Method for producing a rotor of a flow engine

Abstract

The invention relates to a method for producing a rotor of a flow engine, namely an integrally bladed rotor with an integral outer shroud, comprising at least the following steps: a rotor blank comprising the integral rotor blades and the integral outer shroud is first produced by means of a generative production method; the rotor blank is then subjected to a separating surface treatment at flow-guiding sections and is subjected, separately therefrom, to a machining surface treatment at non-flow-guiding sections.

Claims

1. A method for producing a rotor of a turbo machine, the rotor comprising an integrally bladed rotor with integral outer shroud, comprising the following steps: producing, by a generative production method, a rotor blank comprising the integral moving blades and the integral outer shroud; and subjecting the rotor blank, on flow-conducting sections, to an abrasive cutting surface treatment and, separately, on non-flow-conducting sections, to a chip-machining surface treatment.

2. The method according to claim 1, wherein the rotor blank comprising the integral moving blades and the integral outer shroud is produced by selective laser melting.

3. The method according to claim 2, wherein a metal powder is used as a metal powder for the selective laser melting, the metal powder having the following composition, in percent by weight: 5.50-6.75 Al, 3.50-4.50 V, 0.30 Fe, 0.08 C, 0.05 N, 0.20 O, 0.015 H, and Ti in the remainder.

4. The method according to claim 1, wherein the rotor blank is subjected to a flow grinding on flow-conducting sections.

5. The method according to claim 1, wherein the rotor blank is subjected to a turning on non-flow-conducting sections.

6. The method according to claim 5, wherein the rotor blank is subjected to a flow grinding on flow-conducting sections.

7. The method according to claim 5, wherein the flow grinding is performed prior to the turning.

8. The method according to claim 1, wherein the rotor blank is subjected to a heat treatment prior to the abrasive cutting surface treatment and prior to the chip-machining surface treatment.

9. The method according to claim 1, wherein the rotor blank is subjected to a hot-isostatic pressing prior to the abrasive cutting surface treatment and prior to the chip-machining surface treatment.

10. A method for producing a rotor of a turbo machine, the rotor comprising an integrally bladed rotor with integral outer shroud, comprising: producing, by a generative production method, a rotor blank comprising the integral moving blades and the integral outer shroud; and subjecting the rotor blank, on flow-conducting sections, to an abrasive cutting surface treatment and, separately, on non-flow-conducting sections, to a chip-machining surface treatment, and wherein at least one of: the rotor blank is subjected to a flow grinding on flow-conducting sections, the rotor blank is subjected to a turning on non-flow-conducting sections, and the rotor blank is subjected to a hot-isostatic pressing prior to the abrasive cutting surface treatment and prior to the chip-machining surface treatment.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The FIGURE is a block diagram illustrating method steps of the method for producing a rotor of a turbo machine according to the invention.

DETAILED DESCRIPTION OF THE PRESENTLY PREFERRED EMBODIMENTS

(2) The present invention relates to a method for producing a rotor of a turbo machine, in particular of a compressor or alternatively of a turbine.

(3) The method produces an integrally bladed rotor with integral outer shroud, in the case of which moving blades of the rotor are thus an integral part of a radially inner rotor basic body, and wherein the rotor furthermore comprises an outer shroud radially outside which is connected to the moving blades in a fixed manner radially outside.

(4) In the present invention, a rotor blank is initially produced by a generative production method, comprising integral moving blades and the integral outer shroud. Accordingly, the moving blades are an integral part of a rotor basic body, while the outer shroud is likewise an integral part of the rotor blank. Following this step, the rotor blank is subjected, on flow-conducting sections, to an abrasive cutting surface treatment, and, separately thereof, to a chip-machining surface treatment on non-flow-conducting sections.

(5) The method for producing an integrally bladed rotor with integral outer shroud according to the invention manages to do without welded connections.

(6) Further details of the method according to the invention are described in the following, making reference to the block diagram of the FIGURE, wherein in the FIGURE, shown in continuous line drawing are obligatory method steps of the method according to the invention, wherein blocks shown in dashed line drawing are not mandatory part of the method for producing an integrally bladed rotor with integral outer shroud according to the invention.

(7) In step 10, geometry data of the rotor to be produced are provided, wherein the geometry data are design data, which are based on process conditions and based on a material selection for the rotor to be produced.

(8) Based on the geometry data provided in step 10, the production of the rotor by a generative production method takes place in a step 11, wherein the rotor blank comprises a rotor basic body, integral moving blades and an integral outer shroud.

(9) Preferentially, selective laser melting is used as generative production method in step 11, wherein method-related details of the selective laser melting are known.

(10) Preferentially, a powder is used as metal powder for the selective laser melting in step 11, which in percent by weight has the following composition:

(11) TABLE-US-00001 5.50-6.75 Al Aluminium 3.50-4.50 V (Vanadium) 0.30 Fe (Iron) 0.08 C (Carbon) 0.05 N (Nitrogen) 0.20 O (Oxygen) 0.015 H (Hydrogen) Ti (Titanium) in the remainder

(12) A rotor for a turbo machine with integral moving blades and integral outer shroud can be particularly advantageously produced from such a metal powder by selective laser melting.

(13) The rotor blank produced in step 11 by selective laser melting can be subjected in the optional method step 12 to a heat treatment and/or a hot-isostatic pressing. By way of this step, component properties of the rotor blank can be adjusted or influenced prior to the downstream method steps 13 and 14.

(14) In the obligatory method steps 13 and 14, a surface treatment of the rotor blank on flow-conducting sections and on non-flow-conducting sections are performed separately from one another by different surface treatment methods, wherein preferentially in step 13 flow-conducting sections and subsequently in step 14 non-flow-conducting sections of the rotor blank are preferentially subjected to the surface treatment.

(15) In the step 13, in which the flow-conducting sections of the rotor blank are subjected to a surface treatment, an abrasive cutting surface treatment is employed, preferentially a flow grinding.

(16) Following this step, a chip-machining surface treatment of the rotor blank on non-flow-conducting sections, preferentially by turning, takes place in the method step 14.

(17) With the method according to the invention it is possible to produce, without restrictions in terms of geometry freedom, an integrally bladed rotor with integral outer shroud. A rotor blank is produced by a generative production method, preferentially by selective laser melting, namely preferentially consisting of a metal powder of a titanium alloy. The rotor blank produced by selective laser melting is then subjected to a surface treatment, namely separately from one another via suitably adapted surface treatment methods on flow-conducting sections and on non-flow-conducting sections.

(18) The process chain according to the invention allows the production of aerodynamically and thermodynamically optimized integrally bladed rotor with integral outer shrouds without welded connections and can be realized in light-weight construction.

(19) Thus, while there have shown and described and pointed out fundamental novel features of the invention as applied to preferred embodiments thereof, it will be understood that various omissions and substitutions and changes in the form and details of the method described may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that method steps shown and/or described in connection with any disclosed embodiment of the invention may be incorporated in any other disclosed or described or suggested embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.