Patent Grant
7527476
The invention relates to a rotor assembly for a gas turbine engine compressor, and particularly to a rotor assembly for a low pressure compressor or fan of a gas turbine engine. The invention also relates to an annulus filler for a gas turbine engine compressor rotor assembly.
A compressor for a gas turbine engine includes at least one rotor assembly including a rotor disc having an array of rotor blades mounted thereon. The rotor blades extend radially outwardly from the disc and may be rotated to draw air through the rotor assembly, the air passing through an annular area (the “rotor air annulus”) defined between the rotor disc and an outer casing surrounding the tips of the rotor blades.
It is important that the rotor air annulus has a smooth radially inner surface for air to flow over as it passes through the rotor assembly. One way of ensuring this is to produce rotor blades with integral platforms, the platforms forming an inner wall of the rotor air annulus in use. The blade and platform are manufactured as a single unit from a common material. An alternative practice is to use “annulus fillers”. The annulus fillers are located between adjacent rotor blades and include a smooth radially outer surface which constitutes or forms part of the inner wall of the rotor air annulus in use. Annulus fillers may be manufactured from relatively lightweight materials and, in the event of damage, may be replaced independently of the rotor blades.
It is known to provide annulus fillers with features for removably attaching them to the rotor disc. An annulus filler may be provided with a hook member at its axially rear end, the hook member sliding into engagement with part of the rotor disc and/or a component located axially behind the rotor assembly, for example a rear fan air seal. Typically, each annulus filler is slid axially backwards to cause the hook member to engage, and then retained in place by a front attachment disc which is fastened over the fronts of all the annulus fillers located around the rotor disc. The front attachment disc may be bolted into place and this may also hold the nose cone in place at a front of the engine.
It is often necessary to remove fan blades and annulus fillers to check for cracks in the blades or to replace damaged components. In the prior art design, in order to remove an annulus filler, it is necessary to remove the nose cone and the front attachment disc before the annulus filler can be removed. This is relatively complex and time consuming.
According to the invention there is provided a rotor assembly for a gas turbine engine compressor, the rotor assembly including:
The annulus filler may include an axially forward end and an axially rear end, its airflow surface extending substantially between the forward and the rear end.
The securing arrangement may include a first retaining means provided at the forward end of the annulus filler, and a second retaining means provided at the rear end of the annulus filler.
The first retaining means may include a hook member provided on the forward end of the annulus filler, and a recess provided in the rotor disc, the hook member being shaped to engage the recess. The hook member may extend from the remainder of the annulus filler in a forward and radially outward direction.
The second retaining means may also include a hook member, provided on the rear end of the annulus filler, for engaging a complementary formation provided in the rotor disc or in an adjacent part. The hook member may be biased into a position where it is in engagement with the formation.
The annulus filler may include a resilient portion which provides the bias for the securing arrangement. The resilient portion may comprise a springy piece of material which forms part of the annulus filler. The annulus filler may be shaped such that when the springy piece of material is compressed, the hook member of the second retaining means may be brought out of engagement with its complementary formation.
The rotor disc and the annulus filler may be profiled such that together their radially outer surfaces form a smooth airflow surface for air being drawn through the rotor assembly. The rotor disc may form an axially forward part of that airflow surface and the annulus filler an axially rearward part.
The annulus filler may include an outer wall which forms part of the airflow surface and an inner wall which locates adjacent the disc. The area between the outer and inner wall may be substantially hollow but may include a triangulated structure for additional strength.
The resilient portion of the annulus filler may comprise a leg extending from the inner wall of the annulus filler. The leg may be oriented at an acute angle to the inner wall. The resilience of the leg may allow it to be pushed towards the inner wall, thus reducing this angle.
The annulus filler may comprise an extrusion. The annulus filler may be made of aluminium.
In one embodiment of the invention, the second retaining means includes a hook member provided at a radially outer part of the rear of the annulus filler, for engagement with a recess in a fan rear air seal. The hook member and recess may be so shaped that inwards movement of the hook member allows it to be brought out of engagement with the recess, preferably by manually bringing it forwards. The hook member may be located on an arm which forms part of the annulus filler, the resilience of the material of the annulus filler allowing some flexing of the arm. The arm may flex about its proximal end, this being located in a radially inner region of the annulus filler.
In this embodiment, the resilient portion of the annulus filler may comprise a springy leg extending from the inner wall of the annulus filler, the leg biasing the annulus filler radially outwardly. Radially inwards movement of the annulus filler against the bias of the leg may thereby allow the hook member to be disengaged from the recess. The outer wall of the annulus filler may include an opening adjacent to the hook member of the second retaining means, to allow space for the hook member to move forwards.
The annulus filler may be shaped such that once the second retaining means has been released, the annulus filler may be pivoted about the first retaining means, allowing the hook member of the first retaining means to be released from its associated recess.
In an alternative embodiment, the second retaining means includes a hook member provided at a radially inner part of the rear of the annulus filler, the hook member engaging a complementary formation on the rotor disc. The hook member and the formation may be shaped such that radially inwards movement of the hook member allows it to be brought out of engagement with the formation, preferably by moving the hook member rearwards. The hook member may be located on an arm formed as part of the annulus filler, the resilience of the material of the annulus filler allowing some flexing of the arm. The arm may flex about its proximal end, this being located in a radially mid region of the annulus filler.
In this embodiment, the resilient portion of the annulus filler may again comprise a springy leg extending from the inner wall of the annulus filler, the leg biasing the annulus filler radially outwards.
According to the invention there is provided an annulus filler for securing to a rotor disc of a rotor assembly according to any preceding, embodiment, the annulus filler in use providing a radially inner airflow surface for air being drawn through the rotor assembly of the gas turbine engine, the annulus filler including retaining means forming part of the securing arrangement for securing the annulus filler to the rotor disc and the annulus filler being configured such that it is biased into a condition in which the securing arrangement mechanically retains the annulus filler on the disc but is movable against the bias to allow the annulus filler to be removed from the disc.
The annulus filler may include any of the additional features defined in the preceding paragraphs.
An embodiment of the invention will be described for the purpose of illustration only with reference to the accompanying drawings in which:—
Referring to
Referring to
The blades are spaced apart on the rotor disc 18, and a leading part of the space between each two adjacent blades is bridged by a portion 24 of the rotor disc 18. By “leading” it is meant the part of the rotor assembly through which air passes first. A rear part of the space between each two adjacent blades is bridged by an annulus filler 26. The annulus filler 26 thus occupies only part of the space between the blades, but in some cases could also occupy the forward region 24. The term “annulus filler” as used herein is intended to cover both complete and partial or “mini” fillers (i.e. annulus fillers which occupy the whole or part of the space between the blades).
The leading portion 24 of the disc 18, together with the annulus filler 26, form a smooth inner surface of the rotor air annulus, as described in more detail below.
The annulus filler 26 includes an axially forward end 28, an axially rear end 30 and an airflow surface 32 which extends substantially between the forward and the rear end.
The annulus filler includes an outer wall 27 which provides the smooth airflow surface and an inner wall 29 which locates adjacent to the disc 18. An area 31 between the inner wall and the outer wall may be substantially hollow or may be triangulated for additional strength.
The annulus filler 26 is secured to the rotor disc 18 by means of a securing arrangement. The annulus filler is configured such that it is biased into a condition in which the securing arrangement mechanically retains the annulus filler on the disc. However, the annulus filler may be moved against its bias to allow the annulus filler to be removed from the disc 18.
The securing arrangement includes a first retaining means 34 provided at the forward end 28 of the annulus filler 26. The first retaining means includes a hook member 36 which extends smoothly forwards and slightly radially outwards from the forward end 28 of the annulus filler 26.
The hook member 36 may fit into a complementary recess 38 formed in the rotor disc 18. It may be seen that the hook member 36 may be brought into full engagement with the recess 38 by a combination of forwards and rotational movement of the annulus filler relative to the rotor disc 18.
The securing arrangement further includes a second retaining means 40 provided at the rear end 30 of the annulus filler 26. The second retaining means also includes a hook member 42 which is able to fit into a complementary formation 44 in a rear fan air seal 46. The rear fan air seal 46 locates just behind the rotor disc 18 and separates higher pressure air in a region 48 from the fan region. The rear fan air seal 46 is typically made of titanium. The hook member 42 and the complementary formation 44 are shaped such that radially inwards movement of the hook member 42 allows the hook member to be released from the formation 44 by manually bringing it an axially forward direction. A tab 50 attached to the hook member 42 is provided to allow for this manual manipulation.
The hook member 42 is biased into a radially outwards position in which it is retained in engagement with the formation 44. The biasing is provided by a resilient portion of the annulus filler in the form of a springy leg 52. The springy leg 52 extends from the inner wall 29 of the annulus filler.
The springy leg 52 biases the rear end 30 of the annulus filler 26 radially outwardly, thus retaining the hook member 42 in engagement with the formation 44.
The hook member 44 is located on a distal end of an arm 62 which is only attached to the remainder of the annulus filler 26 at a pivot point 64. There is a space 63 between the distal end of the arm 62 and an adjacent part 65 of the outer wall 27.
To disengage the second retaining means, the rear end 30 of the annulus filler 26 may be pushed radially inwardly against the bias of the springy leg 52. With the rear end 30 in this slightly radially inner position, the tab 50 may be manipulated to bring the hook member 42 forwards into the space 63, pivoting the arm 62 about the pivot point 64. This allows the hook member 42 to be brought out of engagement with the formation 44.
The space 63 may be partially sealed against the annulus air in a similar manner to that shown in
The whole annulus filler may then be rotated slightly in an anti-clockwise direction as viewed in
Referring to
The annulus filler 26 of the
Again, the resilient portion of the annulus filler comprises a springy leg 52 which extends away from the inner wall of the annulus filler at an acute angle.
In this embodiment, to release the annulus filler 26 from the rotor disc 18, the rear end 30 of the annulus filler may again be pushed radially inwardly against the resilience of the springy leg 52. This allows the arm 62 to be pivoted in an anti-clockwise direction as viewed in
The annulus filler may be an extrusion. It may be manufactured by extruding lengthwise, and then cut up into appropriate lengths which are subsequently bent to accommodate the curved shape of the rotor disc 18. The extrusion may be aluminium.
As an alternative, it may be possible to use injection moulded plastics materials, as this area of the engine does not get very hot and no significant strength is required.
The annulus fillers according to the preferred embodiments of the invention are very easy to remove. Whereas in the prior art it was necessary to remove the nose cone and the front attachment disc in order to remove the annulus fillers, in the preferred embodiments of the invention, the annulus fillers may simply be snapped into and out of place as described above. The annulus fillers are therefore much quicker to remove. Further, the annulus fillers should be cheaper to manufacture than in the prior art.
Whilst endeavouring in the foregoing specification to draw attention to those features of the invention believed to be of particular importance it should be understood that the Applicant claims protection in respect of any patentable feature or combination of features hereinbefore referred to and/or shown in the drawings whether or not particular emphasis has been placed thereon.
| Number | Date | Country | Kind |
|---|---|---|---|
| 0411966.5 | May 2004 | GB | national |
| Number | Name | Date | Kind |
|---|---|---|---|
| 2873088 | Neumann | Feb 1959 | A |
| 3703341 | Garofalo | Nov 1972 | A |
| 3822963 | Goldberg | Jul 1974 | A |
| 4863354 | Asselin et al. | Sep 1989 | A |
| Number | Date | Country |
|---|---|---|
| 586041 | Mar 1947 | GB |
| 2 364 748 | Feb 2002 | GB |
| Number | Date | Country | |
|---|---|---|---|
| 20050265847 A1 | Dec 2005 | US |
