NESTED CHANNEL DUCTS FOR NOZZLE CONSTRUCTION AND THE LIKE
摘要
<p>A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel is formed in a surface of a gas turbine engine component, and the channel is adapted for conveying a fluid flow from an inlet to an outlet. At least a first sealing member is disposed within the channel and divides the channel into at least a first discrete conduit and a second discrete conduit. A second sealing member encloses the channel to define the second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.</p>
申请公布号
WO2004020805(A1)
申请公布日期
2004.03.11
申请号
WO2003CA01251
申请日期
2003.08.22
申请人
PRATT & WHITNEY CANADA CORP.;PROCIW, LEV, ALEXANDER;SHAFIQUE, HARRIS;SOKALSKI, JOHN;PELLETIER, CLAUDE, RAYMOND
发明人
PROCIW, LEV, ALEXANDER;SHAFIQUE, HARRIS;SOKALSKI, JOHN;PELLETIER, CLAUDE, RAYMOND