Invention Grant
- Patent Title: Aeroengine thrust reverser
- Patent Title (中): 航空发动机推力反向器
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Application No.: US11797444Application Date: 2007-04-03
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Publication No.: US07866142B2Publication Date: 2011-01-11
- Inventor: Peter K Beardsley , Glenn A Knight
- Applicant: Peter K Beardsley , Glenn A Knight
- Applicant Address: GB London
- Assignee: Rolls-Royce plc
- Current Assignee: Rolls-Royce plc
- Current Assignee Address: GB London
- Agency: Manelli Denison & Selter PLLC
- Agent Jeffrey S. Melcher
- Priority: GB0608985.8 20060506
- Main IPC: F02K3/02
- IPC: F02K3/02
Abstract:
A gas turbine engine comprising a core engine a fan and a fan casing surrounding the fan and extending rearwardly to attach to an array of outlet guide vanes characterised in that a cascade is rigidly attached to the fan casing and is connected to the core engine via a second support.
Public/Granted literature
- US20080072571A1 Aeroengine thrust reverser Public/Granted day:2008-03-27
Information query
