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公开(公告)号：WO2017184552A1
公开(公告)日：2017-10-26
申请号：PCT/US2017/028049
申请日：2017-04-18
Applicant: ENGINEERED ARRESTING SYSTEMS CORPORATION
Inventor： TULLY, Andrew , PAGE, Dennis , WITHERS, Robert , NEELD, Kenneth , ORNER JR., Richard, L.
Abstract: Embodiments of the present invention provide improvements to UAV launching systems. The disclosed launching system eliminates the use of hydraulic fluid and compressed nitrogen or air by providing an electric motor-driven tape that causes movement of a shuttle along a launcher rail. The shuttle is detachable from the motor-driven tape, such that stoppage of the tape can be separate from stoppage of the shuttle. Embodiments further provide a secondary arrestment strap. Further embodiments provide an anti-rollback latch system.
Abstract translation: 本发明的实施例提供对无人飞行器发射系统的改进。 所公开的发射系统通过提供导致梭子沿着发射器轨道移动的电动马达驱动的胶带来消除使用液压流体和压缩的氮气或空气。 梭子可以从电机驱动的胶带上拆下来，这样胶带的停止可以与梭子的停止分开。 实施例还提供了二级止动带。 其他实施例提供了一种防回滚闩锁系统。
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公开(公告)号：WO2015073091A1
公开(公告)日：2015-05-21
申请号：PCT/US2014/052829
申请日：2014-08-27
Applicant: ENGINEERED ARRESTING SYSTEMS CORPORATION
Inventor： TULLY, Andrew , PAGE, Dennis , WITHERS, Robert , NEELD, Kenneth , ORNER, Richard L.
CPC classification number: B64F1/08 , B64C2201/084
Abstract: Embodiments of the present invention provide improvements to UAV launching systems. The disclosed launching system eliminates the use of hydraulic fluid and compressed nitrogen or air by providing an electric motor-driven tape that causes movement of a shuttle along a launcher rail.
Abstract translation: 本发明的实施例提供了对UAV发射系统的改进。 所公开的发射系统通过提供使电动机驱动的带子沿着发射轨运动，从而消除了液压流体和压缩的氮气或空气的使用。
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公开(公告)号：EP4019400A1
公开(公告)日：2022-06-29
申请号：EP22157497.3
申请日：2017-04-18
Applicant: Engineered Arresting Systems Corporation
Inventor： TULLY, Andrew , PAGE, Dennis , WITHERS, Robert , NEELD, Kenneth , ORNER JR, Richard L , SCHNEIDER, Kirk F. , WHITSEL, Scott J.
Abstract: Embodiments of the present invention provide improvements to UAV launching systems. The disclosed launching system eliminates the use of hydraulic fluid and compressed nitrogen or air by providing an electric motor-driven tape that causes movement of a shuttle along a launcher rail. The shuttle is detachable from the motor-driven tape, such that stoppage of the tape can be separate from stoppage of the shuttle. Embodiments further provide a secondary arrestment strap. Further embodiments provide an anti-rollback latch system.
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公开(公告)号：EP3038922A1
公开(公告)日：2016-07-06
申请号：EP14861600.6
申请日：2014-08-27
Applicant: Engineered Arresting Systems Corporation
Inventor： TULLY, Andrew , PAGE, Dennis , WITHERS, Robert , NEELD, Kenneth , ORNER, Richard L. Jr.
CPC classification number: B64F1/08 , B64C2201/084
Abstract: Embodiments of the present invention provide improvements to UAV launching systems. The disclosed launching system eliminates the use of hydraulic fluid and compressed nitrogen or air by providing an electric motor-driven tape that causes movement of a shuttle along a launcher rail.
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