters.
摘要翻译：一种用于动力车辆的独奏操作的训练系统，其中所述系统包括：用于电子控制地面车辆的速度和方向或飞行器的速度，方向和高度的提供装置; - 提供由多个间隔传感器描绘的虚拟外壳训练区域; - 与所述车辆相关联的提供装置，用于与每个所述传感器进行通信和从每个所述传感器接收指令; - 可以使用从所述传感器接收的指令来控制所述用于电子控制的装置，使得所述车辆的运动被限制到所述虚拟外壳训练区域，并且在所述虚拟外壳训练区域内，地面车辆的速度和方位飞行车辆的速度，方向和高度在预设参数内控制。

5. 发明授权

US08608103B2 Personal flight device incorporating radiator cooling passage 有权
标题翻译：散热器冷却通道的个人飞行装置
公开(公告)号：US08608103B2
公开(公告)日：2013-12-17
申请号：US13001254
申请日：2009-05-13
申请人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
发明人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
IPC分类号： B64C39/02 , B64C29/00 , F01P1/00
CPC分类号： B64C39/026 , B64D33/10 , F01P3/18
摘要： A personal flight device which includes a housing which is securable to a pilot having at least one pair of ducted fans, one fan of the at least one pair of ducted fans is mounted to one side of the housing, the other fan of the at least one pair of ducted fans mounted to the other side of the housing. Each fan rotates about an axis of rotation so as to draw air through the corresponding duct from an entry end of the duct to an exit end of the duct. At least one radiator is also provided. Each engine of the at least one engine is cooled by a radiator of the at least one radiator. Each radiator of the at least one radiator is associated with at least one passage having an entry end in communication with one surface of the radiator and an exit end adjacent the entry end of one duct of the ducted fans.
摘要翻译：一种个人飞行装置，其包括可安装到具有至少一对导管风扇的飞行员的壳体，所述至少一对导管风扇的一个风扇安装到所述壳体的一侧，所述另一个风扇至少安装在壳体另一侧的一对导管风扇。每个风扇围绕旋转轴线旋转，以便将空气从管道的进入端通过相应的管道到管道的出口端。还提供至少一个散热器。所述至少一个发动机的每个发动机由所述至少一个散热器的散热器冷却。所述至少一个散热器的每个散热器与至少一个具有与所述散热器的一个表面连通的入口端和与所述管道风扇的一个管道的入口端相邻的出口端的通道相关联。

6. 发明授权

US08695916B2 Personal flight vehicle including control system 失效
标题翻译：个人飞行器包括控制系统
公开(公告)号：US08695916B2
公开(公告)日：2014-04-15
申请号：US13001319
申请日：2009-05-13
申请人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
发明人： Glenn Neil Martin , Colin Cecil Dodge , Mark John Daniel
IPC分类号： B64C39/02 , B64C29/00
CPC分类号： B64C39/026 , B64C15/02
摘要： A personal flight device includes a housing securable to the pilot. The device includes at least one pair of ducted fans, one fan of each pair mounted to each side of the housing. The axis of rotation of each fan is fixed relative to the housing. At least one engine is mounted on the housing for driving the fans and both fans rotate in the same direction for producing thrust. Three pairs of control surfaces, with one control surface of each pair is mounted below each fan of the one or each pair of fans.
摘要翻译：个人飞行装置包括可安装到飞行员的外壳。该装置包括至少一对导管风扇，每对的一个风扇安装在壳体的每一侧。每个风扇的旋转轴线相对于外壳是固定的。至少一个发动机安装在壳体上用于驱动风扇，并且两个风扇沿相同方向旋转以产生推力。每对风扇的每个风扇下面安装三对控制面，每对控制面都有一个控制面。

7. 发明申请

US20120107776A1 TRAINING SYSTEM OF A POWERED VEHICLE 有权
标题翻译：动力车的训练系统
公开(公告)号：US20120107776A1
公开(公告)日：2012-05-03
申请号：US13383833
申请日：2010-07-15
申请人： Glenn Neil Martin , Vanessa Louise Martin
发明人： Glenn Neil Martin , Vanessa Louise Martin
IPC分类号： G09B19/16
CPC分类号： G09B9/042 , G09B9/02 , G09B9/048 , G09B9/052 , G09B9/08 , G09B19/165 , G09B19/167
摘要： A training system for the solo operation of a powered vehicle, wherein the system includes: —providing means for electronic control of the speed and orientation of a ground vehicle or of the speed, orientation and height of a flying vehicle; —providing a virtual enclosure training area delineated by a plurality of spaced sensors; —providing means associated with said vehicle for communicating with, and receiving instructions from, each of said sensors; —whereby instructions received from said sensors may be used to control said means for electronic control such that movement of said vehicle is restricted to said virtual enclosure training area, and within said virtual enclosure training area, the speed and orientation of a ground vehicle or the speed, orientation and height of a flying vehicle controlled within preset parameters.
摘要翻译：一种用于动力车辆的独奏操作的训练系统，其中所述系统包括：用于电子控制地面车辆的速度和方向或飞行器的速度，方向和高度的提供装置; - 提供由多个间隔传感器描绘的虚拟外壳训练区域; - 与所述车辆相关联的提供装置，用于与每个所述传感器进行通信和从每个所述传感器接收指令; - 可以使用从所述传感器接收的指令来控制所述用于电子控制的装置，使得所述车辆的运动被限制到所述虚拟外壳训练区域，并且在所述虚拟外壳训练区域内，地面车辆的速度和方位飞行车辆的速度，方向和高度在预设参数内控制。

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