BACKGROUND
This disclosure relates to a compressor diffuser for use in an auxiliary power unit, for example. In particular, the disclosure relates to the interface between vanes of the diffuser and an adjacent shroud housing.
A typical auxiliary power unit utilizes a turbine section that receives compressed air from a compressor section to rotationally drive a component. In some auxiliary power units, a diffuser is arranged between the compressor section and the turbine section. In one type of diffuser, fixed radial vanes are arranged in a passage between a compressor exit and a turbine inlet. A shroud housing is bolted to the diffuser to seal the radial vanes against the shroud housing provide an air-tight passage.
SUMMARY
An auxiliary power unit is disclosed that includes a compressor section having a compressor inlet and a compressor exit. A turbine section is arranged downstream from the compressor exit. A diffuser is disposed in fluid communication with and between the compressor section and the turbine section. The diffuser has multiple generally radially extending circumferentially arranged vanes. A shroud housing is secured against the vanes. A damper is arranged between at least one vane and the shroud housing and configured to damp vibration of the at least one vane relative to the shroud housing during operation of the auxiliary power unit.
BRIEF DESCRIPTION OF THE DRAWINGS
The disclosure can be further understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
FIG. 1 is a partial cross-sectional view of an example auxiliary power unit.
FIG. 2 is an enlarged view of an area indicated in FIG. 1.
FIG. 3A is a broken partial cross-sectional view of a vane and a shroud housing.
FIG. 3B is a broken partial perspective view of the shroud housing.
FIG. 3C is a broken partial perspective view of the vane on a diffuser.
FIG. 4 is a side elevational view of a portion of the diffuser and vane in engagement with the shroud housing.
FIG. 5 is a partial cross-sectional view of a portion of the shroud housing with a diffuser vane damper.
DETAILED DESCRIPTION
An auxiliary power unit (APU) 10 is illustrated in FIG. 1. The APU 10 includes a compressor section 12 that receives fluid from a fluid source 16 through a compressor inlet 14. A diffuser 18 is arranged downstream from a compressor exit 17 of the compressor section 12. The diffuser 18 is used to regulate the output pressure from the compressor section 12 through a diffuser outlet 20.
A turbine section 22 receives the compressed, diffused fluid from the diffuser outlet 20 at a turbine inlet 24. A combustor (not shown) is provided between the diffuser outlet 20 and the turbine inlet 24 to provide a further heated fluid to the turbine section 22. Combusted, compressed fluid expands over the turbine section 22 rotationally driving an output shaft 28, about an axis A, that is operatively connected to the turbine section 22 and expelling the expanded fluid through a turbine outlet 26. The output shaft 28 rotationally drives a driven component 30.
The diffuser 18 is a fixed vane-type diffuser and is generally bowl-shaped. In the example, a plurality of circumferentially spaced radially extending vanes 32 (FIG. 3C) are integral with an annular base 34 of the diffuser 18. The vanes 32 include opposing sides 38 extending between leading and trailing ends 40, 42. Axially arranged vanes 36 are circumferentially spaced about an outer diameter 37 of the diffuser 18 and integrally formed with the base 34 in the example. By “integral” it is meant that the vanes 32, 36 cannot be removed by non-destructive means. In one example, the vanes 32, 36 are machined from base 34 and outer diameter 37, respectively, which may be provided by a forged or cast blank of titanium, Inconel or stainless steel, for example.
Referring to FIG. 2, a shroud housing 44 is secured over the vanes 32 of the diffuser 18 to define the fluid passage from the exit 17 through the diffuser 18 to the turbine outlet 26. In the example, trailing ends 42 of the vanes 32 (FIGS. 3A and 3C) include holes 46 through which fasteners 48 are disposed to clamp the diffuser 18 to the shroud housing 44, which includes corresponding holes 49 (FIG. 3B). The fasteners 48 may be provided by a threaded fastener arrangement, as shown in FIGS. 1 and 2, or using non-threaded elements. It is desirable to seal and fully engage the vanes 32 to the shroud housing 44. There are thirty-five radial vanes 32 in one example diffuser 18, and it is difficult to securely clamp the shroud housing 44 over the vanes 32 such that the shroud surface 52 faces and uniformly engages each vane surface 50. As a result, the shroud housing 44 and vanes 32 may vibrate against one another resulting in portions of the vane 32, such as the leading end 40, to crack.
Referring to FIGS. 3A, 4 and 5, a damper 56 is provided between and aligned with the shroud housing 44 and the vane 32. In one example, a recess 54, which may be cylindrical in shape, is provided in the shroud housing 44 in an uncompressed condition. The damper 56, which may be a flexible polymeric material, such as silicone, is provided in the recess 54 such that an end 58 of the damper 56 is proud of the shroud surface 52. By “flexible” it is meant a material having a durometer of about 85-95 shore A. It should be understood that other flexible, heat-resistant damping materials may be used. The damper 56 is in a compressed condition with the shroud housing 44 secured to the diffuser 18 with the fasteners 48 in an assembled state. Thus, the leading ends 40 are prevented from vibrating against the shroud housing 44. An adhesive 60, such as glue, may be provided between the damper 56 opposite the end 58 and a bottom 62 of the recess 54 to retain the damper 56, which is in the uncompressed condition, securely within the recess 54 when in an unassembled state before and during assembly, as shown in FIG. 5.
Although an example embodiment has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of the claims. For that reason, the following claims should be studied to determine their true scope and content.
Patent Application
20110302912
