Two-stage fluid driven turbine
AssigneeThe Boeing Company
InventorsJohn R. Anderson, Sidney W. Welling
Life of this patent
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Abstract
A two-stage turbine includes a first stage comprising a first stator having blades configured for accelerating the drive fluid to supersonic velocities and directing the fluid to the impulse blades of the first rotor. The turbine's second stage includes a second stator having blades configured for directing the fluid from the first stage to the reaction blades of a second rotor at a sonic velocity. Efficient operation of the turbine over a broad range of drive fluid velocities is achieved by providing the stators and rotors with elliptical leading edges to form high angles of attack and providing extended stator tail sections to control fluid flow to the rotors.
Claims5
A fluid driven turbine comprising:
- a first stage including a first stator and a first rotor, said first stator including a plurality of blades predeterminedly configured to accelerate said drive fluid and direct said drive fluid to said first rotor at a supersonic velocity, said first rotor including impulse blades for responding to said fluid drive from said first stator to produce a rotation of said first rotor, the leading edges of said first stator and first blades having predetermined elliptical sections oriented to form a predetermined angle of attack for providing high efficiency operation over a broad range of turbine operating velocities;
- and
- a second stage including a second stator and a second rotor, said second stator including a plurality of blades configured to receive drive fluid from said first stage and direct said drive fluid to said second rotor at sonic velocity, said second rotor including a plurality of reaction blades for responding to said drive fluid from said second stator to produce rotation of said second rotor, the leading edges of said second stator and second rotor blades having predetermined elliptical sections oriented to form a predetermined angle of attack for providing high efficiency operation over a broad range of turbine operating velocities and the trailing edges of said first and second rotors being elliptical in configuration.
Dependencies are inferred from the claim text.