-
公开(公告)号：US20150344147A1
公开(公告)日：2015-12-03
申请号：US14728644
申请日：2015-06-02
IPC分类号： B64D39/06
摘要： The present disclosure refers an aerial refueling coupling for in-flight parameter measuring, including a body configured to receive and support a probe and a removable shell that covers at least part of the body. The aerial refueling coupling includes a sensor system for detecting at least one parameter related to in-flight refueling operation, a data processing device configured to provide a measure at least relative to parameters detected by the sensor system, a portable storage system, and a power supply system comprising at least on battery for supplying energy, and a ram air turbine for their activation when the aerial refueling coupling is in-flight. The data processing device, the storage system and the power supply system are mounted onto the body covered by the shell.
摘要翻译： 本公开涉及用于飞行中参数测量的空中加油联轴器，包括构造成接收和支撑探针的主体和覆盖身体的至少一部分的可移除壳体。 空中加油联轴器包括用于检测与飞行中加油操作有关的至少一个参数的传感器系统;数据处理装置，被配置为至少提供相对于由传感器系统检测到的参数，便携式存储系统和功率 供应系统至少包括用于供应能量的电池，以及当空中加油联轴器在飞行中时用于其激活的冲压空气涡轮机。 数据处理装置，存储系统和电源系统安装在被外壳覆盖的主体上。
-
公开(公告)号：US09409652B2
公开(公告)日：2016-08-09
申请号：US14292003
申请日：2014-05-30
CPC分类号： B64D39/06 , G05D16/103 , Y10T137/7793
摘要： The present invention refers to a dual pressure regulation system to ensure a proper pressure regulation during the Aerial REFUELING operations with Hose and Drogue systems. More specifically is directed to dual redundant fuel pressure regulation systems. The pressure regulator system comprises two pressure regulators (10, 20) located in series and a control element (30) for controlling the movement of both regulators operatively connected downstream (34) the second pressure regulator (20) such that the movement of the pressure regulators (10, 20) is independently controlled by the control element (30) according to the delivery pressure downstream the second regulator (20).
摘要翻译： 本发明涉及一种双重压力调节系统，以确保在使用软管和Drogue系统的空中补充操作期间适当的压力调节。 更具体地涉及双重冗余燃料压力调节系统。 压力调节器系统包括串联的两个压力调节器（10,20）和用于控制可操作地连接在第二压力调节器（20）的下游（34）上的两个调节器的运动的控制元件（30），使得压力 根据第二调节器（20）下游的输送压力，调节器（10,20）由控制元件（30）独立控制。
-
3.发明申请HOSE&DROGUE IN-FLIGHT REFUELING SYSTEM WITH AN ACTIVE FUEL PRESSURE CONTROL 审中-公开具有活性燃料压力控制的软管和喷射式飞行补给系统公开(公告)号：US20150284107A1
公开(公告)日：2015-10-08
申请号：US14553314
申请日：2014-11-25
摘要： The present invention provides a hose&drogue in-flight refueling system that avoids overpressure risks in the refueling operation and optimizes the performance of the fuel supply during its operational life and throughout all the flow rates.The hose&drogue in-flight refueling system comprises a pressure sensing unit capable of measuring continuously the fuel pressure at the end of the hose and a control unit in the tanker aircraft which is operatively communicated through a communication link with the pressure sensing unit and with the fuel pump and is adapted to use the measures of the fuel pressure at the end of the hose to control that the fuel supplied at the beginning of the hose has the pressure needed to achieve a target pressure at the end of the hose.
摘要翻译： 本发明提供了一种软管和冷藏式飞行中加油系统，其避免在加油操作中的过压风险，并且在其使用寿命期间以及在所有流量下优化燃料供应的性能。 软管和冷藏式飞行中加油系统包括压力检测单元，其能够连续地测量软管端部的燃料压力和油罐飞行器中的控制单元，该控制单元通过与压力感测单元和燃料的通信链路可操作地连通 并且适于使用软管端部的燃料压力的措施来控制在软管开始处供应的燃料具有在软管末端达到目标压力所需的压力。
-
公开(公告)号：US09731835B2
公开(公告)日：2017-08-15
申请号：US14728644
申请日：2015-06-02
摘要： The present disclosure refers an aerial refueling coupling for in-flight parameter measuring, including a body configured to receive and support a probe and a removable shell that covers at least part of the body. The aerial refueling coupling includes a sensor system for detecting at least one parameter related to in-flight refueling operation, a data processing device configured to provide a measure at least relative to parameters detected by the sensor system, a portable storage system, and a power supply system comprising at least on battery for supplying energy, and a ram air turbine for their activation when the aerial refueling coupling is in-flight. The data processing device, the storage system and the power supply system are mounted onto the body covered by the shell.
-
公开(公告)号：US20150368893A1
公开(公告)日：2015-12-24
申请号：US14764022
申请日：2013-01-23
发明人： Juan Manuel Ros Garcia , Javier Camacho Diez , Luis Casillas Gamboa , Carlos Miguel Iglesias Sanz
摘要： A modular adaptable housing architecture for building temporary shelters and residential units in emergency situations is provided and includes an oval cross-section, which can be increased and extended in a flexible manner, involving the mechanically articulated assembly of successive structural modules formed by pairs of crosswise-arranged ovoid frames in order to support a panel-based inner floor slab, with the shell being formed by sheets, while providing a level floor solution in which the floor is elevated above the ground using the curvature of the elliptical supporting section of each frame or retractable supporting parts of the frames. The result is a self-tensioning geometry shelter, which can be adapted to suit the terrain and occupancy requirements, which is stable, strong and environmentally friendly, and which can be transported in disassembled parts and quickly assembled at any location without requiring any additional work and enabling a finish typical of the locality.
摘要翻译： 提供了一种用于在紧急情况下建造临时避难所和住宅单元的模块化适应性住房结构，其包括椭圆形横截面，其可以灵活地增加和延伸，涉及由相互交叉的成对形成的连续结构模块的机械铰接组件 - 安排的卵形框架，以便支撑基于面板的内部楼板，其中壳体由板材形成，同时提供使用每个框架的椭圆形支撑部分的曲率地板在地面上方升高的地板层 或框架的伸缩支撑部件。 结果是一个自张紧的几何避难所，可以适应地形和占用要求，这是稳定，强大和环保的，可以拆卸的部件运输，并在任何位置快速组装，而不需要任何额外的工作 并实现典型的本地化。
-
公开(公告)号：US20150203210A1
公开(公告)日：2015-07-23
申请号：US14292003
申请日：2014-05-30
IPC分类号： B64D39/06
CPC分类号： B64D39/06 , G05D16/103 , Y10T137/7793
摘要： The present invention refers to a dual pressure regulation system to ensure a proper pressure regulation during the Aerial REFUELING operations with Hose and Drogue systems. More specifically is directed to dual redundant fuel pressure regulation systems. The pressure regulator system comprises two pressure regulators (10, 20) located in series and a control element (30) for controlling the movement of both regulators operatively connected downstream (34) the second pressure regulator (20) such that the movement of the pressure regulators (10, 20) is independently controlled by the control element (30) according to the delivery pressure downstream the second regulator (20).
摘要翻译： 本发明涉及一种双重压力调节系统，以确保在使用软管和Drogue系统的空中补充操作期间适当的压力调节。 更具体地涉及双重冗余燃料压力调节系统。 压力调节器系统包括串联的两个压力调节器（10,20）和用于控制可操作地连接在第二压力调节器（20）的下游（34）上的两个调节器的运动的控制元件（30），使得压力 根据第二调节器（20）下游的输送压力，调节器（10,20）由控制元件（30）独立控制。
-
-
-
-
-
搜索结果
6 条记录 (耗时 0.012 秒)
