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公开(公告)号:US20140248149A1
公开(公告)日:2014-09-04
申请号:US14258003
申请日:2014-04-21
申请人: The Boeing Company
发明人: Steven D. Richardson
IPC分类号: B64C27/82
CPC分类号: B64C27/82 , B64C3/385 , B64C15/02 , B64C15/14 , B64C27/18 , B64C27/24 , B64C27/26 , Y02T50/14
摘要: A method of operating an aircraft having a rotor/wing assembly and a nozzle comprises vectoring the nozzle into a position for creating vertical thrust, and using the rotor/wing assembly and the nozzle together to create vertical thrust during a rotary mode of operation.
摘要翻译: 操作具有转子/翼组件和喷嘴的飞行器的方法包括将喷嘴引导到用于产生垂直推力的位置,并且在旋转操作模式期间将转子/翼组件和喷嘴一起使用以产生垂直推力。
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公开(公告)号:US09878785B2
公开(公告)日:2018-01-30
申请号:US14258003
申请日:2014-04-21
申请人: The Boeing Company
发明人: Steven D. Richardson
CPC分类号: B64C27/82 , B64C3/385 , B64C15/02 , B64C15/14 , B64C27/18 , B64C27/24 , B64C27/26 , Y02T50/14
摘要: A method of operating an aircraft having a rotor/wing assembly and a nozzle comprises vectoring the nozzle into a position for creating vertical thrust, and using the rotor/wing assembly and the nozzle together to create vertical thrust during a rotary mode of operation.
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公开(公告)号:US10065735B2
公开(公告)日:2018-09-04
申请号:US15840979
申请日:2017-12-13
申请人: The Boeing Company
发明人: Steven D. Richardson
CPC分类号: B64C27/82 , B64C3/385 , B64C15/02 , B64C15/14 , B64C27/18 , B64C27/24 , B64C27/26 , Y02T50/14
摘要: A method of operating an aircraft having a rotor/wing assembly and a nozzle comprises vectoring the nozzle into a position for creating vertical thrust, and using the rotor/wing assembly and the nozzle together to create vertical thrust during a rotary mode of operation.
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公开(公告)号:US20180170536A1
公开(公告)日:2018-06-21
申请号:US15840979
申请日:2017-12-13
申请人: The Boeing Company
发明人: Steven D. Richardson
CPC分类号: B64C27/82 , B64C3/385 , B64C15/02 , B64C15/14 , B64C27/18 , B64C27/24 , B64C27/26 , Y02T50/14
摘要: A method of operating an aircraft having a rotor/wing assembly and a nozzle comprises vectoring the nozzle into a position for creating vertical thrust, and using the rotor/wing assembly and the nozzle together to create vertical thrust during a rotary mode of operation.
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