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序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
41 一种节能环保气化式二级燃烧器 CN201410628179.5 2014-11-10 CN104406166A 2015-03-11 杜荣建
发明涉及一种节能环保气化式二级燃烧器,包括液体进管、液体夹套、气体出管及喷火盘,在圆筒形液体夹套下部的外缘柱面上连通固装液体进管,在液体夹套外缘柱面的上部位置连通固装气体出管,该气体出管向下回转后连通固装呈平状态的圆环形喷火盘,该喷火盘的外缘连通均布间隔制有多个喷火口。本燃烧器是在燃烧器的喷火筒内同轴安装该二级燃烧器,设置在圆柱状喷火头的前端,通过乙醇液体燃料的挥发在喷火盘前端点燃,液体燃料以气态方式燃烧,同时可燃烧圆柱状喷火头所未燃烧充分的燃料,不但增加了火焰强度,提高燃烧器的能,同时也达到了节能效果。
42 气化燃烧器 CN201310280089.7 2013-07-05 CN104279558A 2015-01-14 蔡巍; 曹琴; 付玉玲; 孙继国; 李本伟; 王鹏; 邵天成; 姜志军
发明公开了一种气化燃烧器,涉及燃烧器技术领域。解决了现有技术存在容易过热损坏、使用寿命较短的技术问题。本发明提供的气化燃烧器,包括螺旋槽气化器、气化油枪、连接管以及进油管,其中:所述螺旋槽气化器设置有内腔,所述进油管的出油口与所述螺旋槽气化器的进油口相连通;所述螺旋槽气化器的出油口通过所述连接管与所述气化油枪的进油口相连通;所述气化油枪的燃料出口朝向或嵌入于所述螺旋槽气化器的内腔。本发明用于防止燃烧器的气化油枪堵塞,同时提高燃烧器的耐热性以及使用寿命。
43 控制流体的射流运动 CN88103204 1988-04-15 CN1018018B 1992-08-26 拉塞尔·埃斯克特; 古阿曼·杰罗尔德·内森
一种流体混合装置,它带有一个腔,腔中设有一个流体进口和一个相对的流体出口。该装置使完全占据入口的第一流体的流动与出口上游的腔壁分离。流动分离和出口间的距离相对于腔的宽度足够长,以使分离了的流动自身不对称地重新附着到出口上游的腔壁上并经出口不对称地喷出该腔。在重新附着状态下的第一流体的逆向流动和/或通过出口诱发的第二流体的流动由此在流动分离和重新附着之间的腔中涡旋,并诱发分离/重新附着流动的旋进。这种旋进增强该流动与来自腔外的第二流体的混合。
44 控制流体的射流运动 CN88103204 1988-04-15 CN1032385A 1989-04-12 拉塞尔·埃斯克特; 古阿曼·杰罗尔德内森
一种流体混合装置,它带有一个腔,腔中设有一个流体进口和一个相对的流体出口。该装置使完全占据入口的第一流体的流动与出口上游的腔壁分离。流动分离和出口间的距离相对于腔的宽度足够长,以使分离了的流动自身不对称地重新附着到出口上游的腔壁上并经出口不对称地喷出该腔。在重新附着状态下的第一流体的逆向流动和/或通过出口诱发的第二流体的流动由此在流动分离和重新附着之间的腔中涡旋,并诱发分离/重新附着流动的旋进。这种旋进增强该流动与来自腔外的第二流体的混合。
45 HEATING SYSTEM EP15757835.2 2015-03-05 EP3126748A1 2017-02-08 MURILLO, Luis
This invention materially enhances the quality of the environment and mankind by contributing to the restoration or maintenance of the basic life-sustaining natural elements, by reducing the amount of carbon monoxide introduced to the atmosphere from a combustion system, achieved by furnishing a system's approach to optimize the amount of oxygen to be chemically combined with fuel upon ignition of both allowing the correct amount of carbon to combine with the correct amount of oxygen thus fully release the thermal energy stored therein.
46 Verfahren und Brenner zur Verfeuerung von Brennstoff EP88106197.2 1988-04-19 EP0289851A3 1989-05-24 Bilawa, Hans; Neumann, Eberhard, Dipl.-Ing.

Die Erfindung betrifft ein Verfahren sowie einen Brenner, wobei ein Teil des Brennstoffes durch einen äußeren Ringkanal (1) zugeführt und am Austritts­ende auf eine hohe Geschwindigkeit beschleunigt wird, während ein weiterer Teil des Brennstoffes durch einen zweiten, inneren Ringkanal (2) zugeführt und am Austrittsende auf eine niedrige Geschwin­digkeit verzögert wird. Auf diese Weise erfolgt eine Stabilisierung und Regelung der Hauptflam­me durch eine permanente Pilotflamme.

47 Mixing using a fluid jet EP88303422.5 1988-04-15 EP0287392A2 1988-10-19 Luxton, Russell Estcourt; Nathan, Graham Jerrold

A fluid mixing device comprising:

    wall structure defining a chamber (6) having a fluid inlet (1) and a fluid outlet (4) disposed generally opposite the inlet;

    said chamber being larger in cross-section than said inlet at least for a portion of the space between said inlet and outlet;

    flow separation means (2) to cause a flow of a first fluid wholly occupying said inlet to separate from said wall structure upstream of the outlet;

    wherein the distance between said flow seaparation means and said outlet is sufficiently long in relation to the width of the chamber for the separated flow to reattach itself asymmetrically (22) to the chamber wall structure upstream of the outlet and to exit the chamber through the outlet asymmetrically (23), whereby a reverse flow (26) of said first fluid at said reattachment and/or a flow (24) of a second fluid induced from the exterior of the chamber through said outlet swirls in the chamber between said flow separation and said reattachment and thereby induces precession of said separated/reattached flow, which precession enhances mixing of the flow with said second fluid to the exterior of the chamber.

48 METHOD FOR BURNING A LIQUID FUEL AND BURNER FOR CARRYING OUT SAID METHOD EP79400317 1979-05-21 EP0006774A3 1980-01-23 LE MER, JOSEPH
49 배기 덕트 KR1020180011192 2018-01-30 KR1020180089311A 2018-08-08
(과제) 혼합기를하향으로분출시키는버너의하측에설치된연소케이싱의하부에형성된배기구에접속되는하부의유입구(41)를가지며, 연소케이싱의외측면을따라서상측으로연장되는기립덕트부(42)를구비하는배기덕트로서, 연소케이싱의상기외측면의법선방향을전후방향, 전후방향에직교하는수평방향을횡방향으로하고, 기립덕트부(42)는전후방향치수가횡방향치수보다도작은편평형상으로형성되는것에있어서, 기립덕트부(42)의전측과후측의판부(42a, 42b) 간의배기통로폭이불규칙하게되는것을억제할수 있고, 또한대형화도회피할수 있도록한다. (해결수단) 기립덕트부(42)의내부에전측판부(42a)와후측판부(42b)를연결하는상하방향으로긴 연결리브(421)가형성된다.
50 Catalytic burner apparatus for Stirling engine EP10194517.8 2010-12-10 EP2351965B1 2017-04-12 Roychoudhury, Subir; Baird, Benjamin D.; MAastanduno, Richard T.; Crowder, Bruce; Fazzino, Paul
51 DISPOSITIF D'INJECTION MULTIPOINT POUR MOTEUR D'AÉRONEF EP14821722.7 2014-11-20 EP3071886A1 2016-09-28 CHALAUD, Sébastien
The invention relates to a multi-point fuel injection device (1) for an aircraft engine (M), comprising an inlet line (10), at least two injection lines (11, 12), and a purge line (14), a fuel distributor member (2) connected to each line and comprising a moveable element (22) which comprises an injection passage (223), in which the moveable element (22) additionally comprises a purge passage (226), and is configured to adopt a first range of positions in which the injection passage (223) interconnects the inlet line (10) and the injection lines (11, 12), and a second range of positions in which the injection passage (223) interconnects the inlet line (10) and at least a first injection line (11) while the purge passage (226) interconnects the purge line (14) and at least a second injection line (12), the device being characterized in that it additionally comprises an actuator adapted to move the moveable element into a safety position when a failure of the distribution member is detected, the injection passage (223) interconnecting, in this safety position of the moveable element (22), the inlet line (10) and the first injection line (11) while the purge passage (226) does not interconnect the purge line (14) to any of the injection lines (12).
52 Catalytic burner apparatus for Stirling engine EP10194517.8 2010-12-10 EP2351965A1 2011-08-03 Roychoudhury, Subir; Baird, Benjamin D.; MAastanduno, Richard T.; Crowder, Bruce; Fazzino, Paul

The invention provides an apparatus for generating heat and transferring the heat to a heater head of an external combustion engine, preferably, a Stirling engine. Fuel and air are introduced into a combustion chamber (10) and mixed to form an air/fuel mixture. The air/fuel mixture is combusted over a combustion catalyst (1) positioned in physical contact with a heat spreader (12), which itself is positioned in physical contact with a heat acceptor surface (2). The heat acceptor surface is secured in thermal communication with the heater head. Depending upon the design of the heater head, heat flux from the heat acceptor surface into the heater head may occur radially or non-radially.

53 Oxy/Oil swirl burner EP98302205.4 1998-03-24 EP0877202B1 2004-06-02 Feldermann, Christian Juan
54 Oxy/Oil swirl burner EP98302205.4 1998-03-24 EP0877202A3 1999-06-23 Feldermann, Christian Juan

A liquid fuel burner (10) is provided with a central fuel outlet (18) having a generally divergent conical inner surface, formed of two contiguous divergent conical surfaces (20a, 20b) of different angles of divergence, and a plurality of oxygen outlets (22) shaped and positioned for creating a converging, rotating stream of oxygen which intersects with any liquid fuel issuing from the fuel outlet (18). Such oxygen/fuel interaction results in two zones of combustion and a recirculation effect which assists in the complete or substantially complete combustion of undesirable exhaust gas components. The oxygen and fuel are preferably supplied such that their velocities are approximately equal at the point at which the two zones of combustion meet.

55 Brenneranordnung EP87117450.4 1987-11-26 EP0274630B1 1991-01-23 Füglistaller, Cornel; Keller, Jakob, Dr.; Sattelmayer, Thomas, Dr.
56 Mixing using a fluid jet EP88303422.5 1988-04-15 EP0287392A3 1989-09-27 Luxton, Russell Estcourt; Nathan, Graham Jerrold

A fluid mixing device comprising:

    wall structure defining a chamber (6) having a fluid inlet (1) and a fluid outlet (4) disposed generally opposite the inlet;

    said chamber being larger in cross-section than said inlet at least for a portion of the space between said inlet and outlet;

    flow separation means (2) to cause a flow of a first fluid wholly occupying said inlet to separate from said wall structure upstream of the outlet;

    wherein the distance between said flow seaparation means and said outlet is sufficiently long in relation to the width of the chamber for the separated flow to reattach itself asymmetrically (22) to the chamber wall structure upstream of the outlet and to exit the chamber through the outlet asymmetrically (23), whereby a reverse flow (26) of said first fluid at said reattachment and/or a flow (24) of a second fluid induced from the exterior of the chamber through said outlet swirls in the chamber between said flow separation and said reattachment and thereby induces precession of said separated/reattached flow, which precession enhances mixing of the flow with said second fluid to the exterior of the chamber.

57 ANNULAR NOZZLE BURNER AND METHOD OF OPERATION. EP87901817 1987-02-05 EP0294386A4 1989-03-07 TUCKER JAMES R; HANSEN ERIC R
58 Verfahren und Vorrichtung zum Erhitzen von Verbrennungsluft und Brennstoff in Heizungsanlagen EP82103501.1 1982-04-24 EP0078876A1 1983-05-18 Jovy, Herbert, Dr.; Schuster, Wilhelm; Wittekind, Jürgen

Durch Wärmeaustausch einerseits aus dem Kesselraum (21) der Heizungsanlage und andererseits aus dem Brennraum eines Brenners wird einströmende und zweimal umgeleitete Verbrennungsluft auf hohe Temperaturen erwärmt. Bevor die erhitzte Verbrennungsluft in den Brennraum (9) eintritt, wird sie über die Oberflächen einer in den Brennraum ragenden Düse (10) und eines Abschnitts eines die Düse (10) tragenden Düsenstockes (15) geführt, erwärmt dabei den durch den Düsenstock (15) zuströmenden, hier elektrisch vorerwärmten Brennstoff weiter und trifft dann in einer Hochtemperaturkammer (9a) im Brennraum (9) mit dem aus der Düse (10) austretenden erwärmten Brennstoff zusammen, wird unter Verwirbelung mit diesem vermischt und das Luft-Brennstoffgemisch im Brennraum (9a) verbrannt.

59 DUCTED FUEL INJECTION EP17738928.5 2017-01-12 EP3402980A1 2018-11-21 MUELLER, Charles, J.
Various technologies presented herein relate to enhancing mixing inside a combustion chamber to form one or more locally premixed mixtures comprising fuel and charge-gas to enable minimal, or no, generation of soot and/or other undesired emissions during ignition and subsequent combustion of the locally premixed mixtures. To enable sufficient mixing of the fuel and charge-gas, a jet of fuel can be directed to pass through a bore of a duct causing charge-gas to be drawn into the bore creating turbulence to mix the fuel and the drawn charge-gas. The duct can be located proximate to an opening in a tip of a fuel injector. The various technologies presented herein can be utilized in a number of combustion systems, such as compression-ignition (CI) reciprocating engines, spark- ignition (SI) reciprocating engines, gas-turbine (GT) engines, burners and boilers, wellhead/refinery flaring, etc.
60 DISPOSITIF D'INJECTION MULTIPOINT ET PROCÉDÉ D'INJECTION POUR MOTEUR D'AÉRONEF EP14821722.7 2014-11-20 EP3071886B1 2018-09-05 CHALAUD, Sébastien
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