FUEL STABILIZATION SYSTEM AND FUEL STABILIZATION METHOD FOR FUEL SUPPLY SYSTEM

    公开(公告)号:JP2006322454A

    公开(公告)日:2006-11-30

    申请号:JP2006131008

    申请日:2006-05-10

    Abstract: PROBLEM TO BE SOLVED: To provide a fuel stabilization system capable of removing dissolved oxygen from fuel to raise fuel temperature and being adapted to different demand conditions for removing oxygen. SOLUTION: This fuel stabilization system 10 is provided with a fuel tank 12 for supplying fuel to an engine 15 by a fuel pump 14. Dissolved oxygen is removed from fuel by a fuel stabilization assembly 16 provided with a plurality of oxygen removers 18, 20, 22, 24, 26 arranged in parallel. A part 30 of dissolved oxygen is removed from fuel by each fuel oxygen remover and is exhausted to the outside. Temperature of flowing-in fuel is within a scope of limit temperatures for preventing promotion of generation of insoluble substance under the presence of dissolved oxygen. Since fuel flowing out of the fuel stabilization assembly 16 contains less amount of dissolved oxygen, it is possible to heat fuel up to higher temperatures. Fuel is moved and heated by a heat transfer device 32. Efficiency of the engine is improved by improved temperature characteristic of fuel. COPYRIGHT: (C)2007,JPO&INPIT

    Mixer assembly for gas turbine engine
    2.
    发明专利
    Mixer assembly for gas turbine engine 有权
    燃气轮机发动机混合器总成

    公开(公告)号:JP2012154618A

    公开(公告)日:2012-08-16

    申请号:JP2012010601

    申请日:2012-01-23

    CPC classification number: F23R3/343 F23R3/14 F23R3/18 F23R3/286 Y02T50/675

    Abstract: PROBLEM TO BE SOLVED: To provide a mixer assembly 200 for a gas turbine engine 10.SOLUTION: The mixer assembly 200 includes a main mixer 220 and a pilot mixer 210 concentrically arranged with respect to the main mixer. The main mixer encloses at least part of the pilot mixer. The pilot mixer includes an annular housing 212 defining a cavity 208 to be partitioned from the main mixer. The housing has a front portion 202 and a rear portion 204, a diameter of the rear portion being larger than that of the front portion. The pilot mixer further includes a fuel nozzle 152 enclosed by the front portion of the housing and a partition 214 located downstream of the nozzle and connecting the front portion to the rear portion of the housing. The partition 214 is substantially perpendicular to the rear portion 204 of the housing and defines a corner 206 between the rear portion and the partition.

    Abstract translation: 要解决的问题:提供一种用于燃气涡轮发动机10的混合器组件200.解决方案:混合器组件200包括主混合器220和相对于主混合器同心布置的先导混合器210。 主混合器至少包含一部分先导混合器。 导向混合器包括限定要从主混合器分隔的空腔208的环形壳体212。 壳体具有前部202和后部204,后部的直径大于前部的直径。 先导式混合器还包括由壳体的前部包围的燃料喷嘴152和位于喷嘴下游并将前部连接到壳体的后部的分隔件214。 分隔件214基本上垂直于壳体的后部204并且在后部和分隔件之间限定了角部206。 版权所有(C)2012,JPO&INPIT

    FUEL DEOXYGENATION FOR IMPROVED COMBUSTON PERFORMANCE

    公开(公告)号:CA2545896A1

    公开(公告)日:2006-12-22

    申请号:CA2545896

    申请日:2006-05-04

    Abstract: A method and device of this invention includes a fuel deoxygenator and a heating device for removing dissolved oxygen from fuel and then heating that fuel to a temperature above the temperature that would otherwise produce undesirable insoluble materials from a hydrocarbon fuel. The temperature of the fuel and the amount of dissolved oxygen that is removed from the fuel are adjusted according to the combustion process and optimization of desired combustion characteristic s.

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