Completed Materials & Manufacturing Engineering

Project 4: Next Generation Fan System

In plain English

AI plain-English summary

Rolls-Royce is building lighter fan blades and casings for jet engines out of composite materials instead of metal. The core problem is that metal fan systems are heavy, which limits how much fuel an aircraft can burn and how many passengers it can carry. By switching to composites, the blades and their surrounding casing can shed significant weight per aircraft—the equivalent of carrying seven more passengers and their luggage. The project focused on making these blades, which range from very short to very long, more cheaply and precisely, and on assembling them more efficiently. It also cut the time for a key manufacturing step called debulking by a large margin. If these techniques reach production, future civil aircraft could be noticeably lighter and more fuel-efficient, lowering operating costs for airlines and reducing emissions. The work has already created and secured dozens of jobs in the UK supply chain and strengthened the relationship between Rolls-Royce and the National Composites Centre, leading to further industrial research across aerospace, marine, and nuclear sectors.

View original technical description
Rolls-Royce is developing a composite fan system for deployment in future civil gas turbine engines. The primary aim of a composite fan system is to deliver a significant weight saving. The blades and associated composite engine casings will form part of the new CTi fan system that could reduce weight by up to 1,500lb per aircraft, the equivalent of carrying seven more passengers and their luggage. This project sought to develop, understand and demonstrate aspects of manufacturing technologies required for the production of composite fan blades ranging in length from 60” to 140”. Specific areas of research included: cost reduction; development of manufacturing methods for structural metalwork to very strict tolerances; and improvements to blade assembly techniques. This project raised the Manufacturing Capability Readiness Level (MCRL) to 4, enabling improvements in composite laminate conformance and overall blade dimensional conformance, resulting in blades that offer improved aerodynamic performance and resistance to impact from foreign bodies. Stability and technical capability of the manufacturing process have been demonstrated under controlled conditions. The rate of manufacture for defined components has been demonstrated using a defined manufacturing process. Significant improvements in cycle time have been secured - for example the debulking process, used to remove unwanted variability from design geometry during the composite lay-up process, has been reduced in time by 60%. Rolls-Royce is developing a new, pre-production facility to test these manufacturing techniques in conjunction with the National Composites Centre (NCC) in Bristol, creating a hub of composite knowledge. It is expected that 120 jobs will be secured by the end of 2019 due to the investment. The facility will support the ongoing scope of research and development in gas turbine composite manufacturing technologies. In the UK, 30 people have been employed directly by GKN Aerospace on this project. In the supply chain it is estimated that a further 20 jobs have been generated. These jobs should be secured over the next 4 years towards production. At the National Composites Centre 6 new jobs were created by this project. The project significantly strengthened the relationship between Rolls-Royce and the NCC, expanding the capability of the Centre for industrial research. This has led directly to Rolls-Royce placing further industrial research work at the Centre across Aerospace, Marine and Nuclear sectors. “Working with Rolls-Royce… has benefited the National Composites Centre (NCC) in terms of improving the technical capability of NCC resource and has demonstrated [that] the NCC can deliver technically complex projects, resulting in substantial [projects] being won from Rolls-Royce.” Matt Hocking, NCC Technology Programme Manager

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Related Research

Grants with similar aims, by meaning.

SILOET 2: Project 4 Lightweight Composite Casing Manufacturing Development
SILOET 2: Project 3: Lightweight Fan System Design and Operation
Project 1: Tighter Specification Aerofoils
Project 5: Advanced Fabrication
Project 3: Affordable Blisks

Original classification

Large Project

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