公开(公告)号：US20140110530A1

公开(公告)日：2014-04-24

申请号：US14086914

申请日：2013-11-21

Applicant: Astrium SAS

Inventor： Christophe Chavagnac ,  Jerome Bertrand ,  Hugues Laporte-Weywada ,  Olivier Poulain ,  Philippe Matharan ,  Robert Laine

IPC: B64G1/00

CPC classification number: B64G1/005 ,  B64D27/023 ,  B64D2027/026 ,  B64G1/002 ,  B64G1/14 ,  B64G1/401 ,  Y02T50/44

Abstract: An aircraft having propulsion units for both conventional aircraft flight in the atmosphere and for high-altitude operation as a rocket. The aircraft is divided into a payload compartment and a compartment containing rocket propulsion unit propellant or fuel, and includes a long transverse wing with a small back-sweep to favour lift in the dense layers of the atmosphere and to thus make it possible to climb to high altitudes at a subsonic speed before using the rocket propulsion units. The return flight portion is performed by gliding or controlled as for a conventional aircraft.

Abstract translation: 一架飞机具有用于常规飞机在大气中飞行和作为火箭进行高空作战的推进装置。 飞机分为有效载荷舱和包含火箭推进装置推进剂或燃料的舱室，并且包括具有小的反向扫掠的长横翼，以有利于在大气层的致密层中的升力，从而使其可以爬上 在使用火箭推进装置之前，亚音速的高海拔高度。 返回飞行部分通过滑翔或受控于常规飞机执行。

公开(公告)号：US09145215B2

公开(公告)日：2015-09-29

申请号：US14086914

申请日：2013-11-21

Applicant: Astrium SAS

Inventor： Christophe Chavagnac ,  Jerome Bertrand ,  Hugues Laporte-Weywada ,  Olivier Poulain ,  Philippe Matharan ,  Robert Laine

IPC: B64G1/14 ,  B64D27/02 ,  B64G1/00 ,  B64G1/40

CPC classification number: B64G1/005 ,  B64D27/023 ,  B64D2027/026 ,  B64G1/002 ,  B64G1/14 ,  B64G1/401 ,  Y02T50/44

Abstract: An aircraft having propulsion units for both conventional aircraft flight in the atmosphere and for high-altitude operation as a rocket. The aircraft is divided into a payload compartment and a compartment containing rocket propulsion unit propellant or fuel, and includes a long transverse wing with a small back-sweep to favor lift in the dense layers of the atmosphere and to thus make it possible to climb to high altitudes at a subsonic speed before using the rocket propulsion units. The return flight portion is performed by gliding or controlled as for a conventional aircraft.

Abstract translation: 一架飞机具有用于常规飞机在大气中飞行和作为火箭进行高空作战的推进装置。 飞机分为有效载荷舱和包含火箭推进装置推进剂或燃料的舱室，并且包括具有小的反向扫掠的长横翼，以有利于在大气层的致密层中的升力，从而使其可以爬上 在使用火箭推进装置之前，亚音速的高海拔高度。 返回飞行部分通过滑翔或受控于常规飞行器进行。

公开(公告)号：US20130241773A1

公开(公告)日：2013-09-19

申请号：US13879705

申请日：2011-10-06

Applicant: ASTRIUM SAS

Inventor： Robert Laine

IPC: G01S1/02

CPC classification number: G01S1/02 ,  G01S1/10 ,  G01S3/30 ,  G01S5/0247

Abstract: According to the invention, a transmitting beacon (4) comprises at least two transmitting current loops (6.1, 6.2, 6.3) which are mutually orthogonal and capable of transmitting electromagnetic waves (5.1, 5.2, 5.3), as well as means (7) for supplying power to said transmitting current loops (6.1, 6.3) in series.

Abstract translation: 根据本发明，发射信标（4）包括至少两个相互正交且能够传送电磁波（5.1,5.2,5.3）的传输电流环（6.1,6.2,6.3）以及装置（7）， 用于向所述发射电流环（6.1,6.3）串联供电。