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1. 发明申请

WO03080437A2 METHOD AND SYSTEM FOR MOUNTING RADIO AVIONICS 审中-公开
标题翻译：安装无线电影像的方法和系统
公开(公告)号：WO03080437A2
公开(公告)日：2003-10-02
申请号：PCT/US0308009
申请日：2003-03-18
申请人： LANDES MARK JAMES , L ESPERANCE VICTOR D
发明人： LANDES MARK JAMES , L ESPERANCE VICTOR D
IPC分类号： B64D43/00 , B64D
CPC分类号： B64D43/00 , H05K7/18
摘要： A mounting bar system permitting infinite adjustability in mounting avionics-components trays and Dzus-mounted avionics in at least one aircraft cockpit instrument panel assembly. Each mounting bar is slotted along its longitudinal axis. The slot is made to include the shape of a T such that a wider channel exists below the opening of the slot. Spring-loaded nut assemblies set to receive mounting screws from the avionics-components trays are fit within the T slot. Friction provided by the spring holds the nut assembly at any desired location within the T slot. As the nut assembly can be positioned at any location within the T slot, the mounting bar can readily be adjusted to support any avionics-components tray intended for at least one aircraft cockpit instrument panel assembly.
摘要翻译：安装杆系统允许在至少一个飞行器驾驶舱仪表板组件中安装航空电子设备组件托盘和Dzus安装的航空电子设备的无限可调性。每个安装杆沿其纵向轴线开槽。槽被制成包括T的形状，使得较宽的通道存在于槽的开口下方。设置为接收来自航空电子元件托盘的安装螺钉的弹簧加载螺母组件安装在T槽内。由弹簧提供的摩擦将螺母组件固定在T槽内的任何所需位置。由于螺母组件可以定位在T槽内的任何位置，安装杆可以容易地被调节以支持旨在用于至少一个飞行器驾驶舱仪表板组件的任何航空电子部件托盘。

2. 发明申请

WO2003080437A3 METHOD AND SYSTEM FOR MOUNTING RADIO AVIONICS 审中-公开
公开(公告)号：WO2003080437A3
公开(公告)日：2003-10-02
申请号：PCT/US2003/008009
申请日：2003-03-18
申请人： LANDES, Mark, James , L'ESPERANCE, Victor, D.
发明人： LANDES, Mark, James , L'ESPERANCE, Victor, D.
IPC分类号： A47F5/00
摘要： A mounting bar system permitting infinite adjustability in mounting avionics-components trays (694) and Dzus-mounted avionics in at least one aircraft cockpit instrument panel assembly. Each mounting bar (210) is slotted (270) along its longitudinal axis. The slot (270) is made to include the shape of a T such that a wider channel (260) exists below the opening (220) of the slot. Spring-loaded nut assemblies (300) set to receive mounting screws (280) from the avionics-components trays (694) are fit within the T slot (270). Friction provided by the spring (330) holds the nut assembly (300) at any desired location within the T slot (270). As the nut assembly (300) can be positioned at any location within the T slot, the mounting bar (210) can readily be adjusted to support any avionics-components tray intended for at least one aircraft cockpit instrument panel assembly.

3. 发明申请

WO2016061271A1 SHIELD SNIPPING SYSTEMS 审中-公开
标题翻译：屏蔽系统
公开(公告)号：WO2016061271A1
公开(公告)日：2016-04-21
申请号：PCT/US2015/055595
申请日：2015-10-14
申请人： LANDES, Mark, James
发明人： LANDES, Mark, James
IPC分类号： H01B7/38 , H01B15/00 , H01B5/12
CPC分类号： H02G1/1212 , H02G1/1292 , H02G1/1297
摘要： This invention relates to providing a system for improved wire stripping systems. More particularly this invention relates to providing a system relating to the stripping of a shield jacket of a twisted wire, especially twisted-pair wire.
摘要翻译：本发明涉及提供一种用于改进的剥线系统的系统。更具体地，本发明涉及提供一种涉及剥离绞线，特别是双绞线的屏蔽护套的系统。

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