公开(公告)号：US08662944B2

公开(公告)日：2014-03-04

申请号：US13429267

申请日：2012-03-23

Applicant: Mark Allan Page ,  Christopher John Page ,  Matthew Robert McCue ,  Michael Karl Kohl ,  Patrick Quincey Stout ,  Neil Wayne Roberts

Inventor： Mark Allan Page ,  Christopher John Page ,  Matthew Robert McCue ,  Michael Karl Kohl ,  Patrick Quincey Stout ,  Neil Wayne Roberts

IPC: B60F3/00

CPC classification number: B60F3/0007 ,  B60F3/0038 ,  B60F3/0092 ,  B60H1/24 ,  B60H3/0007 ,  B60L9/00 ,  B63G8/18 ,  B63G8/36 ,  B63H21/17

Abstract: A vehicle is provided that is amphibious to include submersible operations. The vehicle has wings configured to generate a sufficient dive force to oppose buoyancy of the vehicle, when desired, which are disposed on opposing sides of a central hull. The vehicle is configured to enable easy transition from land operations to water operations, to include water surface travel as well as submerged travel.

Abstract translation: 提供一种水陆两用的车辆，包括潜水作业。 车辆具有被构造成产生足够的潜水以抵抗车辆的浮力的翼，当需要时，它们设置在中央船体的相对侧上。 该车辆配置为能够轻松地从陆地作业过渡到水上作业，包括水面旅行以及淹没的旅行。

公开(公告)号：US20130078876A1

公开(公告)日：2013-03-28

申请号：US13429267

申请日：2012-03-23

Applicant: Mark Allan Page ,  Christopher John Page ,  Matthew Robert McCue ,  Michael Karl Kohl ,  Patrick Quincey Stout ,  Neil Wayne Roberts

Inventor： Mark Allan Page ,  Christopher John Page ,  Matthew Robert McCue ,  Michael Karl Kohl ,  Patrick Quincey Stout ,  Neil Wayne Roberts

IPC: B60F3/00 ,  B63H21/17

CPC classification number: B60F3/0007 ,  B60F3/0038 ,  B60F3/0092 ,  B60H1/24 ,  B60H3/0007 ,  B60L9/00 ,  B63G8/18 ,  B63G8/36 ,  B63H21/17

Abstract: A vehicle is provided that is amphibious to include submersible operations. The vehicle has wings configured to generate a sufficient dive force to oppose buoyancy of the vehicle, when desired, which are disposed on opposing sides of a central hull. The vehicle is configured to enable easy transition from land operations to water operations, to include water surface travel as well as submerged travel.

Abstract translation: 提供一种水陆两用的车辆，包括潜水作业。 车辆具有被构造成产生足够的潜水以抵抗车辆的浮力的翼，当需要时，它们设置在中央船体的相对侧上。 该车辆配置为能够轻松地从陆地作业过渡到水上作业，包括水面旅行以及淹没的旅行。

公开(公告)号：US20120248259A1

公开(公告)日：2012-10-04

申请号：US13429156

申请日：2012-03-23

Applicant: Mark Allan Page ,  Matthew Robert McCue ,  Robert Anthony Godlasky

Inventor： Mark Allan Page ,  Matthew Robert McCue ,  Robert Anthony Godlasky

IPC: B64C27/24

CPC classification number: B64C29/02 ,  B64C39/024 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/162 ,  B64C2201/165

Abstract: An aircraft for use in fixed wing flight mode and rotor flight mode is provided. The aircraft can include a fuselage, wings, and a plurality of engines. The fuselage can comprise a wing attachment region further comprising a rotating support. A rotating section can comprise a rotating support and the wings, with a plurality of engines attached to the rotating section. In a rotor flight mode, the rotating section can rotate around a longitudinal axis of the fuselage providing lift for the aircraft similar to the rotor of a helicopter. In a fixed wing flight mode, the rotating section does not rotate around a longitudinal axis of the fuselage, providing lift for the aircraft similar to a conventional airplane. The same engines that provide torque to power the rotor in rotor flight mode also power the aircraft in fixed wing flight mode.

Abstract translation: 提供了一种用于固定翼飞行模式和转子飞行模式的飞机。 飞机可以包括机身，机翼和多个发动机。 机身可以包括还包括旋转支撑件的翼连接区域。 旋转部分可以包括旋转支撑件和机翼，其中多个发动机附接到旋转部分。 在转子飞行模式中，旋转部分可以围绕机身的纵向轴线旋转，为类似于直升机的转子的飞机提供升降机。 在固定翼飞行模式中，旋转部分不围绕机身的纵向轴线旋转，为类似于常规飞机的飞机提供升降机。 在转子飞行模式下为转子提供动力的相同发动机也为固定翼飞行模式下的飞机提供动力。

公开(公告)号：US08991751B2

公开(公告)日：2015-03-31

申请号：US13429156

申请日：2012-03-23

Applicant: Mark Allan Page ,  Matthew Robert McCue ,  Robert Anthony Godlasky

Inventor： Mark Allan Page ,  Matthew Robert McCue ,  Robert Anthony Godlasky

IPC: B64C29/02 ,  B64C39/02

CPC classification number: B64C29/02 ,  B64C39/024 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/162 ,  B64C2201/165

Abstract: An aircraft for use in fixed wing flight mode and rotor flight mode is provided. The aircraft can include a fuselage, wings, and a plurality of engines. The fuselage can comprise a wing attachment region further comprising a rotating support. A rotating section can comprise a rotating support and the wings, with a plurality of engines attached to the rotating section. In a rotor flight mode, the rotating section can rotate around a longitudinal axis of the fuselage providing lift for the aircraft similar to the rotor of a helicopter. In a fixed wing flight mode, the rotating section does not rotate around a longitudinal axis of the fuselage, providing lift for the aircraft similar to a conventional airplane. The same engines that provide torque to power the rotor in rotor flight mode also power the aircraft in fixed wing flight mode.

Abstract translation: 提供了一种用于固定翼飞行模式和转子飞行模式的飞机。 飞机可以包括机身，机翼和多个发动机。 机身可以包括还包括旋转支撑件的翼连接区域。 旋转部分可以包括旋转支撑件和机翼，其中多个发动机附接到旋转部分。 在转子飞行模式中，旋转部分可以围绕机身的纵向轴线旋转，为类似于直升机的转子的飞机提供升降机。 在固定翼飞行模式中，旋转部分不围绕机身的纵向轴线旋转，为类似于常规飞机的飞机提供升降机。 在转子飞行模式下为转子提供动力的相同发动机也为固定翼飞行模式下的飞机提供动力。