VHBR Engine - IP Turbine Technology

Topic description

Scope:

The development and demonstration of various technologies required to deliver a High-Speed Low Pressure Turbine module for very high bypass ratio engine application (Aerodynamic, Aeromechanical, Material, Manufacturing and Methods) maximising turbine efficiency within a compact structure in order to maximize and validate overall performance, structural integrity, reduced weight, cost and noise benefits. Includes the design, development, build and test of modules required to demonstrate these technologies at a scale suitable for large engines in whole engine ground and flight testing.

Please refer for the full and formal topic description to Annex I of the Clean Sky 2 Work Plan 2014-2015 (see under the tab "Topic Conditions and Documents")