公开(公告)号：US20160031544A1

公开(公告)日：2016-02-04

申请号：US14781937

申请日：2014-04-04

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Yohann CORABOEUF

IPC: B64C1/14 ,  B64D15/00 ,  B64G1/22

CPC classification number: B64C1/1492 ,  B64D15/00 ,  B64G1/22

Abstract: The invention relates to a glass panel for an aircraft suitable for a suborbital flight and an aeronautical flight, including an outer panel made of polycarbonate or aluminosilicate for temperature resistance, a main panel for pressure resistance, sized according to standard aeroplane safety factors, and an inner panel, providing redundancy for the main panel, sized with a minimum pressure margin, the outer, main and internal redundancy panels being separated from one another by spaces. The invention also relates to an aircraft including windscreen elements and portholes made using the glass panel.

Abstract translation: 本发明涉及一种用于适用于亚轨道飞行和航空飞行的飞行器的玻璃面板，包括由聚碳酸酯或硅铝酸盐制成的耐温性外板，根据标准飞机安全系数尺寸的耐压主板，以及 内部面板，为主面板提供冗余，尺寸为最小压力裕度，外部，主要和内部冗余面板通过间隔彼此分开。 本发明还涉及一种包括使用玻璃面板制成的挡风玻璃元件和舷窗的飞行器。

公开(公告)号：US20150360791A1

公开(公告)日：2015-12-17

申请号：US14763859

申请日：2014-02-04

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Samuel CHEVROLLIER ,  Robert ABADIE-LAHAILLE ,  Pascal MEZIERES ,  Benjamin FAURE ,  Jérôme BERTRAND ,  Yohann CORABOEUF ,  Angélique SANTERRE

IPC: B64D37/04 ,  B64G1/40 ,  B64D37/30 ,  B64D37/06

CPC classification number: B64D37/04 ,  B64D37/06 ,  B64D37/30 ,  B64G1/402 ,  F16C11/0695 ,  F17C2205/0192 ,  F17C2221/08 ,  F17C2270/0197

Abstract: The invention concerns a tank retainer for retaining a tank in the fuselage of an aircraft which includes, between the tank and a frame rigidly connected to the fuselage of the aircraft, a hinged retaining means and a fastening rod on which said hinged retaining means is mounted. Advantageously, the hinged retaining means is intended to be connected to a rear end of the tank and the fastening rod is suitable for being mounted on the frame rigidly connected to the fuselage of the aircraft and, preferably, the hinged retaining means comprises a ball joint.

Abstract translation: 本发明涉及一种用于将坦克保持在飞行器的机身中的坦克保持器，其包括在坦克和刚性地连接到飞行器的机身的框架之间，铰接的保持装置和紧固杆，所述铰接的保持装置安装在该紧固杆上 。 有利地，铰接的保持装置旨在连接到罐的后端，并且紧固杆适于安装在刚性地连接到飞行器的机身的框架上，并且优选地，铰接的保持装置包括球形接头 。

公开(公告)号：US20160257435A1

公开(公告)日：2016-09-08

申请号：US14901328

申请日：2014-07-04

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Yohann CORABOEUF ,  Jean-Philippe DUTHEIL

IPC: B64G1/40 ,  B64G5/00 ,  B64F5/00 ,  B64G1/14

CPC classification number: B64G1/401 ,  B64F5/50 ,  B64G1/14 ,  B64G1/641 ,  B64G5/00 ,  F02K9/97 ,  F05D2240/90

Abstract: The invention relates to a propulsion unit for a reusable launch vehicle including a rocket engine supported by a cradle. According to the invention, the cradle includes at least three attachment elements for assembling the unit on the structure of the vehicle to which the unit is to be connected, the at least three attachment elements defining a plane for removing the unit, and in which the unit includes one or more fluid and/or electric links of the engine, each one of the links including a free end to be assembled with a corresponding circuit for supplying the vehicle, to which the unit is to be connected, the tip of at least some of the free ends being contained in the removal plane.

Abstract translation: 本发明涉及一种用于可重复使用的运载火车的推进装置，其包括由支架支撑的火箭发动机。 根据本发明，托架包括至少三个附接元件，用于将单元组装在车辆的结构上，该单元将要连接到该结构，该至少三个附接元件限定用于移除该单元的平面，并且其中 单元包括发动机的一个或多个流体和/或电气连杆，每个链节包括一个待组装的自由端，该自由端与用于供应车辆的相应的电路组装，该单元将被连接至该至少一个 一些自由端被包含在移除平面中。

公开(公告)号：US20150360792A1

公开(公告)日：2015-12-17

申请号：US14765399

申请日：2014-02-04

Applicant: ASTRIUM SAS ,  AIRBUS DEFENCE AND SPACE SAS

Inventor： Benjamin FAURE ,  Jérôme BERTRAND ,  Yohann CORABOEUF ,  Samuel CHEVROLLIER ,  Robert ABADIE-LA-HAILLE ,  Pascal MEZIERES ,  Angélique SANTERRE

IPC: B64D37/04 ,  B64G1/40 ,  B64D37/30 ,  B64D37/06

CPC classification number: B64G1/402 ,  B64D37/04 ,  B64D37/06 ,  B64D37/30 ,  F17C13/00 ,  F17C13/008 ,  F17C2201/0119 ,  F17C2201/054 ,  F17C2205/0192 ,  F17C2221/08 ,  F17C2223/0161 ,  F17C2270/0194 ,  F17C2270/0197

Abstract: The present invention relates to a device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first means for retaining the tank along a vertical axis Z on each of a first and second end of the tank, a second means for retaining the tank along a horizontal axis Y, perpendicular to the main axis, on the first end of the tank, and a third means for retaining in a ball-and-socket joint, the means being located around the vertical axis and connected to the second end of the tank.

Abstract translation: 本发明涉及一种用于安装和支撑具有主轴线X的大致圆柱形或锥形槽的装置，该主轴线包括一对第一装置，用于沿着垂直轴线Z在第一和第二端 罐，第二装置，用于沿着垂直于主轴线的水平轴线Y在罐的第一端上保持箱体，以及用于保持在球窝接头中的第三装置，该装置位于 垂直轴并连接到油箱的第二端。