Pivot for a plain bearing and gearset with reduced thermal stress
The invention relates to a pivot pin ( 5 ) for an epicyclic gear train sliding bearing, the pivot pin having axially opposed, laterally open circumferential grooves ( 25 a ), providing flexibility to the pivot pin and which radially separate two axially opposite lateral end portions of a central shank from two lateral cantilevered portions ( 27 a, 27 b ) of the pivot pin. At least one of the cantilevered lateral portions is hollowed out by at least one recess ( 65 a ).
1. A pivot pin for a planetary gear sliding bearing, the pivot pin having:
a portion forming a central shank extending around an axial passage of the pivot pin having an axis, and
axially opposed circumferential grooves, which are open laterally and which radially separate two axially opposed lateral end portions of the central shank from two axially opposite lateral cantilevered portions of the pivot pin,
characterised in that at least one of the cantilevered lateral portions is hollowed out by at least one recess.
2. A pivot pin according to claim 1 , which is in one piece, with its central shank and its cantilevered lateral portions being in one piece.
3. A pivot pin according to claim 1 , wherein, on the lateral side of said at least one recess, said lateral cantilevered portion is circumferential but not annular.
4. A pivot pin according to claim 1 , wherein, on the lateral side of said at least one recess:
the circumferential groove has, away from said at least one recess, at least one depth in a direction in which the circumferential groove extends towards the inside of the pivot pin, from a free lateral end of said cantilevered lateral portion to a bottom end of said circumferential groove, and
the pivot pin having a circumference, said at least one recess extends over at least 10% of the circumference of the pivot pin and/or said depth of the circumferential groove.
5. A pivot pin according to claim 3 , wherein, on the lateral side of said at least one recess:
the circumferential groove has, away from said at least one recess, at least one depth in a direction in which the circumferential groove extends towards the inside of the pivot pin, from a free lateral end of said cantilevered lateral portion to a bottom end of said circumferential groove, and
the pivot pin having a circumference, said at least one recess extends over at least 10% of the circumference of the pivot pin and/or said depth of the circumferential groove.
6. A pivot pin according to claim 1 , characterized in that it comprises at least two recesses hollowed out respectively in one and the other of the two cantilevered lateral portions.
7. A pivot pin according to claim 3 , characterized in that it comprises at least two recesses hollowed out respectively in one and the other of the two cantilevered lateral portions.
8. A pivot pin according to claim 4 , characterized in that it comprises at least two recesses hollowed out respectively in one and the other of the two cantilevered lateral portions.
9. A planetary gear train of an aircraft gas turbine engine, comprising an outer ring gear and planet pinions meshing with a central pinion and with an outer ring gear and each mounted for free rotation on a planet carrier, each planet pinion being able to rotate about a planet axis matching one said axis of the axial passage, via a pivot pin according to claim 1 .
10. A planetary gear train of an aircraft gas turbine engine, comprising an outer ring gear and planet pinions meshing with a central pinion and with an outer ring gear and each mounted for free rotation on a planet carrier, each planet pinion being able to rotate about a planet axis matching one said axis of the axial passage, via a pivot pin according to claim 3 .
11. A planetary gear train of an aircraft gas turbine engine, comprising an outer ring gear and planet pinions meshing with a central pinion and with an outer ring gear and each mounted for free rotation on a planet carrier, each planet pinion being able to rotate about a planet axis matching one said axis of the axial passage, via a pivot pin according to claim 4 .
12. A planetary gear train of an aircraft gas turbine engine, comprising an outer ring gear and planet pinions meshing with a central pinion and with an outer ring gear and each mounted for free rotation on a planet carrier, each planet pinion being able to rotate about a planet axis matching one said axis of the axial passage, via a pivot pin according to claim 5 .
13. A planetary gear train according to claim 9 , further comprising means for supplying oil at an interface between one of said planet pinions and said pivot pin, characterised in that said pivot pin has a radially outer circumferential surface which has a passage for supplying a lubricating liquid, said at least one recess being adjacent to the passage and being angularly located on the side opposite that towards which the lubricant flows on the radially outer circumferential surface when the gear train is allowed to rotate.
14. An aircraft gas turbine engine comprising said planetary gear train according to claim 9 , the central pinion of which surrounds and is solidarized in rotation with a shaft of a compressor of the turbine engine.
15. A turbine engine according to claim 14 , wherein the outer ring is solidarized with a casing or static annular shell of a low-pressure compressor.
16. A turbine engine according to claim 14 , wherein the planet carrier is solidarized with a casing or a static annular shell.
17. A method for making a pivot pin according to claim 1 , an outer circumferential surface of said pivot pin having a supply slot for a lubricating liquid, so that the liquid flows on a circumferential side of said outer circumferential surface when it exits the supply slot, wherein:
temperature fields of the pivot pin are determined by a TEHD model at least at the location of at least one of the cantilevered lateral portions,
at least one zone is identified at this location that the TEHD model indicates as the highest temperature zone(s), and then
a recess is created at the location of said area in said at least one cantilevered lateral portion.
18. A method for making a pivot pin according to claim 3 , an outer circumferential surface of said pivot pin having a supply slot for a lubricating liquid, so that the liquid flows on a circumferential side of said outer circumferential surface when it exits the supply slot, wherein:
temperature fields of the pivot pin are determined by a TEHD model at least at the location of at least one of the cantilevered lateral portions,
at least one zone is identified at this location that the TEHD model indicates as the highest temperature zone(s), and then
a recess is created at the location of said area in said at least one cantilevered lateral portion.
19. A pivot pin for a planetary gear sliding bearing, the pivot pin having:
a portion forming a central shank extending around an axial passage of the pivot pin having an axis, and
axially opposed circumferential grooves, which are open laterally and which radially separate two axially opposed lateral end portions of the central shank from two axially opposite lateral cantilevered portions of the pivot pin,
characterised in that at least one of the cantilevered lateral portions is hollowed out by at least one recess, on the lateral side of said at least one recess, said lateral cantilevered portion is circumferential but not annular, and, on the lateral side of said at least one recess:
the circumferential groove has, away from said at least one recess, at least one depth in a direction in which the circumferential groove extends towards the inside of the pivot pin, from a free lateral end of said cantilevered lateral portion to a bottom end of said circumferential groove, and
the pivot pin having a circumference, said at least one recess extends over at least 10% of the circumference of the pivot pin and/or said depth of the circumferential groove.