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1. 发明授权

US09969487B2 Multiple controllable airflow modification devices 有权
公开(公告)号：US09969487B2
公开(公告)日：2018-05-15
申请号：US14887139
申请日：2015-10-19
申请人： Tamarack Aerospace Group, Inc.
发明人： Nicholas R. Guida
IPC分类号： B64C23/06 , B64C13/16
CPC分类号： B64C23/069 , B64C13/16 , B64C23/076 , Y02T50/164
摘要： An active wing extension includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes multiple controllable airflow modification devices coupled thereto. By virtue of having multiple controllable airflow modification devices, the wing extension is capable of adjusting control surfaces of the multiple controllable airflow modification devices in response to in-flight conditions, to reduce wing loads, improve wing fatigue characteristics, increase range, and/or increase efficiency.

2. 发明申请

US20160009378A1 ADJUSTABLE LIFT MODIFICATION WINGTIP 审中-公开
标题翻译：可调升力修改WINGTIP
公开(公告)号：US20160009378A1
公开(公告)日：2016-01-14
申请号：US14097122
申请日：2013-12-04
申请人： Tamarack Aerospace Group, Inc.
发明人： Nicholas R. Guida
IPC分类号： B64C23/06 , B64C13/16 , B64C5/10
摘要： An adjustable lift modification wingtip may be attached to a baseline wing of an aircraft. The adjustable lift modification wingtip may comprise a horizontal portion including a control surface and a vertical portion coupled to the horizontal portion. The vertical portion may move about an axis that may be substantially perpendicular to the horizontal portion. The control surface and the vertical portion may be adjusted in conjunction to increase wing efficiency at a flight condition.
摘要翻译：可调节的升降机修剪翼尖可以附接到飞行器的基准翼。可调节升降机修剪翼尖可以包括水平部分，其包括控制表面和连接到水平部分的垂直部分。垂直部分可以围绕可以基本上垂直于水平部分的轴线移动。可以结合调整控制表面和垂直部分以在飞行状态下增加机翼效率。

3. 发明申请

US20120187251A1 Multiple Controllable Airflow Modification Devices 有权
标题翻译：多个可控气流修改装置
公开(公告)号：US20120187251A1
公开(公告)日：2012-07-26
申请号：US13438614
申请日：2012-04-03
申请人： Nicholas R. Guida
发明人： Nicholas R. Guida
IPC分类号： B64C23/06 , B64C13/02 , B64C3/58
CPC分类号： B64C23/069 , B64C13/16 , B64C23/076 , Y02T50/164
摘要： An active wing extension includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes multiple controllable airflow modification devices coupled thereto. By virtue of having multiple controllable airflow modification devices, the wing extension is capable of adjusting control surfaces of the multiple controllable airflow modification devices in response to in-flight conditions, to reduce wing loads, improve wing fatigue characteristics, increase range, and/or increase efficiency.
摘要翻译：主动翼延伸部包括基本上平行于飞行器的翼的主体部分，好像它是机翼的延伸部分。主体部分可附接到飞行器机翼并且包括耦合到其上的多个可控气流改变装置。由于具有多个可控气流改变装置，机翼延伸部能够响应于飞行中的条件来调节多个可控气流改变装置的控制表面，以减少机翼负载，改善机翼疲劳特性，增加范围和/或提高效率。

4. 发明授权

US07900877B1 Active winglet 有权
标题翻译：活动小翼
公开(公告)号：US07900877B1
公开(公告)日：2011-03-08
申请号：US12890557
申请日：2010-09-24
申请人： Nicholas R. Guida
发明人： Nicholas R. Guida
IPC分类号： B64C9/00 , B64C23/06
CPC分类号： B64C23/065 , B64C13/16 , B64C23/076 , Y02T50/164
摘要： An active winglet includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing, and an angled portion that projects at an upward angle from the body portion. The body portion is attachable to an aircraft wing and includes a controllable airflow modification device coupled thereto. By virtue of having a controllable airflow modification device, the winglet is capable of adjusting a control surface of the controllable airflow modification device in response to in-flight conditions, to reduce wing loads, increase range, and increase efficiency.
摘要翻译：活动小翼包括基本上平行于飞行器的机翼的主体部分，如同它是机翼的延伸部分，以及从身体部分以向上的角度突出的倾斜部分。主体部分可附接到飞行器机翼并且包括耦合到其上的可控气流改变装置。由于具有可控气流改变装置，小翼能够响应于飞行中的条件来调节可控气流改变装置的控制表面，以减少机翼载荷，增加范围并提高效率。

5. 发明公开

US20240367778A1 MULTIPLE CONTROLLABLE AIRFLOW MODIFICATION DEVICES 审中-公开
公开(公告)号：US20240367778A1
公开(公告)日：2024-11-07
申请号：US18443869
申请日：2024-02-16
申请人： Tamarack Aerospace Group, Inc.
发明人： Nicholas R. Guida
IPC分类号： B64C23/06 , B64C13/16
CPC分类号： B64C23/069 , B64C13/16 , B64C23/076 , Y02T50/10
摘要： An active wing extension includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes multiple controllable airflow modification devices coupled thereto. By virtue of having multiple controllable airflow modification devices, the wing extension is capable of adjusting control surfaces of the multiple controllable airflow modification devices in response to in-flight conditions, to reduce wing loads, improve wing fatigue characteristics, increase range, and/or increase efficiency.

6. 发明授权

US11884383B2 Active winglet 有权
公开(公告)号：US11884383B2
公开(公告)日：2024-01-30
申请号：US16694875
申请日：2019-11-25
申请人： Tamarack Aerospace Group, Inc.
发明人： Nicholas R. Guida
IPC分类号： B64C23/06 , B64C13/16
CPC分类号： B64C23/076 , B64C13/16 , B64C23/065 , Y02T50/10
摘要： An active winglet includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes a controllable airflow modification device coupled thereto. By virtue of having a controllable airflow modification device, the winglet is capable of adjusting a control surface of the controllable airflow modification device in response to in-flight conditions, to reduce wing loads, increase range, and/or increase efficiency.

7. 发明申请

US20150151831A1 Airflow Interrupting Devices 审中-公开
标题翻译：气流中断装置
公开(公告)号：US20150151831A1
公开(公告)日：2015-06-04
申请号：US14097159
申请日：2013-12-04
申请人： Tamarack Aerospace Group, Inc.
发明人： Nicholas R. Guida
IPC分类号： B64C23/06
CPC分类号： B64C23/069 , B64C2003/148 , Y02T50/12 , Y02T50/164
摘要： A flow interrupting device may cause a flow to separate from a wingtip device at a desired angle of attack. The flow interrupting device may be coupled to a leading edge of a wingtip device where a flow disruptor may be configured to alleviate a load on the wingtip device. The flow disrupter may comprise an edge that extends into a boundary layer at a threshold angle of attack that may disrupt the boundary layer and cause a flow to separate from the wingtip device. This separated flow may reduce stresses experienced by the wingtip device and wing during various flight conditions where a transverse flow is encountered.
摘要翻译：流动中断装置可以使得流动以所需的攻角与翼尖装置分离。流动中断装置可以联接到翼尖装置的前缘，其中流动破坏器可以被配置为减轻翼尖装置上的负载。流动扰乱器可以包括以阈值迎角延伸到边界层中的边缘，其可能破坏边界层并导致流动与翼尖装置分离。这种分离的流动可以减少在遇到横向流动的各种飞行条件期间翼尖装置和机翼所经受的应力。

8. 发明申请

US20150008291A1 Active Winglet 有权
标题翻译：活跃翼
公开(公告)号：US20150008291A1
公开(公告)日：2015-01-08
申请号：US14222437
申请日：2014-03-21
申请人： Tamarack Aerospace Group, Inc.
发明人： Nicholas R. Guida
IPC分类号： B64C23/06 , B64C13/20 , B64C13/36 , B64C13/16 , B64C13/00 , B64C13/28
CPC分类号： B64C23/065 , B64C13/16 , B64C23/076 , Y02T50/164
摘要： An active winglet includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes a controllable airflow modification device coupled thereto. By virtue of having a controllable airflow modification device, the winglet is capable of adjusting a control surface of the controllable airflow modification device in response to in-flight conditions, to reduce wing loads, increase range, and/or increase efficiency.
摘要翻译：活动的小翼包括基本上平行于飞机的翼的主体部分，好像它是机翼的延伸部分。主体部分可附接到飞行器机翼并且包括耦合到其上的可控气流改变装置。由于具有可控气流改变装置，小翼能够响应于飞行中的条件来调节可控气流改变装置的控制表面，以减少机翼载荷，增加范围和/或提高效率。

9. 发明授权

US08684315B2 Active winglet 有权
标题翻译：活动小翼
公开(公告)号：US08684315B2
公开(公告)日：2014-04-01
申请号：US13075934
申请日：2011-03-30
申请人： Nicholas R. Guida
发明人： Nicholas R. Guida
IPC分类号： B64C9/00 , B64C23/06
CPC分类号： B64C23/065 , B64C13/16 , B64C23/076 , Y02T50/164
摘要： An active winglet includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes a controllable airflow modification device coupled thereto. By virtue of having a controllable airflow modification device, the winglet is capable of adjusting a control surface of the controllable airflow modification device in response to in-flight conditions, to reduce wing loads, increase range, and/or increase efficiency.
摘要翻译：活动的小翼包括基本上平行于飞机的翼的主体部分，好像它是机翼的延伸部分。主体部分可附接到飞行器机翼并且包括耦合到其上的可控气流改变装置。由于具有可控气流改变装置，小翼能够响应于飞行中的条件来调节可控气流改变装置的控制表面，以减少机翼载荷，增加范围和/或提高效率。

10. 发明授权

US11912398B2 Multiple controllable airflow modification devices 有权
公开(公告)号：US11912398B2
公开(公告)日：2024-02-27
申请号：US17467125
申请日：2021-09-03
申请人： Tamarack Aerospace Group, Inc.
发明人： Nicholas R. Guida
IPC分类号： B64C23/06 , B64C13/16
CPC分类号： B64C23/069 , B64C13/16 , B64C23/076 , Y02T50/10
摘要： An active wing extension includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing. The body portion is attachable to an aircraft wing and includes multiple controllable airflow modification devices coupled thereto. By virtue of having multiple controllable airflow modification devices, the wing extension is capable of adjusting control surfaces of the multiple controllable airflow modification devices in response to in-flight conditions, to reduce wing loads, improve wing fatigue characteristics, increase range, and/or increase efficiency.

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