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公开(公告)号：US11851174B2
公开(公告)日：2023-12-26
申请号：US16819671
申请日：2020-03-16
发明人： Trent Lukaczyk , Michael Colonno
摘要： A vectored thrust control module for an aircraft that includes a servo system that couples to the aircraft structure at an output shaft connection point. A thrust motor assembly is fully supported by the servo system and rotates a bladed component to provide thrust to the aircraft. Further, the thrust motor assembly is rigidly connected with the servo system to rotate together about a longitudinal axis thrust line with respect to the aircraft structure. The bladed component and the thrust motor assembly generate a line of thrust that extends through the connection point of the servo system to the aircraft structure.
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公开(公告)号：US20210373579A1
公开(公告)日：2021-12-02
申请号：US17330549
申请日：2021-05-26
发明人： Trent Lukaczyk , David L. Walter , Michael Colonno
摘要： A method for controlling a thrust vectored aircraft includes mapping aircraft control commands with a flight controller through at least an inner-mixing space and generating output commands.
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公开(公告)号：US10589867B2
公开(公告)日：2020-03-17
申请号：US15355679
申请日：2016-11-18
发明人： Trent Lukaczyk , Michael Colonno
摘要： A vectored thrust control module for an aircraft that includes a servo system that couples to the aircraft structure at an output shaft connection point. A thrust motor assembly is fully supported by the servo system and rotates a bladed component to provide thrust to the aircraft. Further, the thrust motor assembly is rigidly connected with the servo system to rotate together about a longitudinal axis thrust line with respect to the aircraft structure. The bladed component and the thrust motor assembly generate a line of thrust that extends through the connection point of the servo system to the aircraft structure.
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公开(公告)号：US12012223B2
公开(公告)日：2024-06-18
申请号：US17738102
申请日：2022-05-06
发明人： Trent Lukaczyk , Daniel Levy , Michael Colonno
IPC分类号： B64D47/08 , B64C39/02 , G03B17/55 , H04N23/51 , B64U101/30
CPC分类号： B64D47/08 , B64C39/024 , G03B17/55 , H04N23/51 , B64U2101/30
摘要： A camera payload configured for attachment to an unmanned aerial system with a payload interface. The camera payload includes a payload interface that includes a configuration that is structured and arranged to provide tool-free mechanical retention, electrical connections for power, and electrical connections for data; at least one camera mounted in the camera payload; at least one composite skin and at least one internal structure; at least one sealable and removable camera window retained on an outside of the camera payload; and at least one computer arranged within the camera payload.
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公开(公告)号：US11958641B2
公开(公告)日：2024-04-16
申请号：US17738100
申请日：2022-05-06
发明人： Trent Lukaczyk , Daniel Levy , Michael Colonno
IPC分类号： B64U20/87 , B64U101/30 , G03B15/00 , G03B17/55 , G03B17/56
CPC分类号： B64U20/87 , G03B15/006 , G03B17/55 , G03B17/561 , B64U2101/30
摘要： A gimbal configured to be implemented in an unmanned aerial system. The gimbal includes a payload interface; an end effector; a structure that includes composite skins, an internal structure, and integrated seals; integrated drive components; and at least one computer, where excess heat generated by the at least one computer is disposed of through a heat transfer surface integrated into the composite skin of the gimbal.
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公开(公告)号：US20200346747A1
公开(公告)日：2020-11-05
申请号：US16819671
申请日：2020-03-16
发明人： Trent Lukaczyk , Michael Colonno
摘要： A vectored thrust control module for an aircraft that includes a servo system that couples to the aircraft structure at an output shaft connection point. A thrust motor assembly is fully supported by the servo system and rotates a bladed component to provide thrust to the aircraft. Further, the thrust motor assembly is rigidly connected with the servo system to rotate together about a longitudinal axis thrust line with respect to the aircraft structure. The bladed component and the thrust motor assembly generate a line of thrust that extends through the connection point of the servo system to the aircraft structure.
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公开(公告)号：US20170144771A1
公开(公告)日：2017-05-25
申请号：US15355679
申请日：2016-11-18
发明人： Trent Lukaczyk , Michael Colonno
摘要： A vectored thrust control module for an aircraft that includes a servo system that couples to the aircraft structure at an output shaft connection point. A thrust motor assembly is fully supported by the servo system and rotates a bladed component to provide thrust to the aircraft. Further, the thrust motor assembly is rigidly connected with the servo system to rotate together about a longitudinal axis thrust line with respect to the aircraft structure. The bladed component and the thrust motor assembly generate a line of thrust that extends through the connection point of the servo system to the aircraft structure.
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