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公开(公告)号：US20150360797A1
公开(公告)日：2015-12-17
申请号：US14736378
申请日：2015-06-11
Applicant: Engineered Arresting Systems Corporation
Inventor： Robert C. Melish , Kenneth J. Neeld , Richard L. Orner, Jr.
IPC: B64F1/00
CPC classification number: B64F1/02 , B64C2201/182 , B64F1/025
Abstract: Embodiments of the present disclosure relate generally to safe arrestment and recovery of an airborne unmanned air vehicle (UAV). Specific embodiments provide a 360 degree capture engagement cage that can recover a UAV approaching from any direction. The systems described herein may be used regardless of wind direction. The systems described herein may also be used as an air-only based system. Other embodiments may be used as including both an upper and lower tether for the engagement cage.
Abstract translation: 本公开的实施例一般涉及机载无人机（UAV）的安全停止和恢复。 具体实施例提供可以恢复从任何方向接近的UAV的360度捕获接合笼。 可以使用本文描述的系统，而不管风向如何。 本文描述的系统也可以用作仅基于空气的系统。 其他实施例可以用于包括用于接合笼的上部和下部系绳。
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公开(公告)号：US11136142B2
公开(公告)日：2021-10-05
申请号：US16402608
申请日：2019-05-03
Applicant: Engineered Arresting Systems Corporation
Inventor： Christopher J. Levesque , Daniel Glenn Warrick , Kirk F. Schneider , Kenneth J. Neeld
Abstract: A retractable runway edge sheave for use in an aircraft arresting system. The arresting system functions to extend a cable across a runway for capture by a tailhook of an aircraft. The retractable runway edge sheave is designed to raise and lower the cable. The disclosed system may also feature a ramping system.
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Patent Agency Ranking
公开(公告)号：US20160251088A1
公开(公告)日：2016-09-01
申请号：US15048123
申请日：2016-02-19
Applicant: Engineered Arresting Systems Corporation
Inventor： Robert C. Melish , Kenneth J. Neeld , Richard L. Orner, Jr.
CPC classification number: B64F1/02 , B64B1/40 , B64C39/024 , B64C2201/021 , B64C2201/082 , B64C2201/182 , B64D1/02 , B64F1/025
Abstract: Embodiments of the present disclosure relate generally to safe arrestment and recovery of an airborne unmanned air vehicle (UAV). Specific embodiments provide a recovery net that can recover a UAV approaching a cargo plane, the UAV either traveling in the same direction as the cargo plane or in an opposite direction of the cargo plane. The systems described herein may also be used as an air-only based system.
Abstract translation: 本公开的实施例一般涉及机载无人机（UAV）的安全停止和恢复。 具体实施例提供一种恢复网，其可以恢复接近货物的UAV，UAV沿与货物平面相同的方向或者与货物平面相反的方向行进。 本文描述的系统也可以用作仅基于空气的系统。
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公开(公告)号：US11148829B2
公开(公告)日：2021-10-19
申请号：US16501586
申请日：2019-05-03
Applicant: Engineered Arresting Systems Corporation
Inventor： Kirk F. Schneider , Justin S. Agren , Travis L. Chaney , Christopher J. Levesque , Scott A. Smith , Kenneth J. Neeld , Isaac Arroyo-Marquez , Craig H. Scott
IPC: B64F1/02
Abstract: An arresting cable retraction mechanism for use across an aircraft runway. The retraction mechanism functions to extend a cable across a runway (for capture by a tailhook of an aircraft) without causing the cable to recede below the runway surface during an aircraft rollover/deflection event. The arresting cable retraction mechanism is also designed to help prevent damage to a retraction motion actuator due to high speed aircraft rollover. The disclosed system separates components related to retraction vs. deflection due to rollover, such that rollover events do not affect or load the motion actuator used for retraction.
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公开(公告)号：US20190352019A1
公开(公告)日：2019-11-21
申请号：US16501586
申请日：2019-05-03
Applicant: Engineered Arresting Systems Corporation
Inventor： Kirk F. Schneider , Justin S. Agren , Travis L. Chaney , Christopher J. Levesque , Scott A. Smith , Kenneth J. Neeld , Isaac Arroyo-Marquez , Craig H. Scott
IPC: B64F1/02
Abstract: An arresting cable retraction mechanism for use across an aircraft runway. The retraction mechanism functions to extend a cable across a runway (for capture by a tailhook of an aircraft) without causing the cable to recede below the runway surface during an aircraft rollover/deflection event. The arresting cable retraction mechanism is also designed to help prevent damage to a retraction motion actuator due to high speed aircraft rollover. The disclosed system separates components related to retraction vs. deflection due to rollover, such that rollover events do not affect or load the motion actuator used for retraction.
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公开(公告)号：US20190337639A1
公开(公告)日：2019-11-07
申请号：US16402608
申请日：2019-05-03
Applicant: Engineered Arresting Systems Corporation
Inventor： Christopher J. Levesque , Daniel Glenn Warrick , Kirk F. Schneider , Kenneth J. Neeld
IPC: B64F1/02
Abstract: A retractable runway edge sheave for use in an aircraft arresting system. The arresting system functions to extend a cable across a runway for capture by a tailhook of an aircraft. The retractable runway edge sheave is designed to raise and lower the cable. The disclosed system may also feature a ramping system.
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公开(公告)号：US09527604B2
公开(公告)日：2016-12-27
申请号：US14736378
申请日：2015-06-11
Applicant: Engineered Arresting Systems Corporation
Inventor： Robert C. Melish , Kenneth J. Neeld , Richard L. Orner, Jr.
IPC: B64F1/02
CPC classification number: B64F1/02 , B64C2201/182 , B64F1/025
Abstract: Embodiments of the present disclosure relate generally to safe arrestment and recovery of an airborne unmanned air vehicle (UAV). Specific embodiments provide a 360 degree capture engagement cage that can recover a UAV approaching from any direction. The systems described herein may be used regardless of wind direction. The systems described herein may also be used as an air-only based system. Other embodiments may be used as including both an upper and lower tether for the engagement cage.
Abstract translation: 本公开的实施例一般涉及机载无人机（UAV）的安全停止和恢复。 具体实施例提供可以恢复从任何方向接近的UAV的360度捕获接合笼。 可以使用本文描述的系统，而不管风向如何。 本文描述的系统也可以用作仅基于空气的系统。 其他实施例可以用于包括用于接合笼的上部和下部系绳。
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