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公开(公告)号:CA2554309A1
公开(公告)日:2007-03-07
申请号:CA2554309
申请日:2006-07-27
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SABATINO DANIEL R , SAHM MICHAEL K , BAYT ROBERT L , KASLUSKY SCOTT
Abstract: A fuel based thermal management system according to the present inventi on includes a fuel stabilization system which permits the fuel to exceed the traditional coking temperatures. An air-to-fuel heat exchanger operates as an environmental control system (ECS) pre-cooler such that the heat from the engine compresso r bleed air is rejected into the fuel to maintain engine operating efficiency.
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公开(公告)号:CA2488316A1
公开(公告)日:2005-07-20
申请号:CA2488316
申请日:2004-11-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SABATINO DANIEL , SPADACCINI LOUIS J , KASLUSKY SCOTT
Abstract: A fuel based thermal management system includes a fuel stabilization system which permits the fuel to exceed the traditional coking temperatures. High temperature components are arranged along the fuel flow path such that even at the highe r operating temperatures the fuel operates as a heat sink to transfer heat from high temperature components to the fuel. An optimal high temperature ester-based oil permits an oil-loop to exceed current oil temperature limits and achieve a high temperature to permit efficient rejection of heat to the fuel late in the fuel flow path.
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公开(公告)号:CA2488316C
公开(公告)日:2008-02-05
申请号:CA2488316
申请日:2004-11-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SABATINO DANIEL , SPADACCINI LOUIS J , KASLUSKY SCOTT
Abstract: A fuel based thermal management system includes a fuel stabilization system which permits the fuel to exceed the traditional coking temperatures. High temperature components are arranged along the fuel flow path such that even at the highe r operating temperatures the fuel operates as a heat sink to transfer heat from high temperature components to the fuel. An optimal high temperature ester-based oil permits an oil-loop to exceed current oil temperature limits and achieve a high temperature to permit efficient rejection of heat to the fuel late in the fuel flow path.
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公开(公告)号:CA2492309A1
公开(公告)日:2005-07-29
申请号:CA2492309
申请日:2005-01-13
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KASLUSKY SCOTT , SPADACCINI LOUIS J , MCLAUGHLIN ROBERT A
IPC: B64D37/00 , B01D19/00 , B01D61/00 , F02C7/22 , F02C7/232 , F02C7/236 , F02M37/20 , F02M37/22 , B64D37/34
Abstract: A fuel delivery system for a gas turbine engine includes a main fuel pu mp supplying fuel to a fuel-metering device. The operational flow range of the fuel system is dependent on a minimum net positive suction pressure at the main pump inlet required to prevent pump cavitation. A mixture of fuel and dissolved gases increases the minimum net positive suction pressure required to prevent cavitation. A fuel de-aerator including a permeable membrane removes dissolved gases fr om the fuel to eliminate formation of dissolved gases. The elimination of dissolved gases from within the liquid fuel reduces the required net positive suction pressure, enabling a greater operational flow range.
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