Invention Grant
- Patent Title: Geared gas turbine engine
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Application No.: US17193323Application Date: 2021-03-05
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Publication No.: US11542890B2Publication Date: 2023-01-03
- Inventor: Alastair D Moore , Robert J Telling
- Applicant: ROLLS-ROYCE plc
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Agency: Oliff PLC
- Priority: GB1820945 20181221
- Main IPC: F02K3/06
- IPC: F02K3/06 ; F02C7/24

Abstract:
A gas turbine engine generates noise during use, and one particularly important flight condition for noise generation is take-off. A gas turbine engine that has high efficiency provides low noise, in particular from the fan and the turbine that drives the fan. Values are defined for a noise parameter NP that results in a gas turbine engine having reduced combined fan and turbine noise.
Public/Granted literature
- US20210190011A1 GEARED GAS TURBINE ENGINE Public/Granted day:2021-06-24
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