IP Library Granted Patent US 6,029,455
Granted Patent Utility
US 6,029,455 · App. 08/919,353

Turbojet engine combustion chamber with heat protecting lining

Inventor: Denis Sandelis
Patented Case View Patent ↗
Granted: Feb 29, 2000 Filed: Aug 28, 1997
Inventor
Denis Sandelis
Assignee (at issue)
Societe Nationale d'Etude et de Construction de Moteurs d'Aviation - S.N.E.C.M.A

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Quick Facts
Patent No.
US 6,029,455
App. No.
08/919,353
Filed
1997-08-28
Granted
2000-02-29
Kind
A