Journal bearing arrangement

• US 5,102,379 A
• Filed: 03/25/1991
• Issued: 04/07/1992
• Est. Priority Date: 03/25/1991
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Pagluica, Gino, Sundt, Cornelius V.
• Primary Examiner(s): NOT, DEFINED
• Application Number:
  US07/674,267
• Time in Patent Office: 379 Days
• Field of Search: 475/159, 475/317, 475/331, 475/348
• US Class Current: 475/331
• CPC Class Codes: F16C 17/02 for radial load only
• CPC Class Codes: F16C 23/04 self-adjusting
• 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 2057/085 Bearings for orbital gears
• CPC Class Codes: F16H 57/0479 Gears or bearings on planet carriers
• CPC Class Codes: F16H 57/0482 Gearings with gears having orbital motion
• CPC Class Codes: F16H 57/082 Planet carriers

Abstract

A planetary gear system includes a plurality of planet gears, each having a journal bearing and a pin, end supported in a planet carrier. Each pin has a small diameter central portion axially extending for end support. A larger diameter outer portion is integral with the central portion at an inboard merged zone, and has cantilever sections extending outboard from the merged zone. Each pin is sized such that bending of the merged zone in one direction is countered by bending of the cantilever sections in the other direction to achieve a substantially linear bearing surface under load.

Claims

1. A pin for a heavily loaded journal bearing comprising:

a substantially cylindrical central axially extending portion arranged for support only at each of its outboard ends;

a cylindrical outer portion housing an outer surface and is contiguous or integral with said central portion at an inboard merged zone and having cylindrical cantilever sections extending outboard from said merged zone in both directions, said cantilever sections concentrically surrounding and spaced from said central portion outboard of said merged zone, whereby under an applied oil film load said central portion deflects with a bend radius toward the load and said cantilever sections deflect with the bend radius away from the load; and

the geometry and material of said central portion and said outer portion selected such that the deflection of said outer surface under load approaches an axial straight line.

2. A pin as in claim 1, further comprising:

a circumferential inwardly extending rib around the inner periphery of the outboard edge of each cantilever section.

3. A pin as in claim 1, further comprising:

the length of each cantilever section being between 25 percent and 70 percent of the length of said merged zone.

4. A pin as in claim 1, further comprising:

a central axial hole through a substantial portion of said central portion.

5. A pin as in claim 4, further comprising:

an oil distribution recess located in the outer surface of said outer portion axially coextensive with a portion of said merged zone; and

said central axial hole in fluid communication with said oil distribution recess.

6. A high speed heavy load planetary gear assembly comprising:

a ring gear;

a sun gear;

a plurality of planet gears;

a planet carrier;

a journal bearing within each planet gear;

a plurality of pins within said plurality of planet gears, each pin secured at each outboard end to said planet carrier;

each of said pins comprising;

a substantially cylindrical central axially extending portion arranged for support only at each of its outboard ends;

a cylindrical outer portion having an outer surface and is contiguous or integral with said central portion at an inboard merged zone and having cylindrical cantilever sections extending outboard from said merged zone in both directions, said cantilever sections concentrically surrounding and spaced from said central portion outboard of said merged zone, whereby under an applied oil film load said central portion deflects with a bend radius toward the load and said cantilever sections deflect with the bend radius away from the load; and

the geometry and material of said central portion and said outer portion selected such that the deflection of said outer surface under load approaches an axial straight line.

7. A gear assembly as in claim 6, further comprising:

a circumferential inwardly extending rib around the inner periphery of the outboard edge of each cantilever section.

8. A gear assembly as in claim 6, further comprising:

the length of each cantilever section being between 25 percent and 70 percent of the length of said merged zone.

9. A gear assembly as in claim 6, further comprising:

a central axial hole through a substantial portion of said central portion.

10. A gear assembly as in claim 9, further comprising:

an oil distribution recess located in the outer surface of said outer portion axially coextensive with a portion of said merged zone; and

said central axial hole in fluid communication with said oil distribution recess.