Multi-Way Valve of a Fuel System of a Gas Turbine

Abstract

A multi-way valve of a fuel system of a gas turbine is provided. The multi-way valve includes a valve body provided with a cylindrical housing, the wall bounding the housing includes a plurality of openings for supplying and/or removing fluids, wherein a movably supported insert including at least one channel having two additional openings is provided in the housing, whereby two adjoining openings may be fluidically connected to each other.

Description

FIELD OF INVENTION

The invention refers to a multi-way valve of a fuel system of a gas turbine. Furthermore, the invention refers to a fuel system of a gas turbine with a multi-way valve of this type.

BACKGROUND OF INVENTION

In known fuel systems of gas turbines, a so-called “multi-function valve” (MFV) (see FIG. 1) exists for their oil or fuel supply. This MFV comprises a plurality of valves in order to be able to switch over between an oil supply source, a nozzle and a drain line of the fuel system. During the switchover, the valves between the respective pipelines 1 . . . n are controlled at the same time via an actuator in each case.

In this case, the pipelines, particularly in the form of burner connecting lines for diesel oil and water, have to be switched in a way that different operating modes such as diesel-oil operation, emulsion operation and also flushing and draining processes can be carried out.

There is also an actuator in order to control a plurality of like valves for the source (Q₁-Q_n), drain line (S₁-S_n) and nozzle (N₁-N_n) at the same time. These actuators are as a rule electrohydraulic. Therefore, for example “n” valves are moved in the source line by means of one actuator. Consequently, at least three actuators are required.

In addition to the closing of all the valves, the following flow connections are possible:

• Source+drain line (valve in nozzle line closed),
• Source+nozzle (valve in drain line closed) and
• Drain line+nozzle (valve in source line closed).

Known multi-way valves are still comparatively expensive and prone to malfunction.

Furthermore, ball valves of various design are known from a plurality of printed publications. For example, EP 0 240 059 features a hydrostatically balanced ball valve. In addition, a particularly compact shut-off cock with a spherical or cylindrical plug is known from DE 12 09 382. Furthermore, a distributor valve, which has a rotary slide which interconnects a plurality of ports arranged in different planes, is known from U.S. Pat. No. 5,090,194. Furthermore, the arrangement of a rotary slide in a housing is known from DE 596 026. DE 460 190 similarly describes the arrangement of a rotary slide valve in which the valve body can be pivoted around a common axis.

SUMMARY OF INVENTION

It is an object of the invention to create a fuel system of a gas turbine, in which the aforementioned disadvantages are overcome and in particular, a reliable and simple remote operation of the switching processes of the associated valves is possible. Furthermore, new interconnecting possibilities for new gas turbine types are to be created.

The object is achieved with a multi-way valve according to the claims. Advantageous developments of the solution according to the invention are described in the dependent claims. Furthermore, the object is achieved with a fuel system of a gas turbine with a multi-way valve according to the invention.

According to the invention, a multi-way valve of a fuel system of a gas turbine is created, in which multi-way valve provision is made for a valve body which is provided with a cylindrical housing, a plurality of ports for the feed and/or drain of fluids being arranged in the wall of the valve body which delimits the housing, wherein provision is made in the housing for a movably supported insert with at least one passage with two additional ports by means of which two adjacent ports can be fluidically interconnected.

With the solution according to the invention, the ports are arranged lying in one plane perpendicularly to the center axis of the housing, and the insert is formed corresponding to the housing and is supported in the housing in a manner in which it can rotate around its center axis. The rotatable insert forms a control element which is simple to operate.

With the solution according to the invention, the housing, at at least two axial positions, has in each case a plurality of ports which lie in one plane, and the insert, at a distance which corresponds to the spacing of the planes, has at least one passage for each plane in order to fluidically interconnect the ports which lie inside one of the planes. Thus, a plurality of valves which are to be operated at the same time can be formed and operated with only one switching element.

It is provided according to the invention that provision is made for two bridges which are arranged in the valve body and which in each case interconnect ports which are arranged in different planes.

In a first advantageous development of the solution according to the invention, “m” is the number of ports along a circumference along the wall. The insert has a passage, the additional ports of which are arranged in an offset manner to each other by an angle a along its circumference, α=360°/m being applicable to the angle α. In this way, a plurality of switching positions which are distributed on the circumference can be realized.

In a second advantageous development of the solution according to the invention, four ports are distributed uniformly along the circumference of the cylindrical housing and the additional ports of the passage which is arranged in the insert are arranged along the circumference at an angle to each other, which is equal to 90°. This configuration, with adequate switching distance, at the same time offers an adequately large number of switching positions.

In the fuel system according to the invention, the multi-way valve is configured as a 3/3 directional valve and a 4/3 directional valve operationally connected to it. The switching arrangement of this type consisting of the two stated directional valves surprisingly fulfills all the necessary switching functions and at the same time is especially simple, inexpensive and operationally reliable to operate in the process.

In a final advantageous development of the solution according to the invention, a plurality of disk pairs, which are associated in each case with a burner, are arranged in series. In this way, a large number of passages or burners of a gas turbine can be supplied as desired. The disks can be easily operated together by them being rotationally-fixedly arranged on a shaft.

BRIEF DESCRIPTION OF THE DRAWINGS

An exemplary embodiment of the solution according to the invention is subsequently explained in more detail with reference to the attached schematic drawings.

In the drawing:

FIG. 1 shows a schematic diagram of an MFV according to the prior art,

FIG. 2 shows a plan view of a first exemplary embodiment of a multi-way valve according to the invention,

FIG. 3 shows a perspective view of an insert of the multi-way valve according to FIG. 2,

FIG. 4 shows a perspective view of a second exemplary embodiment of a multi-way valve according to the invention with its housing and insert,

FIG. 5 shows a diagram of the switching principle of a fuel system to be realized according to the invention of a gas turbine,

FIG. 6 shows a diagram of the switching principle of a 3/3 directional valve,

FIG. 7 shows a schematic diagram of the switching arrangement according to the invention with a 3/3 directional valve and a 4/3 directional valve, and

FIG. 8 shows a perspective view of an exemplary embodiment of a multi-way valve according to the switching arrangement of FIG. 7.

DETAILED DESCRIPTION OF INVENTION

In the exemplary embodiment which is shown in FIGS. 2 to 4, the previously individual valves of an MFV according to the prior art (compare FIG. 1) are replaced by a multi-way valve or a device 1 with which by rotating or displacing an insert 2 which is installed therein, a switchover between different inlets and outlets can be carried out.

Thus, in the exemplary embodiment which is shown, a bore as a cylindrical housing 3 is provided in a valve body. In the wall which delimits the housing 3, four ports 4, which are offset by 90° in each case and lie in one plane perpendicularly to the center axis of the housing 3, are formed as inlets or outlets.

They are therefore uniformly distributed along the circumference. Two of the ports 4 are fluidically

A). In this case, a (then open) shut-off valve V1 is in the line. A line in which a second (then closed) shut-off valve V2 is located, branches from the line A upstream of the shut-off valve V1 in the flow direction. Running into this line, downstream of the shut-off valve V2 in the flow direction, is a line C into which a flushing medium SM can be fed. In the line C, moreover, a check valve is located. A third shut-off valve V3 enables the flushing medium to be channeled through to a line D (way C-D=path B, C), a fourth valve V4 shutting off a drainage line or discharge line E.

Furthermore, the line B can be flushed with flushing fluid SM through the valves V2 and V1 (way C-B=path D), while at the same time the valve V4 opens the drain line E and the valve V3 prevents flushing fluid SM backflowing into the line C (way D-E=path D).

All the switching functions in the exemplary embodiment which is shown in FIGS. 7 and 8 are realized by means of a combination of a 3/3 directional valve and a 4/3 directional valve which is connected to this at the same time. FIG. 6 shows in this case the basic construction of a 3/3 directional valve which is used.

As is to be seen in FIG. 7, the multi-way valve which is shown there comprises an insert 2 with two disks, specially the disks 8 and 9, in which a passage 6 is located in each case (corresponding to FIGS. 2 to 4). The housing 3 which encloses the disks 8 and 9 contains associated ports so that the disk 8 acts as a 3/3 directional valve and the disk 9 acts as a 4/3 directional valve. The switching positions S1 to S3 which are occupied in each case in the process are to be gathered from the three sub-figures.

In FIG. 8, the entire arrangement according to FIG. 7 is schematically shown in perspective view. In this case, it is to be seen that for realizing the switching arrangement the leads to the first disk 8 and the lines D and E alone lead to the second disk 9. FIG. 8 shows the position S3, wherein the position S2 is occupied by the two rotationally-fixedly interconnected disks 8 and 9 being rotated to the right by 90°, and the position S1 is occupied by rotation to the right by a further 90°.

Claims

1.-6. (canceled)

7. A multi-way valve of a fuel system of a gas turbine, comprising: a valve body provided with a cylindrical housing; anda plurality of ports for the feed and/or drain of fluids arranged in a wall of the valve body which delimits the housing,wherein provision is made in the housing for a movably supported insert including a passage with two additional ports by means of which two adjacent ports may be fluidically interconnected,wherein the plurality of ports are arranged lying in a first plane perpendicularly to first center axis of the housing and in which the insert is formed corresponding to the housing and is supported in the housing in a manner in which the insert may rotate around a second center axis,wherein the housing, at at least two axial positions, includes in each case the plurality of ports which lie in a second plane, and the insert, at a distance which corresponds to a spacing of the planes, includes the passage for each plane in order to fluidically interconnect the plurality of ports which lie inside one of the planes, andwherein provision is made for two bridges which are arranged in the valve body and which in each case interconnect the plurality of ports which are arranged in different planes.

8. The multi-way valve as claimed in claim 7, wherein “m” is a number of the plurality of ports along a circumference along the wall where the insert includes the passage,wherein a plurality of additional ports of the passage are arranged in an offset manner to each other by an angle a along the circumference, andwherein α=360°/m.

9. The multi-way valve as claimed in claim 8, wherein four ports are distributed uniformly along the circumference of the cylindrical housing, andwherein the plurality of additional ports of the passage which is arranged in the insert are arranged along the circumference at an angle to each other, which is equal to 90°.

10. A fuel system of a gas turbine, comprising: a multi-way valve, comprising: a valve body provided with a cylindrical housing, anda plurality of ports for the feed and/or drain of fluids arranged in a wall of the valve body which delimits the housing,wherein provision is made in the housing for a movably supported insert including a passage with two additional ports by means of which two adjacent ports may be fluidically interconnected,wherein the plurality of ports are arranged lying in a first plane perpendicularly to first center axis of the housing and in which the insert is formed corresponding to the housing and is supported in the housing in a manner in which the insert may rotate around a second center axis,wherein the housing, at at least two axial positions, includes in each case the plurality of ports which lie in a second plane, and the insert, at a distance which corresponds to a spacing of the planes, includes the passage for each plane in order to fluidically interconnect the plurality of ports which lie inside one of the planes, andwherein provision is made for two bridges which are arranged in the valve body and which in each case interconnect the plurality of ports which are arranged in different planes, andwherein one plane of the multi-way valve is configured as a 3/3 directional valve and the other plane of the mutli-way valve is configured as a 4/3 directional valve for forming a 5/3 directional valve.

11. The fuel system as claimed in claim 10, wherein a plurality of disk pairs, which are associated in each case with a burner, are arranged in series.

12. A gas turbine with a fuel system, comprising. a multi-way valve, comprising: a valve body provided with a cylindrical housing, anda plurality of ports for the feed and/or drain of fluids arranged in a wall of the valve body which delimits the housing,wherein provision is made in the housing for a movably supported insert including a passage with two additional ports by means of which two adjacent ports may be fluidically interconnected,wherein the plurality of ports are arranged lying in a first plane perpendicularly to first center axis of the housing and in which the insert is formed corresponding to the housing and is supported in the housing in a manner in which the insert may rotate around a second center axis,wherein the housing, at at least two axial positions, includes in each case the plurality of ports which lie in a second plane, and the insert, at a distance which corresponds to a spacing of the planes, includes the passage for each plane in order to fluidically interconnect the plurality of ports which lie inside one of the planes, andwherein provision is made for two bridges which are arranged in the valve body and which in each case interconnect the plurality of ports which are arranged in different planes, andwherein one plane of the multi-way valve is configured as a 3/3 directional valve and the other plane of the mutli-way valve is configured as a 4/3 directional valve for forming a 5/3 directional valve.

13. The gas turbine as claimed in claim 12, wherein a plurality of disk pairs, which are associated in each case with a burner, are arranged in series.