Diffuser part for a gas turbine

Abstract

A diffuser component for a gas turbine is provided, where a fluid flow in the direction of a combustion chamber of the gas turbine can be slowed down by the diffuser component, and a flow cross-section of the diffuser component, which is defined by a diffuser wall is widened to do so. The diffuser wall is at least locally braced, in that at least one stiffening element with a lattice-type structure is provided on the diffuser wall.

Claims

1. A diffuser component for a gas turbine, comprising: a diffuser wall defining a flow cross-section, the flow cross-section increasing in area in a flow direction toward a combustion chamber of the gas turbine to slow a fluid flow through the flow cross-section toward the combustion chamber; at least one stiffening element including a lattice structure connected to the diffuser wall, the at least one stiffening element bracing a section of the diffuser wall; wherein the at least one stiffening element is positioned on an outer side of the diffuser wall that faces away from the fluid flow.

2. The diffuser component in accordance with claim 1, wherein the lattice structure includes individual cells formed by struts running at angles to one another.

3. The diffuser component in accordance with claim 2, wherein the individual cells have at least one chosen from geometrically differing shape and differing size.

4. The diffuser component in accordance with claim 1, wherein the lattice structure includes individual cells having cross-sections shaped as at least one chosen from rectangular, triangular, trapezoidal, circular, elliptical, diamond and honeycomb.

5. The diffuser component in accordance with claim 1, wherein the at least one stiffening element protrudes at a height from the diffuser wall, and the height varies along the diffuser wall.

6. The diffuser component in accordance with claim 1, wherein the at least one stiffening element completely encloses a circumference of the diffuser wall.

7. The diffuser component in accordance with claim 6, wherein the at least one stiffening element extends over more than 60% of a length of the diffuser wall.

8. The diffuser component in accordance with claim 1, wherein the at least one stiffening element extends over only part of the diffuser wall.

9. The diffuser component in accordance with claim 1, wherein the at least one stiffening element includes two stiffening elements spatially separated from one another, with each including a lattice structure on the diffuser wall.

10. The diffuser component in accordance with claim 9, wherein the two stiffening elements are arranged along an extension direction of the diffuser wall pointing from an inlet of the diffuser to an outlet of the diffuser, and at least one chosen from one behind the other and transversely to the extension direction.

11. The diffuser component in accordance with claim 9, wherein the two stiffening elements have at least one chosen from A), B) and C) where: A) is differing heights of protrusion from the diffuser wall; B) is at least one chosen from different lengths and different widths; C) is lattice structures with cells differing in at least one chosen from geometry and size.

12. The diffuser component in accordance with claim 1, and further comprising at least one additional flat stiffening element arranged on the at least one stiffening element.

13. The diffuser component in accordance with claim 12, wherein the at least one additional stiffening element is at least one chosen from provided with a thin metal sheet and welded or brazed to the stiffening element.

14. A gas turbine including the diffuser component in accordance with claim 1, and during operation of the gas turbine, the fluid flow is guided through the diffuser component in the direction of the combustion chamber.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Further advantages and features of the present invention become apparent from the following description of exemplary embodiments shown in the figures.

(2) FIGS. 1A to 1B show schematically in different views a diffuser component known from the state of the art in a condition installed in a gas-turbine engine.

(3) FIGS. 2A to 2C show three different design variants of a diffuser component in accordance with the present invention, each in sectional view and schematically, and each having at least one stiffening element.

(4) FIGS. 3A to 3H show, in top view each, a diffuser wall of a diffuser component in accordance with the present invention having differently designed stiffening elements, each of them being provided on an outer side of the diffuser wall.

(5) FIG. 4A shows in a view matching the FIGS. 2A to 2C a further design variant of a diffuser component in accordance with the present invention, where several flat stiffening elements are provided locally and additionally on a first lattice-type stiffening structure.

(6) FIG. 4B shows in top view the lattice-type stiffening structure of FIG. 4A with two additional flat stiffening elements arranged on said stiffening structure.

DETAILED DESCRIPTION

(7) FIGS. 1A and 1B each show in a sectional view a diffuser component known from the state of the art in the form of a diffuser 6 in a gas-turbine engine. FIG. 1A illustrates schematically in a sectional view the installation situation of the diffuser 6, while FIG. 1B shows an enlarged view of this installation situation. The diffuser 6, designed here as an axial diffuser, is arranged downstream of a compressor rotor stage of the gas-turbine engine and guides an airflow coming from the latter in the direction of a combustion chamber 10 of the gas-turbine engine. FIG. 1A shows here in particular a compressor casing 1, an outlet guide vane 7, the diffuser 6 and parts of the casing of the combustion chamber 10, which are arranged one behind the other along an engine axis M. A compressor rotor disk 4 with compressor rotor hub 3 and compressor rotor 2 is rotatably mounted inside the compressor casing 1. These components form here parts of a high-pressure compressor via which a fluid flow is guided in the direction of an outlet guide vane 7. The fluid flow generated passes here via a gap 5 between the compressor rotor 2 and the outlet guide vane 7 into a casing section for the outlet guide vane 7. The outlet guide vane 7 used to direct the fluid flow is here enclosed between outlet guide vane outer walls 12.

(8) The diffuser 6 is arranged downstream of the outlet guide vane 7. The fluid flow is slowed down by this diffuser 6, in that a flow cross-section defined by the diffuser wall 11 widens in the direction of the combustion chamber 10 starting from an inlet 60 of the diffuser 6 to an outlet 61 of the diffuser 6. The diffuser wall 11 of the diffuser 6 here faces the fluid flow on an inner surface area or inner side 111. On an opposite outer side 110 of the diffuser wall 11, said diffuser wall 11 is connected on the one hand to an outer combustion chamber casing 8 and on the other hand to an inner combustion chamber casing 9.

(9) With the embodiment and arrangement of a diffuser 6 as shown and known from the state of the art, the diffuser wall 11 can during operation of the gas-turbine engine be excited to unwelcome vibrations, which can ultimately even lead to tearing away of the diffuser wall 11 or a part thereof.

(10) To remedy this, it is provided in the design variants in accordance with the invention of FIGS. 2A, 2B and 2C that a lattice-type stiffening structure is provided by means of a separate stiffening element 13 on the outer side 110 of a diffuser wall 11, or a stiffening element 13 of this type with a lattice-type stiffening structure is integrally designed with the outer side 110 of the diffuser wall 11. The stiffening element 13 can extend here along the full circumference of the diffuser wall 11 and also cover it in full on its outer side 110. It can however also be provided in accordance with the design variants of FIGS. 2A, 2B and 2C that a stiffening element 13 with a lattice-type structure is fixed only to a part of the diffuser walls 11 or alternatively is integral with them.

(11) In accordance with the sectional views in FIGS. 2A, 2B and 2C, several stiffening elements 13 separated from one another can be provided along the circumference of the diffuser wall 11 and extend over the diffuser wall 11 with differing lengths l1 and l2 along an extension direction x pointing from the inlet 60 to the outlet 61 of the diffuser 6. Alternatively, it can be provided that an individual stiffening element 13 is provided with a length which changes along the circumference in the extension direction x, so that said element is then shown for example in the sectional view of FIG. 2A with a length l1 in an upper area of the diffuser wall 11 and with a shorter length l2 in an opposite lower area of the diffuser wall 11.

(12) As can be discerned in a comparison of FIGS. 2A and 2B, a height d1 or d2 of the stiffening element 13, by which the lattice-type structure of the respective stiffening element 13 protrudes from the outer side 110 of the diffuser wall 11, can also be varied depending on requirements.

(13) According to FIGS. 2B and 2C when viewed together, a distance a1 or a2 of a stiffening element 13 from the inlet 60 of the diffuser 6 can also be varied. For example, when the diffuser wall 11 is connected to the inner and outer combustion chamber casings 8 and 9 close to the inlet, it can be provided that above all that area of the diffuser wall 11 close to the outlet is braced using the at least one stiffening element 13, in order to prevent unwelcome vibrations.

(14) It can be further discerned from FIG. 2C that not only the length l3 or l4 of a stiffening element 13 and its lattice-type structure along the extension direction x is variable; it can also be seen from this Figure that a stiffening element 13 with a height d3, d4 that changes along the circumference can also be provided on the diffuser wall 11, or at least two stiffening elements 13 with differing thicknesses or heights d3 and d4.

(15) Based on FIGS. 3A to 3H, different variants for the lattice-type (stiffening) structures formed by a stiffening element 13, 13a or 13b are shown as typical examples. Each of these lattice-type structures forms, using several (transverse and longitudinal) struts 131 running at angles to one another and possibly intersecting, several cells 130, 130a, 130b and 130c in order to brace the diffuser wall 11 on its outer side 110. The lattice-type structures shown can of course also be curved here, in order to extend along the diffuser wall of a conical diffuser component 6. The top views of FIGS. 3A to 3H show here areas of stiffening elements 13 which extend preferably completely enclosing the circumference of the diffuser wall 11.

(16) In the design variant of FIG. 3A, the stiffening element 13 forms cells 130 square in cross-section using transverse and longitudinal struts that extend parallel to one another.

(17) In the design variant of FIG. 3B, the cells 130 formed by the lattice-type structure appear rectangular and in particular diamond-shaped.

(18) In the exemplary embodiment of FIG. 3C, two stiffening elements 13a and 13b separated from one another are provided and each form identically designed stiffening segments 132 for the diffuser wall 11. Each of these stiffening segments 132 extends over a base area rectangular in top view and forms cells 130a, 130b and 130c of differing geometry and differing dimensions. The individual stiffening elements 132 can be arranged here along the extension direction x of the diffuser wall 11 directly adjacent to one another or at a distance from one another and fixed to the outer side 110.

(19) In the exemplary embodiment of FIG. 3D, the stiffening element 13 forms a lattice-type structure with triangular cells 130. Each triangular cell 130 has here a base area which is defined by an isosceles triangle.

(20) FIG. 3E illustrates a stiffening element 13 with cells 130 of honeycomb-like design. The stiffening element 13 forms here a lattice-type structure resembling bees' honeycombs, with the individual and identically designed cells 130 having a base area in the form of a regular hexagon.

(21) In the variant of FIG. 3F, the stiffening element 13 forms a lattice structure with geometrically differing cells 130a, 130b. Individual cells 130a are here designed triangular in their base area, while other cells 130b are designed with a diamond-shaped base area.

(22) In the exemplary embodiment in FIG. 3G, stiffening elements 13a and 13b are provided at a distance from one another along the extension direction x. The lattice-type structures of these two stiffening elements 13a and 13b are however designed identical to one another and have in particular several cells 130 with a square base area.

(23) In the exemplary embodiment of FIG. 3H, stiffening elements 13a and 13b arranged offset to one another are provided along the extension direction x and transversely thereto (along an extension direction y perpendicular thereto). These stiffening elements 13a and 13b brace the diffuser wall 11 only locally in a comparatively small area relative to the entire outer surface area of the diffuser wall 11. The individual stiffening elements 13a and 13b here form cells 130a and 130b with differing geometries. While the one stiffening element 13a forms cells 130a with rectangular cross-section, the cells 130b of the other stiffening element 13b are square in cross-section.

(24) FIGS. 4A and 4B illustrate a further design variant of a diffuser component 6 in accordance with the invention. In this variant, at least one additional flat stiffening element 14a or 14b is provided additionally to at least one stiffening element 13 with lattice-type stiffening structure. An additional flat stiffening element 14a or 14b of this type is for example made from a thin metal sheet and is arranged on the lattice-type structure of a stiffening element 13, such that the respective additional flat stiffening element 14a or 14b covers at least part of the lattice-type structure. A stiffening element 14a or 14b can here be welded or brazed for example to the stiffening element 13 and its lattice-type structure.

(25) An additional flat stiffening element 14a or 14b serves here to additionally absorb axial forces during operation of the gas-turbine engine. It is thus possible using appropriately positioned additional flat stiffening elements 14a or 14b to further brace a diffuser wall 11 locally, for example particularly in areas where an increased (vibration) stress can be expected during operation of the gas-turbine engine.

(26) While the stiffening elements 13, 13a and 13b shown in the attached Figures are all provided on an outer side 110 and hence on an outer surface area of the diffuser wall 11, it can nevertheless be provided in one variant that one stiffening element 13, 13a or 13b or several stiffening elements 13, 13a or 13b are (also) provided on an inner side 111 of the diffuser wall 11 facing the fluid flow or are integral therewith. To prevent here a disruptive effect on the fluid flow by the compartments or cells 130, 130a, 130b or 130c of the respective lattice-type structure during operation, an additional flat stiffening element 14a, 14b or several additional flat stiffening elements 14a, 14b can be provided to cover the lattice-type structure(s). A plane inner surface of the additional stiffening element 14a, 14b then faces the fluid flow.

LIST OF REFERENCE NUMERALS

(27) 1 Compressor casing 10 Combustion chamber 11 Diffuser wall 110 Outer side 111 Inner side 12 Outlet guide vane outer wall 13, 13a, 13b Stiffening element 130, 130a, 130b, 130c Cell 131 Strut 132 Stiffening segment 14a, 14b Additional flat stiffening element 2 Compressor rotor 3 Compressor rotor hub 4 Compressor rotor disk 5 Gap between rotor and outlet guide vane 6 Diffuser 60 Inlet 61 Outlet 7 Outlet guide vane 8 Outer combustion chamber casing 9 Inner combustion chamber casing a1, a2 Distance d1, d2, d3, d4 Thickness/height l1, l2, l3, l4 Length M Engine axis x, y, z Extension direction