Epicyclic reduction gear with fluid transfer pipes, and propeller turbomachine for an aircraft with such a reduction gear
US-2016201791-A1 · Jul 14, 2016 · US
US10458279B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10458279-B2 |
| Application number | US-201615759472-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 8, 2016 |
| Priority date | Sep 15, 2015 |
| Publication date | Oct 29, 2019 |
| Grant date | Oct 29, 2019 |
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A bowl for supplying oil to at least two oil-distribution circuits which are connected to a planet carrier of an epicyclic reduction gearbox, the planet carrier rotating and the oil coming from a fixed oil ejector, the bowl being designed to be secured to the planet carrier and having a substantially cylindrical shape and being open radially towards the inside with respect to an axis. The bowl is divided into a circumferential succession of separate cups each designed to communicate with one of the oil distribution circuits A reduction gearbox with its supply device and a method of operation in a turbomachine are also disclosed.
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The invention claimed is: 1. A bowl for supplying oil to at least two oil distribution circuits connected to a planet pinion carrier of an epicyclic reduction gear train, said planet pinion carrier rotating and the oil coming from a fixed means for oil ejection, said bowl being configured to be integral with said planet pinion carrier and having an approximately cylindrical shape, being open radially inwards relative to an axis, wherein it is divided into a circumferential succession of separate cups each arranged to communicate with one of said oil distribution circuits. 2. The bowl according to claim 1 , in which said circumferential succession of cups comprises at least two series of cups alternating circumferentially, defined by circumferential extensions of the different cups between each series. 3. The bowl according to claim 1 , in which said cups are separated circumferentially by circumferential separations and delimited axially on either side by transverse walls of said bowl, each of the transverse walls having an approximately circular transverse internal peripheral edge and the circumferential separation between two successive cups comprising an inner radial edge farther from the axis than said transverse internal peripheral edges, so as to promote circumferential overflowing of the oil retained by centrifugation in a cup. 4. The bowl according to claim 1 , having a U-section internal shape in a radial plane. 5. An oil supply device for an epicyclic reduction gear train comprising a bowl according to claim 1 , further comprising oil distribution circuits connected to said planet pinion carrier of the reduction gear and communicating with said cups, at least one fixed channel for oil feed and a means for oil ejection at the end of said at least one feed channel, configured for ejecting the oil in said bowl. 6. A reduction gear comprising a device according to claim 1 . 7. A method for supplying oil to a reduction gear according to claim 6 in a turbine engine, the method comprising: regulating the oil flow rate sent to the bowl by the oil ejection means, so that the oil recovered from one of the cups supplies an oil distribution circuit with which the latter communicates, and forms, in said cup, a pocket of oil maintained between walls of the latter, for at least one first operating mode of the turbine engine. 8. The method according to claim 7 , further comprising distributing the lubricant between two oil distribution circuits as a function of their oil flow needs, for at least one first operating mode of the turbine engine, by a differentiated circumferential extension of the cups communicating with said two oil distribution circuits. 9. The method according to claim 7 , further comprising regulating the oil flow sent to the bowl by the oil ejection means, so that the oil recovered from a cup supplies the oil distribution circuit with which the latter communicates, and forms, for at least one cup, a pocket of oil that pours out circumferentially to another cup, for at least one second operating mode of the turbine engine.
Features relating to lubrication or cooling {or heating} (control of lubrication or cooling in hydrostatic gearing F16H61/4165) · CPC title
Centrifugal lubrication · CPC title
of the epicyclical, planetary or differential type · CPC title
Gearings with gears having orbital motion · CPC title
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
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