DOUBLE SKINNED PIPE ASSEMBLY

Abstract

A double skinned feed or scavenge pipe assembly comprises; an inner pipe (22) and an outer pipe (23) enclosing the inner pipe and defining an annular space (24) between the inner pipe and the outer pipe and a sleeve (28) configured to slip over the outer pipe (23). Complementary threads (29) are provided on an outer wall of the outer pipe (23) and an inner wall of the sleeve (28). A lock, for example in the form of a locking nut (31) is positioned over the outer pipe (23) when the complementary threads (29) of the outer pipe and sleeve are engaged. The configuration of the assembly is such that, in use, the sleeve (28) is slidable between a first position where the inner pipe (22) is accessible and a second position wherein the inner pipe (22) is completely enclosed.

Claims

1. A double skinned pipe assembly comprising; an inner pipe and an outer pipe enclosing the inner pipe and defining an annular space between the inner pipe and the outer pipe; a sleeve configured to slip over the outer pipe; complementary threads on an outer wall of the outer pipe and an inner wall of the sleeve; and a lock for locking the sleeve in position over the outer pipe when the complementary threads of the outer pipe and sleeve are engaged, wherein the configuration of the assembly is such that, in use, the sleeve is movable between a first position where the inner pipe may be accessed and a second position wherein the inner pipe is completely enclosed.

2. A double skinned pipe assembly as claimed in claim 1 wherein the lock comprises a locking nut which includes a thread which is complementary to the thread on the outer pipe and is arranged to be threaded onto the outer pipe after the sleeve has been threaded onto the outer pipe.

3. A double skinned pipe assembly as claimed in claim 2 wherein the lock further includes a tab washer arranged between the locking nut and the sleeve and receivable in a tab washer groove provided in a mid-portion of the thread, wherein once the sleeve and locking nut are arranged for locking, the tabs of the washer can be bent and engage with the nut and/or sleeve to restrict axial and/or rotational movement thereof.

4. A double skinned pipe assembly as claimed in claim 1 wherein the lock comprises a clamp engageable around the outer pipe or around the outer pipe and the sleeve.

5. A double skinned pipe assembly as claimed in claim 1 wherein the lock is incorporated into the sleeve and/or the outer pipe.

6. A double skinned pipe assembly as claimed in claim 5 wherein the lock comprises a ratchet incorporated into the sleeve, the ratchet configured to restrict rewinding of the sleeve on the thread once the sleeve is secured in the second position.

7. A double skinned pipe assembly as claimed in claim 5 wherein the lock comprises an anti-rotation feature on the outer pipe configured to engage with the sleeve when the sleeve is in the second position.

8. A double skinned pipe assembly as claimed in claim 1 wherein the outer pipe includes a stop against which the sleeve abuts when the sleeve is in the second position.

9. A double skinned pipe assembly as claimed in claim 8 wherein the stop comprises a flange.

10. A double skinned pipe assembly as claimed in claim 8 wherein the stop comprise a plurality of substantially equally spaced radially outward protrusions arranged on the outer pipe against which the sleeve may abut when the sleeve is in the second position.

11. A double skinned pipe assembly as claimed in claim 1 wherein the inner pipe is joined to a body into/out of which the inner pipe feeds or scavenges.

12. A double skinned pipe assembly as claimed in claim 11 wherein the inner pipe is welded to the body.

13. A double skinned pipe assembly as claimed in claim 11 wherein the body comprises a hub of a bearing chamber in a gas turbine engine.

14. A gas turbine engine incorporating a double skinned pipe assembly as claimed in claim 1 wherein the inner pipe is joined to and arranged to feed into or scavenge out of a hub of a bearing chamber.

Description

BRIEF DESCRIPTION OF THE FIGURES

[0015] An embodiment of the invention may be further described with reference to the accompanying Figures in which;

[0016] FIG. 1 shows a section through a gas turbine engine as is known from the prior art and into which a double skinned pipe assembly of the invention might be incorporated;

[0017] FIG. 2 shows an embodiment of a double skinned pipe assembly in accordance with the invention where the inner pipe is accessible;

[0018] FIG. 3 shows the embodiment of FIG. 2 where the inner pipe is fully enclosed.

DETAILED DESCRIPTION OF FIGURES AND EMBODIMENTS

[0019] 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, a high-pressure compressor 14, combustion equipment 15, a high-pressure turbine 16, a low-pressure turbine 17 and an exhaust nozzle 18. A nacelle 20 generally surrounds the engine 10 and defines the intake 12.

[0020] 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 high-pressure compressor 14 and a second air flow which passes through a bypass duct 21 to provide propulsive thrust. The high-pressure compressor 14 compresses the air flow directed into it before delivering that air to the combustion equipment 15.

[0021] In the combustion equipment 15 the air flow is mixed with fuel and the mixture combusted. The resultant hot combustion products then expand through, and thereby drive the high and low-pressure turbines 16, 17 before being exhausted through the nozzle 18 to provide additional propulsive thrust. The high 16 and low 17 pressure turbines drive respectively the high pressure compressor 14 and the fan 13, each by suitable interconnecting shaft.

[0022] Other gas turbine engines to which the present disclosure may be applied may have alternative configurations. By way of example such engines may have an alternative number of interconnecting shafts (e.g. three) and/or an alternative number of compressors and/or turbines. Further the engine may comprise a gearbox provided in the drive train from a turbine to a compressor and/or fan.

[0023] It will be understood that with many moving parts within the engine, it is necessary to maintain a reservoir of oil and provide a network of supply pipes to components in need of lubrication. For example, these pipes may extend radially across the engine between rotating parts to feed bearings in the engine core about which the rotating parts are mounted. For example, the pipe may pass between stages 16, 17 of the turbine 10 and into a bearing structure within which the shaft which drives the turbines is mounted.

[0024] FIGS. 2 and 3 show an assembly in accordance with the invention. In FIG. 2, the assembly is configured to allow access to the inner pipe 22 of the double walled pipe, in FIG. 3 the assembly is configured completely to enclose the inner pipe 22. As can be seen, the double walled pipe comprises an inner pipe 22 and an outer pipe 23 defining an annular space 24 therebetween. The inner wall 22 is joined to a body 26 by a weld 25 and is arranged to deliver a first fluid into the body 26. For example, the body might be a bearing a hub of a bearing structure and the first fluid may be a lubricant for the bearing components.

[0025] The outer pipe 23 terminates short of the welded joint 25 leaving a space 27 sufficient to allow access to the welded joint 25 and the annular space 24.

[0026] A sleeve 28 sits around the outer pipe 23 and has an inner thread which engages with a complementary thread 29 arranged on an outer circumferential surface of the outer pipe 23. It will appreciated that the sleeve 28 can be moved axial with respect to a common central axis of the inner pipe 22 and outer pipe 23 by turning the sleeve 28 about this axis with the complementary threads engaged. As can be seen from FIG. 3, the complementary threads are arranged such that, when fully threaded, the sleeve closes the access space 27, meets the body 28 and encloses the welded joint 25.

[0027] A locking nut 30 also sits around the outer pipe 23 and also has an inner thread which engages with a complementary thread 29 arranged on an outer circumferential surface of the outer pipe 23. Finally a tab washer 31 sits around the outer pipe 23 between the sleeve 28 and locking nut 30. As can be seen in FIG. 3, the tab washer 31 can engage in a circumferential groove 32 which sits in a mid-portion of the thread 29. The outer pipe 23 is provided with a flange 33 against which the sleeve 28 can abut.

[0028] One or both of the threaded adjustable sleeve 28 and threaded locking nut 30 may be provided with flats for a spanner on their outside. After the inner pipe 22 is fixed to the body 26 the adjustable sleeve 28 may be wound along the thread 29 until a desired gap 27 is achieved between the sleeve 28 and the body 26. This gap 27 may be controlled by a slip gauge for example. By reversing the direction of winding along the threads 29, the gap 27 can be closed (see FIG. 3). To lock the sleeve 28 in this position the locking nut 30 is wound tight to the sleeve, restricting its ability to reverse wind. The sleeve 28 and lock nut 30 may be torqued up against each other, for example by using a spanner and the flats. The tab washer 31 can be used to lock the positions of the sleeve 28 and not 30. After torqueing the sleeve 28 and locking nut 30, tabs of the tab washer 31 may be bent up and down to restrict axial and/or rotational movement of the sleeve 28 and nut 30.

[0029] Alternative locking arrangements for locking the sleeve 28 in the “gap-closed” position will no doubt occur to the skilled addressee, the described locking arrangement configuration is not considered essential to the invention.

[0030] 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.