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1.发明授权System, apparatus and method for long endurance vertical takeoff and landing vehicle 有权长寿命垂直起降车的系统，设备及方法公开(公告)号：US09540101B2
公开(公告)日：2017-01-10
申请号：US14507198
申请日：2014-10-06
IPC分类号： B64C27/52 , B64C29/04 , B64C29/02 , B64C39/02 , B64C29/00 , B64C3/42 , B64C5/02 , B64C9/00 , B64C25/10 , B64D27/02 , B64D43/00
CPC分类号： B64C27/52 , B64C3/42 , B64C5/02 , B64C9/00 , B64C13/16 , B64C25/10 , B64C29/00 , B64C29/0033 , B64C29/0091 , B64C29/02 , B64C29/04 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102 , B64C2201/108 , B64C2201/162 , B64C2201/187 , B64D27/02 , B64D43/00
摘要： A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.
摘要翻译： 根据本发明的一个方面的垂直起飞（VTOL）飞机包括机身，具有位于机身尾端的全移动水平稳定器的尾翼，机身具有位于机身的大致中间位置 翼的远端，其中翼被配置成使用位于机身的每一侧上的倾斜铰链在基本上直的机翼构型和倾斜翼结构之间转换。 垂直起落飞行器还可以包括一个或多个可伸缩的弹簧支撑件，其中可伸缩的弹簧支撑构造成从翼的远端中的每一个展开。
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公开(公告)号：US20170277185A1
公开(公告)日：2017-09-28
申请号：US15464786
申请日：2017-03-21
发明人： Jessica E. Duda , John Tylko , David Mindell , Fabrice Kunzi , Michael Piedmonte , John Allee , Joshua Torgerson , Jason Ryan , James Donald Paduano , John Brooke Wissler , Andrew Musto , Wendy Feenstra
CPC分类号： G05D1/0088 , B25J11/00 , B64D43/00 , B64D45/00 , B64D2045/0075 , B64D2045/0085 , G05D1/101
摘要： An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.
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公开(公告)号：US11693407B2
公开(公告)日：2023-07-04
申请号：US16866458
申请日：2020-05-04
发明人： Jessica E. Duda , John Tylko , David Mindell , Fabrice Kunzi , Michael Piedmonte , John Allee , Joshua Torgerson , Jason Ryan , James Donald Paduano , John Brooke Wissler , Andrew Musto , Wendy Feenstra
CPC分类号： G05D1/0088 , B25J11/00 , B64D43/00 , B64D45/00 , G05D1/101 , B64D2045/0075 , B64D2045/0085 , G06N5/02
摘要： An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.
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公开(公告)号：US20200064840A1
公开(公告)日：2020-02-27
申请号：US16504988
申请日：2019-07-08
发明人： Jessica E. Duda , John Tylko , David Mindell , Fabrice Kunzi , Michael Piedmonte , John Allee , Joshua Torgerson , Jason Ryan , James Donald Paduano , John Brooke Wissler , Andrew Musto , Wendy Feenstra
摘要： An aircrew automation system and method for use in an aircraft. The aircrew automation system comprises one or more processors, an optical perception system, an actuation system, and a human-machine interface. The optical perception system monitors, in real-time, one or more cockpit instruments of the aircraft visually to generate flight situation data. The actuation system mechanically engages at least one flight control of the aircraft in response to the one or more flight commands. The human-machine interface provides an interface between a human pilot and the aircrew automation system. The human-machine interface comprises a display device to display a status of the aircraft and the actuation system.
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公开(公告)号：US11881116B2
公开(公告)日：2024-01-23
申请号：US16670038
申请日：2019-10-31
CPC分类号： G08G5/0039 , G05D1/104 , G08G5/0008 , G08G5/0013 , G08G5/0069
摘要： In one example, a method of operating a plurality of aerial vehicles in an environment includes receiving, at a first command module of a first aerial vehicle navigating along a first flight path, sensor data from one or more sensors on board the first aerial vehicle. The sensor data reflects one or more characteristics of the environment. The method further includes determining, via the first command module, a change from a predetermined formation to a different formation for a second aerial vehicle based at least in part on the sensor data, where the predetermined formation and the different formation are relative to the first aerial vehicle. The method also including generating, via the first command module, control signals reflecting the change from the predetermined formation to the different formation and sending the control signals from the first aerial vehicle to the second aerial vehicle.
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公开(公告)号：US09682774B2
公开(公告)日：2017-06-20
申请号：US14507313
申请日：2014-10-06
IPC分类号： B64C13/16 , B64C27/52 , B64C29/04 , B64C29/02 , B64C39/02 , B64C29/00 , B64C3/42 , B64C5/02 , B64C9/00 , B64C25/10 , B64D27/02 , B64D43/00
CPC分类号： B64C27/52 , B64C3/42 , B64C5/02 , B64C9/00 , B64C13/16 , B64C25/10 , B64C29/00 , B64C29/0033 , B64C29/0091 , B64C29/02 , B64C29/04 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/102 , B64C2201/108 , B64C2201/162 , B64C2201/187 , B64D27/02 , B64D43/00
摘要： A vertical take-off and landing (VTOL) aircraft according to an aspect of the present invention comprises a fuselage, an empennage having an all-moving horizontal stabilizer located at a tail end of the fuselage, a wing having the fuselage positioned approximately halfway between the distal ends of the wing, wherein the wing is configured to transform between a substantially straight wing configuration and a canted wing configuration using a canted hinge located on each side of the fuselage. The VTOL aircraft may further includes one or more retractable pogo supports, wherein a retractable pogo support is configured to deploy from each of the wing's distal ends.
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公开(公告)号：US20210134163A1
公开(公告)日：2021-05-06
申请号：US16670038
申请日：2019-10-31
摘要： In one example, a method of operating a plurality of aerial vehicles in an environment includes receiving, at a first command module of a first aerial vehicle navigating along a first flight path, sensor data from one or more sensors on board the first aerial vehicle. The sensor data reflects one or more characteristics of the environment. The method further includes determining, via the first command module, a change from a predetermined formation to a different formation for a second aerial vehicle based at least in part on the sensor data, where the predetermined formation and the different formation are relative to the first aerial vehicle. The method also including generating, via the first command module, control signals reflecting the change from the predetermined formation to the different formation and sending the control signals from the first aerial vehicle to the second aerial vehicle.
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公开(公告)号：US20200301422A1
公开(公告)日：2020-09-24
申请号：US16866458
申请日：2020-05-04
发明人： Jessica E. Duda , John Tylko , David Mindell , Fabrice Kunzi , Michael Piedmonte , John Allee , Joshua Torgerson , Jason Ryan , James Donald Paduano , John Brooke Wissler , Andrew Musto , Wendy Feenstra
摘要： An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.
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公开(公告)号：US10359779B2
公开(公告)日：2019-07-23
申请号：US15464786
申请日：2017-03-21
发明人： Jessica E. Duda , John Tylko , David Mindell , Fabrice Kunzi , Michael Piedmonte , John Allee , Joshua Torgerson , Jason Ryan , James Donald Paduano , John Brooke Wissler , Andrew Musto , Wendy Feenstra
摘要： An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.
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