Invention Grant
- Patent Title: Duct wall for a fan of a gas turbine engine
- Patent Title (中): 燃气涡轮发动机风机的管壁
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Application No.: US12768316Application Date: 2010-04-27
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Publication No.: US08434995B2Publication Date: 2013-05-07
- Inventor: Clare L. Pool , Kenneth F. Udall , Richard G. Stretton , Julian M. Reed
- Applicant: Clare L. Pool , Kenneth F. Udall , Richard G. Stretton , Julian M. Reed
- Applicant Address: GB London
- Assignee: Rolls-Royce PLC
- Current Assignee: Rolls-Royce PLC
- Current Assignee Address: GB London
- Agency: Oliff & Berridge, PLC
- Priority: GB0907582.1 20090505
- Main IPC: F01D21/00
- IPC: F01D21/00

Abstract:
A gas turbine engine fan casing duct wall comprises an intake section and a containment casing, provided respectively with flanges. An acoustic flutter damper is secured between the flanges. The acoustic flutter damper has a skin accommodating an internal structure that dampens fan blade flutter. The skin is secured to the flanges at separate locations. In normal operation of the engine, the internal structure is sufficiently robust to support loads transmitted through the acoustic flutter damper between the intake section and the containment casing. If a blade or blade fragment detaches, the resulting deflection wave in the containment case ruptures the internal structure, and the load path between the intake section and the containment casing passes along the skin, which consequently maintains the connection between the intake duct and the containment casing, while permitting substantial radial deflection of the containment casing relative to the intake section.
Public/Granted literature
- US20100284790A1 DUCT WALL FOR A FAN OF A GAS TURBINE ENGINE Public/Granted day:2010-11-11
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