Turbine generator

Abstract

A turbine generator comprising a turbine rotor comprising a hub and one or more blade stages. Each stage comprising a circumferential array of rotor blades in driving engagement with the hub. A turbine stator comprising a hub and one or more vane stages, each stage comprising a circumferential array of vanes. The turbine rotor and turbine stator being concentrically arranged about a common axis to define an annular flow path. The vane stages and blade stages being axially spaced along the axis and having one or more magnets arranged on the rotor. A generator stator concentrically aligned with the turbine rotor and turbine stator and one or more magnets arranged on the rotor. In use, when the turbine is driven to rotate about the axis, the or each of the magnets on the turbine rotor rotate relative to the generator stator in order to generate electric power.

Claims

1. A turbine generator comprising: a turbine rotor comprising a rotor hub and a blade stage, the blade stage comprising a circumferential array of rotor blades in driving engagement with the rotor hub; a turbine stator comprising a stator hub and a vane stage, the vane stage comprising a circumferential array of vanes; the turbine rotor and the turbine stator being concentrically arranged about a common axis to define an annular flow path, the vane stage and the blade stage being axially spaced along the common axis, and having one or more magnets arranged on the turbine rotor; and a generator stator concentrically aligned with the turbine rotor, the turbine stator, and the one or more magnets whereby, when the turbine rotor is driven to rotate about the common axis, the one or more magnets on the turbine rotor rotate relative to the generator stator in order to generate electric power, wherein each of the rotor blades has a free end and an end attached to the rotor hub, and each of the one or more magnets is attached to the rotor hub adjacent to where a respective one of the ends is attached to the rotor hub.

2. The turbine generator as claimed in claim 1, wherein the generator stator is arranged along the common axis with the turbine stator radially outermost.

3. The turbine generator as claimed in claim 1, wherein the turbine stator is arranged along the common axis with the generator stator radially outermost.

4. The turbine generator as claimed in claim 1, wherein each of the one or more magnets are axially aligned with a rotor stage.

5. The turbine generator as claimed in claim 1, wherein each of the one or more magnets do not extend axially beyond the rotor hub.

6. The turbine generator as claimed in claim 1, wherein each of the one or more magnets abut the rotor hub.

7. The turbine generator as claimed in claim 1, wherein the rotor hub is cylindrical.

8. The turbine generator according to claim 1, wherein the turbine generator is a compressor of a gas turbine engine.

9. A gas turbine engine comprising the turbine generator according to claim 8.

10. The turbine generator according to claim 1, wherein the turbine generator is a steam turbine.

11. The turbine generator according to claim 1, wherein the turbine generator is a turbine of a gas turbine engine.

12. The turbine generator according to claim 1, wherein the turbine generator is a steam turbine for a Rankine cycle.

13. A turbine generator as claimed in claim 1, wherein each of the one or more magnets is fastened to a surface of the rotor hub.

Description

BRIEF DISCUSSION OF THE FIGURES

(1) Embodiments will now be described by way of example only, with reference to the Figures, in which:

(2) FIG. 1 is a Rankine cycle schematic diagram as is known in the art;

(3) FIG. 2 is a sectional side view of a turbine generator as claimed herein;

(4) FIG. 3 is a sectional side view of a turbine generator as claimed herein;

(5) FIG. 4 is a sectional side view of a gas turbine engine comprising a turbine generator as claimed herein.

DETAILED DESCRIPTION OF THE DISCLOSURE

(6) FIGS. 2 and 3 show schematic sectional side views of embodiments of the turbine generators according to the present disclosure. Whilst FIGS. 2 and 3 are generally more applicable for use in conjunction with steam turbines, the arrangement may equally be applied to a gas turbine engine. In these figures, the single rotor turbine-generator (SRTG) mounts the rotating elements of both the prime mover and the generator to a single rotating part. The static element of either the prime mover or the generator will be the core section of the machine, thus inverting the traditional machine layout.

(7) FIG. 2 shows an example arrangement of a SRTG. The electrical generator rotor is of a drum design being hollow and having a wall thickness that is small in relation to its diameter. The rotor has an inner and an outer surface onto which rotating elements of a steam turbine and the generator are mounted. The steam turbine element, which is mounted inside the drum, generates a torque by expanding steam through a number of stages comprising static and rotating aerofoils as in a traditional design. The torque leads to rotation of the drum about a central axis. The generator element of the rotor has permanent magnets, which are mounted to the drum surrounding the central axis. This when rotated within an armature generates electrical power.

(8) Regarding FIG. 2, a rotor hub 21 is shown that is rotatable about a central axis 26. Rotor blades 20 extend radially inwards from the rotor hub 21. A stator hub 23 is positioned along the rotational axis 26 radially inside the rotor hub 21 and has vanes 27 extending radially outwardly from it. These vanes are configured in the classical stator vane configuration. The stator hub 23 is supported by mounts 28. The rotor hub 21 is supported on bearings 24. The rotor hub 21 has a permanent magnet(s) 25 on its radially outer surface. A generator stator 22 circumferentially surrounds the rotor hub 21. Fluid, such as gas, liquid, or vapour, or combinations comprising one or more of the same, enters the rotor chamber as shown by arrow A and exits the flow path as shown by arrow B. In this the steam is supplied to the turbine via a valve, or valves, which regulate its flow. For higher power outputs from the turbine generator, the valves will open and allow higher steam flow. The passage of the fluid over the rotor blades causes the hub and its associated permanent magnets to be rotated within the generator stator. The generator can be coupled to any suitable electrical power system or network.

(9) FIG. 3 shows an example arrangement wherein the rotor hub radially surrounds the electrical generator, and the rotor stages extend radially outwardly from the rotor hub. FIG. 3 shows a rotor hub 31 that is rotatable about an axis 36. Rotor blades 30 extend radially outwards from the rotor hub 31. A stator hub 33 is positioned radially outside the rotor hub 31 and has stator vanes stages 37 extending radially outwards. The rotor hub 31 is supported on bearings 34. The rotor hub 31 has permanent magnets 35 on its radially inner surface. A generator stator 32 is arranged radially inside the rotor hub 31. The generator stator 32 is supported on mounts 38. Fluid, such as gas, liquid, or vapour, or combinations comprising one or more of the same enters a flow path between the rotor and stator hubs as shown by arrows A′ and exits the rotor as shown by arrows B′. The fluid flow through this passage results in a rotation of the rotor hub through interaction between the fluid and the turbine blades mounted to the rotor hubs.

(10) As in conventional generators, the movement of a permanent magnet with respect to a generator stator causes the generator to generate electrical power. The movement of these is driven by the flow of fluid through the passageway over the turbine blades of the SRTG. The components shown extend around the circumference of the rotational axis 26,36. Steam can be fed into these generators from a boiler using any suitable pipe arrangement, and any suitable boiler arrangement. Steam can then be collected at the exit B and fed into a condenser before being fed back into the boiler.

(11) The permanent magnet 25,35 may be a single ring or a plurality of separate permanent magnets distributed, for example evenly distributed, around the circumference of the rotor section 21,31. The permanent magnets 25,35 may be fastened or mechanically coupled to the rotor hub 21,31. The permanent magnets 25,35 are axially aligned with the generator stator 22,32. The permanent magnets 25,35 have an axial length that corresponds with the generator stator 22,32, for example suitable for generating efficient electrical power.

(12) FIGS. 2 and 3 show three stator stages of stator blades 27,37. FIGS. 2 and 3 show two rotor stages of rotor blades 20,30. The rotor stages and stator stages are interspersed. In other examples there may be a greater or less number of rotor or stator stages. In other examples the rotor hub 21,31 may have a different shape, for example conical, frustoconical, curved or made of a plurality of curves. The extremal shape of the rotor hub can be optimised to the requirements of the prime mover. For example, as the working fluid expands along the rotor a larger passage area will be required; thus, leading to a conical shape. The internal shape of the rotor hub can be a plain cylinder. Alternatively, it can be profiled to aid the flow of cooling air over the generator

(13) FIG. 4 shows a sectional side view of a gas turbine 60, comprising a turbine generator according to the present disclosure. The compressor 64 has a plurality of permanent magnets 65 attached to it. A generator stator 67 is arranged radially inside the permanent magnets 65 to form a generator. The permanent magnets 65 and generator stator 67 are axially aligned. The generator stator 67 is supported by a mount 66 to a static part of the gas turbine engine 60. The gas turbine 60 also has a fan 63 and turbine section 68. The turbine section 68 drives the compressor 64 in a conventional manner. In this example of an aviation gas turbine engine the gas turbine would provide motive thrust for the aircraft plus, by virtue of the integrated generator, will provide electrical power output. This may be used to power aircraft electrical systems or may be used within a hybrid propulsion architecture where emery is stored in a battery and used to power motor driven propulsion engines. Alternative gas turbine applications could be pure power generation and could be used in place of conventional gas turbine driven generators.

(14) As the compressor rotor 44 rotates about the rotational axis 41 during operation, the permanent magnets 45 move with respect to the generator stator 47 thereby forming a generator and generating electrical power. The electrical power may be used for auxiliary systems of the gas turbine 40. In alternative arrangements the permanent magnets 45 and generator stator 47 may be arranged on a different rotating component of the gas turbine engine, for example a turbine section, and/or may be on the radially outer part of the rotating part. In other embodiments the permanent magnets 45 and generator stator 47 may be larger or smaller depending on the power requirements. In other embodiments there may be no fan, for example when the gas turbine is for ground based power generation.

(15) It will be understood that the invention is not limited to the embodiments above-described and various modifications and improvements can be made without departing from the concepts described herein. Except where mutually exclusive, any of the features may be employed separately or in combination with any other features and the disclosure extends to and includes all combinations and sub-combinations of one or more features described herein.