发明名称 GAS TURBINE ENGINE SYSTEMS
摘要 - 33 - Gas Turbine Engine SystemsAbstract 5 A gas turbine engine 10 comprises at least one rigid raft assembly that has afluid passageway 210 at least partially embedded therein. The fluid passageway 210 is at least a part of a fluid system. In addition to the fluid passageway 210, the rigid raft assembly 200 also has at least a part of another system. For example, the rigid raft assembly may also include 10 electrical conductors 252, which are part of an electrical system. The rigid raft assembly 200 may be lighter, easier to assemble, more robust and more compact than conventional solutions for providing systems to gas turbine engines.Fig. 215
申请公布号 SG191525(A1) 申请公布日期 2013.07.31
申请号 SG20120092847 申请日期 2012.12.17
申请人 ROLLS-ROYCE PLC 发明人 PAUL BROUGHTON;RICHARD PEACE;GARY ALAN SKINNER;ROBIN CHARLES KENNEA
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