Invention Grant
- Patent Title: Aeroengine bleed valve
- Patent Title (中): 航空发动机泄放阀
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Application No.: US11878542Application Date: 2007-07-25
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Publication No.: US08128347B2Publication Date: 2012-03-06
- Inventor: Jagdish S. Sokhey
- Applicant: Jagdish S. Sokhey
- Applicant Address: GB London
- Assignee: Rolls-Royce PLC
- Current Assignee: Rolls-Royce PLC
- Current Assignee Address: GB London
- Agency: Oliff & Berridge, PLC
- Priority: GB0616847.0 20060825
- Main IPC: F01D17/00
- IPC: F01D17/00

Abstract:
A bleed valve for a gas turbine engine, the valve comprises a diffuser having a plurality of holes through which a bleed fluid flows and into a fluid stream. The diffuser is characterized in that at least some of the holes are at least partially tangentially angled relative to the bleed fluid flow through the valve so that the bleed air forms a vortex to enhance mixing with the fluid stream.
Public/Granted literature
- US20080050218A1 Aeroengine bleed valve Public/Granted day:2008-02-28
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