Jet engine having radial turbine blades and flow-directing turbi

Details Jet engine having radial turbine blades and flow-directing turbi Jet engine having radial turbine blades and flow-directing turbi

1997-10-28

1999-12-07

Freay, Charles G.

Power plants

Reaction motor

Interrelated reaction motors

60 3937, 60 3952, 60 3975, F02R 302, F02C 708

Patent

active

059963360

ABSTRACT:
A jet aircraft engine having an improved turbine section with curved intake manifolds to direct combustion gasses from the engine's combustion chamber into the turbine housing on a chordal flow path through the turbine generally perpendicular to the turbine rotor's axis of rotation. The turbine rotor has a number of radially extending turbine blades for transmitting energy from the combustion gasses to shaft work to drive the engine's fan and compressor. Exhaust manifolds can also be provided, directing the flow of exhaust gasses from the turbine to the engine's intake, and having noise and emissions control capability.

REFERENCES:
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patent: 2648491 (1953-08-01), Wood
patent: 2990685 (1961-07-01), Hoover, Jr.
patent: 3070131 (1962-12-01), Wheatley
patent: 3359908 (1967-12-01), Toma
patent: 3782108 (1974-01-01), Holste
patent: 3923416 (1975-12-01), Frey
patent: 3934418 (1976-01-01), DeBaun
patent: 4073069 (1978-02-01), Basmajian
patent: 4641498 (1987-02-01), Markovitch et al.
Michael Valenti,"Upgrading Jet Turbine Technology," Mechanical Engineering (Dec., 1995).
Michael Valenti,"New Gas-Turbine Designs Push The Envelope," Mechanical Engineering (Aug., 1997).
Franklin van den Hout and Jo Koullen,"A Tiny Turbojet For Model Aircraft," Mechanical Engineering (Aug., 1997).
Bill Gunston, "Jet and Turbine Aero Engines," (1995).

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