Gearbox assembly

US12540669B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12540669-B2
Application numberUS-202318477960-A
CountryUS
Kind codeB2
Filing dateSep 29, 2023
Priority dateFeb 16, 2023
Publication dateFeb 3, 2026
Grant dateFeb 3, 2026

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A gearbox assembly includes a plurality of planet gears secured by a planet carrier. The plurality of planet gears and the planet carrier rotate about a longitudinal centerline axis. A planet pin is disposed in each planet gear. One or more journal bearings are defined by the planet pin and the planet gear, each planet gear rotating about the one or more journal bearings. The gearbox assembly includes an auxiliary lubrication system that stores lubricant therein. The auxiliary lubrication system includes one or more lubricant lines that provide fluid communication between the auxiliary lubrication system and the one or more journal bearings. Rotation of the planet carrier and the one or more journal bearings generates a suction effect that causes the lubricant in the auxiliary lubrication system to flow to the one or more journal bearings during windmilling conditions and during zero gravity conditions or negative gravity conditions.

First claim

Opening claim text (preview).

The invention claimed is: 1 . A gearbox assembly comprising: a plurality of planet gears secured by a planet carrier, the plurality of planet gears and the planet carrier rotating about a longitudinal centerline axis of the gearbox assembly; a planet pin disposed in each planet gear of the plurality of planet gears; one or more journal bearings defined by the planet pin and the planet gear of the plurality of planet gears, each planet gear of the plurality of planet gears rotating about the one or more journal bearings; an auxiliary lubrication system that stores lubricant therein, the auxiliary lubrication system including one or more lubricant lines that provide fluid communication between the auxiliary lubrication system and the one or more journal bearings, wherein rotation of the planet carrier and the one or more journal bearings generates a suction effect that causes the lubricant in the auxiliary lubrication system to flow through the one or more lubricant lines to the one or more journal bearings during windmilling conditions and during zero gravity conditions or negative gravity conditions; and a lubricant transfer device for transferring the lubricant from the one or more lubricant lines to the one or more journal bearings, wherein the lubricant transfer device includes a lubricant transfer device radius measured from the longitudinal centerline axis of the gearbox assembly, the one or more journal bearings include a journal bearing outlet radius measured from the longitudinal centerline axis of the gearbox assembly, and the journal bearing outlet radius is greater than the lubricant transfer device radius. 2 . The gearbox assembly of claim 1 , further comprising a sun gear, a ring gear, an input shaft coupled to the sun gear, and an output shaft coupled to the planet carrier, wherein torque is transferred from the input shaft to the output shaft through the gearbox assembly. 3 . The gearbox assembly of claim 1 , further comprising a sump for storing the lubricant therein, and the one or more lubricant lines include a sump line, wherein the suction effect causes the lubricant to flow from the sump through the sump line to the one or more journal bearings during the windmilling conditions. 4 . The gearbox assembly of claim 1 , wherein the auxiliary lubrication system comprises an auxiliary lubricant reservoir for storing the lubricant therein, and the one or more lubricant lines include an auxiliary lubricant line that provides fluid communication between the auxiliary lubricant reservoir and the one or more journal bearings, and the suction effect causes the lubricant to flow from the auxiliary lubricant reservoir to the one or more journal bearings during the zero gravity conditions or the negative gravity conditions. 5 . The gearbox assembly of claim 4 , wherein the auxiliary lubricant line is coupled to the one or more journal bearings at a position opposite of a pressure distribution on the one or more journal bearings. 6 . The gearbox assembly of claim 1 , further comprising a primary lubrication system comprising: a main lubricant tank that stores lubricant therein; a lubricant pump; and a primary lubricant line that provides fluid communication between the main lubricant tank and the one or more journal bearings, wherein the lubricant pump pumps the lubricant from the main lubricant tank through the primary lubricant line to the one or more journal bearings. 7 . The gearbox assembly of claim 6 , further comprising a sump that stores lubricant therein, and a scavenge line that provides fluid communication from the sump to the main lubricant tank such that the lubricant in the sump flows through the scavenge line to the main lubricant tank. 8 . The gearbox assembly of claim 7 , wherein the auxiliary lubrication system further comprises a scavenge line valve that closes during the windmilling conditions to prevent the lubricant in the sump from flowing through the scavenge line to the main lubricant tank during the windmilling conditions. 9 . A method of operating the gearbox assembly of claim 1 , the method comprising: generating a suction effect in the gearbox assembly by causing the planet carrier and the journal bearings to rotate; causing, by the suction effect, the lubricant in the auxiliary lubrication system to flow through the one or more lubricant lines to the one or more journal bearings during the windmilling conditions and during the zero gravity conditions or the negative gravity conditions; and transferring the lubricant from the one or more lubricant lines to the one or more journal bearings through the lubricant transfer device. 10 . The method of claim 9 , wherein the gearbox assembly further comprises a sun gear, a ring gear, an input shaft coupled to the sun gear, and an output shaft coupled to the planet carrier, the method further comprising transferring torque from the input shaft to the output shaft through the gearbox assembly. 11 . The method of claim 9 , wherein the gearbox assembly further comprises a sump for storing the lubricant therein, and the one or more lubricant lines include a sump line, the method further comprising causing, by the suction effect, the lubricant to flow from the sump through the sump line to the one or more journal bearings during the windmilling conditions. 12 . The method of claim 9 , wherein the auxiliary lubrication system comprises an auxiliary lubricant reservoir for storing the lubricant therein, and the one or more lubricant lines include an auxiliary lubricant line that provides fluid communication between the auxiliary lubricant reservoir and the one or more journal bearings, the method further comprising causing, by the suction effect, the lubricant to flow from the auxiliary lubricant reservoir to the one or more journal bearings during the zero gravity conditions or the negative gravity conditions. 13 . The method of claim 12 , wherein the auxiliary lubricant line is coupled to the one or more journal bearings at a position opposite of a pressure distribution on the one or more journal bearings. 14 . The method of claim 9 , wherein the gearbox assembly further comprises a primary lubrication system comprising a main lubricant tank that stores lubricant therein, a lubricant pump, and a primary lubricant line that provides fluid communication between the main lubricant tank and the one or more journal bearings, the method further comprising pumping, by the lubricant pump, the lubricant from the main lubricant tank through the primary lubricant line to the one or more journal bearings. 15 . The method of claim 14 , wherein the gearbox assembly further comprises a sump that stores lubricant therein, and a scavenge line that provides fluid communication from the sump to the main lubricant tank, the method further comprising causing the lubricant to flow from the sump through the scavenge line to the main lubricant tank. 16 . The method of claim 15 , wherein the auxiliary lubrication system further comprises a scavenge line valve in fluid communication with the scavenge line, the method further comprising closing the scavenge line valve during the windmilling conditions to prevent the lubricant in the sump from flowing through the scavenge line to the main lubricant tank during the windmilling conditions. 17 . The method of claim 10 , where the ring gear is coupled to a static structure such that the ring gear is held fixed. 18 . The method of claim 12 , wherein the auxiliary lubricant reservoir is positioned within the gearbox assembly.

Assignees

Inventors

Classifications

  • F02C7/36Primary

    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

  • for supply of lubricant during tilt or high acceleration, e.g. problems related to the tilt or extreme acceleration of the transmission casing and the supply of lubricant under these conditions · CPC title

  • Grooves with pumping effect for supplying lubricants · CPC title

  • Lubricant guiding means in the wall of or integrated with the casing, e.g. grooves, channels, holes · CPC title

  • Bearing · CPC title

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What does patent US12540669B2 cover?
A gearbox assembly includes a plurality of planet gears secured by a planet carrier. The plurality of planet gears and the planet carrier rotate about a longitudinal centerline axis. A planet pin is disposed in each planet gear. One or more journal bearings are defined by the planet pin and the planet gear, each planet gear rotating about the one or more journal bearings. The gearbox assembly i…
Who is the assignee on this patent?
Ge Avio Srl
What technology area does this patent fall under?
Primary CPC classification F02C7/36. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 03 2026 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 11 related publications on this page (citations in our corpus or others sharing the same primary CPC).