COMBUSTION MODULE FOR A GAS TURBO ENGINE WITH CHAMBER BOTTOM STOP

Number of patents in Portfolio can not be more than 2000

United States of America

SERIAL NO

16423953

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Importance

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Abstract

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The invention concerns a turbo engine comprising a combustion chamber (110) arranged inside the outer housing (112) and comprising an internal revolution wall (118) and an external revolution wall (116). First stop parts (54) and second stop parts (56) fixed respectively to the outer housing and to the combustion chamber are provided, the first and second stop parts being adapted to come to a substantially axial stop two by two by forming stop pairs (58).

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES75015 PARIS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
BONNEFOI, Damien MOISSY-CRAMAYEL, FR 2 0
JOORY, Dan Ranjiv MOISSY-CRAMAYEL, FR 4 1
LUNEL, Romain Nicolas MOISSY-CRAMAYEL, FR 53 333
NAMER, Luc MOISSY-CRAMAYEL, FR 1 0
PIEUSSERGUES, Christophe MOISSY-CRAMAYEL, FR 29 342
RAULIN, Dominique MOISSY-CRAMAYEL, FR 18 185
VILLENAVE, Benjamin Frantz Karl MOISSY-CRAMAYEL, FR 6 1

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