Invention Grant
- Patent Title: Nacelle for gas turbine engine and aircraft comprising the same
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Application No.: US17152075Application Date: 2021-01-19
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Publication No.: US11408306B2Publication Date: 2022-08-09
- Inventor: Fernando L Tejero Embuena , David G. Macmanus , Christopher T J Sheaf
- Applicant: ROLLS-ROYCE plc
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Priority: GB2001971 20200213
- Main IPC: F01D25/24
- IPC: F01D25/24 ; B64D27/12 ; F02C7/04

Abstract:
A nacelle for housing a fan within a gas turbine engine having a longitudinal centre line includes a leading edge and a trailing edge. A nacelle length (Lnac) is defined as an axial distance between the leading edge and the trailing edge. An azimuthal angle (θ) is defined about the longitudinal centre line. The nacelle length (Lnac) varies azimuthally. The nacelle length (Lnac) decreases azimuthally from an inboard end of the nacelle to an outboard end of the nacelle.
Public/Granted literature
- US20210254507A1 NACELLE FOR GAS TURBINE ENGINE AND AIRCRAFT COMPRISING THE SAME Public/Granted day:2021-08-19
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