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1. 发明授权

US07503277B2 Aerostat inflator 有权
标题翻译：气动充气机
公开(公告)号：US07503277B2
公开(公告)日：2009-03-17
申请号：US11539038
申请日：2006-10-05
申请人： James H. Boschma, Jr. , William Douglas McDaniel , Michael McNabb , Michael Ryder , Callum R. Sullivan , Glenn Martin Tierney , Peter K. Van Staagen
发明人： James H. Boschma, Jr. , William Douglas McDaniel , Michael McNabb , Michael Ryder , Callum R. Sullivan , Glenn Martin Tierney , Peter K. Van Staagen
IPC分类号： B64B1/40
CPC分类号： G09F21/06
摘要： A device for deploying an aerostat includes a cylindrical shaped container having an open end and a closed end and a center tube axially oriented in the container. A tapered disc is mounted for axial movement on the center tube, and it has a taper of increasing diameter in an axial direction from the closed end toward the open end of the container. In its operation, the tapered disc is held in a first position while a portion of the aerostat is loaded into the container. It is then moved to a second position wherein the tapered disc holds the loaded portion of the aerostat in the container. Thereafter, the disc is moved to a release position wherein the disc directs deployment of the aerostat from the container.
摘要翻译：用于展开空气净化器的装置包括具有开口端和封闭端的圆柱形容器和在容器中轴向定向的中心管。锥形盘被安装成用于在中心管上轴向运动，并且其具有从容器的封闭端朝向开口端的轴向方向上增加的直径的锥形。在其操作中，锥形盘保持在第一位置，同时一部分空气稳定器被装载到容器中。然后将其移动到第二位置，其中锥形盘保持容器中的空气稳定器的装载部分。此后，盘被移动到释放位置，其中盘指示空气调节器从容器的展开。

2. 发明申请

US20080083848A1 AEROSTAT INFLATOR 有权
公开(公告)号：US20080083848A1
公开(公告)日：2008-04-10
申请号：US11539038
申请日：2006-10-05
申请人： James H. Boschma , William Douglas McDaniel , Michael McNabb , Michael Ryder , Callum R. Sullivan , Glenn Martin Tierney , Peter K. Van Staagen
发明人： James H. Boschma , William Douglas McDaniel , Michael McNabb , Michael Ryder , Callum R. Sullivan , Glenn Martin Tierney , Peter K. Van Staagen
IPC分类号： B64B1/00
CPC分类号： G09F21/06
摘要： A device for deploying an aerostat includes a cylindrical shaped container having an open end and a closed end and a center tube axially oriented in the container. A tapered disc is mounted for axial movement on the center tube, and it has a taper of increasing diameter in an axial direction from the closed end toward the open end of the container. In its operation, the tapered disc is held in a first position while a portion of the aerostat is loaded into the container. It is then moved to a second position wherein the tapered disc holds the loaded portion of the aerostat in the container. Thereafter, the disc is moved to a release position wherein the disc directs deployment of the aerostat from the container.
摘要翻译：用于展开空气净化器的装置包括具有开口端和封闭端的圆柱形容器和在容器中轴向定向的中心管。锥形盘被安装成用于在中心管上轴向运动，并且其具有从容器的封闭端朝向开口端的轴向方向上增加的直径的锥形。在其操作中，锥形盘保持在第一位置，同时一部分空气稳定器被装载到容器中。然后将其移动到第二位置，其中锥形盘保持容器中的空气稳定器的装载部分。此后，盘被移动到释放位置，其中盘指示空气调节器从容器的展开。

3. 发明授权

US07275714B2 Airship docking mechanism 失效
公开(公告)号：US07275714B2
公开(公告)日：2007-10-02
申请号：US11263774
申请日：2005-11-01
申请人： Michael McNabb , Callum R. Sullivan , James H. Boschma, Jr. , Glenn Martin Tierney
发明人： Michael McNabb , Callum R. Sullivan , James H. Boschma, Jr. , Glenn Martin Tierney
IPC分类号： B64B1/02
CPC分类号： B64F1/14 , B64B1/32 , B64B1/66 , B64C11/006
摘要： A system and method for docking an airship to a mooring mast includes a thruster that is mounted to the fore end of the airship. When activated, the thruster generates a thrust vector that is substantially perpendicular to the longitudinal axis of the airship and is selectively directional. In particular, the configuration of the thruster can be changed to vary the direction of the thrust vector around the longitudinal axis to maneuver a connector on the thruster into contact with the mooring mast. Engagement of the connector to the mooring mast then docks the airship to the mooring mast.

4. 发明授权

US07163177B1 Airship ballast system 失效
标题翻译：飞艇镇流器系统
公开(公告)号：US07163177B1
公开(公告)日：2007-01-16
申请号：US11064313
申请日：2005-02-23
申请人： James H. Boschma, Jr. , Callum R. Sullivan , Michael McNabb
发明人： James H. Boschma, Jr. , Callum R. Sullivan , Michael McNabb
IPC分类号： B64B1/70
CPC分类号： B64B1/70
摘要： An airship ballast system includes an engine driven propeller and a cooling tube that is positioned coplanar with the propeller and outside its tip path. One end of the cooling tube is connected to receive exhaust gases from the engine while the other end is connected to a ballast tank. In operation, exhaust gases from the engine are cooled as they transit the cooling tube, and water condensed from the cooled exhaust gases is pumped to the ballast tank to maintain a ballast for the airship.
摘要翻译：飞艇镇流器系统包括发动机驱动的螺旋桨和冷却管，该冷却管定位成与螺旋桨共面并且在其末端路径外。冷却管的一端被连接以接收来自发动机的废气，而另一端连接到压载舱。在操作中，来自发动机的废气在其经过冷却管时被冷却，并且从冷却的废气冷凝的水被泵送到压载舱以维持飞艇的压载。

5. 发明授权

US07219854B2 Cycloidal hybrid advanced surface effects vehicle 失效
标题翻译：环状混合先进表面效果车
公开(公告)号：US07219854B2
公开(公告)日：2007-05-22
申请号：US11072219
申请日：2005-03-04
申请人： James H. Boschma, Jr. , Michael McNabb
发明人： James H. Boschma, Jr. , Michael McNabb
IPC分类号： B64C17/08 , B64C27/22
CPC分类号： B60V1/08 , B60V3/06 , B64B2201/00 , B64C11/006 , B64C35/00 , B64C39/005 , B64C39/04
摘要： A “wing in ground effect” aerial vehicle includes a wing mounted on a fuselage, and two cycloidal propulsion units for providing lift, thrust and longitudinal control. Additional lift is provided by a lighter-than-air gas such as helium contained in the fuselage. Operationally, the two cycloidal propulsion units and the volume of lighter-than-air gas are concertedly regulated to achieve “wing in ground effect” flight. Importantly, the two cycloidal propulsion units may operate in one of several modes, to include a curtate mode, a prolate mode, and a fixed-wing mode. Additionally, the vehicle may hover. Also, a thruster unit is mounted on the fuselage for providing forward thrust in combination with, or in lieu of, the two cycloidal propulsion units.
摘要翻译： “地面效应”飞行器包括安装在机身上的机翼，以及用于提供升力，推力和纵向控制的两个摆线推进单元。附加升降机由比机身中所含的诸如氦气的轻质气体提供。在行动上，两个摆线推进装置和轻型空气气体的体积协调一致，实现“地面效应”飞行。重要的是，两个摆线推进装置可以以多种模式中的一种运行，包括弯曲模式，伸长模式和固定翼模式。此外，车辆可能会悬停。此外，推进器单元安装在机身上，以提供与两个摆线推进装置组合或代替两个摆线推进装置的向前推力。

6. 发明申请

US20080110105A1 SYSTEM AND METHOD FOR ESTABLISHING A PROTECTED WORK AND STORAGE SPACE 审中-公开
标题翻译：建立保护性工作和存储空间的系统和方法
公开(公告)号：US20080110105A1
公开(公告)日：2008-05-15
申请号：US11558798
申请日：2006-11-10
申请人： James H. Boschma , Michael McNabb , Callum R. Sullivan , Gregory Gottlieb
发明人： James H. Boschma , Michael McNabb , Callum R. Sullivan , Gregory Gottlieb
IPC分类号： E04B2/14 , E04B7/08 , E04B1/35
CPC分类号： E04B1/3483 , E04B1/342 , E04B2001/34884 , E04H6/44
摘要： A storage facility for an airship includes a wall that is made from a plurality of box-like ISO containers. The wall surrounds an area on the ground, and a semicylindrical member is affixed to the top of the wall. This creates an enclosed volume over the area for the storage and protection of the airship. Buttresses for supporting the wall can be made from additional containers, and restraints can be used to secure the containers of the facility to each other.
摘要翻译：用于飞艇的存储设备包括由多个箱状ISO容器制成的壁。墙壁围绕地面上的一个区域，半圆柱形构件固定在墙壁的顶部。这将在该区域上创建一个封闭的容积，用于存储和保护飞艇。用于支撑墙壁的扶壁可以由附加的容器制成，并且可以使用约束来将设备的容器彼此固定。

7. 发明申请

US20060196992A1 Cycloidal hybrid advanced surface effects vehicle 失效
标题翻译：环状混合先进表面效果车
公开(公告)号：US20060196992A1
公开(公告)日：2006-09-07
申请号：US11072219
申请日：2005-03-04
申请人： James Boschma , Michael McNabb
发明人： James Boschma , Michael McNabb
IPC分类号： B64C27/22
CPC分类号： B60V1/08 , B60V3/06 , B64B2201/00 , B64C11/006 , B64C35/00 , B64C39/005 , B64C39/04
摘要： A “wing in ground effect” aerial vehicle includes a wing mounted on a fuselage, and two cycloidal propulsion units for providing lift, thrust and longitudinal control. Additional lift is provided by a lighter-than-air gas such as helium contained in the fuselage. Operationally, the two cycloidal propulsion units and the volume of lighter-than-air gas are concertedly regulated to achieve “wing in ground effect” flight. Importantly, the two cycloidal propulsion units may operate in one of several modes, to include a curtate mode, a prolate mode, and a fixed-wing mode. Additionally, the vehicle may hover. Also, a thruster unit is mounted on the fuselage for providing forward thrust in combination with, or in lieu of, the two cycloidal propulsion units.
摘要翻译： “地面效应”飞行器包括安装在机身上的机翼，以及用于提供升力，推力和纵向控制的两个摆线推进单元。附加升降机由比机身中所含的诸如氦气的轻质气体提供。在行动上，两个摆线推进装置和轻型空气气体的体积协调一致，实现“地面效应”飞行。重要的是，两个摆线推进装置可以以多种模式中的一种运行，包括弯曲模式，伸长模式和固定翼模式。此外，车辆可能会悬停。此外，推进器单元安装在机身上，以提供与两个摆线推进装置组合或代替两个摆线推进装置的向前推力。

8. 发明申请

US20070095974A1 Airship docking mechanism 失效
标题翻译：飞艇对接机制
公开(公告)号：US20070095974A1
公开(公告)日：2007-05-03
申请号：US11263774
申请日：2005-11-01
申请人： Michael McNabb , Callum Sullivan , James Boschma , Glenn Tierney
发明人： Michael McNabb , Callum Sullivan , James Boschma , Glenn Tierney
IPC分类号： B64B1/02 , B64F1/14
CPC分类号： B64F1/14 , B64B1/32 , B64B1/66 , B64C11/006
摘要： A system and method for docking an airship to a mooring mast includes a thruster that is mounted to the fore end of the airship. When activated, the thruster generates a thrust vector that is substantially perpendicular to the longitudinal axis of the airship and is selectively directional. In particular, the configuration of the thruster can be changed to vary the direction of the thrust vector around the longitudinal axis to maneuver a connector on the thruster into contact with the mooring mast. Engagement of the connector to the mooring mast then docks the airship to the mooring mast.
摘要翻译：将飞艇对接到系泊桅杆的系统和方法包括安装在飞艇前端的推进器。当被激活时，推进器产生基本上垂直于飞艇的纵轴的推力矢量，并且是选择性的。特别地，可以改变推进器的构造以改变围绕纵向轴线的推力矢量的方向，以操纵推进器上的连接器以与系泊桅杆接触。连接器与系泊桅杆的接合然后使飞艇停靠在系泊桅杆上。

9. 发明申请

US20070036641A1 Cycloidal turbine 审中-公开
标题翻译：旋流涡轮机
公开(公告)号：US20070036641A1
公开(公告)日：2007-02-15
申请号：US11200223
申请日：2005-08-09
申请人： Michael McNabb , James Boschma
发明人： Michael McNabb , James Boschma
IPC分类号： F03D7/06
CPC分类号： F03B17/067 , Y02E10/28
摘要： A water turbine for generating mechanical energy from a flowing fluid includes a rigid base that can be secured at a fixed position relative to the fluid flow. On the base, a substantially disk-shaped hub is rotatably mounted and at least one blade is positioned on the hub for rotation with the hub around a hub axis. Also, each blade is rotatably mounted onto the hub for rotation of the blade relative to the hub. For the turbine, each blade defines a chord line, and for each blade, a pitch angle can be defined as the instantaneous angle between the blade's chord line and the direction of fluid flow. The turbine also includes a sprocket and chain assembly to rotationally interconnect the hub to each blade. This assembly allows the pitch angle for each blade to be selectively varied during hub rotation.
摘要翻译：用于从流动流体产生机械能的水轮机包括刚性基座，其可以固定在相对于流体流动的固定位置。在基座上，可旋转地安装基本盘形的轮毂，并且至少一个叶片定位在轮毂上，以使轮毂围绕轮毂轴线旋转。此外，每个叶片可旋转地安装在轮毂上以相对于轮毂转动叶片。对于涡轮机，每个叶片限定弦线，并且对于每个叶片，俯仰角可以被定义为叶片的弦线和流体流动方向之间的瞬时角度。涡轮机还包括链轮和链条组件，以将轮毂与每个叶片旋转地互连。该组件允许在轮毂旋转期间每个叶片的俯仰角被选择性地变化。

10. 发明申请

US20070001054A1 AIRSHIP BALLAST SYSTEM 失效
标题翻译： AIRSHIP BALLAST系统
公开(公告)号：US20070001054A1
公开(公告)日：2007-01-04
申请号：US11064313
申请日：2005-02-23
申请人： James Boschma , Callum Sullivan , Michael McNabb
发明人： James Boschma , Callum Sullivan , Michael McNabb
IPC分类号： B64B1/58
CPC分类号： B64B1/70
摘要： An airship ballast system includes an engine driven propeller and a cooling tube that is positioned coplanar with the propeller and outside its tip path. One end of the cooling tube is connected to receive exhaust gases from the engine while the other end is connected to a ballast tank. In operation, exhaust gases from the engine are cooled as they transit the cooling tube, and water condensed from the cooled exhaust gases is pumped to the ballast tank to maintain a ballast for the airship.
摘要翻译：飞艇镇流器系统包括发动机驱动的螺旋桨和冷却管，该冷却管定位成与螺旋桨共面并且在其末端路径外。冷却管的一端被连接以接收来自发动机的废气，而另一端连接到压载舱。在操作中，来自发动机的废气在其经过冷却管时被冷却，并且从冷却的废气冷凝的水被泵送到压载舱以维持飞艇的压载。

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