Oil baffle for gas turbine fan drive gear system

Abstract

A geared architecture includes a carrier that has spaced apart walls with circumferentially spaced mounts that interconnect the walls. The mounts provide circumferentially spaced apart apertures between the mounts at an outer circumference of the carrier. A sun gear and intermediate gears are arranged about and intermesh with the sun gear. The intermediate gears are supported by the carrier. The intermediate gears extend through the apertures to intermesh with a ring gear. A baffle is supported relative to the carrier and includes a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubricant on the at least one of the sun gear and intermediate gears. The lubrication passage includes a primary passage that extends laterally between the walls and first and second passages and is in communication with the primary passage and respectively terminates near the sun gear and intermediate gears.

Claims

1. A geared architecture comprising: a carrier, having spaced apart walls with circumferentially spaced mounts interconnecting the walls, the mounts providing circumferentially spaced apart apertures between the mounts at an outer circumference of the carrier; a sun gear and intermediate gears arranged about and intermeshing with the sun gear, the intermediate gears supported by the carrier, the intermediate gears extending through the apertures to intermesh with a ring gear; and a baffle supported relative to the carrier including a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubricant on the at least one of the sun gear and intermediate gears, wherein the lubrication passage includes a primary passage extending laterally between the walls and first and second passages in communication with the primary passage and respectively terminating near the sun gear and intermediate gears.

2. The geared architecture according to claim 1, comprising a tube extending through a hole in one of the walls, the tube in communication with the primary passage.

3. The geared architecture according to claim 1, comprising a ring gear intermeshing with the intermediate gears and an output shaft interconnected to the ring gear, and an input shaft interconnected to the sun gear.

4. The geared architecture according to claim 3, wherein the carrier is fixed relative to a housing.

5. The geared architecture according to claim 4, wherein the housing supports a torque frame that is secured to the mounts.

6. The geared architecture according to claim 1, wherein the baffle is secured to the carrier with fasteners.

7. The geared architecture according to claim 1, wherein the baffle is integral with carrier.

8. A geared architecture comprising: a carrier; a sun gear and intermediate gears arranged about and intermeshing with the sun gear, the intermediate gears supported by the carrier; a baffle supported relative to the carrier including a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubricant on the at least one of the sun gear and intermediate gears; and a spray bar external to the carrier and in communication with the lubrication passage, the spray bar terminating near the sun gear for directing lubricant on the sun gear.

9. The geared architecture according to claim 8, comprising a tube extending through a hole in one of the walls, the tube in communication with the primary passage.

10. The geared architecture according to claim 8, comprising a ring gear intermeshing with the intermediate gears and an output shaft interconnected to the ring gear, and an input shaft interconnected to the sun gear.

11. The geared architecture according to claim 10, wherein the carrier is fixed relative to a housing.

12. The geared architecture according to claim 11, wherein the housing supports a torque frame that is secured to the mounts.

13. The geared architecture according to claim 8, wherein the baffle is secured to the carrier with fasteners.

14. The geared architecture according to claim 8, wherein the baffle is integral with carrier.

15. A method of designing a geared architecture comprising: defining a carrier having spaced apart walls with circumferentially spaced mounts interconnecting the walls, the mounts defined to provide circumferentially spaced apart apertures between the mounts at an outer circumference of the carrier; defining a sun gear and intermediate gears arranged about and intermeshing with the sun gear, the intermediate gears defined to be supported by the carrier, the intermediate gears defined to extend through the apertures to intermesh with a ring gear; and defining a baffle supported relative to the carrier including a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubricant on the at least one of the sun gear and intermediate gears, wherein the lubrication passage includes a primary passage extending laterally between the walls and first and second passages in communication with the primary passage.

16. The method according to claim 15, comprising defining a tube extending through a hole in one of the walls, the tube configured to be in communication with the primary passage.

17. The method according to claim 15, comprising defining a ring gear intermeshing with the intermediate gears and an output shaft interconnected to the ring gear, and defining an input shaft interconnected to the sun gear.

18. The method according to claim 17, comprising defining the carrier to be fixed relative to a housing.

19. The method according to claim 18, comprising defining the housing to support a torque frame that is configured to be secured to the mounts.

20. The method according to claim 15, comprising defining the baffle to be secured to the carrier with fasteners.

21. The method according to claim 15, comprising defining the baffle to be integral with carrier.

22. A method of designing a geared architecture comprising: defining a carrier; defining a sun gear and intermediate gears arranged about and intermeshing with the sun gear, the intermediate gears configured to be supported by the carrier; defining a baffle configured to be supported relative to the carrier including a lubrication passage near at least one of the sun gear and intermediate gears for directing a lubricant on the at least one of the sun gear and intermediate gears; and defining a spray bar external to the carrier and in communication with the lubrication passage, the spray bar configured to terminate near the sun gear for directing lubricant on the sun gear.

23. The method according to claim 22, comprising defining a tube extending through a hole in one of the walls, the tube configured to be in communication with the primary passage.

24. The method according to claim 22, comprising defining a ring gear intermeshing with the intermediate gears and an output shaft interconnected to the ring gear, and defining an input shaft interconnected to the sun gear.

25. The method according to claim 24, comprising defining the carrier to be fixed relative to a housing.

26. The geared architecture according to claim 25, comprising defining the housing to support a torque frame that is configured to be secured to the mounts.

27. The method according to claim 22, comprising defining the baffle to be secured to the carrier with fasteners.

28. The method according to claim 22, comprising defining the baffle to be integral with carrier.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a partial cross-sectional view of a front portion of a gas turbine engine illustrating a turbo fan, epicyclic gear train and a compressor section.

(2) FIG. 2 is a cross-sectional view of the epicyclic gear train shown in FIG. 1.

(3) FIG. 3 is an end view of the epicyclic gear train taken along line 3-3 in FIG. 2 with a pair of star gears shown in phantom in an installation position.

(4) FIG. 4 is an enlarged view of a portion of the epicyclic gear train shown in FIG. 3 with a sun gear and star gears shown in phantom.

(5) FIG. 5 is an enlarged view of a portion of the epicyclic gear train shown in FIG. 2.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

(6) A portion of a gas turbine engine 10 is shown schematically in FIG. 1. The turbine engine 10 includes a fixed housing 12 that is constructed from numerous pieces secured to one another. A compressor section 14 having compressor hubs 16 with blades are driven by a turbine shaft (not shown) about an axis A. A turbo fan 18 is supported on a turbo fan shaft 20 that is driven by a compressor shaft 24, which supports the compressor hubs 16, through an epicyclic gear train 22.

(7) In the example arrangement shown, the epicyclic gear train 22 is a star gear train. Of course, the claimed invention also applies to other epicyclic gear trains such as a planetary arrangement. Referring to FIG. 2, the epicyclic gear train 22 includes a sun gear 28 that is connected to the compressor shaft 24, which provides rotational input, by a splined connection 30.

(8) In the example arrangement shown, the compressor shaft is a two-part shaft having a first shaft 24a and a second shaft 24b. The first shaft 24a is connected to the second shaft 24b via a connection member 31, which is a bolt and nut in this example.

(9) A carrier 34 is fixed to the housing 12 by a torque frame 36. The carrier 34 supports intermediate gears (which are star gears 32 in the arrangement shown) that are coupled to the sun gear 28 by meshed interfaces 26 between the teeth of the sun and star gears 28, 32. A ring gear 38 surrounds the carrier 34 and is coupled to the star gears 32 by meshed interfaces 44. The ring gear 38, which provides rotational output, is secured to the turbo fan shaft 20 by connection 42.

(10) In one example, the torque frame 36 grounds the carrier 34 to the housing 12 in a known manner. For example, mounts 53 have apertures 56 receiving fingers of the torque frame 36, as shown in FIGS. 2 and 3. Pins 48 that extend through spherical bearings 46 and bushings 52 secure the fingers to the carrier 34. Fasteners 50 retain the pins 48 to the carrier 34.

(11) The carrier 34 is a unitary structure manufactured from one piece for improved structural rigidity and ease of assembly. The carrier 34 includes spaced apart side walls 60 that are interconnected by the mounts 54, which are generally wedge-shaped members, as best shown in FIG. 3. The mounts 54 and side walls 60 are unitary with one another. The mounts 54 have opposing curved surfaces 58 that are in close proximity to the star gears 32 and generally follow the curvature of the teeth of the star gears 32 so that any oil on the curved surfaces 58 will likely find its way to the star gears 32 for additional lubrication.

(12) The mounts 54 are circumferentially spaced about the carrier 34 to provide apertures 98 through which the star gears 32 extend to engage the ring gear 38. Returning to FIG. 2, the side walls 60 include holes 62 for receiving a journal bearing 64 that supports each of the star gears 32. Each journal bearing 64 is retained within the carrier 34 by retainers 66 fastened to the side walls 60.

(13) Oil baffles 68 are arranged between the side walls 60 near each of the mounts 54, best shown in FIG. 2. Referring to FIGS. 4 and 5, the baffles 68 include ends 72 that abut the mounts 54, in the example shown. The baffles 68 also include opposing curved surfaces 70 arranged in close proximity to the star gears 28. The curved surfaces 58, 70 are contiguous with and adjoin one another, in the example shown, and provide gear pockets 102 that receive the star gears 32. A gear pocket 104, which receives the sun gear 28, is also provided between a surface 73 on each of the baffles 68 opposite the ends 72.

(14) In one example, one of the side walls 60 includes holes 74 that receive fasteners 76 which secure each of the baffles 68 to the carrier 34. The baffles 68 include a lubrication passage provided by a primary passage 86 that fluidly communicates with a lubricant distributor 78. The lubricant distributor 78 is fed oil from a lubricant supply 96. In one example, the baffles 68 include openings 82 that receive a tube 80 extending through a hole 83 in the side wall 60. Seals 84 seal the tube 80 to the opening 82 and lubricant distributor 78. Other tubes 92 having seals 84 are used to provide oil to an external spray bar 94 through another lubrication passage (spray bar passage 93 that extends through one of the baffles 68). The external spray bar 94 is secured to the carrier 34 and sprays oil in the vicinity of the sun gear 28 near the splined connection 30 (shown in FIGS. 2 and 5).

(15) The primary passage 86 is in communication with first and second passages 88, 90 that spray oil on the teeth of the sun and star gears 28, 32. In the example shown, the first and second passages 88, 90 are arranged ninety degrees from one another.

(16) With the example baffles 68, lubricant distribution is integrated into the baffle so that separate components are eliminated. The baffles 68 can be constructed from a different, lighter weight material than the carrier 34.

(17) The example carrier 34 can be constructed from one piece, which improves the structural integrity of the carrier. A central opening 100 is machined in at least one of the side walls 60 and provides the gear pocket 104. Gear pockets 102 are machined between the side walls 60 and mounts 54 for each of the star gears 32 and form apertures 98 at an outer circumference of the carrier 34. Referring to FIG. 3, the star gears 32 are inserted into the central opening 100 and moved radially outwardly so that they extend through the apertures 98 and are preferably in abutment with the mounts 54 (position indicated by dashed lines in FIG. 3). In this position, there is an adequate gap, t, between the teeth of adjacent star gears 32 to accommodate a width, w, of the end 72 of the baffles 68. Once the baffles 68 have been inserted, the star gears 32 can be repositioned, as shown by the solid lines, and the sun gear 28 can be inserted into the central opening 100 so that it meshes with the star gears 32. The baffles 68 are secured to the carrier 34 using fasteners 76. The tubes 80, 92 can be inserted and the rest of the lubricant distribution system can be connected.

(18) Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.