公开(公告)号：US20160167793A1

公开(公告)日：2016-06-16

申请号：US14970570

申请日：2015-12-16

Applicant: AIRBUS GROUP SAS

Inventor： Jean-Francois GENESTE

IPC: B64D25/02 ,  B60R21/231

CPC classification number: B64D25/02 ,  B60R19/205 ,  B60R21/231 ,  B64D25/00 ,  B64D2201/00 ,  B64G1/62

Abstract: A protection system (15) includes an inflatable bag (16) connected to inflation elements able and intended to be activated so as to inflate the inflatable bag in the event of and/or upon the prediction of an impact. The inflatable bag (16) has a substantially annular overall shape when inflated. Such a protection system (15) is advantageously intended to protect the passengers in a helicopter.

Abstract translation: 保护系统（15）包括连接到能够且预期被启动的充气元件的充气袋（16），以便在预测碰撞和/或预测碰撞的情况下使充气袋膨胀。 充气袋（16）在膨胀时具有基本环形的整体形状。 这种保护系统（15）有利地用于保护直升机中的乘客。

公开(公告)号：US20160311560A1

公开(公告)日：2016-10-27

申请号：US15102980

申请日：2014-12-08

Applicant: AIRBUS GROUP SAS

Inventor： Jean-Francois GENESTE

IPC: B64G1/44 ,  B64G1/40 ,  H02S30/10 ,  B64G1/50 ,  H02S10/40 ,  B64G1/22 ,  B64G1/42

CPC classification number: B64G1/446 ,  B64G1/222 ,  B64G1/402 ,  B64G1/423 ,  B64G1/503 ,  B64G2001/224 ,  H02S10/40 ,  H02S30/10 ,  Y02E10/52

Abstract: A spacecraft (10) includes: a body (20), a surface of revolution (40), rigidly connected to the body, the spacecraft including a heat engine positioned at the centre of the surface of revolution (40), and the surface of revolution includes a first portion (411) forming a solar concentrator for concentrating solar radiation in the direction of the heat engine and a second portion (412), coaxial with the first portion (411), and such that the first portion (411) and the second portion (412) form, relative to each other, a Cassegrain solar concentrator, of which a focal point is located at the heat engine.

Abstract translation: 航天器（10）包括：主体（20），与所述主体刚性连接的旋转表面（40），所述航天器包括位于所述旋转表面（40）的中心的热引擎，以及 旋转包括形成用于将太阳辐射集中在热机的方向上的太阳能聚光器的第一部分（411）和与第一部分（411）同轴的第二部分（412），并且使得第一部分（411）和 第二部分（412）相对于彼此形成一个卡塞格伦太阳能集中器，其焦点位于热机上。

公开(公告)号：US20160185470A1

公开(公告)日：2016-06-30

申请号：US14984832

申请日：2015-12-30

Applicant: AIRBUS GROUP SAS

Inventor： Jean-Francois GENESTE

IPC: B64G1/66 ,  H01L35/30 ,  B64G1/58

CPC classification number: B64G1/66 ,  B64G1/421 ,  B64G1/446 ,  B64G1/50 ,  B64G1/503 ,  B64G1/58 ,  H01L35/30

Abstract: A device for the recovery of a proportion of the energy which is dissipated, by the Joule effect, by the equipment of a predetermined satellite in a vacuum atmosphere, includes at least one radiative panel (10) which is designed to permit the cooling of the satellite (20) payload, and a thermoelectric generator, the heat source (12) of which is supplied with infrared photons by the radiative panels (10), whereby the latter are configured to concentrate the infrared photons towards the heat source (12).

Abstract translation: 用于通过焦耳效应由真空气氛中的预定卫星的设备回收一部分能量的装置包括至少一个辐射板（10），其被设计成允许冷却 卫星（20）有效载荷和热电发生器，其热源（12）由辐射板（10）供应红外光子，由此其构造成将红外光子集中到热源（12）。