Invention Grant
- Patent Title: Cavity ventilation
- Patent Title (中): 腔通气
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Application No.: US12591151Application Date: 2009-11-10
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Publication No.: US09097140B2Publication Date: 2015-08-04
- Inventor: Zahid M. Hussain
- Applicant: Zahid M. Hussain
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE PLC
- Current Assignee: ROLLS-ROYCE PLC
- Current Assignee Address: GB London
- Agency: Oliff PLC
- Priority: GB0822639.1 20081212
- Main IPC: F02K3/02
- IPC: F02K3/02 ; F01D25/14 ; F02K3/06 ; F02C7/18

Abstract:
A ventilation arrangement for an annular cavity located about the core engine of a gas turbine, the annular cavity having an axis and an inner wall located about the axis and an outer wall radially spaced from the inner wall, the outer wall being interposed between the cavity and an engine bypass duct. The ventilation arrangement comprises a plurality of ventilation ducts passing through said outer wall and providing for fluid communication between the bypass duct and the cavity and a flow diverter arranged at an oblique angle to a radial alignment with said axis so as to induce in the ventilation flow from said ducts a vortical flow within the cavity about the inner wall such that said vortical flow has a vortex width of magnitude substantially equal to that of a diameter of the annular cavity. The ducts may be shaped to provide the flow diverter. The internal geometry of the ducts may provide for a sudden expansion to control the exit profile of the flow into the cavity.
Public/Granted literature
- US20100146986A1 Cavity ventilation Public/Granted day:2010-06-17
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