OPERATING METHOD OF COMBUSTION EQUIPMENT AND COMBUSTION EQUIPMENT

    公开(公告)号:JPH08166108A

    公开(公告)日:1996-06-25

    申请号:JP16125195

    申请日:1995-06-27

    Abstract: PURPOSE: To reduce the emission of harmful substances related especially to the emission of NOx even in the case of employing liquid fuel and gaseous fuel or further even in the case of mixing operation of both fuels. CONSTITUTION: Mixture 6 consisting of air 3 and re-cycled flue gas 4 is conducted to flow into a burner 100 as combustion air 115 for a first combustion stage 1. Then, the heat amount of high-temperature gas from the first combustion stage 1 is regulated before sending the same into a second combustion stage 2, and mixture 14 consisting of the fuel 15 and the re-cycled flue gas 4 is introduced into the high-temperature gas to generate combustion in the second combustion stage 2 by self-ignition.

    COMBUSTION APPARATUS
    2.
    发明专利

    公开(公告)号:JPH08189641A

    公开(公告)日:1996-07-23

    申请号:JP18433095

    申请日:1995-07-20

    Abstract: PROBLEM TO BE SOLVED: To suppress discharge of all toxic materials such as UHC, CO generated at burning by providing a notable cross sectionally enlarged part for self- igniting a fuel and air mixture at a second stage in a mixer for forming the mixture at a first stage in a multi-stage burner. SOLUTION: A first stage 1 has a mixer 100 for forming a fuel and air mixture 19 at a head side, a catalyst 3 disposed at the downstream side of the mixer 100 and completely burns the mixture 19 by the catalyst 3. A vortex- inducing unit 200 is disposed at the downstream side of the catalyst 3, and thereby hot gas, 3, turns into a swirling flow. Gas fuel and/or liquid fuel 9 can be injected in a gas main flow 4 at the downstream side of the unit 200. A second stage 2, provided continuing to the flowing direction forms an intrinsic burning zone 11, has a notable cross sectional enlarged part 12, which specifies the flow cross sectional area of the starting end side of the stage 2, thereby effectively self-igniting the mixture 19 to stabilize a flame surface 21.

    BURNER FOR OPERATING COMBUSTION ENGINE, GAS TURBINE GROUP COMBUSTION CHAMBER OR COMBUSTION FACILITY

    公开(公告)号:JPH06241423A

    公开(公告)日:1994-08-30

    申请号:JP1658094

    申请日:1994-02-10

    Abstract: PURPOSE: To provide an operating method for a burner for operating a heat engine to use fuel containing a highly reactive gas component in addition to combustion of normal oil or natural gas and having a medium calorific value without needing for dilution by steam and nitrogen before combustion. CONSTITUTION: For fuel 15 containing a highly reactive gas component and having a medium calorific value, at least one row of nozzles 10 are arranged on the periphery of partial conical bodies 1 and 2 near the burner outlet at a distance of approximately maximum 30% of a nominal burner diameter. For the highly reactive fuel 15, one fuel conduit 11 and a distributing passage 17 are arranged in a range of a nozzle 10. Further, two systems for injecting two gaseous fuels 14 and 15 are constituted unrelatedly independently from each other.

    COOLING DEVICE FOR COOLING SURFACE IN IMPACT TYPE

    公开(公告)号:JPH06294330A

    公开(公告)日:1994-10-21

    申请号:JP33252493

    申请日:1993-12-27

    Abstract: PURPOSE: To conduct impingement cooling for a cooling surface by avoiding unfavorable lateral flow, and by evading preliminary heating of cooling air, in a type in which a cooling surface and a cover surface are disposed in parallel each other. CONSTITUTION: Trapezoid molding members 7 which are connected to one another via a cooling surface 5 in a direction orthogonal to a flow direction of cooling air between the cooling surface 5 forming an inside of a combustion chamber and a cover surface 6 disposed in parallel thereto and which are opened respectively in their narrow sides are arranged at a constant distance. The cooling air is introduced into a feed chamber through a supplying face 1 of the member 7 facing in the cover surface 6, and impinges on the cooling surface 5 through perforations 8. Heated air is intruded into a trapezoidal backflow passage 3 through a gap between overflow surfaces 2, but cooling action for air exiting from the neighboring members 7 is not impaired in this case. A cooling surface 4 is cooled impingingly thereby.

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