公开(公告)号：US20110139939A1

公开(公告)日：2011-06-16

申请号：US13001254

申请日：2009-05-13

Applicant: Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

Inventor： Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

IPC: B64C39/02 ,  B64C27/20 ,  F01P1/00

CPC classification number: B64C39/026 ,  B64D33/10 ,  F01P3/18

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US08608103B2

公开(公告)日：2013-12-17

申请号：US13001254

申请日：2009-05-13

Applicant: Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

Inventor： Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

IPC: B64C39/02 ,  B64C29/00 ,  F01P1/00

CPC classification number: B64C39/026 ,  B64D33/10 ,  F01P3/18

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20110133037A1

公开(公告)日：2011-06-09

申请号：US13001319

申请日：2009-05-13

Applicant: Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

Inventor： Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

IPC: B64C39/02 ,  B64C27/20 ,  B64C29/00 ,  B64C11/00 ,  B64C9/02 ,  B64C13/00 ,  B64C15/02

CPC classification number: B64C39/026 ,  B64C15/02

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US08695916B2

公开(公告)日：2014-04-15

申请号：US13001319

申请日：2009-05-13

Applicant: Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

Inventor： Glenn Neil Martin ,  Colin Cecil Dodge ,  Mark John Daniel

IPC: B64C39/02 ,  B64C29/00

CPC classification number: B64C39/026 ,  B64C15/02

Abstract: 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.

Abstract translation: 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。