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公开(公告)号：US20240277094A1
公开(公告)日：2024-08-22
申请号：US18640825
申请日：2024-04-19
Applicant: GALVION LTD.
Inventor： Stéphane LEBEL
CPC classification number: A42B3/04 , A42B3/221 , A42B3/326 , F41H1/04 , F41H11/04 , G02C3/02 , G02C7/022 , G02C2202/04
Abstract: A helmet assembly includes a face shield and a single, center top mounting arrangement that operatively connects a center top location of the face shield to a center front mount on the helmet. The face shield can be raised and lowered about a pivot axis provided in the mounting arrangement between a tilted up, non-use position and a lowered, deployed position. The mounting arrangement can include a detent and two recesses, wherein the detent engages a first recess at a slightly forwardly displaced position to allow ventilation between the helmet and mandible and the face shield and a second recess at the tilted up, non-use position. The recess and detent engagement can be overcome by easy manual force acting on the face shield to reposition the face shield.
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公开(公告)号：US11231254B1
公开(公告)日：2022-01-25
申请号：US16266394
申请日：2019-02-04
Inventor： Hunter I. Stephens , Stephen M. Cunningham , Andrew J. Lichtsinn , Travis M. Edwards , Michael L. Anderson , Cory A. Cooper
Abstract: A system for defeating a threat unmanned aerial vehicle. The system includes a friendly unmanned aerial vehicle, a capturing device configured to be suspended from the friendly unmanned aerial vehicle for arresting a threat unmanned aerial vehicle, and one or more load-limited release mechanisms for removably suspending a releasable portion of the capturing device from the friendly unmanned aerial vehicle. In certain embodiments, the load-limited release mechanisms are configured to release the entirety of the capturing device from the friendly unmanned aerial vehicle upon capture of the threat unmanned aerial vehicle. In other embodiments, the load limited release mechanisms are configured to release only a peripheral portion of the capturing device to reposition a captured unmanned aerial vehicle to a central portion of the capturing device for carrying the captured vehicle to a remote location.
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公开(公告)号：US09848665B2
公开(公告)日：2017-12-26
申请号：US12875108
申请日：2010-09-02
Applicant: Marie-Pierre Gendron , Stéphane Lebel , Martin Bélanger , Richard Coomber , Stephan Morency
Inventor： Marie-Pierre Gendron , Stéphane Lebel , Martin Bélanger , Richard Coomber , Stephan Morency
CPC classification number: A42B3/04 , A42B3/221 , A42B3/326 , F41H1/04 , F41H11/04 , G02C3/02 , G02C7/022 , G02C2202/04
Abstract: A helmet attachment system is usable to attach a mandible or face or mouth guard. The helmet attachment system also comprises a pair of attachment bases, each arranged on a side of the helmet near to an ear covering of the helmet. The attachment bases each include a metal base plate covered by an attached body block. Each attachment base provides provisions for attaching opposite ends of a mandible to the bases. The metal base plate includes hooks for engaging an edge of the helmet. A pair of strap assemblies is provided, each strap assembly connected to one attachment base. The strap assemblies extend rearward and are connected to the back rail by a buckle member on the end of each strap assembly. The back rail includes a pair of buckle member-receiving slots. The straps assemblies and the hooks provided on the attachment bases secure the attachment bases to the helmet.
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公开(公告)号：US09228807B1
公开(公告)日：2016-01-05
申请号：US13763954
申请日：2013-02-11
Applicant: Lockheed Martin Corporation
Inventor： Kenneth M. Adams
CPC classification number: F41H11/04 , B64B1/44 , G05D1/0011
Abstract: A barrier for providing defense against attack from airborne cruise missiles includes a buoyant lighter than air structure. A curtain is suspended from structure and depends from the structure to a level approximately even with the surface. The barrier is deployed across a path identified as a potential attack path for an incoming threat. An incoming missile strikes the curtain which is adapted such that at least a portion of the curtain separates from the barrier and envelopes or entangles the incoming missile. The portion of the curtain covers the flight control planes of the missile and deprives the missile of lift. The missile falls to the surface short of its intended target. The intended target may be a ship which may deploy the barrier at a selected distance from the ship along a determined path of attack.
Abstract translation: 提供防空袭巡航导弹袭击的障碍包括比空中结构更轻的轻型飞机。 窗帘从结构上悬挂下来，从结构到大致均匀的表面。 屏障部署在被识别为传入威胁的潜在攻击路径的路径上。 进入的导弹撞击窗帘，其适于使得至少一部分窗帘与屏障分开并包围或缠绕进入的导弹。 窗帘的一部分覆盖了导弹的飞行控制飞机，并剥夺了导弹的电梯。 导弹落在与目的不符的地面上。 预期的目标可以是可以沿着确定的攻击路径沿着选定的距离从船舶部署障碍物的船。
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公开(公告)号：US20240093975A1
公开(公告)日：2024-03-21
申请号：US18038344
申请日：2021-11-22
Applicant: PATRIA LAND OY
Inventor： Matti SAARIKKO , Jari LEMMETYINEN , Vesa TOIVONEN , Markku PAIJA
Abstract: A projectile and method for stopping aerial vehicles. The projectile comprises a shell—and a bunch of filaments. The bunch is wound in a coil and placed inside the shell. The projectile according to the solution may be brought to a target by different methods and utilising different means. For example, the projectile may be fired with compressed air or a propulsion charge, by using a compressed air weapon or rocket launcher. In addition, the projectile may be taken to the target by using a rocket or aerial vehicle.
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Patent Agency Ranking
公开(公告)号：US11757561B2
公开(公告)日：2023-09-12
申请号：US16476793
申请日：2018-01-09
Applicant: Airshare, Inc.
Inventor： Richard Jonathan Whittaker
CPC classification number: H04K3/92 , B64C39/024 , F41H11/04 , F41H13/0006 , G05D1/0022 , H04K3/41 , H04K3/43 , H04K3/827 , B64U2201/20 , H04K2203/22 , H04K2203/36
Abstract: The invention provides a system and method for intercepting a target UAV by releasing a plurality of countermeasure (CM) objects in a projected path thereof to form a 3D countermeasure cloud. Pieces of flexible materials configured to become ensnared in the propellers of the target UAV or otherwise interfere with their ability to provide lift and thrust capabilities to the UAV. A UAV interception control system may track the target UAV and compute a location probability volume therefor using a modified Kalman filter to decide on a projected interception location and time.
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公开(公告)号：US20210108896A1
公开(公告)日：2021-04-15
申请号：US16995276
申请日：2020-08-17
Applicant: Robert LEVY , David ORNAI
Inventor： Robert LEVY , David ORNAI
Abstract: A combined net structure is disclosed that comprises a non-planar coarse net with a grid-like structure comprising a plurality of coarse cables wherein longitudinal coarse cables intersect with latitudinal coarse cables to form a plurality of coarse cells and cutouts of a fine net attached to the coarse net, wherein the fine net comprises a plurality of adjacent fine cables. Each non-edge fine cable is attached to two adjacent fine cables on each of its sides at a plurality of locations along their lengths forming attachment points, wherein the fine net is arranged in a form of an array of fine quadrangular cells with said attachment points constituting the vertices of the fine quadrangular cells. System that comprises the combined net structures are disclosed as well.
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公开(公告)号：US06931994B2
公开(公告)日：2005-08-23
申请号：US10301302
申请日：2002-11-21
Applicant: Richard M. Lloyd
Inventor： Richard M. Lloyd
IPC: F41H11/04 , F41H13/00 , F42B12/20 , F42B12/22 , F42B12/32 , F42B12/58 , F42B12/60 , F42B12/64 , F42C19/095
CPC classification number: F42B12/205 , F42B12/22 , F42B12/60 , F42B12/64
Abstract: A tandem warhead for destroying a target, the tandem warhead including a kinetic energy rod section with a plurality of lengthy individual projectiles, a blast fragmentation section deployable proximate the target, and a guidance subsystem for deploying the projectiles of the kinetic energy rod section first in the trajectory path of the target and for deploying the blast fragmentation section second proximate the target.
Abstract translation: 用于摧毁目标的串联弹头，串联弹头包括具有多个长度独立的射弹的动能棒部分，靠近目标部署的爆炸碎片部分，以及用于部署动能棒部分的射弹的引导子系统 目标的轨迹路径和用于部署爆炸碎片部分第二接近目标。
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公开(公告)号：US20050126421A1
公开(公告)日：2005-06-16
申请号：US10301302
申请日：2002-11-21
Applicant: Richard Lloyd
Inventor： Richard Lloyd
IPC: F41H11/04 , F41H13/00 , F42B12/20 , F42B12/22 , F42B12/32 , F42B12/58 , F42B12/60 , F42B12/64 , F42C19/095
CPC classification number: F42B12/205 , F42B12/22 , F42B12/60 , F42B12/64
Abstract: A tandem warhead for destroying a target, the tandem warhead including a kinetic energy rod section with a plurality of lengthy individual projectiles, a blast fragmentation section deployable proximate the target, and a guidance subsystem for deploying the projectiles of the kinetic energy rod section first in the trajectory path of the target and for deploying the blast fragmentation section second proximate the target.
Abstract translation: 用于摧毁目标的串联弹头，串联弹头包括具有多个长度独立的射弹的动能棒部分，靠近目标部署的爆炸碎片部分，以及用于部署动能棒部分的射弹的引导子系统 目标的轨迹路径和用于部署爆炸碎片部分第二接近目标。
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公开(公告)号：US5583311A
公开(公告)日：1996-12-10
申请号：US407107
申请日：1995-03-17
Applicant: Ulrich Rieger
Inventor： Ulrich Rieger
CPC classification number: F41H11/04
Abstract: An intercept device for flying objects is formed of a lightweight, small-volume, packable structure made of a tear-resistant, pliable material, which can be stretched to a large, two-dimensional or three-dimensional expansion by means of a deployment device. To reduce the velocity of the intercepted flying objects, activatable, aerodynamic resistance bodies are incorporated into the structure. To end the intercept procedure, elements are integrated into the structure, which consist of material that can be destroyed from outside by means of high-energy beams and/or chemical reagents, or that destroys itself, or the structure as a whole consists of such material.
Abstract translation: 用于飞行物体的拦截装置由轻质，小体积的可压缩结构形成，该结构由耐撕裂，柔韧的材料制成，其可以通过展开装置拉伸至大的二维或三维扩张 。 为了减少被拦截的飞行物体的速度，可激活的空气动力学阻力体被结合到结构中。 为了结束拦截程序，将元件整合到结构中，该结构由可以通过高能量束和/或化学试剂从外部破坏的材料组成，或者破坏其自身，或者整个结构由此构成 材料。
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