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Sub-Project 3 for Booster

SP3 evaluates the slow and high-speed booster (low-pressure compressors) concepts applicable to the different configurations.

Objectives


• SP3 will investigate and test highly loaded Booster technology adapted for the 3 different engine configurations presented in VITAL, i.e. the Direct Drive TurboFan (DDTF), the Contra Rotative TurboFan (CRTF)and Geared TurboFan (GTF)
• SP3 will design and test a composite rotor to reduce Booster weight
• SP3 will develop a numerical tool to predict erosion

Challenge

Booster01




Approach

• A low speed highly loaded scaled down stage will be designed and tested. Casing treatment and secondary flow models will be validated
• A Booster composite rotor will be designed to reach the weight reduction target. An erosion model will be developed
• A low speed DDTF/CRTF highly loaded full scale Booster will be designed and tested, implementing casing treatments
• A high speed GTF scaled down Booster will be designed and tested

Expected results

Booster02




See more

Sub-Project 1 for whole engine assessment
SP1 oversees the technical unity of the other sub-projects, and is in charge of design for each of the three engine architectures.
Sub-Project 2 for Fan modules
SP2 tests new fan module concepts and measures their aero-acoustic performance (contra-fan or lightweight fan).
Sub-Project 4 for Structures
SP4 focuses on new lightweight structural material (Hot and cold structures form the engine " back bone"). They provide basic engine stiffness and transfer high mechanical loads to and from the engine interior. Therefore the structures contributes to 15 - 20% of the engine weight.
Sub-Project 5 for Low pressure shaft
SP5 tests new concepts for a low-pressure shaft (which has to handle higher torque loads because of the slower fan speed). (Source : Brochure)
Sub-Project 6 for Low pressure turbine
SP6 seeks to identify new, lighter and quieter turbine concepts.
Sub-Project 7 for Installation
SP7 evaluates the impact of installing a high-bypass-ratio engine under the wing.