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。