公开(公告)号：WO2022098741A1

公开(公告)日：2022-05-12

申请号：PCT/US2021/057875

申请日：2021-11-03

Applicant: KOPP, Ken E. ,  WOOD, Ryan S.

Inventor： KOPP, Ken E. ,  WOOD, Ryan S.

IPC: G21B1/05 ,  G21B1/11 ,  G21B1/21

Abstract: An aneutronic fusion apparatus is disclosed that uses a lithium ammonia fuel mixture as a supercritical fusion fuel of solvated electrons thereby lowering the coulomb barrier to achieve small scale fusion. The integration of alpha sources, magnetic confinement, electrical arcing, and pressure allow for fusion events and chain reactions. The process operates in a cyclical fashion fusing atoms then fizzling creating a diamagnetic pressure in the plasma whose output energy is inductively harvested. Atypical embodiment device includes: a chamber; a magnetic confinement coil surrounding at least a portion of the chamber; electrodes extending into the chamber defining a gap. A device having bidirectional electrode rod arrays has a first array with rods extending in a first direction, a last electrode rod array having rods extending in a second direction opposite the first direction, and one or more intervening electrode rod arrays each having rods extending in both directions.

公开(公告)号：WO2011005858A2

公开(公告)日：2011-01-13

申请号：PCT/US2010/041205

申请日：2010-07-07

Applicant: FRONTLINE AEROSPACE, INC. ,  WOOD, Ryan S. ,  STEWARD, W. Gene ,  WATERS, Mark

Inventor： WOOD, Ryan S. ,  STEWARD, W. Gene ,  WATERS, Mark

IPC: F02C7/12 ,  F02C3/04 ,  F01D25/12 ,  F01P3/12

CPC classification number: F01P3/12 ,  F01D25/12 ,  F01D25/145 ,  F01P2060/12 ,  F02C7/143 ,  F02C7/18 ,  Y02T50/675

Abstract: Systems, apparatuses and methods ("utilities") for use in "internally" cooling the compressor of a gas turbine engine so as to approximate isothermal compression and thereby increase the power and/or efficiency of the engine. In one arrangement, a "cooling jacket" or heat exchanger having coolant circulating or passing therethrough may be mounted around an outer surface of the compressor to absorb heat or thermal energy generated from the compressor. In another arrangement, the stator blades of the compressor may include passages through which a coolant may be circulated or passed to absorb heat from air passing through the compressor.

Abstract translation: 在“内部”使用的系统，设备和方法（“公用设施”）可以用于“内部” 冷却燃气涡轮发动机的压缩机以接近等温压缩并由此增加发动机的功率和/或效率。 在一种布置中，“冷却套” 或具有循环或穿过其中的冷却剂的热交换器可安装在压缩机的外表面周围以吸收从压缩机产生的热或热能。 在另一种布置中，压缩机的定子叶片可以包括通道，冷却剂可以通过该通道循环或通过以从通过压缩机的空气吸收热量。

公开(公告)号：WO2010053961A2

公开(公告)日：2010-05-14

申请号：PCT/US2009/063234

申请日：2009-11-04

Applicant: FRONTLINE AEROSPACE, INC ,  WOOD, Ryan S.

Inventor： WOOD, Ryan S.

IPC: F03D1/00 ,  F03D11/02

CPC classification number: F03D1/025 ,  F01D1/24 ,  F03D1/04 ,  F03D9/25 ,  F03D15/00 ,  F03D15/10 ,  F05B2240/40 ,  F05B2260/4031 ,  F05D2240/40 ,  F05D2260/4031 ,  Y02E10/72

Abstract: Wind turbine devices are presented that use counter rotating rotor assemblies 24, 34 in a horizontal axis wind turbine (HAWT) arrangement. This reduces the torque applied to the HAWT 10 thereby reducing the structural requirements of a wind energy generation system. Additionally, the counter rotating rotor assemblies 24, 34 cooperatively rotate an output shaft 50. In one arrangement, this shaft 50 is a vertical shaft which allows removing power generation equipment 60 from the axis of rotation of a HAWT to a position below the wind turbine and/or located on the ground.

Abstract translation: 提出了风力涡轮机装置，其使用水平轴风力涡轮机（HAWT）布置中的反向旋转转子组件24,34。 这降低了施加到HAWT 10的转矩，从而降低了风能发电系统的结构要求。 另外，反转转子组件24,34协同地旋转输出轴50.在一种布置中，该轴50是垂直轴，其允许将发电设备60从HAWT的旋转轴线移除到风力涡轮机下方的位置 和/或位于地面上。

公开(公告)号：WO2010036419A2

公开(公告)日：2010-04-01

申请号：PCT/US2009/046601

申请日：2009-06-08

Applicant: FRONTLINE AEROSPACE, INC. ,  WOOD, Ryan, S. ,  CUMMINGS, Donald, B. ,  HALL, David, W.

Inventor： WOOD, Ryan, S. ,  CUMMINGS, Donald, B. ,  HALL, David, W.

IPC: B64C29/00 ,  B64C27/22 ,  B64C27/24

CPC classification number: B64C29/0025 ,  B64C39/024 ,  B64C39/068 ,  B64C2201/021 ,  B64C2201/088 ,  B64C2201/162

Abstract: A vertical take off and landing (VTOL) aircraft (100), which may be a UAV aircraft, is disclosed. The VTOL includes a ducted fan assembly (120) that provides the capability of vertical takeoff and landing, hovering and traveling of slow speeds. In addition, a pusher fan assembly (140) of the VTOL permits high-speed forward flight, which increases the range of the aircraft.

Abstract translation: 公开了可以是UAV飞机的垂直起降（VTOL）飞机（100）。 VTOL包括一个涵道风扇组件（120），可提供垂直起飞和着陆，悬停和低速行驶的能力。 另外，VTOL的推进器风扇组件（140）允许高速向前飞行，这增加了飞机的航程。

公开(公告)号：WO2010036419A3

公开(公告)日：2010-06-03

申请号：PCT/US2009046601

申请日：2009-06-08

Applicant: FRONTLINE AEROSPACE INC ,  WOOD RYAN S ,  CUMMINGS DONALD B ,  HALL DAVID W

Inventor： WOOD RYAN S ,  CUMMINGS DONALD B ,  HALL DAVID W

IPC: B64C29/00 ,  B64C27/22 ,  B64C27/24

CPC classification number: B64C29/0025 ,  B64C39/024 ,  B64C39/068 ,  B64C2201/021 ,  B64C2201/088 ,  B64C2201/162

Abstract: A vertical take off and landing (VTOL) aircraft (100), which may be a UAV aircraft, is disclosed. The VTOL includes a ducted fan assembly (120) that provides the capability of vertical takeoff and landing, hovering and traveling of slow speeds. In addition, a pusher fan assembly (140) of the VTOL permits high-speed forward flight, which increases the range of the aircraft.

Abstract translation: 披露了可能是无人机的垂直起降（VTOL）飞机（100）。 VTOL包括一个风扇风扇组件（120），它提供垂直起飞和降落，悬停和慢速行驶的能力。 此外，垂直起落架的推进器风扇组件（140）允许高速向前飞行，这增加了飞行器的范围。

公开(公告)号：WO2011005858A3

公开(公告)日：2011-06-16

申请号：PCT/US2010041205

申请日：2010-07-07

Applicant: FRONTLINE AEROSPACE INC ,  WOOD RYAN S ,  STEWARD W GENE ,  WATERS MARK

Inventor： WOOD RYAN S ,  STEWARD W GENE ,  WATERS MARK

IPC: F02C7/12 ,  F01D25/12 ,  F01P3/12 ,  F02C3/04

CPC classification number: F01P3/12 ,  F01D25/12 ,  F01D25/145 ,  F01P2060/12 ,  F02C7/143 ,  F02C7/18 ,  Y02T50/675

Abstract: Systems, apparatuses and methods ("utilities") for use in "internally" cooling the compressor of a gas turbine engine so as to approximate isothermal compression and thereby increase the power and/or efficiency of the engine. In one arrangement, a "cooling jacket" or heat exchanger having coolant circulating or passing therethrough may be mounted around an outer surface of the compressor to absorb heat or thermal energy generated from the compressor. In another arrangement, the stator blades of the compressor may include passages through which a coolant may be circulated or passed to absorb heat from air passing through the compressor.

Abstract translation: 用于“内部”冷却燃气涡轮发动机的压缩机以便近似等温压缩并由此增加发动机的功率和/或效率的系统，装置和方法（“实用程序”）。 在一种布置中，可以在压缩机的外表面周围安装有冷却剂循环或通过的“冷却套”或热交换器，以吸收由压缩机产生的热量或热能。 在另一种布置中，压缩机的定子叶片可以包括通道，冷却剂可以通过该通道循环或通过，以吸收来自通过压缩机的空气的热量。

公开(公告)号：WO2010053961A3

公开(公告)日：2010-09-16

申请号：PCT/US2009063234

申请日：2009-11-04

Applicant: FRONTLINE AEROSPACE INC ,  WOOD RYAN S

Inventor： WOOD RYAN S

IPC: F03D1/00 ,  F03D11/02

CPC classification number: F03D1/025 ,  F01D1/24 ,  F03D1/04 ,  F03D15/00 ,  F05B2240/40 ,  F05B2260/4031 ,  F05D2240/40 ,  F05D2260/4031 ,  Y02E10/72

Abstract: Wind turbine devices are presented that use counter rotating rotor assemblies 24, 34 in a horizontal axis wind turbine (HAWT) arrangement. This reduces the torque applied to the HAWT 10 thereby reducing the structural requirements of a wind energy generation system. Additionally, the counter rotating rotor assemblies 24, 34 cooperatively rotate an output shaft 50. In one arrangement, this shaft 50 is a vertical shaft which allows removing power generation equipment 60 from the axis of rotation of a HAWT to a position below the wind turbine and/or located on the ground.

Abstract translation: 呈现了在水平轴风力涡轮机（HAWT）装置中使用反向转动转子组件24,34的风力涡轮机装置。 这降低了施加到HAWT 10的扭矩，从而降低了风力发电系统的结构要求。 此外，反向转动转子组件24,34协同地转动输出轴50.在一种布置中，该轴50是垂直轴，其允许将发电设备60从HAWT的旋转轴线移除到风力涡轮机下方的位置 和/或位于地面上。