RE: RR SP8 Apr 2025 09:31
Flyingdale
What you say is Not strictly true.
“Rolls-Royce manufactures propulsion engines at several locations, including Derby, England, and in North America, with facilities in Cypress, California, Reston, VA, and Novi, Michigan, among other.
Here's a more detailed breakdown:
Derby, England: This is a major manufacturing hub for Rolls-Royce, including the Trent XWB engine, which is the exclusive powerplant for the Airbus A350.
Cypress, California: This facility focuses on research and development of ceramic matrix composite (CMC) materials and processes for next-generation aircraft engine components.
Reston, VA: Rolls-Royce North America is located here.
Novi, Michigan: This is a regional headquarters for MTU America, a wholly owned subsidiary of Rolls-Royce Power Systems AG.
Aiken, South Carolina: MTU America has manufacturing operations here.
Mankato, Minnesota: MTU Onsite Energy is located here.
Bristol, UK: Rolls-Royce has a new facility in Bristol that develops jet engine technologies for cleaner, quieter, and more efficient engines.
Thailand: Rolls-Royce has a strong presence in Thailand, with Leistritz and Senior Aerospace supporting the manufacture of compressor blades for Trent engines, and Triumph Structures providing the Trent 700 fan case lining.
Malaysia: Rolls-Royce has a 25-year agreement with UMW Aerospace Sdn. Bhd. to build and assemble fan cases for Trent 1000 and Trent 7000 aero engines.
Singapore: Rolls-Royce has a campus in Singapore, where UMW delivered its first made-in-Malaysia Trent 1000 fan case.
Canada: Rolls-Royce has over 1,000 employees in Canada.
India: Force MTU Power Systems, a joint venture between Force Motors and Rolls-Royce Power Systems AG, manufactures MTU Series 1600, 10 and 12 cylinder diesel engines for power generation, under floor rail and other applications.
Germany: Rolls-Royce Power Systems AG is a major part of the company's global operations.
Rauma, Finland: Rolls-Royce has a test bed 80 facility, which is the largest of its kind, sized for engines of up to 140,000 lbf (620 kN) of thrust. “