公开(公告)号：US20120023966A1

公开(公告)日：2012-02-02

申请号：US13217646

申请日：2011-08-25

Applicant: Noémie Dion Ouellet ,  Daniel David Snook ,  Lisa Anne Wichmann ,  Samuel David Draper ,  Scott Allen Rittenhouse

Inventor： Noémie Dion Ouellet ,  Daniel David Snook ,  Lisa Anne Wichmann ,  Samuel David Draper ,  Scott Allen Rittenhouse

IPC: F02C7/26

CPC classification number: F02C7/277 ,  F01D13/02 ,  F01D19/00 ,  F02C3/36 ,  F02C7/18 ,  F02C9/52 ,  F05D2220/76 ,  F05D2260/85 ,  F05D2270/061 ,  F05D2270/082 ,  Y02T50/675 ,  Y02T50/677

Abstract: Ambient air is compressed into a compressed ambient gas flow and delivered to a turbine combustor. At least one of an exhaust port, a bypass conduit, or an extraction conduit is opened to vent the power plant. A turbine shaft is rotated at an ignition speed and a fuel stream is delivered to the turbine combustor for mixing with the compressed ambient gas flow to form a combustible mixture. The combustible mixture is burned and forms a recirculated gas flow that drives the turbine. The recirculated gas flow is recirculated using the recirculation loop. The turbine is operated at a target operating speed and then reaches substantially stoichiometric combustion. At least a portion of the recirculated gas flow is extracted using an extraction conduit that is fluidly connected to the turbine compressor.

Abstract translation: 环境空气被压缩成压缩的环境气流并输送到涡轮机燃烧器。 打开排气口，旁通管道或抽取管道中的至少一个以排放发电厂。 涡轮轴以点火速度旋转，并且燃料流被输送到涡轮机燃烧器以与压缩的环境气流混合以形成可燃混合物。 可燃混合物被燃烧并形成驱动涡轮机的再循环气流。 再循环气体循环使用再循环回路。 涡轮机以目标操作速度运行，然后达到基本上化学计量的燃烧。 使用流体连接到涡轮压缩机的抽出管道提取至少一部分再循环的气流。

公开(公告)号：US08052378B2

公开(公告)日：2011-11-08

申请号：US12406277

申请日：2009-03-18

Applicant: Samuel David Draper

Inventor： Samuel David Draper

IPC: F01D5/08

CPC classification number: F01D5/186 ,  F05D2250/25 ,  F05D2260/221 ,  F05D2260/2212 ,  Y02T50/673 ,  Y02T50/676

Abstract: A turbine airfoil is disclosed. The airfoil includes one of a turbine shroud, liner, vane or blade, including an airfoil sidewall having a film-cooling hole that extends between an airfoil cooling circuit and an airfoil surface. The airfoil also includes an insert disposed in the film-cooling channel having a body. The body has a proximal end configured for disposition proximate the airfoil surface and a distal end. The body is also configured to define a passageway that extends between the distal end and proximal end upon disposition in the film-cooling hole.

Abstract translation: 公开了一种涡轮机翼型。 翼型件包括涡轮机罩，衬套，叶片或叶片中的一个，包括具有在翼型件冷却回路和翼型件表面之间延伸的膜冷却孔的翼型侧壁。 翼型件还包括设置在具有主体的薄膜冷却通道中的插入件。 主体具有被配置为靠近翼面表面和远端的近端。 主体还构造成限定在配置在薄膜冷却孔中时在远端和近端之间延伸的通道。

公开(公告)号：US20110094230A1

公开(公告)日：2011-04-28

申请号：US12606478

申请日：2009-10-27

Applicant: Matthias Finkenrath ,  Gabor Ast ,  Matthew Lehar ,  Thomas Frey ,  Samuel David Draper ,  Richard Aumann ,  Stephanie Marie-Noelle Hoffmann

Inventor： Matthias Finkenrath ,  Gabor Ast ,  Matthew Lehar ,  Thomas Frey ,  Samuel David Draper ,  Richard Aumann ,  Stephanie Marie-Noelle Hoffmann

IPC: F02C6/16 ,  B23P11/00 ,  B01D50/00 ,  B01D53/22 ,  B01D53/62

CPC classification number: F02C6/16 ,  B01D53/1475 ,  B01D53/22 ,  B01D2257/504 ,  F02C1/02 ,  F05D2260/61 ,  Y02C10/04 ,  Y02C10/10 ,  Y02E60/15 ,  Y10T29/49826

Abstract: A system includes a compression system fluidly coupled to a compartment to compress a first quantity of gas for storage in the compartment, the compression system including a compression path to convey the first quantity of gas; an expansion system fluidly coupled to the compartment to expand a second quantity of gas from the compartment, the expansion system including an expansion path to convey the second quantity of gas; a first path fluidly coupled to the compression path to convey the first quantity of gas to the compartment; a second path fluidly coupled to the expansion path to convey the second quantity of gas from the compartment to the expansion system; and a separation unit fluidly coupled to one of the first path, second path, compression path, and expansion path, wherein the separation unit removes a quantity of carbon dioxide from one of the first and second quantities of gas.

Abstract translation: 系统包括流体耦合到隔室的压缩系统以压缩第一量的气体以存储在隔室中，该压缩系统包括用于传送第一量气体的压缩路径; 膨胀系统，其流体地联接到所述隔间以从所述隔室膨胀第二量的气体，所述膨胀系统包括用于输送所述第二量气体的膨胀路径; 流体地联接到所述压缩路径以将所述第一量的气体输送到所述隔间的第一路径; 第二路径，其流体地联接到所述膨胀路径，以将所述第二量的气体从所述隔间输送到所述膨胀系统; 以及分离单元，其流体地联接到第一路径，第二路径，压缩路径和扩展路径中的一个，其中分离单元从第一和第二量的气体中的一个中去除一定量的二氧化碳。

公开(公告)号：US20100218477A1

公开(公告)日：2010-09-02

申请号：US12395225

申请日：2009-02-27

Applicant: Samuel David Draper ,  David Matthew Polizzotti ,  Chandrashekhar Ganpatrao Sonwane

Inventor： Samuel David Draper ,  David Matthew Polizzotti ,  Chandrashekhar Ganpatrao Sonwane

IPC: F02C3/26 ,  C10L5/00

CPC classification number: C10L9/02 ,  B01D71/16 ,  B01D71/20 ,  B01D71/56 ,  B01D71/68 ,  C02F1/441 ,  C02F2101/10 ,  C02F2101/14 ,  C02F2101/16 ,  C02F2101/206 ,  C02F2103/34 ,  C02F2303/18 ,  C02F2303/185 ,  C02F2303/24 ,  C10L9/06 ,  Y02E20/16

Abstract: A process for treating coal includes contacting the coal with a leaching agent configured to remove a mineral from the coal; forming a wastewater stream comprising water and a concentration of a contaminant; and contacting the wastewater stream with a first side of a reverse osmosis membrane under pressure, wherein a permeate stream comprising a reduced concentration of the contaminant permeates the reverse osmosis membrane and flows from a second side of the reverse osmosis membrane, and a concentrate stream comprising an increased concentration of the contaminant is retained on the first side of the reverse osmosis membrane.

Abstract translation: 包括处理煤的方法包括使煤与被配置成从煤中除去矿物的浸出剂接触; 形成包含水和污染物浓度的废水流; 以及在压力下使废水流与反渗透膜的第一侧接触，其中包含污染物浓度降低的渗透物流渗入反渗透膜并从反渗透膜的第二侧流出，并且含有 在反渗透膜的第一侧保留污染物浓度增加。

公开(公告)号：US20100092280A1

公开(公告)日：2010-04-15

申请号：US12250904

申请日：2008-10-14

Applicant: Samuel David Draper

Inventor： Samuel David Draper

IPC: F02C3/26 ,  F02C7/16

CPC classification number: F02C3/26 ,  F05D2220/75 ,  F05D2250/185 ,  F05D2260/205 ,  F05D2260/2322 ,  Y02E20/16 ,  Y02T50/671 ,  Y02T50/676

Abstract: A gas turbine includes a combustor configured to burn a hydrocarbon fuel input and provide a combustion product hot gas output to a turbine inlet having a turbine inlet temperature exceeding about 2200° F., the hot gas output also includes ash in an amount of 0.1% or more by weight of the hydrocarbon fuel input. The turbine also includes a stationary nozzle configured to receive the hot gas output that includes a plurality of circumferentially spaced vanes and a vane cooling circuit located within vane sidewalls configured for circulation of steam as a coolant. The turbine also includes a rotatable rotor configured to receive the hot gas output exiting the nozzle that includes a plurality of buckets and a bucket cooling circuit located within the bucket sidewalls and shank that is configured for circulation of steam as a coolant for the bucket.

Abstract translation: 燃气轮机包括燃烧器，该燃烧器构造成燃烧碳氢化合物燃料输入并提供燃烧产物热气输出到具有超过约2200°F的涡轮机入口温度的涡轮机入口，热气体输出还包括0.1％ 或更多的烃燃料输入。 涡轮机还包括固定喷嘴，其被配置为接收热气体输出，其包括多个周向间隔开的叶片和位于叶片侧壁内的叶片冷却回路，所述叶片侧壁被配置为作为冷却剂循环蒸汽。 涡轮机还包括可旋转的转子，其被配置为接收离开喷嘴的热气体输出，该热气体输出包括多个铲斗，以及位于铲斗侧壁和柄内的铲斗冷却回路，其构造成用于循环作为用于铲斗的冷却剂的蒸汽。

公开(公告)号：US20090044542A1

公开(公告)日：2009-02-19

申请号：US11840369

申请日：2007-08-17

Applicant: Robert Thomas Thatcher ,  Samuel David Draper ,  Erin Kelly Bauknight, JR. ,  Harold Lamar Jordan, JR.

Inventor： Robert Thomas Thatcher ,  Samuel David Draper ,  Erin Kelly Bauknight, JR. ,  Harold Lamar Jordan, JR.

IPC: F02C9/00 ,  F01D21/00 ,  F01D7/02

CPC classification number: F04D27/001 ,  F04D27/0207

Abstract: A gas turbine including a compressor, the gas turbine including a sensor for measuring a clearance of blades in the compressor; and a controller for receiving clearance information and using the information to control the gas turbine for prevention of at least one of a surge and rubbing of the blades.

Abstract translation: 一种包括压缩机的燃气轮机，所述燃气涡轮机包括用于测量压缩机中​​叶片间隙的传感器; 以及控制器，用于接收间隙信息并使用该信息来控制燃气轮机以防止叶片的浪涌和摩擦中的至少一个。

公开(公告)号：US06705831B2

公开(公告)日：2004-03-16

申请号：US10176443

申请日：2002-06-19

Applicant: Samuel David Draper

Inventor： Samuel David Draper

IPC: F01D518

CPC classification number: F28F1/02 ,  F01D5/185 ,  F01D5/187 ,  F01D25/12 ,  F05D2260/607 ,  F23M5/085 ,  F23R3/002 ,  F28D7/08 ,  F28D7/087 ,  F28D2021/0029 ,  F28F2250/04 ,  F28F2260/02 ,  Y02T50/673 ,  Y02T50/676

Abstract: A linked microcircuit for providing coolant gas flow through an aircraft part, comprising at least one inlet through which a coolant gas may enter, a circuit channel extending from the at least one inlet through which the coolant gas may flow wherein the circuit channel is formed from the superimposition of a plurality of alternating serpentine circuits, and at least one outlet appended to the circuit channel through which the coolant gas may exit the circuit channel.

Abstract translation: 用于提供冷却剂气体流过飞机部件的连接微电路，包括至少一个入口，冷却剂气体可以通过所述入口进入，从所述至少一个入口延伸的电路通道，所述冷却剂气体可通过所述入口流动，其中所述电路通道由 多个交替的蛇形电路的叠加和附加到电路通道的至少一个出口，冷却剂气体可以通过该出口离开电路通道。

公开(公告)号：US08713947B2

公开(公告)日：2014-05-06

申请号：US13217610

申请日：2011-08-25

Applicant: Samuel David Draper ,  Kenneth William Kohl

Inventor： Samuel David Draper ,  Kenneth William Kohl

IPC: F02C1/08

CPC classification number: F02C3/34 ,  F01K23/10 ,  F01K23/14 ,  F02C6/04 ,  F05D2260/61

Abstract: A power plant arrangement and method of operation is provided. The power plant arrangement includes at least one main air compressor and at least one gas turbine assembly. Each assembly includes a turbine combustor for mixing a portion of compressed ambient gas with a portion of a recirculated low oxygen content gas flow and a fuel stream for burning to form the recirculated low oxygen content gas flow. A recirculation loop for recirculating at least a portion of the recirculated low oxygen content gas flow from the turbine to a turbine compressor is provided. At least one auxiliary apparatus is fluidly connected to the main air compressor and may be at least partially powered by the compressed ambient gas flow.

Abstract translation: 提供了电厂布置和操作方法。 发电厂装置包括至少一个主空气压缩机和至少一个燃气轮机组件。 每个组件包括涡轮机燃烧器，用于将一部分压缩的环境气体与一部分再循环的低氧含量气体流和用于燃烧的燃料流混合以形成再循环的低氧含量气体流。 提供了一种再循环回路，用于将至少一部分再循环的低氧含量气体流从涡轮再循环到涡轮压缩机。 至少一个辅助设备流体地连接到主空气压缩机，并且可以至少部分地由压缩的环境气流供电。

公开(公告)号：US08171716B2

公开(公告)日：2012-05-08

申请号：US11846209

申请日：2007-08-28

Applicant: James Anthony West ,  Samuel David Draper ,  Hasan Ul Karim ,  Christopher John Mordaunt

Inventor： James Anthony West ,  Samuel David Draper ,  Hasan Ul Karim ,  Christopher John Mordaunt

IPC: F02C1/00

CPC classification number: F23N1/022 ,  F23D14/62 ,  F23K2401/201 ,  F23R3/286 ,  Y02E20/16

Abstract: A gas turbine system including a source of gas coupled to a source of fuel wherein the gas and the fuel are combined to form a mixture of gas and fuel prior to the mixture being introduced to a fuel nozzle of the gas turbine system.

Abstract translation: 一种燃气轮机系统，包括联接到燃料源的气体源，其中气体和燃料在混合物被引入燃气轮机系统的燃料喷嘴之前被组合以形成气体和燃料的混合物。

公开(公告)号：US08166766B2

公开(公告)日：2012-05-01

申请号：US12889147

申请日：2010-09-23

Applicant: Samuel David Draper

Inventor： Samuel David Draper

IPC: F02C1/00

CPC classification number: F02C6/00 ,  F01K11/02 ,  F02C1/06 ,  F05D2270/082 ,  Y02E20/16

Abstract: A split heat recovery steam generator (HRSG) arrangement including a first HRSG coupled to a turbine and thereby receptive of a portion of the exhaust gases to deliver the portion of the exhaust gases to a compressor, a second HRSG coupled to the turbine and thereby receptive of a remaining portion of the exhaust gases, which includes an NOx catalyst and a CO catalyst sequentially disposed therein to remove NOx and CO from the exhaust gases and an air injection apparatus to inject air into the second HRSG between the NOx catalyst and the CO catalyst to facilitate CO consumption at the CO catalyst.

Abstract translation: 一种分体式热回收蒸汽发生器（HRSG），其包括耦合到涡轮机的第一HRSG，从而接收一部分排气以将排气的一部分输送到压缩机，第二HRSG耦合到涡轮，从而接收 的废气的剩余部分，其包括依次设置在其中以从废气中除去NOx和CO的NOx催化剂和CO催化剂，以及空气注入装置，以将空气注入到NOx催化剂和CO催化剂之间的第二HRSG中 以促进CO催化剂的CO消耗。