公开(公告)号：US08043576B2

公开(公告)日：2011-10-25

申请号：US12689469

申请日：2010-01-19

Applicant: Gerard D Agnew ,  Robert H Cunningham ,  Philip D Butler ,  Robert D Collins

Inventor： Gerard D Agnew ,  Robert H Cunningham ,  Philip D Butler ,  Robert D Collins

IPC: B01J8/02

CPC classification number: H01M8/0631 ,  B01J10/007 ,  C01B3/38 ,  C01B2203/0227 ,  C01B2203/0277 ,  C01B2203/066 ,  C01B2203/0838 ,  C01B2203/1035 ,  C01B2203/1241 ,  H01M2008/1293

Abstract: A reformer module (10) comprises a hollow support member (12) having at least one passage (14) extending longitudinally therethrough. The hollow support member (14) has an external surface (20), a barrier layer (22) arranged on at least a portion of the external surface (20) of the hollow support member (12), a catalyst layer (24) arranged on the barrier layer (22) and a sealing layer (26) arranged on the catalyst layer (24) and the external surface (20) of the hollow support member (12) other than the at least a portion of the external surface of the hollow support member (12). By providing the barrier layer (22) and the catalyst layer (24) on the exterior surface (20) of the hollow support member (12), the distribution of the barrier layer (22) and/or the catalyst layer (24) may be more precisely controlled and thus a non-uniform distribution of barrier layer (22) and/or catalyst layer (24) may be achieved.

Abstract translation: 重整器模块（10）包括具有至少一个纵向延伸通过的通道（14）的中空支撑构件（12）。 中空支撑构件（14）具有外表面（20），布置在中空支撑构件（12）的外表面（20）的至少一部分上的阻挡层（22），布置在中空支撑构件 在所述阻挡层（22）上的密封层（26）和布置在所述催化剂层（24）上的密封层（26）和所述中空支撑构件（12）的外表面（20）之外，所述外表面的至少一部分 中空支撑构件（12）。 通过在中空支撑构件（12）的外表面（20）上设置阻挡层（22）和催化剂层（24），阻挡层（22）和/或催化剂层（24）的分布可以 可以更精确地控制，因此可以实现阻挡层（22）和/或催化剂层（24）的不均匀分布。

公开(公告)号：US07749465B2

公开(公告)日：2010-07-06

申请号：US11312378

申请日：2005-12-21

Applicant: Gerard D. Agnew ,  Robert H. Cunningham ,  Philip D. Butler ,  Robert D. Collins

Inventor： Gerard D. Agnew ,  Robert H. Cunningham ,  Philip D. Butler ,  Robert D. Collins

IPC: B01J8/02

CPC classification number: H01M8/0631 ,  B01J10/007 ,  C01B3/38 ,  C01B2203/0227 ,  C01B2203/0277 ,  C01B2203/066 ,  C01B2203/0838 ,  C01B2203/1035 ,  C01B2203/1241 ,  H01M2008/1293

Abstract: A reformer module (10) comprises a hollow support member (12) having at least one passage (14) extending longitudinally therethrough. The hollow support member (14) has an external surface (20), a barrier layer (22) arranged on at least a portion of the external surface (20) of the hollow support member (12), a catalyst layer (24) arranged on the barrier layer (22) and a sealing layer (26) arranged on the catalyst layer (24) and the external surface (20) of the hollow support member (12) other than the at least a portion of the external surface of the hollow support member (12). By providing the barrier layer (22) and the catalyst layer (24) on the exterior surface (20) of the hollow support member (12), the distribution of the barrier layer (22) and/or the catalyst layer (24) may be more precisely controlled and thus a non-uniform distribution of barrier layer (22) and/or catalyst layer (24) may be achieved.

Abstract translation: 重整器模块（10）包括具有至少一个纵向延伸通过的通道（14）的中空支撑构件（12）。 中空支撑构件（14）具有外表面（20），布置在中空支撑构件（12）的外表面（20）的至少一部分上的阻挡层（22），布置在中空支撑构件 在所述阻挡层（22）上的密封层（26）和布置在所述催化剂层（24）上的密封层（26）和所述中空支撑构件（12）的外表面（20）之外，所述外表面的至少一部分 中空支撑构件（12）。 通过在中空支撑构件（12）的外表面（20）上设置阻挡层（22）和催化剂层（24），阻挡层（22）和/或催化剂层（24）的分布可以 可以更精确地控制，因此可以实现阻挡层（22）和/或催化剂层（24）的不均匀分布。

公开(公告)号：US06237343B1

公开(公告)日：2001-05-29

申请号：US09302364

申请日：1999-04-30

Applicant: Philip D Butler

Inventor： Philip D Butler

IPC: F02G300

CPC classification number: F23R3/40 ,  F23R3/14 ,  F23R3/34

Abstract: A gas turbine engine (10) combustion chamber (28) comprises a primary combustion zone (36) and a secondary combustion zone(40) in which lean mixtures of fuel and air are burned. Air is supplied to a first mixing duct (50) through a swirler (52). Air is supplied to an additional mixing duct (58) through a swirler (54) and hydrocarbon fuel is supplied to the additional mixing duct (58) through a swirler (66). The hydrocarbon fuel and air is mixed and reacted in a catalytic partial oxidation reaction zone (60) which produces a product gas comprising a mixture of hydrogen, carbon monoxide, carbon dioxide, water and unreacted hydrocarbon fuel. Additional hydrocarbon fuel is supplied from apertures (72) and is mixed with the product gas in a mixing chamber (68) and this mixture is supplied to the first mixing duct (50) and mixes with the air. The first mixing duct (50) supplies a lean mixture of fuel into the primary combustion zone (36). The arrangement enables the combustion chamber (28) to operate with more stability or at leaner fuel to air ratios.

Abstract translation: 燃气涡轮发动机（10）燃烧室（28）包括主燃烧区（36）和二次燃烧区（40），燃料和空气的稀混合物被燃烧。 空气通过旋流器（52）供应到第一混合管道（50）。 空气通过旋流器（54）供应到附加的混合管道（58），碳氢化合物燃料通过旋流器（66）供应到附加混合管道（58）。 碳氢化合物燃料和空气在催化部分氧化反应区（60）中混合和反应，催化部分氧化反应区产生包含氢，一氧化碳，二氧化碳，水和未反应的烃燃料的混合物的产物气体。 额外的碳氢化合物燃料由孔（72）供应，并与产物气体混合在混合室（68）中，并将该混合物供应至第一混合管道（50）并与空气混合。 第一混合管道（50）将燃料的贫混合物供应到主燃烧区域（36）中。 该布置使得燃烧室（28）能够以更稳定的或更稀的燃料与空气比运行。

公开(公告)号：US20100135872A1

公开(公告)日：2010-06-03

申请号：US12689469

申请日：2010-01-19

Applicant: Gerard D Agnew ,  Robert H Cunningham ,  Philip D Butler ,  Robert D Collins

Inventor： Gerard D Agnew ,  Robert H Cunningham ,  Philip D Butler ,  Robert D Collins

IPC: B01J8/02

CPC classification number: H01M8/0631 ,  B01J10/007 ,  C01B3/38 ,  C01B2203/0227 ,  C01B2203/0277 ,  C01B2203/066 ,  C01B2203/0838 ,  C01B2203/1035 ,  C01B2203/1241 ,  H01M2008/1293

Abstract: A reformer module (10) comprises a hollow support member (12) having at least one passage (14) extending longitudinally therethrough. The hollow support member (14) has an external surface (20), a barrier layer (22) arranged on at least a portion of the external surface (20) of the hollow support member (12), a catalyst layer (24) arranged on the barrier layer (22) and a sealing layer (26) arranged on the catalyst layer (24) and the external surface (20) of the hollow support member (12) other than the at least a portion of the external surface of the hollow support member (12). By providing the barrier layer (22) and the catalyst layer (24) on the exterior surface (20) of the hollow support member (12), the distribution of the barrier layer (22) and/or the catalyst layer (24) may be more precisely controlled and thus a non-uniform distribution of barrier layer (22) and/or catalyst layer (24) may be achieved.

Abstract translation: 重整器模块（10）包括具有至少一个纵向延伸通过的通道（14）的中空支撑构件（12）。 中空支撑构件（14）具有外表面（20），布置在中空支撑构件（12）的外表面（20）的至少一部分上的阻挡层（22），布置在中空支撑构件 在所述阻挡层（22）上的密封层（26）和布置在所述催化剂层（24）上的密封层（26）和所述中空支撑构件（12）的外表面（20）之外，所述外表面的至少一部分 中空支撑构件（12）。 通过在中空支撑构件（12）的外表面（20）上设置阻挡层（22）和催化剂层（24），阻挡层（22）和/或催化剂层（24）的分布可以 可以更精确地控制，因此可以实现阻挡层（22）和/或催化剂层（24）的不均匀分布。