Invention Application
- Patent Title: EFFICIENT AIRCRAFT ENGINE
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Application No.: US17731673Application Date: 2022-04-28
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Publication No.: US20220268216A1Publication Date: 2022-08-25
- Inventor: Roderick M TOWNES , Michael J WHITTLE , Pascal DUNNING
- Applicant: ROLLS-ROYCE plc
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Priority: GB1813081.5 20180810
- Main IPC: F02C7/36
- IPC: F02C7/36 ; F01D5/28

Abstract:
A highly efficient gas turbine engine is a system wherein the fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.
Public/Granted literature
- US12037942B2 Efficient aircraft engine Public/Granted day:2024-07-16
Information query
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