Marc Georges Loubet | Researchain

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Archive | 1990

HEAT PROTECTIVE LINING FOR AN AFTERBURNER OR TRANSITION DUCT OF A TURBOJET ENGINE

Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1988

Assembly of two bodies having distinctly different coefficients of expansion

Jean Georges Bouiller; Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1988

Assembly method for two parts having different thermal expansion coefficients

Jean Georges Bouiller; Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1990

Heat insulation structure for an afterburner liner or turbine transition piece

Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1990

Chemise de protection thermique pour canal de post-combustion ou de transition d'un turboréacteur

Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1988

Transition channel for a jet engine

Philippe Marc Denis Gastebois; Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1988

Transition pipe for a jet pipe assembly of a turbojet engine

Philippe Marc Denis Gastebois; Marc Georges Loubet; Gerard Ernest Andre Jourdain

Archive | 1992

METODO DE ENSAMBLADURA DE DOS PIEZAS DE MATERIALES QUE TIENEN DIFERENTES COEFICIENTES DE DILATACION TERMICA.

Jean Georges Bouiller; Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1990

Heat protective liner of passage for afterburning or transition of turbojet engine

Gerard Ernest Andre Jourdain; Marc Georges Loubet

Archive | 1989

Heat shield shroud for post-combustion channel or transition of a turbojet

Gerard Ernest Andre Jourdain; Marc Georges Loubet

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Collaboration

Dive into the Marc Georges Loubet's collaboration.

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Archive Network Publication Hotspot Collaboration

Network

Latest external collaboration on country level. Dive into details by clicking on the dots.

Hotspot

Dive into the research topics where Marc Georges Loubet is active.

Publication

Featured researches published by Marc Georges Loubet.

HEAT PROTECTIVE LINING FOR AN AFTERBURNER OR TRANSITION DUCT OF A TURBOJET ENGINE

Assembly of two bodies having distinctly different coefficients of expansion

Assembly method for two parts having different thermal expansion coefficients

Heat insulation structure for an afterburner liner or turbine transition piece

Chemise de protection thermique pour canal de post-combustion ou de transition d'un turboréacteur

Transition channel for a jet engine

Transition pipe for a jet pipe assembly of a turbojet engine

METODO DE ENSAMBLADURA DE DOS PIEZAS DE MATERIALES QUE TIENEN DIFERENTES COEFICIENTES DE DILATACION TERMICA.

Heat protective liner of passage for afterburning or transition of turbojet engine

Heat shield shroud for post-combustion channel or transition of a turbojet

Collaboration

Dive into the Marc Georges Loubet's collaboration.