By submitting this form, you are agreeing to the Terms of Use and Privacy Policy.
Coming Soon
INTRODUCTION
The power part of an aircraft propulsion system is an aircraft engine, often known as an aero engine. Although some aircraft have been rocket-powered and several small unmanned aerial vehicles have employed electric motors recently,the piston engines and gas turbines still account for the majority of aircraft engines.
Propellers are not included but other parts and accessories required for its operation such as turbo superchargers are; An aeroplane is propelled by the push created by its powertrain, or engine. A propeller produces thrust in conjunction with reciprocating and turboprop engines. By accelerating the airflow through the engine, turbofan and the jet engines produce thrust.
GLOBAL AIRCRAFT HIGH-POWERED ENGINE MARKET SIZE AND FORECAST
The Global Aircraft High-powered engine Market accounted for $XX Billion in 2022 and is anticipated to reach $XX Billion by 2030, registering a CAGR of XX% from 2023 to 2030.
NEW PRODUCT LAUNCH
In order to compete with the Engine Alliance GP7000, Rolls-Royce plc created the Trent 900, a high-powered engine, to power the Airbus A380. This first application, which was first made for the Boeing 747-500/600X, was eventually discarded. Instead, it was made for the A3XX, which was introduced as the A380.
It was certified by the EASA and originally tested by on an A340 testbed. The Trent 900 has a 2.95 m fan and the three shaft architecture of the Rolls-Royce Trent family, producing up to 374 kN . It features a bypass ratio of 8.5-8.7:1 and an overall pressure ratio of 37-39:1.
The Trent 900 is a member of the Rolls-Royce Trent series and is an axial flow are high powered engine with three coaxial shafts. The 6-stage HP compressor and the 8-stage IP compressor are both powered by a single stage turbine, with the HP spool rotating anticlockwise to the other two.
The 2.95 m fan with sweeping blades is driven by a 5-stage LP turbine. It is the run by an EEC and has a single annular combustor. It has a certified thrust range of 334.29 to 374.09 kN.
COMPANY PROFILE
THIS REPORT WILL ANSWER FOLLOWING QUESTIONS