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公开(公告)号：US09677234B2
公开(公告)日：2017-06-13
申请号：US13647070
申请日：2012-10-08
Applicant: Engineered Arresting Systems Corporation
Inventor： Sofia Wynnytsky , Mark Slimko , Reggie Torrez , Robert Withers , Hugh K. Delong, III , Danny Warrick , Kirk F. Schneider , Thomas H. Ross , Marcos Villa-Gonzales , Dennis Page , John Patrick McGinley , Peter T. Mahal , Richard L. Orner, Jr.
CPC classification number: E01F15/145 , E01F15/06 , E01F15/065
Abstract: Vehicle restraints and fence systems that offer better protection to the driver and vehicle in the event of an accident where the car becomes airborne and leaves the road or track, and catch fences for halting the overrun of a car leaving a racetrack. The catch fences may have pivotable poles and a cable extending between the poles. Net or fencing is installed between the poles, supported by the cable. The poles may be angled or curved, with a plurality of cables extending therebetween or with a net extending from the poles and attached to a Steel and Foam Energy Reduction barrier.
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Patent Agency Ranking
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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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：US10118713B2
公开(公告)日：2018-11-06
申请号：US14999290
申请日：2016-04-20
Applicant: Engineered Arresting Systems Corporation
Inventor： Andrew Tully , Dennis Page , Robert Withers , Kenneth Neeld , Richard L. Orner, Jr. , Kirk F. Schneider , Scott J. Whitsel
IPC: B64F1/08
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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