Techspace Aero S.a.

Techspace Aero

Safran Aero Boosters Sa

Georges Broers

Nicolas Raimarckers

Albert Cornet

Georges Duchaine

David Depaepe

Denis Bajusz

Xavier Wery

Thomas Colmant

Marc Strengnart

Yves Culot

André Lhoest

Nicholas Raimarckers

Antoine Stephany

The invention relates to a gas flow separator dividing the flow into a primary and a secondary stream, especially for a dual rotor axial turbomachine. The separator comprises a splitter nose of the turbomachine and includes a generally wedge-shaped leading edge in the gas flow to be split. The flow separator also comprises a metal blade having a longitudinal section in the form of an 'S' and located in the nose in contact with the back of the leading edge and extending from the leading edge to a rear end of the separator at some distance from the leading edge, so as to be in contact with a heat source, such as a heat exchanger, located at some distance from the leading edge.

Gas flow separator with a thermal bridge de-icer

A turbo-engine stator blading is disclosed. The turbo-engine stator blading includes a crown of fixed blades mounted on a ring. Each blade includes a platform and each blade is fastened to the ring. The ring includes a plurality of individual receptacles for the each of the platforms, the receptacles being machined in the thickness of the ring, the form of each receptacle being complementary to that of the corresponding platform. By means of the receptacles, the mounting of the blades within the blading is both simple and accurate.

Turbo-engine stator blading, turbo-engine comprising the blading and turbo-engine blade

Growing community of inventors

Hoeselt, Belgium

Georges Broers