DIVERTER VALVE

Abstract: In a tandem fan gas turbine engine two fan compressor stages are provided connected by a flow duct (14) housing a diverter valve (26) which can be used to admit the flow from the first fan to the second fan or to divert it to exhaust through an auxiliary outlet in which case the second fan draws ambient air in through an auxiliary inlet. The connecting duct is annular in cross section because an inner cylindrical wall surrounds the shaft driving the front fan. The diverter valve which therefore has to operate in the annular duct comprises a pair of flat side lobes (40, 42) connected by curved plates which straddle the inner wall. The valve is operated by a rotary actuator (54) in synchronism with closure means which obstruct or open the auxiliary outlet and inlet.

Description: The invention relates to a diverter valve for a variable cycle gas turbine engine. In particular the invention concerns a valve for selectively changing the flowpath of working fluid through a tandem fan engine. The present invention is particularly concerned with variable cycle gas turbine engines of the type described in our UK Patents Nos GB 1,389,347 and GB 1,415,679. These engines have a first axial flow compressor, sometimes referred to as a front fan and a core engine incorporating a further fan type compressor, thus giving rise to the idea of tandem fans. The two compressor fan stages may be driven by separate turbines. A tandem fan engine can be operated alternatively in series-flow or parallel-flow modes. In the first the whole of flow output of the first fan is ducted to the second compressor fan thereby effectively supercharging the core engine. In the alternative the flow output of the front fan is discharged from the communicating duct and the second fan draws air into the core engine through an auxiliary inlet. The flow from the first fan may be discharged into a by-pass duct or directed to one or more discharge nozzles, these may be fixed or vectorable. To selectively redirect the fluid flowpath in the communicating duct between the two fan stages a diverter valve is provided, together with auxiliary inlet and outlet apertures. Examples of diverter valves are described in the above mentioned patents. The present invention is intended to provide a simpler valve design which is lighter and more efficient than these earlier proposals. According to the present invention a diverter valve for use in a annular flow duct defined by inner and outer concentric duct walls has a valve means pivotable between a first blocking position in which the margins of the valve means seal against the inner and outer duct walls to stem flow along the duct and a second position in which the valve means causes minimum obstruction to flow in the duct, and further the valve means (26) comprises four integrally joined sections (40, 42, 50, 52) which surround the inner duct wall (28), these four sections comprise a pair of flat side lobes (40,42) on opposite sides of the inner duct wall (28) and a pair of semi-cylindrical transverse portions (50,52) spaced apart towards opposite ends of the side lobes (40,42) and curving in opposite directions with radii conforming substantially to the curvature of the inner duct wall (28). Preferably the transverse portions of the valve means are curved to lie flush with the inner wall of the duct when the valve occupies a second position in which position the side lobes also lie parallel to the axis of the duct. The present invention and one embodiment of the valve will now be described in more detail, by way of example only, with reference to the accompanying drawings in which: Figures 1 and 2 are part sectioned schematic views of a tandem fan engine showing the diverter valve in parallel-flow and series-flow modes respectively, Figure 3 is a detailed isometric view of the diverter valve of figure 1 in the parallel-flow position, and Figure 4 is a sectioned side view corresponding to figure 3. Referring to figure 1 and 2 there is shown a tandem fan gas turbine engine (10) comprising in flow series a first axial flow compressor (12), a fluid flow duct (14) a second axial flow compressor (16), combustion means (18), turbine means (20) connected by shafts (not shown) to drive the compressors (12 and 16), a jet pipe (22) and a rear exhaust nozzle (14). The diverter valve (26) is located between the tandem fans or compressors (12 and 16) and therefore is housed within the flow duct (14). Drive to the front fan (12) is therefore carried by means of an axial forward extending shaft (see figure 1) which passes through the duct (14) and is surrounded by an inner cylindrical housing or wall (28). The duct is further defined by an outer co-axial cylindrical wall (30). The duct (14) is therefore annular in transverse section. One end of duct (14), towards the left in the drawings, is in open communication with the rear of the first fan (12) to receive fluid flow therefrom and the opposite end of the duct, towards the right in the drawings, is in open communication with the front face of the second fan (16) to supply fluid to the core engine. The duct (14), in addition to housing the diverter valve (26), is also provided in its outer wall (30) with apertures (32 and 34) which may be selectively opened and closed. For simplicity in the drawings the apertures are illustrated as having sliding covers or doors (36 and 38) respectively, although it should be understood that in practice other means of closure may be provided for example shutters. In an alternative arrangement each aperture is provided with closure means comprising a plurality of movable slats or vanes which are disposed transversely, with respect to the longitudinal axis of the engine, and which are mounted for pivotal movement each about its lengthwise axis. The slats or vanes may be shaped in section to help entrain air into the duct in the open position. In the closed position the slats may overlap slightly or the front and trailing edges may abut in order to effectively seal the apertures. In figure 1 the covers (36 and 38) are slid to positions which open the apertures (32 and 34), while in figure 2 the are shown in their alternative positions closing the apertures. The apertures, as can be seen from figure 1, are offset in opposite directions with respect to the axis of the diverter valve (26) so that, when the valve is deployed as in figure 1, aperture (32) is downstream of the valve while aperture (34) is upstream of the valve. Thus, when the engine and consequently both fans are operating with the diverter valve raised as shown the upstream aperture becomes an auxiliary outlet for flow leaving the front fan while the downstream aperture acts as an auxiliary inlet permitting the second fan to draw ambient air into the core engine. Constructional details of the diverter valve (26) can best be seen in figures 3 and 4, basically the movable valve member or members pivot about a transverse axis in the duct (14) in the manner of a butterfly valve. The valve (26) comprises a pair of side lobes (40 and 42) disposed on either side of the inner axial cylindrical wall (28). These side lobes consist of flat plates pivotally and symmetrically mounted for rotation about a common axis (44) which also passes perpendicularly through the axis of the duct (14). The plates (40 and 42) have straight sides along their inner margins adjacent to the inner wall (28) of the annular duct so that in the first or raised position of the valve as shown in figures 3 and 4 these sides are tangential to the wall (28) at the points of intersection with the rotational axis (44). The shape of the lobes (40 and 42) is of a section of an ellipse defined by an oblique section through the outer wall (30) of the duct. Thus, when the valve is raised to its first position the outer margins (46 and 48) of the lobes contact the inner surface of the outer wall (30) on a corresponding oblique section. Sealing means may be provided along these outer margins. The valve member further comprises curved plates (50 and 52) which straddle the inner cylindrical wall (28) passing over and under it between the inner edges of the side lobes respectively above and below the rotational axis (44). The curvature of these plates has substantially the same radius of that of the inner wall (28) of the annular duct (14) so that they lay flush with the wall (28) in the lowered or second position of the valve. In the end view the curved plates (50 and 52) are semi-circular so that their sides extend as far as the centre line of the duct. The plates are also spaced apart axially on either side of transverse pivotal axis (44) which bisects the side lobes (40 and 42). Thus, when the lobes (40 and 42) and the curved straddling section (50 and 52) are all lowered in the second position of the diverter valve the sides of the plates (50 and 52) meet the inner edges of the lobes (40 and 42) from above and below respectively. The adjacent edges of these four members (40, 42, 50 and 52) may be rigidly joined to form a single composite valve member so that all parts move in unison. Rotary actuation means 54 is provided operatively connected to rotate the valve about axis (44). The inner and outer margins (56 and 58) of curved plate (50), and margins (60 and 62) of curved plate (52), that is their proximal and distal edges having regard to their pivotal mounting, are required to sealingly engage the inner and outer walls (28 and 30) of the annular duct (14) in the first or raised position of the valve (26). Thus, the loci of these edges is determined by the intersection at an inclined angle of the surfaces of three cylinders of different radii. The outer duct wall (30) comprises a first cylinder of larger radius and the inner duct wall (28) comprises a second cylinder of small radius disposed co-axially with respect to the first cylinder. The valve member (14) can be considered as two halves of a third cylinder of the same radius as the second cylinder but disposed with its axis inclined relative to the axis of the other two cylinders. The loci of the distal edges (58 and 60) are defined by the intersection of the third part-cylindrical surfaces with the second cylindrical surface. In order to effect efficient sealing these edges may be provided with lip seal means (not shown in the drawings). If a certain degree of leakage past the valve (26) may be tolerated or is desired, the shape of the edges of the curved plates may be simplified as one way of achieving this. For example, the proximal edges (56 and 60) of the curved straddle plates (50 and 52) instead of following the intersection loci of two oblique cylinders alternatively may be formed according to the intersection of one cylinder by a plane perpendicular to its axis. This would generate roughly triangular shaped gaps between each curved plate and the inner duct wall in the region of the pivotal axis. For the purpose of flow diversion when the valve (26) is raised apertures (32 and 34) are formed in the outer duct wall (30) on opposite, that is upstream and downstream, sides of the valve. Aperture closure means in the form of sliding doors (36 and 38) operated by actuating means (72 and 74) to open and close the doors is synchronised with operation of valve actuation means (54). Alternative aperture closure means such as shutters or hinged flaps may be provided for selectively opening and closing the apertures. Operation of the aperture closing means in combination with the diverter valve will be readily appreciated by comparison of figures 1 and 2 which show the valve raised and lowered respectively. When the diverter valve (26) is lowered as in figure 2 the aperture doors are arranged to be closed and fluid flows virtually unimpeded along the duct (14). In this position the side lobes (40 and 42) of the valve are arranged to be aligned with the flow direction so as to present minimum disturbance. In figure 1, however, the valve (26) is raised and constitutes an effective block to airflow along the duct (14) from the front fan towards the second fan. The aperture doors are arranged to be open and air passed into the duct by the front fan (12) is able to exit the duct (14) through the aperture (32) upstream of the valve (26). The aperture (34) downstream of the valve is also open allowing ambient air to be drawn into the duct by the second fan (16). The apertures (32 and 34) thus constitute auxiliary outlets and inlets respectively.

Claims: A diverter valve for use in an annular flow duct defined by inner and outer concentric duct walls (28,30) has a valve means (26) pivotable between a first blocking position in which the margins of the valve means seal against the inner and outer duct walls (28,30) to stem flow along the duct and a second position in which the valve means (26) causes minimum obstruction to flow in the duct characterised in that: the valve means (26) comprises four integrally joined sections (40, 42, 50, 52) which surround the inner duct wall (28), these four sections comprise a pair of flat side lobes (40,42) on opposite sides of the inner duct wall (28) and a pair of semi-cylindrical transverse portions (50,52) spaced apart towards opposite ends of the side lobes (40, 42) and curving in opposite directions with radii conforming substantially to the curvature of the inner duct wall (28). A diverter valve as claimed in claim 1 further characterised in that: the transverse portions of the valve means (26) are curved to lie flush with the inner wall (28) of the duct when the valve occupies the second position. A diverter valve as claimed in claim 2 wherein the flat side lobes (40, 42) are pivotable about a transverse axis (44) which bisects the lobes and in the second valve position the lobes (40, 42) lie parallel to the axis of the duct. A diverter valve as claimed in any preceding claim wherein the transverse portions (50, 52) and the side lobes (40, 42) are joined to move in unison about a common pivotal axis (44). A diverter valve as claimed in any preceding claims furthers characterised in that: at least two apertures (32, 34) are formed in the outer wall (30) of the duct and positioned relative to the valve means (26) so that when the valve occupies the first position the apertures lie on opposite sides of the valves means. A diverter valve as claimed in claim 5 wherein further means (36, 38) are provided for closing said apertures (32, 34). A diverter valve as claimed in claim 6 further characterised in that the means (36,38) for closing said apertures (32, 34)is operated in synchronism with means (54) for pivoting the valve means (26) such that when the valve means (26) occupies the first position the apertures (32, 34) are closed and when the valve means occupies the second position the apertures (32, 34) are open. A diverter valve as claimed in any one of the preceding claims characterised in that the valve (26) is positioned between first and second compressors (12,16) of a gas turbine engine (10) and the flow duct (14) receives fluid from the first compressor (12) and delivers fluid to the second compressor (16). A diverter valve as claimed in claim 8 in combination with any one of claims 5 to 7 in which a first of the apertures (32) comprises an auxiliary air inlet positioned to admit air to the second compressor (16) when the valve is in the said first position and a second of the apertures (34) comprises an auxiliary outlet to exhaust fluid from the first compressor (12).

Inventors: TONKS, ROBERT CHARLES
Applicants: ROLLS-ROYCE PLC
Application year: 1990
Main classification: F02K3
IPC codes: F16K1, F02K3, F01D17, F02C9