Invention Grant
- Patent Title: Aeroengine ventilation system
- Patent Title (中): 航空发动机通风系统
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Application No.: US11783996Application Date: 2007-04-13
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Publication No.: US07861513B2Publication Date: 2011-01-04
- Inventor: Richard G. Stretton
- Applicant: Richard G. Stretton
- Applicant Address: GB London
- Assignee: Rolls-Royce PLC
- Current Assignee: Rolls-Royce PLC
- Current Assignee Address: GB London
- Agency: Oliff & Berridge, PLC
- Priority: GB0607794.5 20060420
- Main IPC: F02K3/02
- IPC: F02K3/02

Abstract:
A gas turbine engine comprising a ventilation zone defined between a core engine casing and a core fairing and having a discharge nozzle, the engine further comprises a pre-cooler having a flow of coolant therethrough and which coolant being ducted into the ventilation zone wherein an additional ventilation zone outlet system is provided and comprises a variable area outlet.
Public/Granted literature
- US20070245711A1 Aeroengine ventilation system Public/Granted day:2007-10-25
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