公开(公告)号：US20240228067A1

公开(公告)日：2024-07-11

申请号：US18557222

申请日：2022-04-14

Applicant: AIRBUS DEFENCE AND SPACE SAS

Inventor： Delphine CARPONCIN ,  Sébastien LEFOLL ,  Christophe FIGUS

IPC: B64G1/50 ,  B33Y80/00 ,  B64G1/10 ,  B64G1/58

CPC classification number: B64G1/503 ,  B64G1/1028 ,  B64G1/58 ,  B33Y80/00

Abstract: A thermoregulated thermomechanical structure for a focal plane suitable for operating in a space environment is disclosed having an interface for supporting dissipative electronic equipment, the structure being monolithic, metallic and including a radiator and a first two-phase heat-transfer fluid transport cavity, extending within the radiator and providing direct thermal transport between the interface and the radiator. The structure also includes a second cavity encapsulating a phase change material.

公开(公告)号：US20200247565A1

公开(公告)日：2020-08-06

申请号：US16637473

申请日：2018-08-07

Applicant: Airbus Defence and Space SAS

Inventor： Delphine CARPONCIN ,  Christophe FIGUS

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

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.