Power plants – Combustion products used as motive fluid – With variable oxidizer control
Patent
1992-03-12
1993-08-17
Bertsch, Richard A.
Power plants
Combustion products used as motive fluid
With variable oxidizer control
60759, F23R 322
Patent
active
052358054
ABSTRACT:
An oxidizer intake flow control system is disclosed for a gas turbine engine combustion chamber. The chamber has an oxidizer intake assembly which extends through the wall of the chamber such that an inlet aperture of the oxidizer intake and an exhaust aperture of the oxidizer intake are located on opposite sides of the wall defining the combustion chamber. An oxidizer intake sleeve defines a central passage through which oxidizer may pass into the combustion chamber. The intake passage extends along a central axis and the intake assembly is attached to the wall of the combustion chamber such that it is rotatable about this central axis. The inlet aperture and/or the exhaust aperture is located in a plane extending non-perpendicularly to the central axis. The combustion chamber may have several oxidizer intake assemblies extending through the combustion chamber walls. The intake assemblies may be interconnected such that they may be simultaneously rotated with respect to the combustion chamber wall.
REFERENCES:
patent: 3099134 (1963-07-01), Calder et al.
patent: 3280555 (1966-10-01), Charpentier et al.
patent: 3490230 (1970-01-01), Pillsbury et al.
patent: 3593518 (1971-07-01), Gerrard
patent: 3958413 (1976-05-01), Cornelius et al.
patent: 4050240 (1977-09-01), Vaught
Barbier Gerard Y. G.
Bardey Xavier M. H.
Desaulty Michel A. A.
Meunier Serge M.
Bertsch Richard A.
Societe Nationale d'Etude et de Construction de Moteurs d'Aviati
Thorpe Timothy S.
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