公开(公告)号：USD589868S1

公开(公告)日：2009-04-07

申请号：US29297606

申请日：2007-11-14

Applicant: Philippe Matharan ,  Olivier Poulain ,  Valéry Auger ,  Hugues Laporte-Weywada ,  Christophe Chavagnac ,  Jérôme Bertrand

Designer： Philippe Matharan ,  Olivier Poulain ,  Valéry Auger ,  Hugues Laporte-Weywada ,  Christophe Chavagnac ,  Jérôme Bertrand

公开(公告)号：US08702041B2

公开(公告)日：2014-04-22

申请号：US12443359

申请日：2007-10-17

Applicant: Christophe Chavagnac ,  Jérôme Bertrand ,  Hugues Laporte-Weywada ,  Olivier Poulain ,  Philippe Matharan ,  Robert Laine

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

IPC: B64G1/14 ,  B64G1/26 ,  B64G1/40 ,  B64D27/02 ,  B64C39/12

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机执行。

公开(公告)号：US20100276545A1

公开(公告)日：2010-11-04

申请号：US12443359

申请日：2007-10-17

Applicant: Christophe Chavagnac ,  Jérôme Bertrand ,  Hugues Laporte-Weywada ,  Olivier Poulain ,  Philippe Matharan ,  Robert Laine

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

IPC: B64G1/14 ,  B64C1/00

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

Abstract: This aircraft comprises both propulsion units (7, 16, 17) for conventional aircraft flight in the atmosphere and for high-altitude operation as a rocket. It is divided into a payload compartment (8) and a compartment (13) essentially containing rocket propulsion unit ergols. It comprises a long transverse wing (3) with a small back-sweep to favour the lift in the dense layers of the atmosphere and make it possible to climb to high altitudes at a subsonic speed before using the rocket propulsion units. The return is performed by gliding or controlled as for a conventional aircraft.

Abstract translation: 这架飞机包括用于常规飞机在大气中飞行并作为火箭进行高空作战的推进装置（7,16,17）。 它分为有效载荷隔室（8）和基本上包含火箭推进单元麦角的舱室（13）。 它包括长横翼（3），具有小的反向扫掠，有利于大气层中的升力，并且可以在使用火箭推进装置之前以亚音速爬升到高海拔地区。 返回通过滑翔或控制来执行，如同常规飞机。