Turbofan engine comprising an spicyclic transmission having bearing journals

• US 6,964,155 B2
• Filed: 12/30/2002
• Issued: 11/15/2005
• Est. Priority Date: 12/30/2002
• Status: Expired due to Term

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Duong, Loc Q., McCune, Michael E.
• Primary Examiner(s): Rodriguez, William H.
• Application Number:
  US10/334,020
• Publication Number:
  US 20040128978A1
• Time in Patent Office: 1,051 Days
• Field of Search: 602/261, 475/331, 384/297, 384/913
• US Class Current: 60/226.1
• CPC Class Codes: F02C 7/36 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 Class Codes: F05D 2260/40311 of the epicyclical, planetary or differential type
• CPC Class Codes: F16C 23/041 with edge relief
• CPC Class Codes: F16H 1/2836 by allowing limited movement of the planets relative to the planet carrier or by using free floating planets
• CPC Class Codes: F16H 57/082 Planet carriers
• CPC Class Codes: Y10S 384/913 Metallic compounds

Abstract

A planet gear journal for an epicyclic gear system is asymmetrically formed to compensate for carrier twist. The asymmetry may be between a pair of opposed outwardly open annular channels inboard of a bearing surface of the journal. A particular application is the planetary gear system of a geared turbofan engine.

Claims

1. An epicyclic transmission comprising:

a sun gear;

a plurality of planet gears meshed with the sun gear;

a ring gear surrounding and meshed with the planet gears;

a plurality of journals, each journal carrying at least an associated one of the planetary gears and having a central longitudinal axis defining opposite first and second directions; and

a gear carrier having a first and second portions respectively supporting the journals on first and second sides of the planet gears, wherein each said journal has;

an outer portion extending from a first outer rim to a second outer rim of said outer portion;

an inner portion extending from a first end to a second end of said outer portion; and

a transition portion joining the inner and outer portions, the transition portion having first and second ends, respectively forming bases of first and second compartments open in the first and second directions, the first and second compartments being asymmetric to each other.

2. The transmission of claim 1 wherein the plurality of journals provide a portion of a torsional coupling between the first and second gear carrier portions.

3. The transmission of claim 1 wherein the second compartment is deeper than the first compartment.

4. The transmission of claim 1 wherein the gear carrier does not have a torque frame coupling.

5. A turbofan engine comprising:

a turbine;

a fan; and

the transmission of claim 1 coupling the turbine to the fan to permit the turbine to drive the fan with a reduction.

6. The turbofan engine of claim 5 wherein the fan is forward of the turbine and has an operative bypass ratio of at least 4.0.

7. An epicyclic transmission comprising:

a sun gear receiving an input power;

a plurality of planet gears meshed with the sun gear;

a ring gear surrounding and meshed with the planet gears;

a plurality of journals, each journal carrying at least an associated one of the planetary gears and having a central longitudinal axis defining opposite first and second directions; and

a gear carrier having a first and second portions respectively supporting the journals on first and second sides of the planet gears, the first portion coupling the carrier to a load to deliver an output power or react a torque, wherein each said journal has;

an outer portion extending from a first outer rim to a second outer rim of said outer portion;

an inner portion extending from a first end to a second end of said inner portion; and

means for joining the outer and inner portions and controlling planet gear to journal film thickness in response to carrier twist.

8. The transmission of claim 7 wherein said means comprises a transition portion joining the inner and outer portions, the transition portion having first and second ends, respectively forming bases of first and second compartments open in the first and second directions, the first and second compartments being asymmetric to each other.

9. A journal having:

a central longitudinal axis defining opposite first and second directions;

an outer portion extending from a first outer rim to a second outer rim of said outer portion;

an inner portion extending from a first end longitudinally beyond the first outer rim to a second end of said inner portion longitudinally beyond the second outer rim; and

a transition portion joining the inner and outer portions, the transition portion having first and second ends, respectively forming bases of first and second compartments open in the first and second directions, the first and second compartments being continuous annular channels asymmetric to each other.

10. The journal of claim 9 wherein the first compartment has a first depth from the first outer rim and the second compartment has a second depth from the second outer rim, the second depth being greater than the first depth.

11. The journal of claim 9 wherein the inner portion has a central bore.

12. A method for optimizing the configuration of a gear-carrying bearing journal in an epicyclic gear system to provide desired gear to journal film thickness upon carrier twist, the method comprising the steps of:

inducing carrier twist in the journal under pre-deterntined operating conditions;

observing film thickness associated with the carrier twist; and

repeating the steps of;

revising the configuration by varying at least one parameter of a longitudinal asymmetry of the journal;

inducing said carrier twist in the journal; and

observing film thickness of the journal associated with the carrier twist,

until the film thickness associated with a particular revised configuration falls within a desired range.

13. The method of claim 12 performed as a computer simulation.

14. The method of claim 12 wherein said varying includes varying relative depth of first end second channels extending longitudinally inward and radially inboard of a bearing surface of the journal.

15. The method of claim 12 wherein said varying includes varying relative diameter of first and second journal shaft portions radially inboard of first and second annular channels in the journal.

16. The method of claim 12 wherein said varying includes varying thickness profiles of first and second journal portions radially outboard of first and second annular channels in the journal.

17. The method of claim 12 wherein said varying includes varying an asymmetry of first and second compartments in respective first and second longitudinal ends of the journal.

18. An engine comprising:

a turbine;

a fan; and

a transmission coupling the turbine to the fan to permit the turbine to drive the fan with a reduction and comprising;

a sun gear;

a plurality of planet gears meshed with the sun gear;

a ring gear surrounding and meshed with the planet gears;

a plurality of journals, each journal carrying at least an associated one of the planetary gears and having a central longitudinal axis defining opposite first and second directions; and

a gear carrier having a first and second portions respectively supporting the journals on first and second sides of the planet gears,

wherein each said journal has;

a central longitudinal axis defining opposite first and second directions;

an outer portion extending from a first outer rim to a second outer rim of said outer portion;

an inner portion extending from a first end to a second end of said inner portion; and

a transition portion joining the inner and outer portions, the transition portion having first and second ends, respectively forming bases of first and second compartments open in the first and second directions, the first and second compartments being asymmetric to each other.

19. The engine of claim 18 wherein the fan is forward of the turbine.

20. The engine of claim 18 wherein the fan is forward of the turbine and has an operative bypass ratio of at least 4.0.

21. The engine of claim 18 wherein the gear carrier does not have a torque frame coupling.