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1. 发明申请

US20190176981A1 Vertical Takeoff and Landing ("VTOL") Aircraft 审中-公开
公开(公告)号：US20190176981A1
公开(公告)日：2019-06-13
申请号：US15836771
申请日：2017-12-08
申请人： Ian Todd Gaillimore , Kenneth Dean Driver
发明人： Ian Todd Gaillimore , Kenneth Dean Driver
IPC分类号： B64C29/04 , B64C25/66 , B64C3/14 , B64C3/16 , B64C3/32 , B64C39/08
摘要： The invention is to an optionally piloted aircraft that can takeoff and land conventionally or vertically, and can convert between the two. The aircraft is immune to one or more engine failures during vertical flight through multiple engines and the use of a virtual nozzle. Aerodynamic controls are similarly redundant. Hovering flight is enabled with a novel stabilization system. Long range efficient cruise is achieved by turning off some engines in flight and sealing them into an aerodynamic fairing to achieve low drag. The resulting aircraft is capable of CTOL and VTOL, and is capable of converting between the two modes while in the air or on the ground. The aircraft can also be easily taxied on the ground in the conventional manner. Automatic controls considerably reduce the amount of training a pilot needs to fly and land the aircraft in either VTOL or CTOL mode.

2. 发明授权

US09387929B2 Vertical takeoff and landing (“VTOL”) aircraft 有权
标题翻译：垂直起飞和着陆（“VTOL”）飞机
公开(公告)号：US09387929B2
公开(公告)日：2016-07-12
申请号：US13843163
申请日：2013-03-15
申请人： Ian Todd Gaillimore , Kenneth Dean Driver
发明人： Ian Todd Gaillimore , Kenneth Dean Driver
IPC分类号： B64C39/12 , B64C29/00
CPC分类号： B64C39/12 , B64C29/0016 , B64C29/0066
摘要： The invention is to an optionally piloted aircraft that can takeoff and land conventionally or vertically, and can convert between the two. The aircraft is immune to one or more engine failures during vertical flight through multiple engines and the use of a virtual nozzle. Aerodynamic controls are similarly redundant. Hovering flight is enabled with a novel stabilization system. Long range efficient cruise is achieved by turning off some engines in flight and sealing them into an aerodynamic fairing to achieve low drag. The resulting aircraft is capable of CTOL and VTOL, and is capable of converting between the two modes while in the air or on the ground. The aircraft can also be easily taxied on the ground in the conventional manner. Automatic controls considerably reduce the amount of training a pilot needs to fly and land the aircraft in either VTOL or CTOL mode.
摘要翻译：本发明涉及一种可任意驾驶的飞行器，其可以通常地或垂直地起飞和降落，并且可以在两者之间进行转换。飞机在通过多台发动机的垂直飞行和使用虚拟喷嘴的一个或多个发动机故障中是免疫的。空气动力学控制也是相似的。悬停飞行启用了一个新的稳定系统。通过关闭飞行中的一些发动机并将其密封成气动整流罩以实现低阻力来实现远程有效巡航。所得飞机能够进行CTOL和VTOL，并且能够在空中或地面上在两种模式之间进行转换。飞机也可以以常规方式轻松地在地面上进行运送。自动控制大大减少了飞行员以垂直起降或CTOL模式飞行和着陆飞机所需的训练量。

3. 发明申请

US20170129604A1 Vertical Takeoff and Landing ("VTOL") Aircraft 审中-公开
公开(公告)号：US20170129604A1
公开(公告)日：2017-05-11
申请号：US15207369
申请日：2016-07-11
申请人： Ian Todd Gaillimore , Kenneth Dean Driver
发明人： Ian Todd Gaillimore , Kenneth Dean Driver
IPC分类号： B64C39/12 , B64C29/00
CPC分类号： B64C39/12 , B64C29/0016 , B64C29/0066
摘要： The invention is to an optionally piloted aircraft that can takeoff and land conventionally or vertically, and can convert between the two. The aircraft is immune to one or more engine failures during vertical flight through multiple engines and the use of a virtual nozzle. Aerodynamic controls are similarly redundant. Hovering flight is enabled with a novel stabilization system. Long range efficient cruise is achieved by turning off some engines in flight and sealing them into an aerodynamic fairing to achieve low drag. The resulting aircraft is capable of CTOL and VTOL, and is capable of converting between the two modes while in the air or on the ground. The aircraft can also be easily taxied on the ground in the conventional manner. Automatic controls considerably reduce the amount of training a pilot needs to fly and land the aircraft in either VTOL or CTOL mode.

4. 发明申请

US20140339354A1 Vertical Takeoff and Landing ("VTOL") Aircraft 有权
标题翻译：垂直起飞和着陆（“垂直起降”）飞机
公开(公告)号：US20140339354A1
公开(公告)日：2014-11-20
申请号：US13843163
申请日：2013-03-15
申请人： Ian Todd Gaillimore , Kenneth Dean Driver
发明人： Ian Todd Gaillimore , Kenneth Dean Driver
IPC分类号： B64C29/00
CPC分类号： B64C39/12 , B64C29/0016 , B64C29/0066
摘要： The invention is to an optionally piloted aircraft that can takeoff and land conventionally or vertically, and can convert between the two. The aircraft is immune to one or more engine failures during vertical flight through multiple engines and the use of a virtual nozzle. Aerodynamic controls are similarly redundant. Hovering flight is enabled with a novel stabilization system. Long range efficient cruise is achieved by turning off some engines in flight and sealing them into an aerodynamic fairing to achieve low drag. The resulting aircraft is capable of CTOL and VTOL, and is capable of converting between the two modes while in the air or on the ground. The aircraft can also be easily taxied on the ground in the conventional manner. Automatic controls considerably reduce the amount of training a pilot needs to fly and land the aircraft in either VTOL or CTOL mode.
摘要翻译：本发明涉及一种可任意驾驶的飞行器，其可以通常地或垂直地起飞和降落，并且可以在两者之间进行转换。飞机在通过多台发动机的垂直飞行和使用虚拟喷嘴的一个或多个发动机故障中是免疫的。空气动力学控制也是相似的。悬停飞行启用了一个新的稳定系统。通过关闭飞行中的一些发动机并将其密封成气动整流罩以实现低阻力来实现远程有效巡航。所得飞机能够进行CTOL和VTOL，并且能够在空中或地面上在两种模式之间进行转换。飞机也可以以常规方式轻松地在地面上进行运送。自动控制大大减少了飞行员以垂直起降或CTOL模式飞行和着陆飞机所需的训练量。

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