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公开(公告)号：WO2004033924A3
公开(公告)日：2004-12-23
申请号：PCT/US0331694
申请日：2003-10-03
Applicant: AVID LLC , LUMPKIN WAYNE
Inventor： LUMPKIN WAYNE
Abstract: A symmetric clamp structure having a first arm and a second arm. Both the first arm and the second arm having coaxial threaded bores through the distal ends of each arm. The symmetric clamp structure also includes a screw having a shank, the shank having a head at one end and being threaded at a second opposite end. The threaded portion of the shank is sized and has a pitch appropriate for threadably engaging the screw with the threaded bores through the distal end of both the first and second arm of the clamp structure. The shank of the screw also has a clearance portion between the threaded portion and the head. The screw is threadably engaged with one of the first or second threaded bores such that the head abuts the arm opposite the threaded engagement. The clearance portion has an outer diameter sized to clear the tips of the threads of the threaded bores and a length at least equal to the axial length of each threaded bore. Preferably the axial length of the clearance portion exceeds the axial length of each threaded bore.
Abstract translation: 一种具有第一臂和第二臂的对称夹紧结构。 第一臂和第二臂都具有穿过每个臂的远端的同轴螺纹孔。 对称夹紧结构还包括具有柄的螺钉，柄的一端具有头部并且在相对的第二端具有螺纹。 柄部的螺纹部分的尺寸被确定并且具有适合于通过夹紧结构的第一臂和第二臂的远端将螺钉与螺纹孔螺纹接合的螺距。 螺钉的柄部在螺纹部分和头部之间也具有间隙部分。 螺钉与第一或第二螺纹孔中的一个螺纹接合，使得头部与螺纹接合相对地邻接臂。 间隙部分具有外径，其尺寸被确定为清除螺纹孔的螺纹的尖端，并且其长度至少等于每个螺纹孔的轴向长度。 优选地，间隙部分的轴向长度超过每个螺纹孔的轴向长度。
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Patent Agency Ranking
公开(公告)号：WO2004033281A3
公开(公告)日：2004-07-22
申请号：PCT/US0331693
申请日：2003-10-03
Applicant: AVID LLC , LUMPKIN WAYNE
Inventor： LUMPKIN WAYNE
CPC classification number: B62K21/26 , Y10T16/466 , Y10T16/469 , Y10T16/48 , Y10T16/498
Abstract: A grip for a cycle includes a cylindrical liner extending along a liner axis between a first and a second end. The cylindrical liner has at least two elongate slots extending axially along a lengthwise portion of the cylindrical liner, each elongate slot overlapping a lengthwise part of another elongate slot, the overlapping elongate slots being radially offset. An over molding overlies a lengthwise of the cylindrical liner. The elongate slots are preferably disposed in a first set of at least two elongate slots extending along a first axial line in the liner and a second set of at least two elongate slots extending along a second axial line in the liner. The first and second axial lines are radially offset and the first set of elongate slots overlaps the second set of elongate slots. A first elongate slot may intercept a first end of the cylindrical liner. A compression member is provided in operative association with a circumference of an axial segment of the cylindrical liner. The axial segment includes at least a lengthwise portion of the first elongate slot. The compression member is operable between a relaxed state not compressing the axial segment and a compression segment compressing the axial segment about its circumference. The axial segment is preferably proximate the first end of the cylindrical liner.
Abstract translation: 用于循环的握把包括在第一端和第二端之间沿着衬垫轴线延伸的圆柱形衬里。 圆柱形衬套具有至少两个沿着圆柱形衬套的纵向部分轴向延伸的细长槽，每个细长槽与另一细长槽的纵向部分重叠，重叠的细长槽径向偏移。 包覆成型覆盖在圆柱形衬垫的纵向上。 细长狭槽优选地设置在沿着衬里中的第一轴线延伸的第一组至少两个细长狭槽中，以及沿着衬里中的第二轴线延伸的第二组至少两个细长狭槽。 第一和第二轴线径向偏移并且第一组细长狭槽与第二组细长狭槽重叠。 第一细长槽可以拦截圆柱形衬里的第一端。 压缩构件设置成与圆柱形衬套的轴向区段的周边可操作地相关联。 轴向段包括第一细长槽的至少一个纵向部分。 压缩构件可在不压缩轴向区段的松弛状态与压缩轴向区段围绕其周边的压缩区段之间操作。 轴向段优选靠近圆柱形衬套的第一端。
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3.发明申请DUAL-USE MODULAR PROPULSION SURVEILLANCE VEHICLE WITH DETACHABLE UNMANNED AIRBORNE VEHICLES 审中-公开两用模块化推进式无人机可拆卸无人机
公开(公告)号：WO2008085536A2
公开(公告)日：2008-07-17
申请号：PCT/US2007/069569
申请日：2007-05-23
Applicant: AVID, LLC , WILSON, Samuel, B. , GELHAUSEN, Paul , TURNBULL, Andy , ROBERTS, Michael , GUERERRO, Ignacio , BECKER, Kim
Inventor： WILSON, Samuel, B. , GELHAUSEN, Paul , TURNBULL, Andy , ROBERTS, Michael , GUERERRO, Ignacio , BECKER, Kim
IPC: B64C37/02
CPC classification number: B64C39/024 , B64C2201/028 , B64C2201/162 , B64C2201/206 , B64D5/00
Abstract: The present invention provides a system for reconnaissance using autonomous unmanned airborne vehicles (UAV). The system comprises a mothership, which is generally a fixed wing fuel tank capable of providing a suitable surface for flight (lift) and one or more elements for attachment of individual UAVs. The system further comprises one or more UAVs that are detachably connected to the mothership, and which are independently controllable for reconnaissance and tracking. The system and its individual parts are reusable and independently controllable, permitting low cost reconnaissance over wide areas of geography.
Abstract translation: 本发明提供一种使用自主无人驾驶飞行器（UAV）进行侦察的系统。 该系统包括母舰，其通常是能够提供用于飞行（升力）的适当表面的固定翼燃料箱和用于附接个别无人机的一个或多个元件。 该系统还包括一个或多个可拆卸地连接到母舰的无人机，并且这些无人机可独立控制用于侦察和跟踪。 该系统及其各部分可重复使用并可独立控制，可在广泛的地理区域进行低成本侦察。
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公开(公告)号：WO2004033924A2
公开(公告)日：2004-04-22
申请号：PCT/US2003/031694
申请日：2003-10-03
Applicant: AVID, LLC , LUMPKIN, Wayne
Inventor： LUMPKIN, Wayne
IPC: F16B
Abstract: A symmetric clamp structure having a first arm and a second arm. Both the first arm and the second arm having coaxial threaded bores through the distal ends of each arm. The symmetric clamp structure also includes a screw having a shank, the shank having a head at one end and being threaded at a second opposite end. The threaded portion of the shank is sized and has a pitch appropriate for threadably engaging the screw with the threaded bores through the distal end of both the first and second arm of the clamp structure. The shank of the screw also has a clearance portion between the threaded portion and the head. The screw is threadably engaged with one of the first or second threaded bores such that the head abuts the arm opposite the threaded engagement. The clearance portion has an outer diameter sized to clear the tips of the threads of the threaded bores and a length at least equal to the axial length of each threaded bore. Preferably the axial length of the clearance portion exceeds the axial length of each threaded bore.
Abstract translation: 具有第一臂和第二臂的对称夹具结构。 第一臂和第二臂都具有穿过每个臂的远端的同轴螺纹孔。 对称夹具结构还包括具有柄部的螺钉，所述柄部在一端具有头部并且在第二相对端处被螺纹连接。 柄的螺纹部分的尺寸设计成适合于通过夹紧结构的第一和第二臂的远端将螺钉与螺纹孔螺纹接合。 螺杆的柄部还具有在螺纹部分和头部之间的间隙部分。 螺钉与第一或第二螺纹孔中的一个螺纹接合，使得头部抵靠与螺纹接合相对的臂。 间隙部分具有外径，其尺寸设置成能够清除螺纹孔的螺纹的尖端，并且至少等于每个螺纹孔的轴向长度的长度。 优选地，间隙部分的轴向长度超过每个螺纹孔的轴向长度。
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5.发明申请DUAL-USE MODULAR PROPULSION SURVEILLANCE VEHICLE WITH DETACHABLE UNMANNED AIRBORNE VEHICLES 审中-公开双用途模拟推进监控车辆与可拆卸的无人驾驶飞机
公开(公告)号：WO2008085536A3
公开(公告)日：2008-10-02
申请号：PCT/US2007069569
申请日：2007-05-23
Applicant: AVID LLC , WILSON SAMUEL B , GELHAUSEN PAUL , TURNBULL ANDY , ROBERTS MICHAEL , GUERERRO IGNACIO , BECKER KIM
Inventor： WILSON SAMUEL B , GELHAUSEN PAUL , TURNBULL ANDY , ROBERTS MICHAEL , GUERERRO IGNACIO , BECKER KIM
CPC classification number: B64C39/024 , B64C2201/028 , B64C2201/162 , B64C2201/206 , B64D5/00
Abstract: The present invention provides a system for reconnaissance using autonomous unmanned airborne vehicles (UAV). The system comprises a mothership, which is generally a fixed wing fuel tank capable of providing a suitable surface for flight (lift) and one or more elements for attachment of individual UAVs. The system further comprises one or more UAVs that are detachably connected to the mothership, and which are independently controllable for reconnaissance and tracking. The system and its individual parts are reusable and independently controllable, permitting low cost reconnaissance over wide areas of geography.
Abstract translation: 本发明提供一种使用自主无人驾驶飞行器（UAV）进行侦察的系统。 该系统包括母舰，其通常是能够为飞行（提升）提供合适的表面的固定翼燃料箱和用于附接各个无人机的一个或多个元件。 该系统还包括一个或多个UAV，其可拆卸地连接到母舰，并且可独立控制以用于侦察和跟踪。 该系统及其各个部件是可重复使用的并且可独立控制，允许在广泛的地理区域进行低成本侦察。
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公开(公告)号：WO2004033281A2
公开(公告)日：2004-04-22
申请号：PCT/US2003/031693
申请日：2003-10-03
Applicant: AVID, LLC , LUMPKIN, Wayne
Inventor： LUMPKIN, Wayne
IPC: B62K
CPC classification number: B62K21/26 , Y10T16/466 , Y10T16/469 , Y10T16/48 , Y10T16/498
Abstract: A grip for a cycle includes a cylindrical liner extending along a liner axis between a first and a second end. The cylindrical liner has at least two elongate slots extending axially along a lengthwise portion of the cylindrical liner, each elongate slot overlapping a lengthwise part of another elongate slot, the overlapping elongate slots being radially offset. An over molding overlies a lengthwise of the cylindrical liner. The elongate slots are preferably disposed in a first set of at least two elongate slots extending along a first axial line in the liner and a second set of at least two elongate slots extending along a second axial line in the liner. The first and second axial lines are radially offset and the first set of elongate slots overlaps the second set of elongate slots. A first elongate slot may intercept a first end of the cylindrical liner. A compression member is provided in operative association with a circumference of an axial segment of the cylindrical liner. The axial segment includes at least a lengthwise portion of the first elongate slot. The compression member is operable between a relaxed state not compressing the axial segment and a compression segment compressing the axial segment about its circumference. The axial segment is preferably proximate the first end of the cylindrical liner.
Abstract translation: 用于循环的把手包括沿第一和第二端之间的衬套轴线延伸的圆柱形衬套。 圆柱形衬套具有沿着圆柱形衬套的纵向部分轴向延伸的至少两个细长槽，每个细长槽与另一个细长槽的纵向部分重叠，重叠的细长槽径向偏移。 超过模制物在圆柱形衬套的纵向上覆盖。 细长槽优选地设置在沿着衬套中的第一轴线延伸的至少两个细长狭槽的第一组中，以及沿衬套中的第二轴线延伸的至少两个细长槽的第二组。 第一和第二轴线径向偏移，并且第一组细长槽与第二组细长槽重叠。 第一细长槽可以拦截圆柱形衬套的第一端。 压缩构件设置成与圆柱形衬套的轴向段的圆周可操作地相关联。 轴向段至少包括第一细长槽的纵向部分。 压缩构件在不压缩轴向段的松弛状态和围绕其圆周压缩轴向段的压缩段之间可操作。 轴向段最好靠近圆柱形衬套的第一端。
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