Planetary gearbox

Patent metadata

Field	Value
Publication number	US-11629650-B2
Application number	US-202217651918-A
Country	US
Kind code	B2
Filing date	Feb 22, 2022
Priority date	Mar 8, 2021
Publication date	Apr 18, 2023
Grant date	Apr 18, 2023

Abstract

A planetary gearbox having a sun gear, a plurality of planet gears, a ring gear, and a plurality of journal bearing pins. At its axially forward face side and/or at its axially rearward face side, each planet gear forms a recess that extends inside the planet gear starting from the face side. The planet gear forms a protrusion at its axially forward face side and/or at its axially rearward face side. The protrusion has an axial extent and a radial extent, wherein the radial extent is limited at the respective face side to the area between the planet gear inner bore and the radial inner limit of the respective recess in the planet gear, and wherein the protrusion is configured to provide for a flow path for oil emerging from the journal bearing that guides the oil away from the journal bearing.

First claim

We claim:

1. A planetary gearbox comprising:
a sun gear which is configured to rotate about a rotational axis of the planetary gearbox, the rotational axis defining an axial direction of the planetary gearbox;
a plurality of planet gears which are driven by the sun gear, each planet gear comprising an inner bore, an axially forward face side and an axially rearward face side;
a ring gear, the planet gears meshing with the ring gear; and
a plurality of journal bearing pins, each of the journal bearing pins being located in an inner bore of one of the planet gears, wherein in each case a journal bearing pin and a planet gear form a journal bearing;
wherein at its axially forward face side and/or at its axially rearward face side, each planet gear forms a recess that extends towards a mid-plane of the planet gear;
wherein the planet gear forms a protrusion at its axially forward face side and/or at its axially rearward face side, the protrusion having an axial extent and a radial extent, wherein the radial extent is limited at the respective face side to the area between the planet gear inner bore and the radial inner limit of the respective recess in the planet gear, and wherein the protrusion is configured to provide for a flow path for oil emerging from the journal bearing that guides the oil away from the journal bearing in a direction having an axial component;
wherein the protrusion has a radially inner underside, a radially outer top side, and an axially outer end forming a transition between the underside and the top side, wherein the underside of the protrusion provides for an initial flow path of the oil emerging from the journal bearing; and
wherein the underside of the protrusion comprises a sloped surface extending at an angle with respect to the axial direction.

2. The planetary gearbox of claim 1 , wherein the underside of the protrusion comprises two sloped surfaces, a first sloped surface adjacent to the journal bearing and a second sloped surface adjacent to the first sloped surface, wherein the first sloped surface is more angled with respect to the axial direction than the second sloped surface.

3. The planetary gearbox of claim 2 , wherein the first sloped surface extends, in a sectional view of the planet gear, at an angle (α) to the axial direction which lies in the range between 30° and 60°, and in that the second sloped surface extends, in a sectional view of the planet gear, at an angle (β) to the axial direction which lies in the range between 5° and 25°.

4. The planetary gearbox of claim 1 , wherein the underside of the protrusion is formed by a single sloped surface, wherein the single sloped surface extends at an angle (α) to the axial direction which lies in the range between 30° and 60°.

5. The planetary gearbox of claim 1 , wherein the axially outer end of the protrusion forms an oil separation edge for separating oil from the planet gear.

6. The planetary gearbox of claim 1 , wherein the axially outer end of the protrusion is in the form of a hook-like projection that extends in a radially outward direction, the hook-like projection comprising an outer surface that extends radially.

7. The planetary gearbox of claim 6 , wherein the hook-like projection forms a top surface which extends at right angles to the radially extending outer surface of the projection, wherein the top surface and the radially extending outer surface form an oil separation edge.

8. The planetary gearbox of claim 7 , wherein the top side of the protrusion comprises a groove configured to collect residual oil that has passed around the axially outer end of the protrusion, and wherein the groove comprises a groove side wall that runs perpendicular to the top surface of the hook-like projection, wherein the top surface and the groove side wall form an oil separation edge.

9. The planetary gearbox of claim 1 , wherein the top side of the protrusion comprises a groove configured to collect residual oil that has passed around the axially outer end of the protrusion.

10. The planetary gearbox of claim 1 , wherein the underside of the protrusion comprises a sloped surface and an axially extending surface, wherein the sloped surface is adjacent the journal bearing.

11. The planetary gearbox of claim 10 , wherein the protrusion forms, in sectional view, a rectangular structure.

12. The planetary gearbox of claim 1 , wherein the underside of the protrusion comprises an inner groove that is formed adjacent a sloped surface, wherein the sloped surface is formed adjacent the journal bearing.

13. The planetary gearbox of claim 12 , wherein the axially outer end of the protrusion is formed by a radially inward pointing hook, wherein the hook is adjacent the inner groove.

14. The planetary gearbox of claim 1 , wherein the recess at the axially forward face side and/or the recess at the axially rearward face side comprises a radially outer surface that is inclined at an angle (γ) larger than 0° with respect to the axial direction.

15. The planetary gearbox of claim 1 , wherein the protrusion extends over 360° in the circumferential direction of the planet gear.

16. A gas turbine engine comprising:
an engine core comprising a turbine, a compressor, and a core shaft connecting the turbine to the compressor;
a fan located upstream of the engine core, the fan comprising a plurality of fan blades; and a planetary gearbox of claim 1 that receives an input from the core shaft and outputs drive to the fan so as to drive the fan at a lower rotational speed than the core shaft.

Assignees

• Rolls Royce Plc

Inventors

• Berthold Martin
• Young Colin

Classifications

• F16H57/08

  of gearings with members having orbital motion · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F02C7/36 Primary

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F16H57/0479

  Gears or bearings on planet carriers · CPC title

• F05D2260/98

  Lubrication · CPC title