Turbomachine with angular air delivery

Power plants – Combustion products used as motive fluid – Coaxial combustion products generator and turbine

Reexamination Certificate

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Details

C060S752000

Reexamination Certificate

active

07549294

ABSTRACT:
A turbomachine assembly comprising: an annular compression section; a casing formed by an outer annular shell (204) and an inner annular shell (206) secured inside the outer shell by means of a plurality of radial support arms (208); an annular combustion section housed inside the casing; and an annular turbine section. The air coming from the compression section presents rotary motion with an angle of inclination relative to a longitudinal axis (X-X) of the turbomachine, and the combustion section includes angular distribution means for determining air flow direction so as to impart on the gas leaving the combustion section rotary motion with an angle of inclination that is equal to or greater than the angle of inclination of the air leaving the compression section, said angular distribution means being formed by the support arms (208), each of which presents an angle of inclination relative to the longitudinal axis (X-X) of the turbomachine that is greater than or equal to the angle of inclination of the air leaving the compression section.

REFERENCES:
patent: 4638628 (1987-01-01), Rice
patent: 4996838 (1991-03-01), Melconian
patent: 1 145 438 (1963-03-01), None
patent: 195 41 303 (1997-05-01), None
patent: 0 590 297 (1994-04-01), None
patent: 1 173 468 (1959-02-01), None

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