公开(公告)号：US07150143B2

公开(公告)日：2006-12-19

申请号：US10624114

申请日：2003-07-21

申请人： Louis Andrew Schick ,  Anthony John Dean

发明人： Louis Andrew Schick ,  Anthony John Dean

IPC分类号： F02C3/20 ,  F02C5/00 ,  F02C6/00 ,  F02C6/18

CPC分类号： F02C3/20 ,  F02C3/28 ,  F02C5/00 ,  F02C6/18 ,  F02K7/02 ,  F02K7/06 ,  H01M8/04022 ,  H01M8/04089 ,  H01M8/0612 ,  Y02E20/16

摘要： A power system includes a fuel cell module adapted to receive a first fuel and a pulse detonation combustor adapted to receive and detonate a second fuel and exhaust a number of detonation products to create thrust for propulsion, mechanical work extraction or electrical power production.

摘要翻译： 电力系统包括燃料电池模块，其适于接收第一燃料和脉冲爆震燃烧器，其适于接收和引爆第二燃料并排出多个爆燃产物以产生用于推进，机械作业提取或电力产生的推力。

公开(公告)号：US06315519B1

公开(公告)日：2001-11-13

申请号：US09300692

申请日：1999-04-27

申请人： Bharat Sampathkumaran Bagepalli ,  Gregory Scot Corman ,  Anthony John Dean ,  Paul Stephen DiMascio ,  Massoud Mirdamadi

发明人： Bharat Sampathkumaran Bagepalli ,  Gregory Scot Corman ,  Anthony John Dean ,  Paul Stephen DiMascio ,  Massoud Mirdamadi

IPC分类号： F01D1108

CPC分类号： F01D11/08 ,  F01D25/246 ,  F04D29/023 ,  F04D29/083 ,  F05D2300/10 ,  F05D2300/6033 ,  Y02T50/672

摘要： A turbine inner shroud and a turbine assembly. The turbine assembly includes a turbine stator having a longitudinal axis and having an outer shroud block with opposing and longitudinally outward facing first and second sides having open slots. A ceramic inner shroud has longitudinally inward facing hook portions which can longitudinally and radially surround a portion of the sides of the outer shroud block. In one attachment, the hook portions are engageable with, and are positioned within, the open slots.

摘要翻译： 涡轮内护罩和涡轮组件。 涡轮组件包括具有纵向轴线的涡轮机定子，并且具有外护罩块，外护罩块具有相对且纵向向外的第一和第二侧面具有敞开的槽。 陶瓷内护罩具有纵向向内的钩部，其可以纵向和径向地围绕外护罩块的侧面的一部分。 在一个附件中，钩部分可与开放槽接合并位于开口槽内。

公开(公告)号：US06301899B1

公开(公告)日：2001-10-16

申请号：US09299792

申请日：1999-03-17

申请人： Anthony John Dean ,  Steven George Goebel

发明人： Anthony John Dean ,  Steven George Goebel

IPC分类号： F02C100

CPC分类号： F23R3/286 ,  F23C7/004 ,  F23D2206/10

摘要： A mixer for a combustor includes a swirler having a plurality of vanes disposed at an upstream end of a mixing duct. A centerbody extends downstream from the vanes and includes a fuel chamber integrally joined to the vanes. Fuel injection openings extend from the chamber into passages between the vanes.

摘要翻译： 用于燃烧器的混合器包括旋流器，其具有设置在混合管道的上游端的多个叶片。 中心体从叶片的下游延伸并且包括与叶片整体接合的燃料室。 燃料喷射开口从腔室延伸到叶片之间的通道中。

公开(公告)号：US20110256487A1

公开(公告)日：2011-10-20

申请号：US13168310

申请日：2011-06-24

申请人： Anthony John Dean ,  David Michael Chapin ,  Donnell Eugene Crear

发明人： Anthony John Dean ,  David Michael Chapin ,  Donnell Eugene Crear

IPC分类号： F23D99/00

CPC分类号： F23J3/023 ,  B08B7/0007 ,  F28G7/00 ,  F28G7/005

摘要： A detonation device cleaning system includes a vessel having a main body including an outer surface and an inner surface that collectively define an interior chamber. A detonation combustor cleaning device is mounted to the vessel. The detonation combustor cleaning device includes at least one combustion chamber that defines a combustion flow path. The at least one combustion chamber includes a deflection member arranged along the combustion flow path. An ignition device is operatively connected to the at least one combustion chamber. The ignition device is selectively activated to ignite fuel within the at least one combustion chamber to produce a shockwave that moves in a first direction along the combustion flow path, is redirected back along the flow path within the at least one combustion chamber, and passes into the interior chamber to dislodge particles clinging to the inner surface of the vessel.

摘要翻译： 爆炸装置清洁系统包括具有主体的容器，主体包括外表面和共同界定内腔的内表面。 爆炸燃烧器清洁装置安装在容器上。 爆震燃烧器清洁装置包括限定燃烧流路的至少一个燃烧室。 所述至少一个燃烧室包括沿着燃烧流动路径布置的偏转构件。 点火装置可操作地连接到至少一个燃烧室。 点火装置被选择性地启动以点燃至少一个燃烧室内的燃料以产生沿着燃烧流动路径在第一方向上移动的冲击波，沿着至少一个燃烧室内的流动路径被重定向回来，并且进入 内部室以移除粘附到容器内表面的颗粒。

公开(公告)号：US07841167B2

公开(公告)日：2010-11-30

申请号：US11561155

申请日：2006-11-17

申请人： Adam Rasheed ,  Anthony John Dean ,  Peirre Francois Pinard ,  Christian Lee Vandervort ,  Venkat Eswarlu Tangirala

发明人： Adam Rasheed ,  Anthony John Dean ,  Peirre Francois Pinard ,  Christian Lee Vandervort ,  Venkat Eswarlu Tangirala

IPC分类号： F02K5/02

CPC分类号： F02C5/11 ,  F02C5/02 ,  F02K7/04

摘要： An engine contains at least one pulse detonation combustor which is surrounded by a bypass flow air duct, through which bypass air flow is directed. The bypass air duct contains at least one converging-diverging structure to dampen or choke the upstream propagation of shock waves from the pulse detonation combustor through the bypass flow air duct. The bypass air also serves to cool the outer surfaces of the pulse detonation combustor. The bypass air flow is controlled in tandem with the heat release from the PDC to provide the appropriate amount of thermal energy to a downstream energy conversion device, such as a turbine. A mixing plenum is positioned downstream of the pulse detonation combustor and bypass flow air duct.

摘要翻译： 发动机包含至少一个脉冲爆震燃烧器，其被旁路气流导管包围，旁路气流通过旁路气流引导。 旁路空气管道包含至少一个会聚发散结构，以阻尼或阻塞来自脉冲爆震燃烧器的冲击波的上游传播通过旁路流动空气管道。 旁路空气还用于冷却脉冲爆震燃烧器的外表面。 旁路空气流与PDC的放热一起控制，以向下游能量转换装置（例如涡轮机）提供适当量的热能。 混合气室位于脉冲爆震燃烧器和旁路流动空气管道的下游。

公开(公告)号：US20090293817A1

公开(公告)日：2009-12-03

申请号：US12129909

申请日：2008-05-30

申请人： Anthony John Dean ,  David Michael Chapin ,  Donnell Eugene Crear

发明人： Anthony John Dean ,  David Michael Chapin ,  Donnell Eugene Crear

IPC分类号： F28G11/00

CPC分类号： F23J3/023 ,  B08B7/0007 ,  F28G7/00 ,  F28G7/005

摘要： A detonation combustor cleaning device includes at least one combustion chamber having combustion flow path and including a deflection member. An ignition device is operatively connected to the at least one combustion chamber is selectively activated to ignite a combustible fuel within the at least one combustion chamber to produce a shockwave that moves in a first direction along the combustion flow path, impacts the deflection member, reverses direction and passes into a vessel to dislodge particles clinging to inner surfaces thereof.

摘要翻译： 爆炸燃烧器清洁装置包括具有燃烧流路并包括偏转构件的至少一个燃烧室。 点火装置可操作地连接到所述至少一个燃烧室，所述燃烧室被选择性地启动以点燃所述至少一个燃烧室内的可燃燃料，以产生沿着所述燃烧流动路径沿第一方向移动并冲击所述偏转构件的冲击波， 方向并进入容器以移除粘附到其内表面的颗粒。

公开(公告)号：US20080310982A1

公开(公告)日：2008-12-18

申请号：US11761564

申请日：2007-06-12

申请人： James Fredric Wiedenhoefer ,  Adam Rasheed ,  Anthony John Dean ,  Venkat Eswarlu Tangirala

发明人： James Fredric Wiedenhoefer ,  Adam Rasheed ,  Anthony John Dean ,  Venkat Eswarlu Tangirala

IPC分类号： F01C1/10

CPC分类号： F01C1/107

摘要： A positive displacement flow separator or combustor contains a rotor portion positioned inside a casing portion to act as a least area rotor which captures a volume and moves the volume along the length of the separator. The rotor portion contains a plurality of lobes which interact with grooves in the casing portion, such that the interaction of the lobes and grooves create barriers which capture the volume. The creation of the volume creates a flow barrier between a downstream end of the separator and an upstream end of the separator.

摘要翻译： 正排量流动分离器或燃烧器包含位于壳体部分内部的转子部分，用作捕获体积并沿着分离器的长度移动体积的最小区域转子。 转子部分包含与壳体部分中的凹槽相互作用的多个凸角，使得凸角和凹槽的相互作用产生捕获体积的障碍物。 卷的创建在分离器的下游端和分离器的上游端之间产生流动阻挡。

公开(公告)号：US20080310981A1

公开(公告)日：2008-12-18

申请号：US11761527

申请日：2007-06-12

申请人： James Fredric Wiedenhoefer ,  Adam Rasheed ,  Pierre Francois Pinard ,  Anthony John Dean ,  Charles Max Byrd

发明人： James Fredric Wiedenhoefer ,  Adam Rasheed ,  Pierre Francois Pinard ,  Anthony John Dean ,  Charles Max Byrd

IPC分类号： F01C1/107

CPC分类号： F01C1/107

摘要： A positive displacement flow separator contains a rotor portion positioned inside a casing portion to act as a least area rotor which captures a volume and moves the volume along the length of the separator. The rotor portion contains a plurality of lobes which interact with grooves in the casing portion, such that the interaction of the lobes and grooves create barriers which capture the volume The creation of the volume creates a flow barrier between a downstream end of the separator and an upstream end of the separator. The flow separator is coupled to a combustion portion to provide a flow of material to the combustion portion.

摘要翻译： 正位移流分离器包含位于壳体部分内部的转子部分，用作捕获体积并沿着分离器的长度移动体积的最小区域转子。 转子部分包含与壳体部分中的凹槽相互作用的多个凸角，使得凸角和凹槽的相互作用产生捕获体积的障碍。容积的产生在分离器的下游端和 分离器的上游端。 流动分离器联接到燃烧部分以向燃烧部分提供材料流。

公开(公告)号：US20080127728A1

公开(公告)日：2008-06-05

申请号：US11565252

申请日：2006-11-30

申请人： Mark Felipe Baptista ,  Adam Rasheed ,  Anthony John Dean

发明人： Mark Felipe Baptista ,  Adam Rasheed ,  Anthony John Dean

IPC分类号： G01H5/00

CPC分类号： G01H5/00

摘要： A pulse detonation device contains a detonation chamber and a propagation portion, and a plurality of mechanical response gauges coupled to an exterior surface of at least one of the detonation chamber and the propagation portion. Signals from the mechanical response gauges are sent to high frequency AC-coupled amplifiers, and the amplified signals are sent to a high frequency data acquisition system. Based on the data from the mechanical response gauges, the velocity of a detonation pressure wave is determined.

摘要翻译： 脉冲爆震装置包括爆轰室和传播部分，以及耦合到爆炸室和传播部分中的至少一个的外表面的多个机械响应计。 来自机械响应量规的信号被发送到高频AC耦合放大器，并且放大的信号被发送到高频数据采集系统。 基于来自机械响应计的数据，确定爆震压力波的速度。

公开(公告)号：US20080115480A1

公开(公告)日：2008-05-22

申请号：US11561155

申请日：2006-11-17

申请人： Adam Rasheed ,  Anthony John Dean ,  Pierre Francois Pinard ,  Christian Lee Vandervort ,  Venkat Eswarlu Tangirala

发明人： Adam Rasheed ,  Anthony John Dean ,  Pierre Francois Pinard ,  Christian Lee Vandervort ,  Venkat Eswarlu Tangirala

IPC分类号： F02C5/00

CPC分类号： F02C5/11 ,  F02C5/02 ,  F02K7/04

摘要： An engine contains at least one pulse detonation combustor which is surrounded by a bypass flow air duct, through which bypass air flow is directed. The bypass air duct contains at least one converging-diverging structure to dampen or choke the upstream propagation of shock waves from the pulse detonation combustor through the bypass flow air duct. The bypass air also serves to cool the outer surfaces of the pulse detonation combustor. The bypass air flow is controlled in tandem with the heat release from the PDC to provide the appropriate amount of thermal energy to a downstream energy conversion device, such as a turbine. A mixing plenum is positioned downstream of the pulse detonation combustor and bypass flow air duct.

摘要翻译： 发动机包含至少一个脉冲爆震燃烧器，其被旁路气流导管包围，旁路气流通过旁路气流引导。 旁路空气管道包含至少一个会聚发散结构，以阻尼或阻塞来自脉冲爆震燃烧器的冲击波的上游传播通过旁路流动空气管道。 旁路空气还用于冷却脉冲爆震燃烧器的外表面。 旁路空气流与PDC的放热一起控制，以向下游能量转换装置（例如涡轮机）提供适当量的热能。 混合气室位于脉冲爆震燃烧器和旁路流动空气管道的下游。