[특허]GEARBOX FOR A GAS TURBINE ENGINE

Gravina, Michele

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GEARBOX FOR A GAS TURBINE ENGINE

특허상세정보
국가/구분	United States(US) Patent 공개
국제특허분류(IPC7판)	F02C-007/36 F16H-057/04 F02C-003/113 F02K-003/06 F16H-057/08
출원번호	US-0163927 (2018-10-18)
공개번호	US-0112985 (2019-04-18)
우선권정보	EP-17425101.7 (2017-10-18)
발명자 / 주소	Gravina, Michele
출원인 / 주소	Gravina, Michele
인용정보	피인용 횟수 : 0 인용 특허 : 0

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An epicyclic gearbox includes a sun gear assembly, a planet gear assembly, and a ring gear assembly engaged with a forward planet gear and an aft planet gear of the planet gear assembly. A first axial shroud is also provided positioned forward of the forward planet gear or aft of the aft planet gear along an axial direction. The first axial shroud covers substantially all of a forward side of the forward planet gear or an aft side of the aft planet gear. The planet gear assembly is coupled to a planet gear carrier, the planet gear carrier including a rad...

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1. An epicyclic gearbox defining an axial direction, a radial direction, and a circumferential direction, the epicyclic gearbox comprising: a sun gear assembly;a planet gear assembly comprising a forward planet gear and an aft planet gear spaced along the axial direction, the forward planet gear and aft planet gear each engaged with the sun gear assembly, the forward planet gear defining an outer circumference and the aft planet gear defining an outer circumference;a ring gear assembly engaged with the forward planet gear and the aft planet gear;a first axial shroud positioned forward of the forward planet gear or aft of the aft planet gear along the axial direction, the first axial shroud covering substantially all of a forward side of the forward planet gear or an aft side of the aft planet gear to contain lubrication fluid within or around the planet gear assembly; anda planet gear carrier, the planet gear assembly coupled to the planet gear carrier, the planet gear carrier comprising a radial shroud including one or more radial shroud surfaces extending along at least a portion of the outer circumference of the forward planet gear and along at least a portion of the outer circumference of the aft planet gear to contain lubrication fluid within or around the planet gear assembly. 2. The epicyclic gearbox of claim 1, wherein the sun gear assembly comprises a forward sun gear and an aft sun gear spaced along the axial direction, wherein the forward planet gear is engaged with the forward sun gear, and wherein the aft planet gear is engaged with the aft sun gear. 3. The epicyclic gearbox of claim 1, wherein the first axial shroud is a forward axial shroud positioned forward of the forward planet gear along the axial direction and covering substantially all of the forward side of the forward planet gear. 4. The epicyclic gearbox of claim 3, further comprising: a second, aft axial shroud positioned aft of the aft planet gear along the axial direction and covering substantially all of the aft side of the aft planet gear. 5. The epicyclic gearbox of claim 4, wherein the forward axial shroud is coupled to the aft axial shroud. 6. The epicyclic gearbox of claim 5, further comprising: a lubrication spray ring comprising a plurality of lubrication spray bars spaced along the circumferential direction, wherein the forward axial shroud is coupled to the aft axial shroud through the plurality of lubrication spray bars of the lubrication spray ring. 7. The epicyclic gearbox of claim 4, wherein the forward axial shroud defines an axial separation from the forward planet gear less than about 0.5 inches, and wherein the aft axial shroud defines an axial separation from the aft planet gear less than about 0.5 inches. 8. The epicyclic gearbox of claim 1, wherein the one or more radial shroud surfaces of the radial shroud extend along at least about 20 percent of the outer circumference of the forward planet gear and of the outer circumference of the aft planet gear. 9. The epicyclic gearbox of claim 1, further comprising: a lubrication spray ring comprising a plurality of lubrication spray bars spaced along the circumferential direction, wherein the plurality of lubrication spray bars includes a first lubrication spray bar and a second lubrication spray bar, wherein the first lubrication spray bar and the second lubrication spray bar are each positioned adjacent to the forward planet gear and the aft planet gear, wherein the first lubrication spray bar includes a radial shroud surface, wherein the second lubrication spray bar also includes a radial shroud surface, wherein the one or more radial shroud surfaces of the radial shroud of the planet gear carrier and the radial shroud surfaces of the first and second spray bars together extend along at least about seventy percent of the outer circumferences of the forward planet gear and of the aft planet gear. 10. The epicyclic gearbox of claim 9, wherein the one or more radial shroud surfaces of the radial shroud of the planet gear carrier and the radial shroud surfaces of the first and second spray bars together extend along at least about eighty percent of the outer circumferences of the forward planet gear and of the aft planet gear. 11. The epicyclic gearbox of claim 9, wherein the one or more radial shroud surfaces of the radial shroud of the planet gear carrier and the radial shroud surfaces of the first and second spray bars together define an average separation with the forward planet gear and the aft planet gear of less than about 0.7 inches. 12. The epicyclic gearbox of claim 1, wherein the forward planet gear is a first forward planet gear of a plurality of forward planet gears, wherein the aft planet gear is a first aft planet gear of a plurality of aft planet gears, wherein each of the plurality of forward planet gears is engaged with the sun gear assembly and the ring gear assembly, wherein each of the plurality of aft planet gears is also engaged with the sun gear assembly and the ring gear assembly, and wherein the first axial shroud is a forward axial shroud positioned forward of the plurality of forward planet gears along the axial direction, covering substantially all of a forward side of each of the plurality of forward planet gears. 13. The epicyclic gearbox of claim 12, further comprising: a second, aft axial shroud positioned aft of the plurality of aft planet gears along the axial direction and covering substantially all of an aft side of each of the plurality of aft planet gears. 14. A gas turbine engine defining an axial direction, the gas turbine engine comprising: a turbine section comprising a turbine;a fan assembly comprising a fan; anda epicyclic gearbox coupling the turbine of the turbine section to the fan of the fan assembly, the epicyclic gearbox comprising: a sun gear assembly;a planet gear assembly comprising a forward planet gear and an aft planet gear spaced along the axial direction, the forward planet gear and aft planet gear each engaged with the sun gear assembly, the forward planet gear defining an outer circumference and the aft planet gear defining an outer circumference;a ring gear assembly engaged with the forward planet gear and the aft planet gear;a first axial shroud positioned forward of the forward planet gear or aft of the aft planet gear along the axial direction, the first axial shroud covering substantially all of a forward side of the forward planet gear or an aft side of the aft planet gear to contain lubrication fluid within or around the planet gear assembly; anda planet gear carrier, the planet gear assembly coupled to the planet gear carrier, the planet gear carrier comprising a radial shroud including one or more radial shroud surfaces extending along at least a portion of the outer circumference of the forward planet gear and along at least a portion of the outer circumference of the aft planet gear to contain lubrication fluid within or around the planet gear assembly. 15. The gas turbine engine of claim 14, wherein the sun gear assembly comprises a forward sun gear and an aft sun gear spaced along the axial direction, wherein the forward planet gear is engaged with the forward sun gear, and wherein the aft planet gear is engaged with the aft sun gear. 16. The gas turbine engine of claim 14, wherein the first axial shroud is a forward axial shroud positioned forward of the forward planet gear along the axial direction and covering substantially all of the forward side of the forward planet gear. 17. The gas turbine engine of claim 16, wherein the epicyclic gearbox further comprises a second, aft axial shroud positioned aft of the aft planet gear along the axial direction and covering substantially all of the aft side of the aft planet gear. 18. The gas turbine engine of claim 17, wherein the forward axial shroud defines an axial separation from the forward planet gear less than about 0.5 inches, and wherein the aft axial shroud defines an axial separation from the aft planet gear less than about 0.5 inches. 19. The gas turbine engine of claim 14, wherein the one or more radial shroud surfaces of the radial shroud extend along at least about 20 percent of the outer circumference of the forward planet gear and of the outer circumference of the aft planet gear. 20. The gas turbine engine of claim 14, wherein the epicyclic gearbox further comprises a lubrication spray ring comprising a plurality of lubrication spray bars spaced along the circumferential direction, wherein the plurality of lubrication spray bars includes a first lubrication spray bar and a second lubrication spray bar, wherein the first lubrication spray bar and the second lubrication spray bar are each positioned adjacent to the forward planet gear and the aft planet gear, wherein the first lubrication spray bar includes a radial shroud surface, wherein the second lubrication spray bar also includes a radial shroud surface, wherein the one or more radial shroud surfaces of the radial shroud of the planet gear carrier and the radial shroud surfaces of the first and second spray bars together extend along at least about seventy percent of the outer circumferences of the forward planet gear and of the aft planet gear.

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GEARBOX FOR A GAS TURBINE ENGINE

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