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1. 发明申请

WO2010104601A1 HEAT ENGINE WITH REGENERATOR AND TIMED GAS EXCHANGE 审中-公开
标题翻译：具有再生器和定时气体交换的热发动机
公开(公告)号：WO2010104601A1
公开(公告)日：2010-09-16
申请号：PCT/US2010/000758
申请日：2010-03-12
申请人： SEALE, Joseph, B. , BERGSTROM, Gary
发明人： SEALE, Joseph, B. , BERGSTROM, Gary
IPC分类号： F02K5/00
CPC分类号： F02G1/0435 , F01K17/06 , F01K19/10
摘要： A Stirling-like system incorporating a heater, a displacer and a regenerator is intermittently coupled to an external system via valves, providing pneumatic power while ridding waste heat. The external system is commonly a Rankine cycle, sharing the working fluid of the Stirling-like system, and can be used for heat pumping, distillation and drying. The Stirling working fluid and the Rankine working fluid are the same material and are exchanged between the two systems. A dual Stirling-like system mates a heat engine with a heat pump, sharing the same pressure-containment, with the dual system intermittently coupled to external environments for convective exchange of heat and cold.
摘要翻译：包含加热器，置换器和再生器的斯特林式系统通过阀间歇地耦合到外部系统，在消除废热的同时提供气动功率。外部系统通常是兰金循环，共享斯特林式系统的工作流体，可用于热泵，蒸馏和干燥。斯特林工作流体和兰金工作流体是相同的材料，并在两个系统之间交换。双重斯特林式系统将热力发动机与热泵相配合，共享相同的压力容纳，双重系统间歇地耦合到外部环境，用于对流换热和冷热。

2. 发明申请

WO2016109408A1 ROTARY WING VTOL WITH FIXED WING FORWARD FLIGHT MODE 审中-公开
标题翻译：带有固定箭头的旋转翼型垂直起飞模式
公开(公告)号：WO2016109408A1
公开(公告)日：2016-07-07
申请号：PCT/US2015/067630
申请日：2015-12-28
申请人： SEALE, Joseph, B. , SLOAN, Walker, M.
发明人： SEALE, Joseph, B. , SLOAN, Walker, M.
IPC分类号： B64C27/24
CPC分类号： B64C27/24 , B64C27/16 , B64C27/18 , B64C29/0033
摘要： An aircraft's two wings and joined thruster propellers or turbines serve as rotary wings in helicopter mode and as fixed wings in airplane mode. The thrusters along the wingspans or at the wing tips drive both rotary wing rotation and airplane flight. Large-angle controlled feathering about the pitch change axes of the left and right wings and thrusters allows them to rotate, relative to each other, between facing and thrusting forward in the same direction for airplane flight or facing and thrusting oppositely for helicopter flight. Optional controls include: helicopter cyclic and collective pitch; airplane roll by differential wing pitch; yaw by differential prop thrust; fuselage pitch by wing pitch change and prop thrust change interacting with an underslung craft e.g.; and fuselage yaw control independent of rotor rotation via a powered rotary mast coupling or a tail responsive to rotor downwash. A teetering rotor hub is a further option.
摘要翻译：一架飞机的两个翼和联合的推进器螺旋桨或涡轮机作为直升机模式的旋转翼和飞机模式下的固定翼。沿翼展或翼尖的推进器驱动旋转翼旋转和飞机飞行。围绕左右翼和推进器的俯仰变化轴的大角度控制羽化使得它们能够相对于彼此在相同方向上向前推动以进行飞机飞行或相对于直升机飞行而相反地旋转。可选控制包括：直升机循环和集体音调; 飞行器通过差速机翼俯仰; 偏差由差速推力推力; 机翼间距通过机翼桨距改变和支撑推力变化与下冲的技术相互作用。和机身偏航控制，独立于转子旋转，通过动力旋转柱杆联轴器或响应于转子下冲洗的尾部。另一种选择是转向轮毂。

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