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公开(公告)号:US08327643B2
公开(公告)日:2012-12-11
申请号:US12790154
申请日:2010-05-28
CPC分类号: F23R3/286 , F23D2900/11101 , F23R3/343
摘要: A main swirler of a triple annular configuration that is partitioned by a pre-filmer and a separator is installed in an inlet port of a main air flow channel. The vicinity of the inner wall of the main air flow channel provided with a main fuel injection port is bulged radially outward from the innermost surface (innermost surface of a small swirler) of a main swirler. Further, a distance from the main fuel injection port and the pre-filmer is set such that an effective opening area between the pre-filmer and “the inner wall of the main air flow channel provided with the main fuel injection port” is equal to an effective opening area of the small swirler. The swirling directions of the swirlers of the main swirler are “clockwise”-“counter-clockwise”-“clockwise” respectively along the radial outward direction when the swirling direction of the innermost swirler is taken as “clockwise”.
摘要翻译: 主空气流通道的入口端安装有由预滤器和分离器分隔的三重环形构造的主旋流器。 设置有主燃料喷射口的主空气流动通道的内壁附近从主旋流器的最内表面(小旋流器的最内表面)径向向外凸出。 此外,与主燃料喷射口和预滤波器的距离被设定为使得设置有主燃料喷射口的主空气流路的预滤波器与内壁之间的有效开口面积等于有效 开口面积小的旋流器。 主旋流器的旋流器的旋转方向分别沿着径向向外的方向顺时针 - 逆时针顺时针旋转,当最内旋流器的旋转方向被取为顺时针方向时。
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公开(公告)号:US20120305673A1
公开(公告)日:2012-12-06
申请号:US13485258
申请日:2012-05-31
申请人: Ryusuke Matsuyama , Masayoshi Kobayashi , Takeo Oda , Atsushi Horikawa , Shigeru Hayashi , Kazuo Shimodaira , Kazuaki Matsuura , Hideshi Yamada , Youji Kurosawa , Hitoshi Fujiwara
发明人: Ryusuke Matsuyama , Masayoshi Kobayashi , Takeo Oda , Atsushi Horikawa , Shigeru Hayashi , Kazuo Shimodaira , Kazuaki Matsuura , Hideshi Yamada , Youji Kurosawa , Hitoshi Fujiwara
IPC分类号: F02M63/00
摘要: A fuel injector includes: a pilot injector configured to spray fuel so as to form a first combustion region in a combustion chamber; and a main injector provided coaxially with the pilot injector so as to surround the pilot injector and configured to supply a fuel-air mixture that is a mixture of the fuel and air to form a second combustion region in the combustion chamber, wherein the pilot injector includes: a center nozzle configured to eject air jet flowing straight in an axial direction on a central axis of the pilot injector; an inside swirler provided on a radially outer side of the center nozzle and configured to cause inflow air to swirl around the central axis; and a pilot fuel injecting portion configured to inject the fuel from between the center nozzle and the inside swirler to air flow in the center nozzle.
摘要翻译: 燃料喷射器包括:引燃喷射器,构造成喷射燃料以在燃烧室中形成第一燃烧区域; 以及主喷射器,其与所述引导喷射器同轴地设置成围绕所述引导喷射器并且构造成供应作为所述燃料和空气的混合物的燃料 - 空气混合物以在所述燃烧室中形成第二燃烧区域,其中所述引导喷射器 包括:中心喷嘴,其构造成喷射在所述先导喷射器的中心轴线上沿轴向直线流动的喷气; 设置在中心喷嘴的径向外侧的内旋流器,其构造成使流入空气围绕中心轴旋转; 以及配置成将来自中心喷嘴和内部旋流器之间的燃料喷射到中心喷嘴中的空气流的引燃燃料喷射部。
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公开(公告)号:US20120304649A1
公开(公告)日:2012-12-06
申请号:US13485383
申请日:2012-05-31
申请人: Ryusuke MATSUYAMA , Masayoshi KOBAYASHI , Takeo ODA , Atsushi HORIKAWA , Shigeru HAYASHI , Kazuo SHIMODAIRA , Kazuaki MATSUURA , Hideshi YAMADA , Youji KUROSAWA , Hitoshi FUJIWARA
发明人: Ryusuke MATSUYAMA , Masayoshi KOBAYASHI , Takeo ODA , Atsushi HORIKAWA , Shigeru HAYASHI , Kazuo SHIMODAIRA , Kazuaki MATSUURA , Hideshi YAMADA , Youji KUROSAWA , Hitoshi FUJIWARA
IPC分类号: F02C7/22
CPC分类号: F23R3/14 , F23R3/286 , Y02T50/675
摘要: A fuel injector includes: a pilot injector configured to spray fuel so as to form a first combustion region in a combustion chamber; and a main injector provided coaxially with the pilot injector so as to surround the pilot injector and configured to supply a fuel-air mixture that is a mixture of the fuel and air to form a second combustion region in the combustion chamber, wherein the main injector includes: a first inflow channel through which the air having a major flow component in an axial direction is taken; a second inflow channel through which the air having a major flow component in a radial direction is taken and which causes the air therein to meet the air from the first inflow channel; and a main fuel injecting portion configured to inject the fuel only to the second inflow channel.
摘要翻译: 燃料喷射器包括:引燃喷射器,构造成喷射燃料以在燃烧室中形成第一燃烧区域; 以及主喷射器,其与所述先导喷射器同轴地设置成围绕所述引燃喷射器并且构造成供应作为所述燃料和空气的混合物的燃料 - 空气混合物以在所述燃烧室中形成第二燃烧区域,其中所述主喷射器 包括:沿轴向方向具有主要流动分量的空气通过该第一流入通道; 第二流入通道,其中沿着径向方向具有主要流动分量的空气通过该第二流入通道引起其中的空气与来自第一流入通道的空气相遇; 以及主燃料喷射部,其构造成仅将燃料喷射到第二流入流路。
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公开(公告)号:US09366442B2
公开(公告)日:2016-06-14
申请号:US13485258
申请日:2012-05-31
申请人: Ryusuke Matsuyama , Masayoshi Kobayashi , Takeo Oda , Atsushi Horikawa , Shigeru Hayashi , Kazuo Shimodaira , Kazuaki Matsuura , Hideshi Yamada , Youji Kurosawa , Hitoshi Fujiwara
发明人: Ryusuke Matsuyama , Masayoshi Kobayashi , Takeo Oda , Atsushi Horikawa , Shigeru Hayashi , Kazuo Shimodaira , Kazuaki Matsuura , Hideshi Yamada , Youji Kurosawa , Hitoshi Fujiwara
摘要: A fuel injector includes: a pilot injector configured to spray fuel so as to form a first combustion region in a combustion chamber; and a main injector provided coaxially with the pilot injector so as to surround the pilot injector and configured to supply a fuel-air mixture that is a mixture of the fuel and air to form a second combustion region in the combustion chamber, wherein the pilot injector includes: a center nozzle configured to eject air jet flowing straight in an axial direction on a central axis of the pilot injector; an inside swirler provided on a radially outer side of the center nozzle and configured to cause inflow air to swirl around the central axis; and a pilot fuel injecting portion configured to inject the fuel from between the center nozzle and the inside swirler to air flow in the center nozzle.
摘要翻译: 燃料喷射器包括:引燃喷射器,构造成喷射燃料以在燃烧室中形成第一燃烧区域; 以及主喷射器,其与所述引导喷射器同轴地设置成围绕所述引导喷射器并且构造成供应作为所述燃料和空气的混合物的燃料 - 空气混合物以在所述燃烧室中形成第二燃烧区域,其中所述引导喷射器 包括:中心喷嘴,其构造成喷射在所述先导喷射器的中心轴线上沿轴向直线流动的喷气; 设置在中心喷嘴的径向外侧的内旋流器,其构造成使流入空气围绕中心轴旋转; 以及配置成将来自中心喷嘴和内部旋流器之间的燃料喷射到中心喷嘴中的空气流的引燃燃料喷射部。
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公开(公告)号:US09429324B2
公开(公告)日:2016-08-30
申请号:US13485383
申请日:2012-05-31
申请人: Ryusuke Matsuyama , Masayoshi Kobayashi , Takeo Oda , Atsushi Horikawa , Shigeru Hayashi , Kazuo Shimodaira , Kazuaki Matsuura , Hideshi Yamada , Youji Kurosawa , Hitoshi Fujiwara
发明人: Ryusuke Matsuyama , Masayoshi Kobayashi , Takeo Oda , Atsushi Horikawa , Shigeru Hayashi , Kazuo Shimodaira , Kazuaki Matsuura , Hideshi Yamada , Youji Kurosawa , Hitoshi Fujiwara
CPC分类号: F23R3/14 , F23R3/286 , Y02T50/675
摘要: A fuel injector includes: a pilot injector configured to spray fuel so as to form a first combustion region in a combustion chamber; and a main injector provided coaxially with the pilot injector so as to surround the pilot injector and configured to supply a fuel-air mixture that is a mixture of the fuel and air to form a second combustion region in the combustion chamber, wherein the main injector includes: a first inflow channel through which the air having a major flow component in an axial direction is taken; a second inflow channel through which the air having a major flow component in a radial direction is taken and which causes the air therein to meet the air from the first inflow channel; and a main fuel injecting portion configured to inject the fuel only to the second inflow channel.
摘要翻译: 燃料喷射器包括:引燃喷射器,构造成喷射燃料以在燃烧室中形成第一燃烧区域; 以及主喷射器,其与所述先导喷射器同轴地设置成围绕所述引燃喷射器并且构造成供应作为所述燃料和空气的混合物的燃料 - 空气混合物以在所述燃烧室中形成第二燃烧区域,其中所述主喷射器 包括:沿轴向方向具有主要流动分量的空气通过该第一流入通道; 第二流入通道,其中沿着径向方向具有主要流动分量的空气通过该第二流入通道引起其中的空气与来自第一流入通道的空气相遇; 以及主燃料喷射部,其构造成仅将燃料喷射到第二流入流路。
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公开(公告)号:US20100308135A1
公开(公告)日:2010-12-09
申请号:US12790154
申请日:2010-05-28
IPC分类号: F02C7/22
CPC分类号: F23R3/286 , F23D2900/11101 , F23R3/343
摘要: A main swirler of a triple annular configuration that is partitioned by a pre-filmer and a separator is installed in an inlet port of a main air flow channel. The vicinity of the inner wall of the main air flow channel provided with a main fuel injection port is bulged radially outward from the innermost surface (innermost surface of a small swirler) of a main swirler. Further, a distance from the main fuel injection port and the pre-filmer is set such that an effective opening area between the pre-filmer and “the inner wall of the main air flow channel provided with the main fuel injection port” is equal to an effective opening area of the small swirler. The swirling directions of the swirlers of the main swirler are “clockwise”-“counter-clockwise”-“clockwise” respectively along the radial outward direction when the swirling direction of the innermost swirler is taken as “clockwise”.
摘要翻译: 主空气流通道的入口端安装有由预滤器和分离器分隔的三重环形构造的主旋流器。 设置有主燃料喷射口的主空气流动通道的内壁附近从主旋流器的最内表面(小旋流器的最内表面)径向向外凸出。 此外,与主燃料喷射口和预滤波器的距离被设定为使得预滤波器与“设置有主燃料喷射口的主空气流路的内壁”之间的有效开口面积等于 小旋流器的有效开放面积。 当最内旋流器的旋转方向为“顺时针”时,主旋流器的旋流器的旋转方向分别沿径向向外方向“顺时针” - “逆时针” - “顺时针”。
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