Turbojet diffuser

Power plants – Combustion products used as motive fluid – Having mounting or supporting structure

Reexamination Certificate

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C060S751000, C415S207000

Reexamination Certificate

active

11039887

ABSTRACT:
A turbojet diffuser disposed between a compressor and a combustion chamber, and secured to an outer upstream annular flange of an outer casing of the combustion chamber by suspension means which comprise a first frustoconical wall extending from the outer longitudinal wall of the diffuser towards the combustion chamber, and a second frustoconical wall extending towards the compressor between the first frustoconical wall and the outer casing of the combustion chamber.

REFERENCES:
patent: 2445661 (1948-07-01), Constant et al.
patent: 5592821 (1997-01-01), Alary et al.
patent: 2002/0092303 (2002-07-01), Al-Roub et al.
patent: 0 523 935 (1993-01-01), None

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