发明名称 HEAT EXCHANGER FOR GAS TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To provide a heat exchanger having a plurality of joined, mutually supporting heat exchanger pipes.SOLUTION: A heat exchanger apparatus (40, 140, 240) for a gas turbine engine includes a plurality of heat exchanger pipes (48, 148, 248) each having first and second ends. The heat exchanger pipes (48, 148, 248) are disposed in a repeating pattern such that each heat exchanger pipe (48, 148, 248) is joined to at least one other heat exchanger pipe. Each heat exchanger pipe (48, 148, 248) can be joined to other heat exchanger pipes (48, 148, 248) at two or more locations.SELECTED DRAWING: Figure 1
申请公布号 JP2016180404(A) 申请公布日期 2016.10.13
申请号 JP20160053241 申请日期 2016.03.17
申请人 GENERAL ELECTRIC CO <GE> 发明人 JEFFREY DOUGLAS RAMBO;GERSTLER WILLIAM DWIGHT;JAMES MICHAEL KOSTKA;JOHN WILLIAM MOORES
分类号 F02C7/06;F01D25/18;F02K3/06;F28D7/08 主分类号 F02C7/06
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