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公开(公告)号：US20160176503A1
公开(公告)日：2016-06-23
申请号：US14590464
申请日：2015-01-06
Applicant: The Boeing Company
Inventor： Jonathan David Gettinger
CPC classification number: B64C39/024 , B64C3/56 , B64C5/12 , B64C2201/102
Abstract: Deployment and control actuation mechanisms are incorporated in unmanned aerial vehicles having folding wings and/or folding canards and/or a folding vertical stabilizer. The folding canards and folding vertical stabilizer can be deployed using respective four-bar over-center mechanisms. Elevators pivotably mounted to the folding canards and a rudder pivotably mounted to the folding vertical stabilizer can be controlled by means of respective twist link mechanisms. The folding wings have respective wing roots that are driven by respective gas springs to pivot on bearings about a wing root hub having control servo wire paths.
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Patent Agency Ranking
公开(公告)号：US20240102320A1
公开(公告)日：2024-03-28
申请号：US17936079
申请日：2022-09-28
Applicant: The Boeing Company
Inventor： Keith Ryan Hollen , Nathan Matthew Knibb , Perry T. Horst , Jonathan David Gettinger , Alexander McGregor , Everett Ryan Eaton , Michael L. Oleshchuk , Sean Craig Sundberg , Angel Rodriguez
Abstract: A wing lock and deployment apparatus for an air launched vehicle includes a driver acted on by a single linear actuation event. The disclosed wing lock and deployment apparatus is capable of unlocking deployable wings of an air launched vehicle, deploying deployable wings of the air launched vehicle from a stored position, and locking deployable wings of the air launched vehicle in a deployed position in sequential order with the one single linear actuation event.
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公开(公告)号：US12188264B2
公开(公告)日：2025-01-07
申请号：US17936079
申请日：2022-09-28
Applicant: The Boeing Company
Inventor： Keith Ryan Hollen , Nathan Matthew Knibb , Perry T. Horst , Jonathan David Gettinger , Alexander McGregor , Everett Ryan Eaton , Michael L Oleshchuk , Sean Craig Sundberg , Angel Rodriguez
Abstract: A wing lock and deployment apparatus for an air launched vehicle includes a driver acted on by a single linear actuation event. The disclosed wing lock and deployment apparatus is capable of unlocking deployable wings of an air launched vehicle, deploying deployable wings of the air launched vehicle from a stored position, and locking deployable wings of the air launched vehicle in a deployed position in sequential order with the one single linear actuation event.
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公开(公告)号：US11952113B1
公开(公告)日：2024-04-09
申请号：US17936091
申请日：2022-09-28
Applicant: The Boeing Company
Inventor： Keith Ryan Hollen , Nathan Adam Kostelecky , Bryan Michael Loris , Jonathan David Gettinger , Alexander McGregor , Everett Ryan Eaton , Michael L. Oleshchuk
Abstract: A wing lock and deployment apparatus for an air launched vehicle includes a ball screw and driver acted on by a single actuation event. The disclosed wing lock and deployment apparatus is capable of unlocking deployable wings of an air launched vehicle, deploying deployable wings of the air launched vehicle from a stored position, and locking deployable wings of the air launched vehicle in a deployed position in sequential order with the one single actuation event.
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公开(公告)号：US20240101245A1
公开(公告)日：2024-03-28
申请号：US17936091
申请日：2022-09-28
Applicant: The Boeing Company
Inventor： Keith Ryan Hollen , Nathan Adam Kostelecky , Bryan Michael Loris , Jonathan David Gettinger , Alexander McGregor , Everett Ryan Eaton , Michael L. Oleshchuk
Abstract: A wing lock and deployment apparatus for an air launched vehicle includes a ball screw and driver acted on by a single actuation event. The disclosed wing lock and deployment apparatus is capable of unlocking deployable wings of an air launched vehicle, deploying deployable wings of the air launched vehicle from a stored position, and locking deployable wings of the air launched vehicle in a deployed position in sequential order with the one single actuation event.
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6.发明授权Mechanisms for deploying and actuating airfoil-shaped bodies on unmanned aerial vehicles 有权在无人驾驶飞行器上部署并致动翼型的机构公开(公告)号：US09533758B2
公开(公告)日：2017-01-03
申请号：US14590464
申请日：2015-01-06
Applicant: The Boeing Company
Inventor： Jonathan David Gettinger
CPC classification number: B64C39/024 , B64C3/56 , B64C5/12 , B64C2201/102
Abstract: Deployment and control actuation mechanisms are incorporated in unmanned aerial vehicles having folding wings and/or folding canards and/or a folding vertical stabilizer. The folding canards and folding vertical stabilizer can be deployed using respective four-bar over-center mechanisms. Elevators pivotably mounted to the folding canards and a rudder pivotably mounted to the folding vertical stabilizer can be controlled by means of respective twist link mechanisms. The folding wings have respective wing roots that are driven by respective gas springs to pivot on bearings about a wing root hub having control servo wire paths.
Abstract translation: 部署和控制致动机构被并入具有折叠翼和/或折叠的猫和/或折叠的垂直稳定器的无人驾驶飞行器中。 可以使用相应的四杆过中心机构来部署折叠式鸭子和折叠式垂直稳定器。 可枢转地安装到折叠卡瓦的电梯和可枢转地安装到折叠垂直稳定器的舵可以通过相应的扭转连杆机构来控制。 折叠翼具有相应的翼根，其由相应的气弹簧驱动，以围绕具有控制伺服线路径的翼根轮毂的轴承枢转。
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