公开(公告)号：US10689134B2

公开(公告)日：2020-06-23

申请号：US15764645

申请日：2016-09-19

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Robert Oldham ,  Philippe Mayo ,  Franck Levallois ,  Christophe Figus ,  Daniel Logut

IPC: B64G1/64 ,  F42B15/36 ,  B64G1/22 ,  B64G1/00

Abstract: Disclosed is a device for controlled separation of a first so-called stationary part and a second so-called mobile part, the stationary part having a stationary connecting surface opposite a mobile connecting surface of the mobile part, the stationary part having a different thermal expansion coefficient from that of the mobile part, the separation device including: at least one connecting agent arranged in a layer between the stationary connecting surface and the mobile connecting surface, at least one device for heating at least one of the stationary part and the mobile part, and at least one system for controlling the heating device.

公开(公告)号：US11505340B2

公开(公告)日：2022-11-22

申请号：US16637473

申请日：2018-08-07

Applicant: Airbus Defence and Space SAS

Inventor： Delphine Carponcin ,  Christophe Figus

IPC: B64G4/00 ,  B21F1/00 ,  B64G99/00 ,  B64G1/22

Abstract: A method for manufacturing in space a rigid structure having a lattice is disclosed. The method includes creating of at least two framework elements from a coil of metal strip or wire, and creating of the lattice by cold-connecting the framework elements.

公开(公告)号：US09957919B2

公开(公告)日：2018-05-01

申请号：US14427963

申请日：2013-09-10

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Christophe Figus

IPC: F02K9/94 ,  F02K9/72 ,  F02K9/10

CPC classification number: F02K9/72 ,  F02K9/10 ,  F02K9/94 ,  F05D2300/501 ,  F05D2300/514

Abstract: An anaerobic propulsion device of hybrid type. The propulsion device includes a combustion chamber into which an oxidant is injected thereto comes into contact with a fuel. The chamber includes an orifice, notably a nozzle, to inject the combustion gases. The fuel takes the form of solids divided into granules, typically grains, powder or beads. The propulsion device further includes a segregation device arranged between a reservoir for granules of solid fuel, and the combustion chamber. The segregation device is configured to prevent granules of fuel in solid form from passing between the reservoir and the combustion chamber. The segregation device includes orifices to allow the passage of the fuel, once the fuel has become pasty, liquid or vaporized.