序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
1 流体环气 CN200480013438.8 2004-05-04 CN100404868C 2008-07-23 B·温克巴赫; S·希特施; A·于内曼
具有单级或多级的流体环气,每一级分别具有一个工作腔(8)、一个偏心支承在其中的叶轮(2)、在轴向两侧限制工作腔的平面控制盘(3,4)以及连接在其上的、用于将输送气体吸入并排出工作室(8)的通道或腔室,其特征在于,控制盘(3,4)具有相同的吸入孔(6)和压出孔(7)地彼此间一致地构成,并且不需要的开孔(6,7)在背离叶轮(2)的侧面上被覆盖
2 流体环气 CN200480013438.8 2004-05-04 CN1791751A 2006-06-21 B·温克巴赫; S·希特施; A·于内曼
具有单级或多级的流体环气,每一级分别具有一个工作腔(8)、一个偏心支承在其中的叶轮(2)、在轴向两侧限制工作腔的平面控制盘(3,4)以及连接在其上的、用于将输送气体吸入并排出工作室(8)的通道或腔室,其特征在于,控制盘(3,4)具有相同的吸入孔(6)和压出孔(7)彼此间一致地构成,并且不需要的开孔(6,7)在背离叶轮(2)的侧面上被覆盖
3 HIGH-STRENGTH LIGHT-WEIGHT LATTICE-CORED ADDITIVE MANUFACTURED COMPRESSOR COMPONENTS US15366871 2016-12-01 US20170182561A1 2017-06-29 Marc J. Scancarello; Robert C. Stover
A light-weight, high-strength compressor component is formed via additive manufacturing that has controlled stiffness and/or deflection levels. The component may have at least one interior region comprising a lattice structure that comprises a plurality of repeating cells. A solid surface is disposed over the lattice structure. The interior region comprises the lattice structure in the body portion of the light-weight, high-strength compressor component. The lattice structure may be used to globally or locally control stiffness and/or deflection levels of the compressor component. Additive manufacturing provides flexibility in forming compressor components with desirably improved strength-to-weight ratios while exhibiting high levels of control over stiffness and/or deflection. Methods of making such compressor components via additive manufacturing processes are also provided.
4 SEAL ASSEMBLY AND METHOD US13124355 2009-10-19 US20110204572A1 2011-08-25 Timothy Shires
A corner seal assembly for a rotor of a rotary engine, the assembly comprising a pair of corner seal elements, each seal element of the pair being arranged to provide a seal between the rotor and a respective one of a pair of opposed end faces of the rotary engine, the seals being arranged to be resiliently coupled to one another whereby the seals exert substantially the same force on each one of the pair of opposed end faces.
5 Liquid ring pump US10556748 2004-05-04 US07648344B2 2010-01-19 Bernd Wenckebach; Silke Heetsch; Alfons Jünemann
Disclosed is a liquid ring pump with one or several stages, each of which comprises a working chamber, an impeller that is eccentrically mounted therein, flat control disks that axially delimit the working chamber on both sides, and ducts or chambers that are located adjacent to the control disks and deliver and discharge the transport gas to and from the working chamber. The inventive liquid ring pump is characterized in that the control disks are embodied in the same manner with identical suction ports and pressure ports while ports that are not needed are covered on the side facing away from the impeller.
6 Method and Apparatus to Manufacture a Progressive Cavity Motor or Pump US14772925 2014-03-04 US20160186747A1 2016-06-30 Julien RAMIER; Peter CARIVEAU; Pierre Lauric DUBESSET
A stator and a method of manufacturing at least a portion of a progressive cavity motor or pump include disposing a cylindrical shell within a cylindrical housing, disposing a stator mold within the cylindrical shell, disposing an elastomeric material between the stator mold and the cylindrical shell, removing the stator mold from within the elastomeric material, thereby forming an elastomeric material layer having a stator profile within the cylindrical shell, and removing the cylindrical shell from within the cylindrical housing, thereby forming a cartridge having the elastomeric material layer disposed within the cylindrical shell.
7 Seal assembly and method US13124355 2009-10-19 US08720898B2 2014-05-13 Timothy Shires
A corner seal assembly for a rotor of a rotary engine, the assembly comprising a pair of corner seal elements, each seal element of the pair being arranged to provide a seal between the rotor and a respective one of a pair of opposed end faces of the rotary engine, the seals being arranged to be resiliently coupled to one another whereby the seals exert substantially the same force on each one of the pair of opposed end faces.
8 Liquid ring pump US10556748 2004-05-14 US20060292000A1 2006-12-28 Bernd Wenckebach; Silke Heetsch; Alfons Junamann
Disclosed is a liquid ring pump with one or several stages, each of which comprises a working chamber, an impeller that is eccentrically mounted therein, flat control disks that axially delimit the working chamber on both sides, and ducts or chambers that are located adjacent to the control disks and deliver and discharge the transport gas to and from the working chamber. The inventive liquid ring pump is characterized in that the control disks are embodied in the same manner with identical suction ports and pressure ports while ports that are not needed are covered on the side facing away from the impeller.
9 Liquid ring gas pump JP2006529735 2004-05-04 JP2007502387A 2007-02-08 アルフォンス・ユーネマン; ジルケ・ヘーチュ; ベルント・ヴェンケバッハ
一つのステージまたは数ステージの液体リングガスポンプであって、各ステージは、作動チャンバ(8)と、作動チャンバ(8)内に偏心して設けられたインペラ(2)と、作動チャンバの軸方向両端において境を接する平坦な制御ディスク(3,4)と、制御ディスク(3,4)に隣接して配置されて移送ガスを作動チャンバ(8)に供給かつ作動チャンバ(8)から排出するダクトまたはチャンバとを備えた液体リングガスポンプを開示する。 本発明の液体リングポンプは、制御ディスク(3,4)が同一の吸引ポート(6)および加圧ポート(7)と同じく一体化されている一方、不要な各ポート(6,7)がインペラ(2)から離れた対向側において覆われていることを特徴とする。
10 Liquid ring gas pump JP2006529735 2004-05-04 JP4324614B2 2009-09-02 アルフォンス・ユーネマン; ジルケ・ヘーチュ; ベルント・ヴェンケバッハ
11 METHOD AND APPARATUS TO MANUFACTURE A PROGRESSIVE CAVITY MOTOR OR PUMP EP14760199 2014-03-04 EP2964951A4 2016-10-26 RAMIER JULIEN; CARIVEAU PETER; DUBESSET PIERRE LAURIC
A stator and a method of manufacturing at least a portion of a progressive cavity motor or pump include disposing a cylindrical shell within a cylindrical housing, disposing a stator mold within the cylindrical shell, disposing an elastomeric material between the stator mold and the cylindrical shell, removing the stator mold from within the elastomeric material, thereby forming an elastomeric material layer having a stator profile within the cylindrical shell, and removing the cylindrical shell from within the cylindrical housing, thereby forming a cartridge having the elastomeric material layer disposed within the cylindrical shell.
12 CORNER SEAL ASSEMBLY FOR A ROTARY ENGINE EP09756345.6 2009-10-19 EP2350438A2 2011-08-03 SHIRES, Timothy
A corner seal assembly for a rotor of a rotary engine, the assembly comprising a pair of corner seal elements, each seal element of the pair being arranged to provide a seal between the rotor and a respective one of a pair of opposed end faces of the rotary engine, the seals being arranged to be resiliently coupled to one another whereby the seals exert substantially the same force on each one of the pair of opposed end faces.
13 METHOD AND APPARATUS TO MANUFACTURE A PROGRESSIVE CAVITY MOTOR OR PUMP EP14760199.1 2014-03-04 EP2964951A1 2016-01-13 RAMIER, Julien; CARIVEAU, Peter; DUBESSET, Pierre Lauric
A stator and a method of manufacturing at least a portion of a progressive cavity motor or pump include disposing a cylindrical shell within a cylindrical housing, disposing a stator mold within the cylindrical shell, disposing an elastomeric material between the stator mold and the cylindrical shell, removing the stator mold from within the elastomeric material, thereby forming an elastomeric material layer having a stator profile within the cylindrical shell, and removing the cylindrical shell from within the cylindrical housing, thereby forming a cartridge having the elastomeric material layer disposed within the cylindrical shell.
14 Flüssigkeitsringgaspumpe EP03011219.7 2003-05-16 EP1477682B1 2008-04-09 Wenckebach, Bernd; Heetsch, Silke; Jünemann, Alfons, Dr.
15 Flüssigkeitsringgaspumpe EP03011219.7 2003-05-16 EP1477682A1 2004-11-17 Wenckebach, Bernd; Heetsch, Silke; Jünemann, Alfons, Dr.

Die Flüssigkeitsringgaspumpe mit einer oder mehreren Stufen, die jeweils einen Arbeitsraum (8), ein darin exzentrisch gelagertes Flügelrad (2), den Arbeitsraum beidseitig axial begrenzende flache Steuerscheiben (3, 4) und sich daran anschließende Kanäle oder Kammern für die Zu- und Abführung des Fördergases zu dem und von dem Arbeitsraum (8) aufweisen, zeichnet sich dadurch aus, daß die Steuerscheiben (3, 4) identisch miteinander mit gleichen Saug- (6) und Drucköffnungen (7) ausgebildet sind und nicht benötigte Öffnungen (6, 7) auf der vom Flügelrad (2) abgewandten Seite zugedeckt sind.

16 SEAL ASSEMBLY AND METHOD PCT/GB2009051403 2009-10-19 WO2010043916A2 2010-04-22 SHIRES TIMOTHY
A corner seal assembly for a rotor of a rotary engine, the assembly comprising a pair of corner seal elements, each seal element of the pair being arranged to provide a seal between the rotor and a respective one of a pair of opposed end faces of the rotary engine, the seals being arranged to be resiliently coupled to one another whereby the seals exert substantially the same force on each one of the pair of opposed end faces.
QQ群二维码
意见反馈