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公开(公告)号：USD843919S1
公开(公告)日：2019-03-26
申请号：US29640150
申请日：2018-03-12
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公开(公告)号：US10150560B2
公开(公告)日：2018-12-11
申请号：US15682126
申请日：2017-08-21
摘要： Described embodiments provide a rotor mounting boom assembly for a personal aircraft. The rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rotors, and one or more rotor controller assemblies. Controller assemblies for each rotor are positioned on the rotor mounting booms such that downwash from the rotor causes increased airflow across the controller assembly to cool the controller assembly components. A rotor controller enclosure includes an air inlet and an air outlet to allow airflow through the enclosure to cool the controller components. The air inlet is positioned relative to the path of the rotor blades such that the downwash from the rotor that flows into the air inlet is maximized. The structure of the enclosure includes features for increasing the airflow through the enclosure.
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公开(公告)号：US20180105268A1
公开(公告)日：2018-04-19
申请号：US15682126
申请日：2017-08-21
CPC分类号： B64C29/0025 , B64C2211/00 , B64D13/006 , B64D2013/0614
摘要： Described embodiments provide a rotor mounting boom assembly for a personal aircraft. The rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rotors, and one or more rotor controller assemblies. Controller assemblies for each rotor are positioned on the rotor mounting booms such that downwash from the rotor causes increased airflow across the controller assembly to cool the controller assembly components. A rotor controller enclosure includes an air inlet and an air outlet to allow airflow through the enclosure to cool the controller components. The air inlet is positioned relative to the path of the rotor blades such that the downwash from the rotor that flows into the air inlet is maximized. The structure of the enclosure includes features for increasing the airflow through the enclosure.
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公开(公告)号：US10424211B1
公开(公告)日：2019-09-24
申请号：US15940703
申请日：2018-03-29
发明人： Uri Tzarnotzky , James Joseph Tighe
摘要： An aircraft cockpit flight display system and method are disclosed. In various embodiments, an indication of a geo-location of an aircraft with which a display device is associated is received. A displayed scene that includes a graphical representation of the aircraft and a surrounding scene the content of which is determined at least in part by the geo-location is displayed via the display device.
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公开(公告)号：USD843306S1
公开(公告)日：2019-03-19
申请号：US29640152
申请日：2018-03-12
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公开(公告)号：US09764833B1
公开(公告)日：2017-09-19
申请号：US15297033
申请日：2016-10-18
CPC分类号： B64C29/0025 , B64C2211/00 , B64D13/006 , B64D2013/0614
摘要： A rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rotors, and one or more rotor controller assemblies. Controller assemblies for each rotor are positioned on the rotor mounting booms such that downwash from the rotor causes increased airflow across the controller assembly to cool the controller assembly components. A rotor controller enclosure includes an air inlet and an air outlet to allow airflow through the enclosure to cool the controller components. The air inlet is positioned relative to the path of the rotor blades such that the downwash from the rotor that flows into the air inlet is maximized. The structure of the enclosure includes features for increasing the airflow through the enclosure.
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