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US 2024/0133352 A1Published application
Duplex Turbine Guide Vane Assembly
AssigneeATRX, Inc.
InventorsJohn A Bossard, John L Bergmans
Life of this patent
Estimating the term…
Abstract
A Duplex Turbine Guide Vane (DTGV) assembly for a turbojet engine includes DTGVs arranged on a non-rotating guide vane ring configured to be positioned coaxially in apposition with a rotatable turbine wheel comprising turbine blades. Each of the DTGVs has an internal channel configured for receiving a gas and delivering the gas toward the turbine blades.
Claims14
A Duplex Turbine Guide Vane (DTGV) assembly for a turbojet engine, said DTGV turbine assembly comprising:
- a plurality of DTGVs arranged on a non-rotating guide vane ring wherein:
- said non-rotating guide vane ring is configured to be positioned coaxially in apposition with a rotatable turbine wheel comprising turbine blades and
- each of the DTGVs comprises an internal channel configured for receiving a gas and delivering said gas toward the turbine blades.
Dependencies are inferred from the claim text.