Inventor

BAUDASSE YANNICK

FR35 patents

⚠️ This page may combine multiple inventors who share the name “BAUDASSE YANNICK”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

BAUDASSE YANNICK

THALES SA

Tape spring retractable deployable structure and method

Device for unfurling and refurling a flexible structure, and a flexible unfurlable structure and satellite both equipped with such a device

Deployable mast with spontaneous autonomous deployment, and satellite

Tape spring deployable structure

Preloading device for a roller screw mechanism guided in rotation

Manipulation of a satellite in space

Angular positioning device comprising two mechanical movement transmission assemblies which are each imbricated at two dead centres

Motorization system with torque suitable for hinge with crossed winding means

Double rotor stepping motor

Deployable tape spring device having a rollable membrane and casing, and satellite including the same

Motorization system for a hinge with crossed winding means with reliability-enhanced rolling

Long-service-life rotary positioning device for space applications

Deployable structure comprising a set of solar generators, system for deploying such a deployable structure and satellite comprising such a system

Angular positioning device with three dead centres

Actuator for systems for guiding space equipment with a variable rate of rotation

Tape with smooth deployment

Control system for a plurality of electric satellite thrusters and electric propulsion device comprising such a control system

BAUDASSE YANNICK

Self-driven articulation for an articulated assembly such as a satellite solar panel

Self-driven articulation and self-regulated articulated assembly

Deployable structure forming an antenna equipped with a solar generator for a satellite

Compact flexible cardan joint and spacecraft comprising such a joint

Through-pivot with flexible elements and spacecraft comprising such a pivot

Device for protecting an optical instrument of a satellite

Reusable device for holding at least one moving object securely autonomously and without shocks, for spacecraft

Actuation system for antenna reflector with deformable reflecting surface

Differential roller screw

Actuation system for mobile elements with dynamically compensated and opposite relative motions

Device for protection of a multibeam optical instrument

Adapted torque motorisation system for deployable spatial structures

CIT ALCATEL

Device for controlling a relative rotation between two articulated elements and a deployable mechanical structure, particularly for a space vehicle, using at least one device of this type

BLANCHARD LAURENT

Boxed unwindable solar generator

LEGRAND SILVAIN

Active tie-rod system for holding and smoothly releasing space appendages

JEANDOT XAVIER

Webbed through pivot

VEZAIN STEPHANE

Large rigid deployable structures and method of deploying and locking such structures

D ABRIGEON LAURENT

System for deploying spatial appendices and spatial appendix comprising such a system