公开(公告)号：US10851659B2

公开(公告)日：2020-12-01

申请号：US15825892

申请日：2017-11-29

Applicant: ANSALDO ENERGIA SWITZERLAND AG

Inventor： Yang Yang ,  Andre Theuer

IPC: F23R3/12 ,  F01D9/04 ,  F23R3/34

Abstract: Disclosed is a vortex generating device having a body, extending between a leading edge and a trailing edge. The body, in profile cross sections taken across the spanwise direction, exhibits an airfoil-shaped geometry. Each airfoil-shaped profile cross section has a camber line extending from the leading edge to the trailing edge, at least two of the camber lines exhibiting different camber angles, such that the body exhibits at least two different flow deflection angles along the spanwise extent. An imaginary trailing edge diagonal extends straight from a first spanwise end of the trailing edge to a second spanwise end of the trailing edge. When seen from the downstream viewpoint, the trailing edge crosses the imaginary trailing edge diagonal exactly once at one diagonal crossing point.

公开(公告)号：US10544940B2

公开(公告)日：2020-01-28

申请号：US15084012

申请日：2016-03-29

Applicant: ANSALDO ENERGIA SWITZERLAND AG

Inventor： Kaspar Loeffel ,  Yang Yang ,  Adnan Eroglu ,  Michael Thomas Maurer ,  Nico Biagioli ,  Alexey Stytsenko ,  Sergey Mylnikov ,  Igor Baibuzenko

IPC: F23R3/28 ,  F23D11/38 ,  F23D14/24 ,  F02C7/22

Abstract: A fuel injector device includes a body having a leading edge and a trailing edge and defining a streamwise direction from the leading edge to the trailing edge. The fuel injector device body includes a first surface and a second surface opposite the first surface, each surface extending between and including the leading edge and the trailing edge, and the surfaces conjoining each other at the leading edge and the trailing edge. The trailing edge, when seen in the streamwise direction, undulates along a trailing edge mean line and, along its extent, deviates in opposite directions from the mean line and includes at least one inflection point along its extent.

公开(公告)号：US10473333B2

公开(公告)日：2019-11-12

申请号：US15098009

申请日：2016-04-13

Applicant: ANSALDO ENERGIA SWITZERLAND AG

Inventor： Yang Yang ,  Michael Düsing

IPC: F23R3/28 ,  F23R3/12 ,  F23R3/18

Abstract: The invention proposes a vortex generating arrangement, especially for a pre-mixing burner of a gas turbine, having an air conducting channel of predetermined height extending between two essentially parallel channel walls and having a predetermined direction of air flow, and having a plurality of vortex generators arranged in the channel. An improved mixing is achieved by the vortex generators each having the shape of a triangular plate, which is arranged essentially perpendicular to the channel walls and oriented relative to the direction of air flow with a predetermined off-axis angle ≠0°, and a first side of the triangular plate being oriented perpendicular to the channel walls.

公开(公告)号：US10443852B2

公开(公告)日：2019-10-15

申请号：US14947386

申请日：2015-11-20

Applicant: Ansaldo Energia Switzerland AG

Inventor： Yang Yang ,  Michael Düsing

IPC: F23R3/28 ,  F23C7/00 ,  F23R3/12 ,  F23R3/18 ,  F23R3/20 ,  F23R3/16 ,  F02C7/22

Abstract: A lobe lance is disclosed for a gas turbine combustor which includes a plurality of N (N≥4) lobe fingers, each configured as a streamlined body with two lateral surfaces. A plurality of nozzles for injecting a gaseous and/or liquid fuel mixed with air are provided whereby lobes running between the nozzles are provided for improving the mixing quality and reducing pressure loss in said combustor. The lobes of each lobe finger have one of two opposite orientations with respect to said flow direction, and the lobes of all lobe fingers follow a predetermined pattern of orientation across the lobe fingers at least one pair of neighboring lobe fingers has the same lobe orientation resulting in a grouped lobe arrangement ( . . . LL . . . or . . . RR . . . ) such that at least two of the vortices generated by the lobe shape downstream of the lobe fingers combine.

公开(公告)号：US10422283B2

公开(公告)日：2019-09-24

申请号：US15041958

申请日：2016-02-11

Applicant: Ansaldo Energia Switzerland AG

Inventor： Yang Yang ,  Nicolas Noiray ,  Michael Dusing

IPC: F23R3/14 ,  F23R3/34 ,  F02C7/22 ,  F23R3/20

Abstract: A fuel injection device for a gas turbine can include streamlined bodies arranged adjacent to one another in a circumferential direction. Each streamlined body can have a fuel nozzle on its trailing edge. The streamlined bodies can be split into at least a first group of streamlined bodies and a second group of streamlined bodies. All the streamlined bodies in the first group being the same and being different from the streamlined bodies in the second group. The first group of streamlined bodies includes at least two streamlined bodies adjacent to one another. Alternatively, the streamlined bodies are clustered in sets of two adjacent streamlined bodies. As yet another alternative, the streamlined bodies can be arranged such that the fuel injection device has a maximum of four-fold rotational symmetry in the plane perpendicular to the central axis.