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公开(公告)号：US10953999B2
公开(公告)日：2021-03-23
申请号：US16543169
申请日：2019-08-16
申请人： John Alcorn , Stewart King , Mark Bales , David Brian Landrum
发明人： John Alcorn , Stewart King , Mark Bales , David Brian Landrum
摘要： An unmanned aerial vehicle docking system can include a docking arm and a docking station. The docking arm can be mounted on the UAV and include a rod with an interface element positioned on top of the rod. The interface element can have charging contacts that are attached to wires that extend down to a charging circuit on the UAV. The docking station can be located separate from the docking arm and have a guidance cone to direct the docking arm to a capture mechanism. Once the interface element is in the capture mechanism, a charging dome is then lowered down onto the top of the interface element to form a circuit between a power source at the docking station and the UAV's battery. Upon completion of the charging process, the charging dome is raised and the capture mechanism releases the interface element of the UAV.
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2.发明授权Subbing layer for antistatic layer on dye-receiving element used in thermal dye transfer 失效用于热染料转移的染料接收元件上的抗静电层用底层
公开(公告)号：US5747415A
公开(公告)日：1998-05-05
申请号：US663960
申请日：1996-06-14
申请人： Bruce Crinean Campbell , Thomas William Martin , Ronald Stewart King , David Randall Williams , Frederick W. Hesser
发明人： Bruce Crinean Campbell , Thomas William Martin , Ronald Stewart King , David Randall Williams , Frederick W. Hesser
IPC分类号： B41M5/382 , B32B5/18 , B41M5/00 , B41M5/40 , B41M5/42 , B41M5/44 , B41M5/50 , B41M5/52 , B41M5/035 , B41M5/38
CPC分类号： B41M5/42 , B41M5/38214 , B41M2205/32 , B41M5/44 , Y10S428/91 , Y10S428/913 , Y10S428/914 , Y10T428/249953
摘要： A dye-receiving element for thermal dye transfer comprising a support having on the front side thereof, in order, a biaxially-oriented composite film laminated thereto and a dye image-receiving layer, the composite film comprising a microvoided thermoplastic core layer and at least one substantially void-free thermoplastic surface layer, the support having on the back side thereof, in order, a biaxially-oriented film laminated thereto, a subbing layer and an antistatic layer, the subbing layer comprising an acrylic monomer, an acrylic homopolymer, an acrylic copolymer, a mixture of polyethylenes and a copolymer or terpolymer of polypropylene, or polypropylene having at least 0.1 g/m.sup.2 of titanium dioxide, the ratio of thickness of the back side film to the composite film being from about 0.45 to about 1.0.
摘要翻译： 一种用于热染料转移的染料接收元件，其包括在其前侧依次具有层压在其上的双轴取向复合膜和染料影像接收层的支撑体，所述复合膜包括微孔热塑性核心层和至少 一个基本上无空隙的热塑性表面层，其背面具有依次的支撑体，层叠有双轴取向膜，底层和抗静电层，该底层包含丙烯酸单体，丙烯酸均聚物， 丙烯酸共聚物，聚乙烯和具有至少0.1g / m 2的二氧化钛的聚丙烯或聚丙烯的共聚物或三元共聚物的混合物，背面膜与复合膜的厚度比为约0.45至约1.0。
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公开(公告)号：US20200071001A1
公开(公告)日：2020-03-05
申请号：US16543169
申请日：2019-08-16
申请人： John Alcorn , Stewart King , Mark Bales , David Brian Landrum
发明人： John Alcorn , Stewart King , Mark Bales , David Brian Landrum
摘要： An unmanned aerial vehicle docking system can include a docking arm and a docking station. The docking arm can be mounted on the UAV and include a rod with an interface element positioned on top of the rod. The interface element can have charging contacts that are attached to wires that extend down to a charging circuit on the UAV. The docking station can be located separate from the docking arm and have a guidance cone to direct the docking arm to a capture mechanism. Once the interface element is in the capture mechanism, a charging dome is then lowered down onto the top of the interface element to form a circuit between a power source at the docking station and the UAV's battery. Upon completion of the charging process, the charging dome is raised and the capture mechanism releases the interface element of the UAV.
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公开(公告)号：US10407182B1
公开(公告)日：2019-09-10
申请号：US15093382
申请日：2016-04-07
申请人： John Alcorn , Stewart King , Mark Bales , David Brian Landrum
发明人： John Alcorn , Stewart King , Mark Bales , David Brian Landrum
摘要： An unmanned aerial vehicle docking system can include a docking arm and a docking station. The docking arm can be mounted on the UAV and include a rod with an interface element positioned on top of the rod. The interface element can have charging contacts that are attached to wires that extend down to a charging circuit on the UAV. The docking station can be located separate from the docking arm and have a guidance cone to direct the docking arm to a capture mechanism. Once the interface element is in the capture mechanism, a charging dome is then lowered down onto the top of the interface element to form a circuit between a power source at the docking station and the UAV's battery. Upon completion of the charging process, the charging dome is raised and the capture mechanism releases the interface element of the UAV.
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