Fluidfoil

Abstract

A fluidfoil includes a selectively fluid chargeable capillary and a flexible body adjacent the capillary, the shape of the flexible body being adjustable in use via controlling the degree to which the capillary is charged and therefore the forces that the capillary exerts on the flexible body.

Claims

1. A fluidfoil comprising: a selectively fluid chargeable capillary; and a flexible body including a core sandwiched between a suction side wall and a pressure side wall of the fluidfoil, the capillary being contained within the core, wherein the shape of the flexible body is adjustable in use via controlling the degree to which the capillary is charged and therefore the forces that the capillary exerts on the flexible body.

2. The fluidfoil according to claim 1, wherein the flexible body is elastic.

3. The fluidfoil according to claim 1, wherein the fluidfoil includes a plurality of the capillaries.

4. The fluidfoil according to claim 3, wherein some or all of the capillaries are arranged in an array of substantially parallel capillaries.

5. The fluidfoil according claim 1, wherein the flow of fluid to and/or from the capillary is valve controlled.

6. The fluidfoil according to claim 1, wherein the fluidfoil is an aerofoil.

7. A variable fluidfoil system comprising: a pump; and the fluidfoil in accordance with claim 1, wherein the pump is arranged to selectively deliver fluid to charge the capillary.

8. The variable fluidfoil system according to claim 7, wherein the system further comprises a reservoir for storing fluid to be pumped by the pump.

9. A fluidfoil comprising: a plurality of selectively fluid chargeable capillaries, the plurality of capillaries being arranged in an array and extending substantially parallel to one another in a substantially chordwise direction; and a flexible body adjacent the plurality of capillaries, the shape of the flexible body being adjustable in use via controlling the degree to which the plurality of capillaries are charged and therefore the forces that the plurality of capillaries exert on the flexible body.

10. The fluidfoil according to claim 9, wherein the flexible body comprises a suction side wall of the fluidfoil.

11. The fluidfoil according to claim 10, wherein the flexible body comprises a pressure side wall of the fluidfoil.

12. The fluidfoil according to claim 11, wherein the flexible body comprises a core of the fluidfoil sandwiched between the suction and pressure side walls.

13. The fluidfoil according to claim 12, wherein the plurality of capillaries are contained within the core.

14. The fluidfoil according to claim 9, wherein a pressure side wall has a higher stiffness than a suction side wall.

15. The fluidfoil according to claim 14, wherein the capillaries of the array are provided adjacent the suction side wall.

16. The fluidfoil according claim 9, wherein the flow of fluid to and/or from the plurality of capillaries is valve controlled.

17. A variable fluidfoil system comprising: a pump; and the fluidfoil in accordance with claim 9, wherein the pump is arranged to selectively deliver fluid to charge the capillaries.

18. The variable fluidfoil system according to claim 17, wherein the system further comprises a reservoir for storing fluid to be pumped by the pump.

19. A fluidfoil comprising: a selectively fluid chargeable capillary; and a flexible body adjacent the capillary, the flexible body including a core sandwiched between a suction side wall and a pressure side wall of the fluidfoil, the pressure side wall having a higher stiffness than the suction side wall, wherein the shape of the flexible body is adjustable in use via controlling the degree to which the capillary is charged and therefore the forces that the capillary exerts on the flexible body.

20. The fluidfoil according to claim 19, wherein the capillary is provided adjacent the suction side wall.

Description

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

(2) FIG. 1 is a sectional side view of a gas turbine engine;

(3) FIG. 2 is a plan view of a fluidfoil in accordance with an embodiment of the invention;

(4) FIG. 3a is a cross-sectional view of the fluidfoil of FIG. 2 taken along the line A-A and shown in a fully discharged condition;

(5) FIG. 3b is a cross-sectional view of the fluidfoil of FIG. 2 taken along the line A-A and shown in a fully charged condition;

(6) FIG. 4 is a schematic of a variable fluidfoil system in accordance with an embodiment of the invention.

(7) With reference to FIG. 1, a gas turbine engine is generally indicated at 10, having a principal and rotational axis 11. The engine 10 comprises, in axial flow series, an air intake 12, a propulsive fan 13, an intermediate pressure compressor 14, a high-pressure compressor 15, combustion equipment 16, a high-pressure turbine 17, and intermediate pressure turbine 18, a low-pressure turbine 19 and an exhaust nozzle 20. A nacelle 21 generally surrounds the engine 10 and defines both the intake 12 and the exhaust nozzle 20.

(8) The gas turbine engine 10 works in the conventional manner so that air entering the intake 12 is accelerated by the fan 13 to produce two air flows: a first air flow into the intermediate pressure compressor 14 and a second air flow which passes through a bypass duct 22 to provide propulsive thrust. The intermediate pressure compressor 14 compresses the air flow directed into it before delivering that air to the high pressure compressor 15 where further compression takes place.

(9) The compressed air exhausted from the high-pressure compressor 15 is directed into the combustion equipment 16 where it is mixed with fuel and the mixture combusted. The resultant hot combustion products then expand through, and thereby drive the high, intermediate and low-pressure turbines 17, 18, 19 before being exhausted through the nozzle 20 to provide additional propulsive thrust. The high 17, intermediate 18 and low 19 pressure turbines drive respectively the high pressure compressor 15, intermediate pressure compressor 14 and fan 13, each by suitable interconnecting shaft.

(10) Referring now to FIGS. 2, 3a and 3b a fluidfoil (in this case an aerofoil) that might be used as a blade or stator vane in the gas turbine engine 10 is generally shown at 30. The fluidfoil 30 has a leading edge 32, a trailing edge 34, a tip 36, a base 38, a pressure side wall 40 and a suction side wall 42.

(11) Passing through the thickness of the fluidfoil 30, there is provided the pressure side wall 40, a core 44 and the suction side wall 42. The core 44 is therefore sandwiched between the side walls 40, 42. Together the side walls 40, 42 and core form a flexible body 46. The core 44 is fabricated from a flexible and elastic elastomer. Each side wall 40, 42 is fabricated from a metallic layer of a composition and thickness selected to give the wall flexibility. In addition, the suction side wall 40 is provided with a region of increased compliance 48 in the form of tooth shaped, spanwise channel cut into its surface. The channel locally reduces the thickness of the suction side wall 42, reducing its stiffness in that region. The pressure side wall 40 as a whole is consequently stiffer than the suction side wall 42 as a whole.

(12) Within the core 44 is an array 50 of substantially parallel capillaries 52. Each capillary 52 is surrounded by core 44 material, each capillary 52 comprising a conduit or void through the core 44. Each capillary 52 runs substantially adjacent the suction side wall 42, in a chordwise direction, substantially from the leading edge 32 to the trailing edge 34. The array as a whole extends substantially from the base 38 to the tip 36 of the fluidfoil 30.

(13) At their ends nearest the leading edge 32, each capillary 52 has an inlet in fluid communication with a common manifold 54. At its end nearest the base 38 the to manifold has an inlet in fluid communication with an artery 56.

(14) Referring now to FIG. 4 a variable fluidfoil system is generally shown at 60. The variable fluidfoil system includes a plurality of fluidfoils 30 as previously described. The manifold 54 of each fluidfoil 30 is fluidly connected to a fluid reservoir 62 by the artery 56, A pump 64 is provided in the artery 56. The speed of the pump 64 is controlled by an engine electronic controller 66.

(15) In use, and with reference to FIGS. 3a, 3b and 4, the chordwise curvature of each of the fluidfoils 30 is selectively adjustable by altering the fluid charge (e.g. fluid pressure) in each of the capillary arrays 50.

(16) Where it is desired to increase the chordwise curvature of the fluidfoils the pump 64 is controlled by the engine electronic controller 66 to increase the fluid pressure within the capillaries 52 using fluid from the reservoir 62. With respect to each fluidfoil 30, as the fluid pressure increases the forces generated by the charged capillaries 52 are sufficient to overcome the elastic forces of the core 44 and limited stiffness of the side walls 40, 42. Because the suction side wall 42 is not as stiff as the pressure side wall 40, it is forced to elongate around the stiffer pressure side wall 40. As this elongation occurs the curvature of the fluidfoil 30 in the chordwise direction increases. FIG. 3b shows the fluidfoil 30 in a fully charged configuration, with a relatively high fluid pressure in the capillaries 52. Consequently the radius of curvature of the fluidfoil 30 in the chordwise direction is relatively small. As can be seen a particular decrease in the radius of curvature occurs at the region of increased compliance 48. Specifically side walls 68 of the channel move apart as increased bending occurs.

(17) Where it is desired to decrease the chordwise curvature of the fluidfoils, one or more discharge valves (not shown) are opened by the engine electronic controller 66, allowing fluid to return to the reservoir 62 via one or more return conduits (not shown). The pump 64 may also be controlled accordingly (e.g. stopped). The opening of the discharge valves reduces the fluid pressure in the capillaries 52 and thereby the forces they exert on their respective flexible bodies 46. With respect to each fluidfoil 30, restorative forces exerted by the elastic core 44 and side walls 68 reduce the fluidfoil 30 curvature in the chordwise direction. If the reduction of pressure in the capillaries 52 is sufficient, the fluidfoil 30 will return to a nominal shape. FIG. 3a shows the fluidfoil 30 in a fully discharged configuration, with a low fluid pressure in the capillaries 52. Consequently the radius of curvature of the fluidfoil 30 in the chordwise direction is relatively large.

(18) As will be appreciated, suitable control of the pump 64 and/or discharge valves will allow selection and maintenance of multiple different radii of curvature in the chordwise direction between and including the curvatures obtained at fully charged (FIG. 3b) and fully discharged (FIG. 3a). Further a feedback monitoring system (not shown) is also provided to monitor the actual shape of the fluidfoil 30. Where the actual shape of the fluidfoil 30 differs from that instructed, the feedback monitoring system allows the engine electronic controller 66 to make one or more compensating adjustments.

(19) 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 various concepts described herein. By way of example it will be appreciated that the above mentioned embodiment alters the shape of the fluidfoil 30 in only the chordwise direction. In other embodiments however alternative shape changes may be controllable and indeed independent control of multiple different shape components may be possible. By way of example, in some embodiments, any one or more of the following may be changed: fluidfoil curvature in one or more selected directions, fluidfoil twist, fluidfoil sweep and fluidfoil lean. Except where mutually exclusive, any of the features may be employed separately or in combination with any other features and the invention extends to and includes all combinations and sub-combinations of one or more features described herein in any form of fluidfoil.