公开(公告)号：US08382438B2

公开(公告)日：2013-02-26

申请号：US11287466

申请日：2005-11-28

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: F01D5/14

CPC classification number: F04D29/324 ,  F01D5/141 ,  F04D29/384 ,  F04D29/681 ,  F05D2240/301 ,  F05D2250/70

Abstract: A blade for an axial-flow turbomachine with a gap-side blade area I which transits into a free blade end and with a hub-side or casing-side blade area II, respectively. Blade 3 forms a flow line profile section with leading edge VK and trailing edge HK which establish forward end point V and rearward end point H, respectively, by a tangent normal to and intersecting with the profile chord, with the distance between these end points being profile depth L. Blade 3 includes an enlargement of profile depth L at a tip of the free blade end which is at least +10 percent and decreases to zero in the blade central section, with the values being non-negative throughout, with the profile enlargement at trailing edge HK being larger than zero at the tip in the gap-side peripheral section.

Abstract translation: 一种用于轴流涡轮机的叶片，其间隙侧叶片区域I分别转移到自由叶片端部以及轮毂侧或套管侧叶片区域II。 叶片3形成具有前缘VK和后缘HK的流动线轮廓部分，其分别通过垂直于轮廓弦的切线并且与轮廓弦相交建立前端点V和后端点H，这些端点之间的距离为 叶片3包括在叶片中心部分中至少为+10％并降至零的自由叶片端部顶端处的轮廓深度L的放大，其中该值在整个中为非负数 在后缘HK处的间隙侧周边部分的尖端处的放大大于零。

公开(公告)号：US08100630B2

公开(公告)日：2012-01-24

申请号：US12382253

申请日：2009-03-11

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: F01D1/24

CPC classification number: F01D5/022 ,  F02C3/064 ,  F02C3/067 ,  F02K3/06 ,  F02K3/072 ,  F05D2260/4031

Abstract: A fluid flow machine includes at least one casing 1 and at least one rotor drum 3 rotatable about a machine axis 4, with stator vanes 8 and rotor blades 7 being arranged in an annulus duct 2 formed between the casing 1 and the rotor drum 3 The annulus duct 2 is divided into an outer annular duct 5 and an inner annular duct 6 by at least one annular flow divider 11, in each of which rotor blades 7 and stator vanes 8 are arranged Outer rotor blades 7a, which are arranged in the outer annular duct 5, are rotatable at a different speed than the inner rotor blades 7b, which are arranged in the inner annular duct 6.

Abstract translation: 流体流动机包括至少一个壳体1和可围绕机器轴线4旋转的至少一个转子滚筒3，其中定子叶片8和转子叶片7布置在形成在壳体1和转子滚筒3之间的环形管道2中。 环形管道2通过至少一个环形分流器11分成外部环形管道5和内部环形管道6，每个环形分流器11中的每个转子叶片7和定子叶片8布置在外部转子叶片7a中，外部转子叶片7a布置在外部 环形管道5可以以与设置在内部环形管道6中的内部转子叶片7b不同的速度旋转。

公开(公告)号：US20100014956A1

公开(公告)日：2010-01-21

申请号：US12498050

申请日：2009-07-06

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: F04D29/38 ,  F04D29/52

CPC classification number: F04D29/526 ,  F04D29/685

Abstract: A fluid-flow machine has at least one row of blades 5 having blade ends moving relative to one of a hub 3 and a casing 1, with a gap 11 positioned therebetween. At least one groove 7 extends essentially in a circumferential direction of the machine is in an area of the gap 11 along at least part of the circumference, with the extension of the groove 7 in the circumferential direction being large as compared to the extension of the groove 7 in the meridional flow direction. A cross-sectional area of the groove 7, in meridional view of the fluid-flow machine, essentially departs from a parallelogrammic shape and, due to its contour, is inclined in an upstream direction. A centroid of the groove cross-sectional area is provided upstream of the center of the groove aperture 12 on the main flow path.

Abstract translation: 流体流动机器具有至少一排叶片5，其叶片端部相对于轮毂3和壳体1之一移动，间隙11位于它们之间。 至少一个沿着机器的圆周方向延伸的凹槽7沿着圆周的至少一部分在间隙11的区域中延伸，槽7在圆周方向上的延伸比第 槽7沿子午线流动方向。 在流体流动机的子午视图中，槽7的横截面积基本上偏离平行四边形形状，并且由于其轮廓在上游方向上倾斜。 沟槽横截面积的重心设置在主流路上的槽孔12的中心的上游。

公开(公告)号：US20090238677A1

公开(公告)日：2009-09-24

申请号：US12320113

申请日：2009-01-16

Applicant: Carsten Clemen ,  Volker Guemmer

Inventor： Carsten Clemen ,  Volker Guemmer

IPC: F04D29/42

CPC classification number: F04D29/685 ,  F04D27/023 ,  F04D27/0238 ,  F04D29/4213 ,  F04D29/682

Abstract: A centrifugal compressor includes a rotor 2, which is rotatably borne in a casing 1. A fluid gap flow between the casing 1 and the rotor 2 is extracted via cutouts in the casing 1.

Abstract translation: 离心压缩机包括可旋转地支承在壳体1中的转子2.壳体1和转子2之间的流体间隙流动通过壳体1中的切口被抽出。

公开(公告)号：US20080310961A1

公开(公告)日：2008-12-18

申请号：US12155950

申请日：2008-06-12

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: F01D5/22

CPC classification number: F01D5/225 ,  F01D5/143 ,  F01D11/001 ,  F01D11/08 ,  F01D17/162 ,  F04D29/685 ,  F05B2240/33 ,  Y02T50/673

Abstract: A fluid-flow machine has a main flow path, in which at least one row of blades (1) is arranged, and a shroud (2) embedded in a cavity (3) of a component, with the component and the blades being in rotary movement relative to each other. The shroud (2), as referred to an axial direction of the fluid-flow machine is arranged between two reference points (A) and (B) at the periphery of the main flow path of the fluid-flow machine and projects beyond a rectilinear connection of the reference points (A) and (B) into the flow path in at least one location of the circumference and in at least one of the areas of the leading or trailing edge of the appertaining blade row.

Abstract translation: 流体流动机具有主流路，其中布置有至少一排叶片（1），以及嵌入在部件的空腔（3）中的护罩（2），其中所述部件和叶片处于 相对于彼此的旋转运动。 流体流动机器的轴向方向上的护罩（2）布置在流体流动机械的主流路的周围的两个参考点（A）和（B）之间，并且突出超过直线 将参考点（A）和（B）连接到圆周的至少一个位置中的流路中，以及在具有叶片行的前缘或后缘的至少一个区域中。

公开(公告)号：US20080219852A1

公开(公告)日：2008-09-11

申请号：US12068147

申请日：2008-02-04

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: F01D5/14

CPC classification number: F01D5/145 ,  F04D29/681 ,  F05D2240/306 ,  F05D2240/31 ,  F05D2270/17 ,  Y02T50/673

Abstract: A fluid-flow machine, especially for an aircraft engine, includes a rotor having rotor blades 3. The rotor blades 3 include, on a suction side 9, at least two zones of different surface finish, with one zone being positioned between a rotor blade 3 leading edge 5, a casing line 1, a line SLM and a line EL and being provided with a boundary layer-energizing surface structure, with the line SLM being a meridional flow line at a Mach number-critical blade height of the rotor, and with the line EL being a connecting line of all points E to form a chord-orthogonal projection line EL.

Abstract translation: 特别是用于飞行器发动机的流体流动机包括具有转子叶片3的转子。 转子叶片3在吸力侧9上包括不同表面光洁度的至少两个区域，其中一个区域位于转子叶片3前缘5，壳体管线1，管线SLM和线EL之间，并且设置 具有边界层激励表面结构，线SLM是转子的马赫数 - 关键叶片高度处的子午线，并且线EL是所有点E的连接线，以形成和弦正交投影 线EL。

公开(公告)号：US07387487B2

公开(公告)日：2008-06-17

申请号：US10996601

申请日：2004-11-26

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: F01D5/14

CPC classification number: F01D5/20 ,  F01D5/145 ,  F04D29/684 ,  F05D2270/101 ,  F05D2270/17 ,  Y02T50/671 ,  Y02T50/673

Abstract: A turbomachine with at least one rotor (6), no or at least one stator (7), and a casing (1), with the rotor (6) comprising several rotor blades (8) attached to a rotating shaft, and with the stator (7) being provided with stationary stator blades (9). The casing (1) is passed by a fluid flowing through rotor (6) and stator (7), and means for the supply of fluid are provided on at least one blade (8, 9) of a blade row of the rotor (6) and/or the stator (7) on aerodynamically critical locations on trailing edge and rim-near surfaces (HRO).

Abstract translation: 具有至少一个转子（6），无或至少一个定子（7）和壳体（1）的涡轮机，转子（6）包括附接到旋转轴的多个转子叶片（8），并且与 定子（7）设有固定定子叶片（9）。 壳体（1）通过流过转子（6）和定子（7）的流体通过，并且用于供应流体的装置设置在转子（6）的叶片排的至少一个叶片（8,9）上 ）和/或定子（7）在后缘和边缘 - 近表面（HRO）上的空气动力学关键位置。

公开(公告)号：US07364404B2

公开(公告)日：2008-04-29

申请号：US10996619

申请日：2004-11-26

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: F04D29/68

CPC classification number: F04D29/688 ,  F01D5/145 ,  F02C6/08 ,  F04D29/324 ,  F04D29/526 ,  F04D29/542 ,  F04D29/682 ,  F05D2240/307 ,  Y02T50/671 ,  Y02T50/673 ,  Y10S415/914

Abstract: A turbomachine includes at least one rotor (6), at least one stator (7), and a casing (1), with the rotor (6) comprising several rotor blades (8) attached to a rotating shaft, and with the stator (7) being provided with stationary stator blades (9), the casing (1) being passed by a fluid flowing through the rotor (6) and stator (7). Provision is made for the removal of fluid on at least one blade (8, 9) of a blade row of the rotor (6) and/or the stator (7) on non-axially symmetrical, aerodynamically critical locations on blade tip and annulus surfaces (SRO).

Abstract translation: 涡轮机包括至少一个转子（6），至少一个定子（7）和壳体（1），转子（6）包括附接到旋转轴的几个转子叶片（8）和定子（ 7）设置有固定的定子叶片（9），壳体（1）被流过转子（6）和定子（7）的流体所通过。 规定用于在叶片尖端和环形空间上的非轴对称的空气动力学关键位置上的至少一个叶片（8,9）上的转子（6）和/或定子（7）的叶片排除流体 表面（SRO）。

公开(公告)号：US20070053779A1

公开(公告)日：2007-03-08

申请号：US11510826

申请日：2006-08-28

Applicant: Volker Guemmer

Inventor： Volker Guemmer

IPC: B64C27/46

CPC classification number: F04D29/324 ,  F01D5/141 ,  F01D5/145 ,  F04D29/544 ,  F05D2240/301 ,  F05D2250/71 ,  Y10S416/02

Abstract: A turbomachine blade with a profile skeleton line extending along a meridional flow line, the blade being radially divided into at least three zones (Z0, Z1, Z2) with profile skeleton lines of each zone (Z0, Z1, Z2) provided in each zone from the respective radially inner to the radially outer boundary to satisfy the equations: α * = α 1 - α P α 1 - α 2 S * = s P S where P is any point of the profile skeleton line, α1 is angle of inclination at blade leading edge, α2 is angle of inclination at blade trailing edge, α* is dimensionless, specific angle of total curvature, S* is dimensionless; specific extension, αP is angle of tangent at any point P of profile skeleton line to central meridional flow line, sP is extension of profile skeleton line at any point P, and S is total extension of profile skeleton line.

Abstract translation: 一种涡轮机叶片，具有沿着子午线流线延伸的轮廓骨架线，叶片径向分成至少三个区域（Z 0，Z 1，Z 2），每个区域的轮廓骨架线（Z 0，Z 1，Z 2）设置在每个区域中，从各自的径向内部到径向外边界以满足以下等式：